Full optical fiber digital inclinometer

08-07-2009 дата публикации
Номер:
CN0100510318C
Принадлежит: Beihang University
Контакты:
Номер заявки: 08-10-20069776
Дата заявки: 17-07-2006

[1]

Technical Field

[2]

The invention relates to a can be used for underground petroleum and natural gas and other wellbore trajectory continuous measurement of the whole optical fiber digital inclinometer.

[3]

Background Art

[4]

Dipmetering the instrument is petroleum and natural gas, coal mine in the measuring well trajectories of the widely-used measuring tool. The inclinometer is mainly composed of a flux gate sensor or mechanical gyro as the angular velocity sensor and accelerometer combination, measuring the azimuth angle and oblique angle of the well borehole. Magnetic flux gate type inclinometer has the advantages of simple structure, low cost, stable performance, but the instrument casing is unable to realize a magnetic interference, such as the measurement of the oil well; mechanical gyroscope type inclinometer can compensate for this shortcoming, however, the rotation of the internal mechanical gyro mechanism, so that the inherent complex structure, easy to be damaged, anti-vibration is poor, drift and large, resulting in poor precision of the mechanical gyroscope inclinometer, short service life (MTBF≤ 500 hours), the operation and maintenance, the use of the mechanical gyroscope type inclinometer, the cost is very high cost. Ifog light of the solid-state structure has the advantages of high reliability, long service life (MTBF≤ 100,000 hours), resistance to impact and vibration, instantaneous start-up, low power consumption, the advantage of large dynamic range, therefore, the use of optical fiber gyro do inclinometer sensor not only can improve the measurement precision of the instrument, the instrument uses range expansion, can also extend the service life thereof. Furthermore, the logging field of the current of the fiftieth 1990s. armor seven-core cable used as a cable logging data transmission, although different logging method has achieved the logging process automation and logging of information of the real-time processing, because of the transmission cable bandwidth limited, however, severely limits the ability of the upload of the downhole measurement signal, a large amount of formation information can not be transmitted to or can not be transmitted to the ground, according to preliminary statistical, electrical logging information only use 30-50%, and acoustic logging and radioactive logging information to only 10%.

[5]

All-optical digital continuous inclinometer is in the field of aviation and space-based optical fiber gyro strapdown inertial measurement technology and optical-fiber communication technology for a new generation of inclinometer, the optical fiber gyro collecting angular speed information and the quartz flexible accelerometer acquisition of the information with the specific inertial space, through logging special optical cable real time is transmitted to the ground work station, and in accordance with the real-time calculation of the track projection method for borehole trajectory characteristic of the characterization of each parameter, the wellbore trajectory three-dimensional pattern and explanation and analysis for logging information. At the same time, the data transmission of this invention the design of the bus structure, can realize a plurality of combined measurement of well logging instrument.

[6]

Content of the invention

[7]

The purpose of this invention is to provide a kind of the whole optical fiber digital inclinometer, the inclinometer the optical fiber gyro as sensor to measure the angular velocity, and ground and underground optical fiber for data transmission, effectively solve the measurement accuracy of the instrument, the instrument uses range expansion, can also extend the service life thereof. Ground work station of the present invention for controlling and switching over the underland ifog continuous inclinometer sensor probe mode of operation, monitoring underland instrument working condition, to provide the required 180-volt AC power supply, to complete real-time processing of the original measurement data, results plotting display; logging cable winch is used for delegation through the logging cable or the optical fiber gyro continuous inclinometer sensor probe assembly; ifog continuous inclinometer sensor probe in the orbit movement along the wellbore, the sensor are respectively sensitive the corresponding respective parameter, and the data transfer on the logging cable to the ground work station.

[8]

This invention is a kind of the whole optical fiber digital inclinometer, by the central processor, signal processor, counter, cable winch, tension sensor, a derrick and lower shaft prospecting tube ; the central processor through the signal processor RS232 interface is connected with the, optical cable winch through the cable is connected with the signal processor, counter installation of the optical cable capstan, optical cable winch is wound with optical fiber cable, is placed in the derrick above the wellhead to be measured, on the headframe is provided with a tension sensor, the tension sensor through one end of the cable with the lower well is connected with one end of probe tube; shaft prospecting tube is arranged on the X-axis optical fiber gyro, Y-axis optical fiber gyro, Z-axis optical fiber gyro, X-axis accelerometer, Y-axis accelerometer, Z-axis accelerometer, magnetic flux gate X axis, Y axis and Z axis magnetic flux gatemagnetic flux gate.

[9]

The central processor of the computer by a known installed in the computer is applied to the full optical fiber digital inclinometer of strapdown inertial combined measurement of the control device, and which is suitable for the position setting shaft prospecting tube initial aligning device. The inertia states Strapdown combined measuring control device comprises a strap-down inertial measurement unit, measuring unit magnetic flux gate , optical cable running speed measuring unit, Kalman filtering processing unit, information comparison A unit, information comparison B unit and information comparison C unit and a zero speed correcting unit; the initial alignment device is through the two position shaft prospecting tube state of the sensing device on the output of the different parameters under difference comparing the parameters of the coordinate system, to obtain the azimuth shaft prospecting tube ψ, φ cross roll angle, tilt angle θ.

[10]

The invention relates to a full optical fiber digital inclinometer has the advantages of: the optical fiber cable for well logging cable original on the basis of the specialized manufacturing, cable core is in the middle of the optical cable, for use in a downhole high-speed data upload; six around the cable core to the cable, for use in a downhole power supply and the lower ground information such as low-speed control command. Protective layer and the jacket is used to protect the well logging cable.

[11]

Description of drawings

[12]

Figure 1 of the present invention is a digital inclinometer a schematic diagram of the optical fiber.

[13]

Figure 2 is a signal flow diagram of a central processor.

[14]

Figure 2A is a schematic diagram of the main control interface to a central processor.

[15]

Figure 2B is principle diagram of combined measurement mode.

[16]

Figure 2C is a structure diagram of the body coordinate system shaft prospecting tube under.

[17]

Figure 2D is a schematic diagram of local geographical coordinate system the measured wellhead.

[18]

Figure 2E is a schematic diagram of the mutual relationship between the two coordinate system.

[19]

Figure 2F is alignment flowchart of initial alignment.

[20]

Fig. 3 is signal processor structure diagram.

[21]

Figure 3A is schematic diagram of a power amplification circuit.

[22]

Figure 3B is photoelectric conversion circuit schematic diagram.

[23]

Figure 4 is a cross-sectional view of the optical cable.

[24]

Figure 4A amplified is a cross-sectional view of the optical cable.

[25]

Figure 4B amplified is a cross-sectional view of the cable.

[26]

Figure 5 is the invention of the external structure of the mechanical framework shaft prospecting machine Figure.

[27]

Figure 5A is pressure pipe internal structure diagram.

[28]

Figure 5B that the sensor assembly frame structure diagram.

[29]

Figure 5C is 1st fixed hardened patterned.

[30]

Figure 5D is underground power frame structure diagram.

[31]

Figure 5E that the upper connector structure diagram.

[32]

In the Figure:   1. A central processor   101. Computer   102. Strapdown inertial measurement

[33]

103. IC   104. The running speed of the optical cable   105. Kalman filter

[34]

106. Information comparison A   107. Information comparison B     108. C information comparison

[35]

2. Signal processor   201.FPGA processor   202. Power amplification circuit   203. Photoelectric conversion circuit

[36]

3. Counter   4. Optical cable winch   5. Tension sensor   6. Derrick   7. The measured wellhead

[37]

8. Optical fiber cable   801. The outer protective jacket   802. Protective layer   803. Cable

[38]

831. Elastic jacket   832. Armored steel wire   833. Cable core   804. Optical fiber cable

[39]

841. The elastic sheath   842. Armored steel wire   843. An elastic corrugated tube   844. Cable core   805. Filler

[40]

9. Surface casing   10. Lower shaft prospecting tube   1001. X-axis optical fiber gyro   1002. Y-axis optical fiber gyro

[41]

1003. Z-axis optical fiber gyro   1004. X-axis accelerometer

[42]

1005. Y-axis accelerometer   1006. Z-axis accelerometer

[43]

1007. Target oil reservoir   1008. The logging track   11. Cable

[44]

12. The body coordinate system   13. Geographic coordinate system

[45]

In the present invention, lower shaft prospecting tube 10 the mechanical frame of the icon of:

[46]

1a. 1st fixing plate   11a. Annular right end frame   12a. Annular left end frame   13a. Strip-shaped hole

[47]

14. Convex hole   2a. 2nd fixed plate   21. Cavity   22. Strip-shaped hole   3a. 3rd fixed plate

[48]

31. Cavity   32. The strip   4a. 1st positioning drum   41. Wedge-shaped hole   42. Mounting surface

[49]

43. Plane   44. Groove   5a. 2nd positioning drum   51. Groove   53. Round hole

[50]

54. Mounting face   6a. X axial mounting table   61. The mounting surface   62. Round hole   7a. Y axial mounting table

[51]

71. Mounting surface   72. Round hole   8a. X axial rectangular cavity   81. The upper panel   82. The lower panel

[52]

83. The notch   84. Annular end frame   9a. Y axial rectangular cavity   91. Left panel   92. Right panel

[53]

93. Upper ring end frame   94. The lower annular end frame   95. The notch   96. walks the filament trough   101a. Pressure-proof shell

[54]

102a. The upper connecting component   103a. Hook   104a. Joint   105a. Through hole   106a. The lower connecting piece

[55]

107a. Thermos   108a. The connecting joint   109a. Underground power frame   110. 1st positioning frame

[56]

111. The front side plate   112. Annular right end frame   113. Annular left end frame   114. Strip-shaped hole   115. Mounting hole

[57]

116. Double transition   117. Hole   118. A rear side plate   119. 1st transformer   120. 2nd transformer

[58]

Mode of execution

[59]

With the combination of the present invention will be further detailed description.

[60]

This invention is a kind of the whole optical fiber digital inclinometer, by the central processor 1, signal processor 2, the counter 3, optical cable winch 4, tension sensor 5, derrick 6, optical cable 8 and lower shaft prospecting tube 10 integral, central processor 1 is connected with the signal processor 2 through the RS232 interface is connected with the, optical cable winch 4 and the signal processor 2 through the cable 11 is connected with the, counter 3 is installed in a cable winch 4 is, optical cable winch 4 is wound with optical fiber cable 8, derrick 6 is placed in the measured wellhead 7 above, derrick 6 is provided with a tension sensor 5, optical cable 8 is connected through a tension sensor 5 and the lower shaft prospecting tube 10 is connected with one end.

[61]

A central processor 1

[62]

Please korsh as shown in Figure 2, the central processor of the present invention 1 to control flow of the: system (installing in the computer 101 combined measuring and controlling device and the initial alignment apparatus) after the power up, self-checking, first, obtain the correct state information after the operation of the measurement parameter setting (see Figure 2B shown); after the end of the measurement parameter setting gyrolevel enter the initial alignment (see Figure 2F shown) state, shaft prospecting tube to obtain the 10 body coordinate system 12 with respect to the local geographical coordinate system 13 of the conversion matrix ; Aligned gyrolevel initial state after the binding, the input local latitude and longitude of the measuring condition of the well; the lower shaft prospecting tube 10 descenting stopped after reaching the designated depth, and velocity error return-to-zero processing, lower shaft prospecting tube 10 enter uplink measurement state; shaft prospecting tube under 10 reach the measured wellhead 7 well after the secondary alignment processing, the wellbore trajectory closed measurement, and the measurement data are stored, analysis, the drawing processing, and outputs the result.

[63]

In the present invention, a central processor 1 by a known computer 101 installed in the computer is applied to the full optical fiber digital inclinometer of strapdown inertial combined measurement of the control device, which is suitable for the and shaft prospecting tube 10 position setting initial aligning device.

[64]

Is applied to the full optical fiber digital inclinometer strapdown inertial combined control the measurement of the device, means to the strapdown inertial measurement output of the posture information, speed information respectively magnetism posture information of the magnetic measurement output, the speed of movement of the cable winch shaft prospecting tube information and the information is still zero after comparing the information, and the information is compared to the output of the Kalman filtering processing to the difference, used to estimate relevant error of strapdown inertial combination to perform correction and compensation. After said correction and compensation of the output of the strapdown inertial measurement of attitude information to the computer for accurate borehole trajectory drawing and display.

[65]

See Figure 2B illustrated, strapdown inertial combined measurement of this invention the control device comprises a strap-down inertial measurement 102, measuring magnetic flux gate 103, measuring the operating speed of the optical cable 104, Kalman filtering processing 105, three information comparison module (information comparison A106, information comparison B107 and information comparison C108) and zero speed correction module (lower shaft prospecting tube 10 is stationary, information), the following can be realized from the various parts of a description of the function.

[66]

A, strapdown inertial measurement 102

[67]

Inertial measurement is divided into platform inertial measurement and strapdown inertial measurement, strapdown inertial measurement is the gyro and accelerometer is directly connected to the machine body is of a kind of inertial measurement mode. Strapdown inertial measurement is used for mathematical platform to replace the platform inertial measurement in the physical platform and a measuring mode. The strapdown inertial measurement has a simple mechanical structure, small size, relatively low cost, but the gyroscope and accelerometer is directly connected to the body, gyroscope and accelerometer to the input dynamic range is large, in the use of the appropriate gyroscope and accelerometer to the requirements of the higher, in addition the mathematical platform in lieu of physical platform of the computer for data processing with higher requirements.

[68]

In the present invention, strap-down inertial measurement 102 first receives the A) optical fiber gyro output of the coordinate system of the organism shaft prospecting tube Ob Xb Yb Zb the angular speed information; and B) an accelerometer to output the coordinate system of the organism shaft prospecting tube Ob Xb Yb Zb of the specific information; and then the the angular velocity information and the states compared to the strength information after processing by track projections, output C) of the speed information for the shaft prospecting tube Vx, Vy, Vz; and D) under the azimuth attitude information shaft prospecting tube ψ, φ cross roll angle, tilt angle θ; finally, the E) the speed information Vx, Vy, Vz B output to the information comparison unit and information comparison unit C; will F) the posture information is outputted to the information comparison A unit.

[69]

Kalman filter 105 output of the state variable X is used for the on-line compensation the inertial measurement states Strapdown 102 error, after compensation under the representation of the output of the posture information shaft prospecting tube azimuth ψ0, roll angle φ0, inclination angle θ0. And these posture information is outputted to the computer display interface (see Figure 2A shown) drawing on the display (drawing well trajectories), in order to facilitate real-time monitoring of the operator.

[70]

Vertical well depth computing unit for computing the deep vertical well, and the well depth parameter is output to the computer display interface display, in order to facilitate real-time monitoring of the operator. Vertical well depth computing unit through the well depth is calculated information and the received length shaft prospecting tube 10 inclination angle θ0 cosine multiplication is vertical of the measured well depth.

[71]

B, measuring magnetic flux gate 103

[72]

magnetic flux gate is a widespread phenomenon of electromagnetic induction phenomenon, it utilizes the high-permeability material in the sensor coil system characteristic of magnetic saturation of the magnetic field is measured by the instrument, is the most widely used one of the weak measuring instrument, its measuring range is 10-12 -10-3 T, this kind of instrument structure is simple, small volume, light weight, low power consumption, good resistance to shock, the measuring range is wide, high sensitivity, high resolution, good stability, suitable for measuring a constant magnetic field or slow changing magnetic field.

[73]

In the present invention, flux gate assembly comprises three orthogonal placement of the magnetic flux the door, in other words magnetic flux gate X axis, Y axis and Z axis magnetic flux gatemagnetic flux gate.

[74]

In the present invention, measuring magnetic flux gate 103 first receiving A) flux gate assembly output of the coordinate system of the organism shaft prospecting tube Ob Xb Yb Zb geomagnetic under the component information; and B) an accelerometer to output the coordinate system of the organism shaft prospecting tube Ob Xb Yb Zb information specific under; then to the geomagnetic the component information and the calculated information is invisibly states compared to the strength , and sets the calculated relative to the magnetic north azimuth angle conversion with respect to true north azimuth angle of the ψc the rear, the output of the azimuth angle of the posture information shaft prospecting tube ψc, roll angle φc, inclination angle θc; finally the C) the posture information is outputted to the information comparison A unit.

[75]

Three, the running speed of the optical cable 104

[76]

Optical cable 8 is connected with one end of the optical cable winch 4 is, on the other end is fixed on the lower shaft prospecting tube 10 on. In the present invention, the next shaft prospecting tube 10 in the well can be through the counter running speed of the 3 obtained by measuring the cable length in unit time increment cable length shaft prospecting tube the operation of obtaining the coordinate system in the machine body Ob Xb Yb Zb information on the speed of the.

[77]

Full optical fiber digital inclinometer in the process of measuring coordinate system of two, one is a local geographical coordinate system Ot Xt Yt Zt   13, a is the coordinate system of the organism shaft prospecting tube Ob Xb Yb Zb   12. These two coordinate system to the coordinate conversion xbybzb=Ctbxtytzt,Said coordinate conversion matrix. Through this coordinate conversion matrix The coordinate system of the organism shaft prospecting tube Ob Xb Yb Zb cable under running speed information into the local geographical coordinate system Ot Xt Yt Zt information the speed under Vxc, Vyc, Vzc, the speed information Vxc, Vyc, Vzc B output to the information comparison unit comparing the speed difference.

[78]

Underland probe tube body coordinate system Ob Xb Yb Zb with local geographical coordinate system Ot Xt Yt Zt the conversion matrix is between Ctb=cosψcos[!phi!]+sinψsin[!theta!]sin[!phi!]-sinψcos[!phi!]+cosψsin[!theta!]sin[!phi!]-cos[!theta!]sin[!theta!]sinψcos[!theta!]cosψcos[!theta!]sin[!theta!]cosψsin[!theta!]-sinψsin[!theta!]cos[!phi!]-sinψsin[!phi!]-cosψsin[!theta!]cos[!phi!]cos[!theta!]cos[!phi!],In this matrix are respectively provided with the angle of the azimuth attitude information shaft prospecting tube ψ, φ cross roll angle, tilt angle θ.

[79]

Four, Kalman filter 105

[80]

Kalman filter 105 receiving

[81]

A) information comparison A unit output of the posture difference value ZKA=ψ-ψc[!theta!]-[!theta!]c[!phi!]-[!phi!]c,and

[82]

B) information comparison difference output speed B unit ZKB=Vx-VxcVy-VycVz-Vzcand

[83]

C) information comparison difference output speed C unit ZKC=Vx-0Vy-0Vz-0,Discrete Kalman filter using the received information the state variable data fusion X= [δrx, δry, δrz, δvx, δvy, δvz, ηx, ηy, ηz, δfx, δfy, δfz, δωx, δωy, δωz] of the optimal estimation, according to the estimated state variable inertial measurement states Strapdown to the on-line error compensation, the output compensation of the posture information shaft prospecting tubeψ0[!theta!]0[!phi!]0=ψ-ηx[!theta!]-ηy[!phi!]-ηzTo the computer display interface 101.

[84]

In the formula, δrx said local geographical coordinate system Ot Xt Yt Zt the X axis component of the position error, δry said local geographical coordinate system Ot Xt Yt Zt the Y axis component of the position error, δrz said local geographical coordinate system Ot Xt Yt Zt the Z axis component of the position error, δvx said local geographical coordinate system Ot Xt Yt Zt the X axis component of the velocity error, δvy said local geographical coordinate system Ot Xt Yt Zt the Y axis component of the velocity error, δvz said local geographical coordinate system 0t Xt Yt Zt the Z axis component of the velocity error, ηx ψ error azimuth angle said, ηy said tilt angle error θ, ηz said roll angle error φ, δfx said X-axis accelerometer error, δfy said Y-axis accelerometer error, δfz said Z-axis accelerometer error, δωx said X-axis optical fiber gyro error, δωy said Y-axis optical fiber gyro error, δωz said Z-axis optical fiber gyro error.

[85]

Kalman filter of the invention 105 to the filtering processing uses discrete Kalman filtering the basic equation, the initial value of the state variable is set to zero.

[86]

Five, information comparison

[87]

In the present invention, the information comparison information comparing A unit 106, information comparison B unit 107 and information comparison C unit 108 composition, wherein

[88]

Information comparison A unit 106, the used for finishing to the inertial measurement states Strapdown 102 the output of the azimuth attitude information shaft prospecting tube ψ, φ cross roll angle, an inclined angle θ with the magnetic measuring 103 output of the azimuth angle of the posture information shaft prospecting tube ψc, roll angle φc, inclination angle θc subtraction output posture difference value ZKA=ψ-ψc[!theta!]-[!theta!]c[!phi!]-[!phi!]cThe Kalman filter 105;

[89]

Information comparison B unit 107, the used for finishing to the inertial measurement states Strapdown 102 output of the information on the speed of shaft prospecting tube Vx, Vy, Vz measuring the movement speed of the optical fiber cable 104 output speed information Vxc, Vyc, Vzc subtraction output speed difference ZKB=Vx-VxcVy-VycVz-VzcThe Kalman filter 105;

[90]

Information comparison C unit 108, the used for finishing to the inertial measurement states Strapdown 102 output of the information on the speed of shaft prospecting tube Vx, Vy, Vz and the lower shaft prospecting tube 10 output static quantity by subtracting the zero-speed information output speed difference ZKC=Vx-0Vy-0Vz-0The Kalman filter 105.

[91]

Six, zero speed correction

[92]

Zero speed correction means in the all-optical digital inclinometer shaft prospecting tube when in the rest position, its speed is zero the phenomenon of strapdown inertial measurement output to correct the speed error. The "zero speed correction" is realized by setting a key, see Figure 2A illustrated. When using the states zero fast correction mode, the running speed of the actual shaft prospecting tube to zero as the output to the information comparison comparative information C unit.

[93]

Strapdown inertial combined measurement of this invention control apparatus can provide four combined measuring mode of operation, each mode through in Figure 2A in the interface of a corresponding key to realizing. Wherein

[94]

Mode a: length + strapdown inertial measurement (measurement mode is set in the (1))

[95]

The combined measurement mode is used for conventional cable logging the quick and continuous measuring, especially suitable for the cased well or with magnetic substances interference measuring track of the well hole.

[96]

The information needed by the combined measurement of the flow: 1st path information, strapdown inertial measurement first receiving A) optical fiber gyro output of the coordinate system of the organism shaft prospecting tube Ob Xb Yb Zb the angular speed information; and B) an accelerometer to output the coordinate system of the organism shaft prospecting tube Ob Xb Yb Zb of the specific information; and then the the angular velocity information and the states compared to the strength information after processing by track projections, output C) of the speed information for the shaft prospecting tube Vx, Vy, Vz; finally the speed information Vx, Vy, Vz B unit output to the information comparison. 2nd path information, through the counter recording length of the cable, is obtained by the coordinate conversion of the running speed of an information exploring Vxc, Vyc, Vzc B unit output to the information comparison. The information comparison unit B 2nd 1st path information in the path information after comparing the speed difference is output to the Kalman filter processing. 3rd path information, the Kalman filtering the output of the state variable X is used for the on-line compensation of measurement error of the inertial states Strapdown , its compensation after the output of the posture information shaft prospecting tube for azimuth ψ0, roll angle φ0, inclination angle θ0. The posture information is outputted to the computer display interface drawing display, in order to facilitate real-time monitoring of the operator. 4th path information, the posture information is outputted to the vertical well depth to the calculating unit to vertical well depth calculation, and output well depth parameter to the computer display interface display, in order to facilitate real-time monitoring of the operator.

[97]

Mode II: strapdown inertial measurement + zero speed correction (measurement mode is set in the (2))

[98]

The combined measurement mode is used in the well logging is not required in the process of continuous measurement, can be used in logging while drilling (MWD) in the process, real-time monitoring of the drilling direction of the drill bit.

[99]

The information needed by the combined measurement of the flow: 1st path information, strapdown inertial measurement first receiving A) optical fiber gyro output of the coordinate system of the organism shaft prospecting tube Ob Xb Yb Zb the angular speed information; and B) an accelerometer to output the coordinate system of the organism shaft prospecting tube Ob Xb Yb Zb of the specific information; and then the the angular velocity information and the states compared to the strength information after processing by track projections, output C) of the speed information for the shaft prospecting tube Vx, Vy, Vz; finally the speed information Vx, Vy, Vz C unit output to the information comparison. 2nd path information, the actual shaft prospecting tube is zero as the operating speed of the output to the information comparison comparative information C unit. C unit in the information compared with the 2nd 1st path information in the path information after comparing the speed difference is output to the Kalman filter processing. 3rd path information, the Kalman filtering the output of the state variable X is used for the on-line compensation of measurement error of the inertial states Strapdown , its compensation after the output of the posture information shaft prospecting tube for azimuth ψ0, roll angle φ0, inclination angle θ0. The posture information is outputted to the computer display interface drawing display, in order to facilitate real-time monitoring of the operator. 4th path information, the posture information is outputted to the vertical well depth to the calculating unit to vertical well depth calculation, and output well depth parameter to the computer display interface display, in order to facilitate real-time monitoring of the operator.

[100]

Mode three: strapdown inertial measurement + magnetic measurement (measurement mode is set in the (3))

[101]

The combined measurement mode for logging operation of the non-magnetic environment interference, to realize high-accuracy continuous measurement.

[102]

The information needed by the combined measurement of the flow: 1st path information, strapdown inertial measurement first receiving A) optical fiber gyro output of the coordinate system of the organism shaft prospecting tube Ob Xb Yb Zb the angular speed information; and B) an accelerometer to output the coordinate system of the organism shaft prospecting tube Ob Xb Yb Zb of the specific information; and then the the angular velocity information and the states compared to the strength information after processing by track projections, output C) said azimuth angle of the posture information shaft prospecting tube ψ, φ cross roll angle, tilt angle θ; finally the attitude information is outputted to the information comparison A unit. 2nd path information, first receives measuring magnetic flux gate A) flux gate assembly output of the coordinate system of the organism shaft prospecting tube Ob Xb Yb Zb geomagnetic under the component information; and B) an accelerometer to output the coordinate system of the organism shaft prospecting tube Ob Xb Yb Zb information specific under; then to the geomagnetic the component information and the calculated information is invisibly states compared to the strength , and sets the calculated relative to the magnetic north azimuth angle conversion with respect to true north azimuth angle of the ψc the rear, under the output of the azimuth angle of the posture information shaft prospecting tube ψc, roll angle φc, inclination angle θc; finally the attitude information is outputted to the information comparison A unit. The information comparison A single $2nd 1st path information in the path information after comparing the posture difference value output to the Kalman filter processing. 3rd path information, the Kalman filtering the output of the state variable X is used for the on-line compensation of measurement error of the inertial states Strapdown , its compensation after the output of the posture information shaft prospecting tube for azimuth ψ0, roll angle φ0, inclination angle θ0. The posture information is outputted to the computer display interface drawing display, in order to facilitate real-time monitoring of the operator. 4th path information, the posture information is outputted to the vertical well depth to the calculating unit to vertical well depth calculation, and output well depth parameter to the computer display interface display, in order to facilitate real-time monitoring of the operator.

[103]

Mode four: strapdown inertial measurement + length + + zero speed amendment magnetic measurement (measurement mode is set in the (4))

[104]

The combined measurement mode is used for auxiliary length and no continuous measuring requirements of various types of logging environment, the use of data integration technology, can provide accurate estimation and compensation strapdown inertial error, which can provide highly accurate measurement result. Its structure see Figure 2B illustrated, the combined measurement of information flow in the specification a detailed account has been associated, is not described here.

[105]

In the present invention, state variables states Calman filter to the real-time on-line estimation. Four kinds of different relevant measurement mode in the Kalman filter processing of the output of the state variable X is the same, but the use of the observed quantity is different.

[106]

A mode when the selected, its corresponding gaugingH1=000000100000000000000010000000000000001000000,After compensation under the posture information shaft prospecting tube that the output of the ψ0[!theta!]0[!phi!]0=ψ-ηx[!theta!]-ηy[!phi!]-ηz.

[107]

HKCEC mode when the selected, its corresponding gaugingH2,3=000100000000000000010000000000000001000000000,After compensation under the posture information shaft prospecting tube that the output of the ψ0[!theta!]0[!phi!]0=ψ-ηx[!theta!]-ηy[!phi!]-ηz.In this invention, the mode II to mode three gauging is the same, the same is output, that is, the mode three to mode two speed difference as the observed quantity.

[108]

When mode IV when the selected, its corresponding gaugingH4=000100000000000000001000000000000000010000000000000000100000000000000001000000000000000010000000,After compensation under the posture information shaft prospecting tube that the output of the ψ0[!theta!]0[!phi!]0=ψ-ηx[!theta!]-ηy[!phi!]-ηz.

[109]

Lower shaft prospecting tube 10 is provided with a fiber optic gyro assembly includes the X-axis optical fiber gyro 1001, Y-axis optical fiber gyro 1002 and Z-axis optical fiber gyro 1003, three optical fiber gyro output angular speed information; accelerometer assembly includes a X-axis accelerometer 1004, Y-axis accelerometer 1005 and Z-axis accelerometer 1006, three accelerometer output specific information; magnetic flux magnetic flux gate door assembly including the X axis, Y axis and Z axis magnetic flux door magnetic flux gate , three magnetic flux gate output geomagnetic the component information.

[110]

The present invention is through the initial aligning state of the two positions under the shaft prospecting tube 10 on the parameters of sensing device outputs of the different coordinate parameter difference comparison, shaft prospecting tube to obtain the 10 azimuth ψ, φ cross roll angle, tilt angle θ, so as to introduce to the known coordinate conversion matrix shaft prospecting tube calculated under 10 reach the target reservoir 1007 is at the time of logging track 1008 measurement precision. By the parameter difference comparison is wanting to carry out the task of initially aligning the control program stored in the whole optical fiber digital inclinometer in the memory of a computer, use of inertial measurement software system under monitoring shaft prospecting tube 7 initial aligning operation state.

[111]

Initial aligning method of the present invention, is the initial alignment tasks wanting to carry out the control program stored in the full optical fiber digital slope level in the memory of a computer, its initial alignment of the inertial measuring system enters the state of the measuring work before, its initial alignment includes the following alignment step (see Figure 2F shown):

[112]

1st step: after system power-on, detecting lower shaft prospecting tube 10 of the working state is normal;

[113]

2nd step: in normal working state, shaft prospecting tube setting of 10 (see Figure 2C shown) where the position of the present position is 1st F, shaft prospecting tube setting of 10 around its spindle ozb rotating 180° to the position after the 2nd position S;

[114]

3rd step: shaft prospecting tube F current collecting 1st position 10 of the assembly output sensor on the X-axis optical fiber gyro data XFOG1, Y-axis optical fiber gyro data YFOG1, Z-axis optical fiber gyro data ZFOG1, X-axis accelerometer data XA1, Y-axis accelerometer data YA1, Z-axis accelerometer data ZA1, and the collected data is output to the full optical fiber digital inclinometer measuring the inertia of the system;

[115]

Nowadays S shaft prospecting tube collecting 2nd position 10 of the assembly output sensor on the X-axis optical fiber gyro data XFOG2, Y-axis optical fiber gyro data YFOG2, Z-axis optical fiber gyro data ZFOG2, X-axis accelerometer data XA2, Y-axis accelerometer data YA2, Z-axis accelerometer data ZA2, and the collected data is output to the full optical fiber digital inclinometer measuring the inertia of the system;

[116]

4th step: step of the above-mentioned 2nd and 3rd step of the sensory data to the central control processing unit for comparison between two positions, to obtain lower shaft prospecting tube 10 azimuth ψ, φ cross roll angle, inclination angle θ, thus obtaining lower shaft prospecting tube 10 body coordinate system Ob Xb Yb Zb with local geographical coordinate system Ot Xt Yt Zt the transformation matrix between the Ctb=cosψcos[!phi!]+sinψsin[!theta!]sin[!phi!]-sinψcos[!phi!]+cosψsin[!theta!]sin[!phi!]-cos[!theta!]sin[!theta!]sinψcos[!theta!]cosψcos[!theta!]sin[!theta!]cosψsin[!theta!]-sinψsin[!theta!]cos[!phi!]-sinψsin[!phi!]-cosψsin[!theta!]cos[!phi!]cos[!theta!]cos[!phi!].

[117]

In the present invention, the representative shaft prospecting tube 10 posture ψ the initial azimuth angle, φ cross roll angle, tilt angle θ can be in the following order by three times: that is,

[118]

Local geographical coordinate system 1st transition coordinate system 2nd transition coordinate system The body coordinate system Ob Xb Yb Zb

[119]

In the formula, Ob1 Xb1 Yb1t Zb1 said local geographical coordinate system Ot Xt Yt Zt around shaft Ot Zt ψ-azimuth angle of rotation obtained after 1st transition coordinate system;

[120]

Ob2 Xb2 Yb2 Zb2 coordinate system of that transition 1st Ob1 Xb1 Yb1t Zb1 around shaft Ob1 Xb1 rotate the elevation angle θ of the coordinate system of the 2nd transition.

[121]

Three coordinate conversion of the conversion matrix a can be obtained:

[122]

Ctb=cosψcos[!phi!]+sinψsin[!theta!]sin[!phi!]-sinψcos[!phi!]+cosψsin[!theta!]sin[!phi!]-cos[!theta!]sin[!theta!]sinψcos[!theta!]cosψcos[!theta!]sin[!theta!]cosψsin[!theta!]-sinψsin[!theta!]cos[!phi!]-sinψsin[!phi!]-cosψsin[!theta!]cos[!phi!]cos[!theta!]cos[!phi!]

[123]

In the formula, b show the shaft prospecting tube 10 body coordinate system 12, t said local geographical coordinate system 13, T is to b is that of the conversion matrix, ψ said azimuth angle, φ said tool face angle, said well deviation angle θ.

[124]

Furthermore, local geographical coordinate system Ot Xt Yt Ztshaft prospecting tube with the 7 body coordinate system Ob Xb Yb Zb the relationship between the two coordinate system is expressed as xbybzb=Ctbxtytzt.

[125]

See Figure 2C, Figure 2D, Figure 2E shown, lower shaft prospecting tube 10 assembly of the sensor in the X-axis optical fiber gyro 1001, Y-axis optical fiber gyro 1002, Z-axis optical fiber gyro 1003, X-axis accelerometer 1004, Y-axis accelerometer 1005 and Z-axis accelerometer 1006 shaft prospecting tube for respectively driving the input of the 10 body coordinate system Ob Xb Yb Zb each of the axial, shaft prospecting tube keep the 10 is stationary, the position of the shaft 1st F when the output of the fiber optic gyro and accelerometer are as follows:

[126]

XFOG1=KFOGX[ωey(cosψsin[!theta!]sin[!phi!]-sinψcos[!phi!])-ωezsin[!phi!]cos[!theta!]]+εx---(1)

[127]

YFOG1=KFOGY[ωeycosψcos[!theta!]+ωezsin[!theta!]]+εy---(2)

[128]

ZFOG1=KFOGZ[ωey(-sinψsin[!phi!]-cosψsin[!theta!]sin[!phi!])+ωezcos[!theta!]cos[!phi!]]+εz---(3)

[129]

XA1=-KAXcos[!theta!]sin[!phi!]+ΔX---(4)

[130]

YA1=KAYsin[!theta!]+ΔY---(5)

[131]

ZA1=KAZcos[!theta!]cos[!phi!]+ΔZ---(6)

[132]

In the formula:

[133]

Said rotation angular rate of the earth at the north direction of the component,

[134]

Said the day approaches the rotation of the components of the angular speed,

[135]

Said local latitude of the well to be measured,

[136]

ωie said rotation angular speed of the earth,

[137]

Said X-axis optical fiber gyro 1001 of the scale factor,

[138]

Said Y-axis optical fiber gyro 1002 of the scale factor,

[139]

Said Z-axis optical fiber gyro 1003 of the scale factor,

[140]

εx said X-axis optical fiber gyro 1001 the constant drift of,

[141]

εy said Y-axis optical fiber gyro 1002 the constant drift of,

[142]

εz said Z-axis optical fiber gyro 1003 the constant drift of,

[143]

Said X-axis accelerometer 1004 of the scale factor,

[144]

Said Y-axis accelerometer 1005 of the scale factor,

[145]

Said Z-axis accelerometer 1006 of the scale factor,

[146]

ΔX said X-axis accelerometer 1004 null bias,

[147]

ΔY said Y-axis accelerometer 1005 null bias,

[148]

ΔZ said Z-axis accelerometer 1006 null bias.

[149]

Uptodate shaft prospecting tube 10 around its spindle ozb rotation after 180 °, arrived at the designated position, the 2nd position is kept resting S, at this moment the-axis optical fiber gyro and accelerometer output data are:

[150]

XFOG2=KFOGX[-ωey(cosψsin[!theta!]sin[!phi!]-sinψcos[!phi!])+ωezsin[!phi!]cos[!theta!]]+εx---(7)

[151]

YFOG2=KFOGY[-ωeycosψcos[!theta!]-ωezsin[!theta!]]+εy---(8)

[152]

ZFOG2=KFOGZ[ωey(-sinψsin[!phi!]-cosψsin[!theta!]sin[!phi!])+ωezcos[!theta!]cos[!phi!]]+εz---(9)

[153]

XA2=KAXcos[!theta!]sin[!phi!]+ΔX---(10)

[154]

YA2=-KAYsin[!theta!]+ΔY---(11)

[155]

ZA2=KAZcos[!theta!]cos[!phi!]+ΔZ---(12)

[156]

Represented by aboving (1)-(12) can derive the X-axis optical fiber gyro 1001 the constant drift of εx, Y-axis optical fiber gyro 1002 the constant drift of εy, Z-axis optical fiber gyro 1003 the constant drift of εz, X-axis accelerometer 1004 the zero-bias ΔX, Y-axis accelerometer 1005 the zero-bias ΔY, Z-axis accelerometer 1006 the zero-bias ΔZ and lower shaft prospecting tube 10 the initial azimuth ψ, φ cross roll angle, tilt angle θ, the position of the two coordinate parameter conversion is as follows:

[157]

[!theta!]=arcsin[(YA1-YA2)/2KAY]---(13)

[158]

[!phi!]=arcsin[-(XA1-XA2)/2KAXcos[!theta!]]---(14)

[159]

ψ=arccos[(YFOG1-YFOG2)/2KFOGYcos[!theta!]-ωeztan/ωey]---(15)

[160]

εx = (XFOG1 +XFOG2)/ 2     (16)

[161]

εy = (YFOG1 +YFOG2)/ 2     (17)

[162]

εZ=ZFOG1-KFOGZ[ωey(-sinψsin[!phi!]-cosψsin[!theta!]sin[!phi!])+ωezcos[!theta!]cos[!phi!]]---(18)

[163]

ΔX = (XA1 +XA2)/ 2     (19)

[164]

ΔY = (YA1 +YA2)/ 2     (20)

[165]

ΔZ=ZA2-KAZcos[!theta!]cos[!phi!]---(21)

[166]

The above formula (13)-(15) value into the conversion matrix In, shaft prospecting tube can be under 10 body coordinate system to the local geographical coordinate system transformation from the array, at the same time the calibrating out the constant drift of shaft optical fiber gyroscope and the-axis accelerometer of the constant bias, is a simple and effective method for the initial alignment.

[167]

Signal processor 2

[168]

In the present invention, signal processor 2 is used for realizing the downhole data receiving the decoding of the well and issuing control instructions and optical cable length encoding and transmitting of data.

[169]

Signal processor 2 by the FPGA logic processor 201, power amplifying circuit 202, and a photoelectric conversion circuit 203 form, FPGA logic processor 201 received by the central processor 1 L output of the optical cable length (length from the measured wellhead 7 to lower shaft prospecting tube 10 at the current position of the optical cable through the cable winch 4 length, its length by the counter 3 read, and the output to the signal processor 2) and the lower shaft prospecting tube 10 running state command, and sends the information encoded in accordance with the Manchester encoded format is then output to the power amplifying circuit; power amplification circuit for amplifying the coding information, filtering processing is output to the photoelectric conversion circuit, the photoelectric conversion circuit for converting an electrical signal to an optical signal, the light intensity signal through the optical cable coupler is coupled into the optical cable 8 (seven mchp armored cable) transferred to the lower shaft prospecting tube 10.

[170]

Signal processor 2 is connected with the hardware circuit: FPGA logic processor 201 Pa is connected to the output end of the resistance R3 is connected in the amplifier U11 the inverting terminal of the 2, FPGA logic processor 201 Pb is connected to the output end of the resistance R4 is connected in the amplifier U11 multiple transceivers complying of 3, amplifier U11 the output of 6 and that of the photoelectric conversion circuit 23 with the transistor Q1 is connected with the base electrode of the; transistor Q1 the collector ground, transistor Q1 and the emitter of transistor Q3 collector, transistor Q2 is connected with the emitting electrode of the, transistor Q3 and the emitter of the emitter through a resistor R23 is connected with -5V voltage, transistor Q3 the base and sliding rheostat R25 coupling; transistor Q2 the emitter of the laser the LD 2 end connection, laser of LD 1 end is grounded, transistor Q2 VBB the base electrode of which is connected with a reference voltage; a transistor Q4 LD the collector of the of the laser 2 is connected to, the emitter through a resistor R22 and -5V voltage associated, base and the amplifier U12 the output of the 6 coupling; amplifier U12 the inverting terminal of the 2 and the slide rheostat R24 end connection, the sliding rheostat multiple transceivers complying R24 is connected with one end of the, sliding rheostat R24 to ground the other end of the, amplifier U12 the output of 6 and the inverting terminal 2 through a resistor R21 connected, amplifier U12 the inverting terminal of the 2 and the diode PD the 1 other end is connected, the diode PD 2 end is connected to the ground. Photoelectric conversion circuit 203 the power amplifying circuit 202 to provide the voltage of the driving signal is converted into the current required for the laser light source, the laser diode drive current offset LD, an offset current is generated. When the data is higher than VBB expressed when the voltage of the, transistor Q1 through a current in, diode LD closed; when the data lower than the VBB expressed when the voltage of the, transistor Q2 in a current is passed through the, diode LD conduction. Generation of the electrical signal from the transmitted data is modulated into a laser light intensity of said optical signal, and then to be coupled into the optical fiber (optical cable 8 of the optical fiber in) for transmission.

[171]

shaft prospecting tube under 10

[172]

The present invention lower shaft prospecting tube 10 mechanical framework has the relations between the three-dimensional coordinate system, and the multi-section type structure, that is, the upper connecting piece 102a a section of, the lower connecting piece 106a a section of, the downhole power supply frame a and is used for mounting a sensor assembly of the skeleton body (Figure 5B shown) for a period of. The invention of the mechanical framework shaft prospecting machine by an upper connecting piece 102a, the lower connecting piece 106a, underground power frame and a sensor assembly frame (see Figure 5, graph 5B shown), the upper connecting piece 102a through joint 104a and the sensor assembly framework of the pressure-proof shell 101a is connected with one end of the, joint 104a and the other is connected with one threaded end of a hook 103a, optical cable 8 is fixed on the hook 103a is, and the via hole 105a passes through; the lower connecting piece 106a with the sensor assembly frame through the joint of the pressure-proof shell 101a the other end is connected with the; underground power frame mounting the sensor assembly framework of the pressure-proof shell 101a inner (see Figure 5A shown). The skeleton body thereof which is used to fix the sensor assembly and the fixed shield a plurality of threaded holes; sensor assembly are respectively installed at different positions on the mechanical frame, and then the plurality of shield cover and the frame body is connected with the screw hole.

[173]

See Figure 5D shown, in the present invention, downhole power source frame is used for mounting of the power supply needed to provide well AC/DC module (AC/DC module is fixed to the 2nd positioning plate 111 upper) and filtering circuit board (filter circuit board is fixed in the 1st positioning plate 110 on), its well as the needed power supply ± 15V, ± 5 V. Downhole power supply frame is an integrated part, its 1st positioning plate 110 and the thermos 107a connected with one threaded end of a, 2nd positioning plate 111 into the upper connecting piece 102a through hole 105a inner. 1st positioning plate 110 is an annular right end of the one end of the frame 112, on the board surface is provided with a strip-shaped hole 114, the mounting holes 115, 1st positioning plate 110 to transition the other end of the circular frame 116, transition circular frame 116 of the central hole 117, transition circular frame 116 and the annular the left end frame 113 is between the front side plate 111, a rear side plate 118, 1st transformer 119 and 2nd transformer 120 in parallel and is fixedly mounted on the front side 111 and a rear side plate 118 on.

[174]

See Figure 5B shown, in the present invention, the skeleton body sensor assembly which is used to fix the sensor assembly (sensor assembly generally has three optical fiber gyro and three accelerometer) and the fixed shield (shield is composed of a plurality of arc-shaped steel plate are respectively through mechanical framework connected to form the screw hole) a plurality of threaded holes; sensor assembly are respectively installed at different positions on the mechanical frame, and then the plurality of shield cover and the frame body is connected with the screw hole, with a plurality of shielding cover the outer shell of the mechanical frame, not only reduces the mutual interference signal between the devices, is also convenient for at the same time in different parts of the sensor assembly, is also reduced the volume of the mechanical frame. Mechanical frame is designed to have between three-dimensional coordinate system, is to ensure the data acquisition range of the sensor assembly, the design of the two-stage mechanical frame is a mounting position of the accelerometer and the continuous fiber gyrolevel for the design of other parts.

[175]

Sensor assembly of this invention in which the framework of the as a reference plane, of the coordinate axes, is fixedly mounted on the framework of the three fiber optic gyro and three accelerometer, a plurality of circuit boards and, is axial as the datum level of the Z is axially divided. Please igur 5B shown, the skeleton comprises positioning the 1st 4a, 2nd positioning drum 5a, X axial mounting table 6a, Y axial mounting table 7a, X axial rectangular cavity 8a, Y axial rectangular cavity 9a and is used for the installation of a circuit board plate 1st 1a, 2nd fixed plate 2a and 3rd fixed plate 3a ., 1st fixed plate 1a is connected with the 1st positioning drum 4a one end of the, 1st positioning drum 4a and the X axis to the rectangular cavity 8a Y is between the axial mounting table 7a and X axial mounting table 6a, X axial rectangular cavity 8a to the rectangular cavity with the Y shaft 9a is between 2nd fixed plate 2a, Y axial rectangular cavity 9a and 2nd positioning drum 5a is between 3rd fixed plate 3a.

[176]

See Figure 5C shown, in the plate 1st 1a is an annular right end of the two ends of the frame 11a, annular left end frame 12a, is provided with a strip-shaped hole on the board surface 13a and the convex hole 14, a convex hole 14 is arranged on the annular right end frame 11a of the inner side, an annular left end frame 12a is connected with the 1st positioning drum 4a and the plane of the inner cavity of the 43 contact, an annular left end frame 12a with the outer diameter of the 1st positioning drum 4a adapted to the inner diameter; the fixed plate 1st 1a which is used for fixing optical fiber gyro inclinometer for oil well downhole instruments in part for a system processor, such as can be used for fixing the circuit board DSP+FPGA, power supply driving circuit board or the like. On the surface of the strip-shaped hole 13a and the convex hole 14 through the connecting line is used.

[177]

In 1st positioning drum 4a is provided with a mounting surface 42, plane 43 and wedge-shaped hole 41, which is used to install the outside groove flat cable 44 ; 1st positioning drum 4a is used for the inner cavity of the axial accelerometer is of Z, Z axial accelerometer is fixed on the mounting surface 42 of the, mounting surface 42 to the mounting surface 71 of the vertical design ensure that Z axial acceleration meter and Y axial accelerometer orthogonal to the sensitive axis, the axial accelerometer of the connection line Z by the wedge-shaped hole 41 extending, groove 44 flat cable can be installed in, the groove 44 for covering the upper part of the shielding cover.

[178]

In Y axial mounting table 7a the mounting surface 71 is arranged on the Y axis for placing the round hole of the accelerometer 72. X axial mounting table 6a mounting surface 61 is provided with a for placing X axial accelerometer round hole 62. Mounting surface 71 to the mounting surface 61 of the vertical design ensure the Y axial accelerometer and X axial accelerometer orthogonal to the sensitive axis. In the present invention, the mounting surface 42 to the mounting surface 71 vertical, the mounting surface 71 to the mounting surface 61 vertical, the mounting surface 42 to the mounting surface 61 vertical, through the fixed position of the acceleration meter three accelerometer orthogonal to the sensitive axis.

[179]

In 2nd fixed plate 2a is provided with an oval cavity 21, the cavity 21 with the center of a strip-shaped hole 22 ; 2nd fixed plate 2a the concave cavity of the two panels 21 are respectively provided with the circuit board, the circuit board and the connecting line of the optical fiber of the fiber optic gyro from the strip-shaped hole 22 through the in. Oval cavity 21 the design of the bending loss of the optical fiber is reduced.

[180]

The X axial rectangular cavity 8a of the upper panel 81 and the lower panel 82 and in parallel with the three-dimensional coordinate system X axis perpendicular, X axial rectangular cavity 8a of the circular end frames 84 is provided with a notch 83. Y axial rectangular cavity 9a of the left face plate 91 and the right panel 92 and the three-dimensional coordinate system is parallel to Y axis vertical, right panel 92 is provided with a on walks the filament trough 96, Y axial rectangular cavity 9a of the upper annular end frame 93 and the lower annular end frame 94 is provided with a notch 95. X axial rectangular cavity 8a and Y axial rectangular cavity 9a is perpendicular to the opening direction, two optical fiber gyro respectively put into the X axial rectangular cavity 8a and Y axial rectangular cavity 9a cavity, through the fixed in different panel position of the optical fiber gyro has an acquisition X-axis direction or Y-axis direction and the character of the data. The notch 83, the notch 95, walks the filament trough 96 walks the filament path of the design optimization, fiber-optic signal transmission loss is reduced.

[181]

In 3rd fixed plate 3a is provided with an elliptical cavity 31, 3rd fixed plate 3a and the 2nd positioning drum 5a the joint provided with a strip-shaped groove 32, the strip 32 is fixed in the optical fiber coupler, 3rd fixed plate 3a the concave cavity of the two panels 31 are respectively provided with the circuit board, the circuit board and the connecting line of the optical fiber from the fiber optic gyro from the strip 32 through the in. Oval cavity 31 the design of the bending loss of the optical fiber is reduced.

[182]

In 2nd positioning drum 5a is provided with a mounting face 53, mounting surface 53 a is opened on the center of the round hole 52, which is used to install the outside groove flat cable 51, groove 51 for covering the upper part of the shielding cover. 2nd positioning drum 5a is arranged in the axial direction of the fiber optic gyro Z, Z axial ifog fixed on the installing surface 53 on, connecting through a round hole 52 extends out to the 3rd fixed plate 3a. Y axial rectangular cavity 9a of the left face plate 91 and the right panel 92 and 2nd positioning drum 5a mounting surface 53 vertical, Y axial rectangular cavity 9a of the left face plate 91 and the right panel 92 to the rectangular cavity with the X shaft 8a of the upper panel 81 and a lower panel 82 are respectively perpendicular to each other, to the rectangular cavity X shaft 8a of the upper panel 81 and a lower panel 82 and the 2nd positioning drum 5a mounting surface 53 vertical ensures the three fiber optic gyroscope orthogonal to the sensitive axis.

[183]

Mechanical frame structure of the present invention by a power distribution of the signal acquisition and filtering circuit board + + + + + circuit board of the circuit board of the top of the top of the top three + + + circuit board only accelerometer, reasonable layout, so that the space utilization is good; the wire and the optical fiber line short is reasonable and, signal interference is small; and such a structure increases the strength of the structure; the space on the basis of the position precision, to be separated from the top part and adds the table signal interference is reduced, and the distribution of the circuit becomes reasonable.

[184]

Optical cable 8

[185]

In the present invention, the optical cable 8 is composed of six cable 803, one optical cable 804, the protective layer 802 and the outer protective jacket 801 composition, six cable 803 surrounds the cable 804 ambient, and filler 805 to fill the space, six cable 803 external is provided with a protective layer 802, the protective layer 802 is arranged in the outer sheath 801 inner. The optical cable 804 by the optical fiber 844 (using single-mode optical fiber), an elastic corrugated tube 843, steel wire (diameter is 0.5-1.5 mm) and the elastic sheath 841 composition, optical fiber 844 external wrapped with an elastic corrugated tube 843, an elastic corrugated tube 843 of the external sleeve with an elastic sheath 841, elastic sheath 841 formed steel wire is wound outside the armored steel wire layer 842. The cable 803 is composed of a cable core 831 (the copper wire), the steel wire (diameter is 0.5-1.5 mm) and the elastic sheath 831 composition, cable core 831 external sleeve with an elastic sheath 831, elastic sheath 831 formed steel wire is wound outside the armored steel wire layer 832. The protective layer 82 is made of PE material; the outer sheath 801 is a polypropylene material, filler 805 is asphalt.

[186]

In this invention, the reading device 3 martin a generation of gram cable is long counter is selected. Derrick 6 selected the typical logging lifting platform Honeywell, is fixed on the same matched with tension sensor 5, tension sensor 5 used for monitoring the optical cable 8 the tension of the bearing, prevent the optical cable 8 by excessive stretching damage.

[187]

The present invention provides a rapid and high-precision measuring wellbore trajectory, the logging information can be uploaded at a high speed the whole optical fiber digital inclinometer; using an optical cable transmission effectively solves the problem that the existing well logging instruments because the traditional logging cable caused by the low transmission speed, a large number of logging information can upload the shortcoming of not; in addition, this invention adopts the design of the bus structure of digital instruments, the combination of a plurality of well logging instrument provides a platform use, can effectively improve the work efficiency of the well logging operation.



[188]

The present invention discloses an all-fibre digital clinometer. It is composed of central processor, signal processor, counter, optical cable capstan winch, tension sensor, derrick and letting-in probe. Said invention also provides their connection mode, and also provides the working principle of said all-fiber digital clinometer and its operation method.



1, a kind of the whole optical fiber digital inclinometer, including optical cable winch (4), counter (3), tension sensor (5), derrick (6), characterized in that also comprises a central processor (1), signal processor (2) and the lower shaft prospecting tube (10); ; a central processor (1) and the signal processor (2) through RS232 interface is connected with the, optical cable winch (4) and the signal processor (2) through cable (11) is connected with the, counter (3) mounted on the cable winch (4) the upper, cable winch (4) is wound with optical cable (8), derrick (6) is placed in the measured wellhead (7) above, derrick (6) is provided with a tension sensor (5), the optical cable (8) is connected through a tension sensor (5) and the lower shaft prospecting tube (10) is connected with one end of the; lower shaft prospecting tube (10) is arranged on the X-axis optical fiber gyro (1001), Y-axis optical fiber gyro (1002), Z-axis optical fiber gyro (1003), X-axis accelerometer (1004), Y-axis accelerometer (1005), Z-axis accelerometer (1006), magnetic flux gate X axis, Y axis and Z axis magnetic flux gatemagnetic flux gate ;

The central processor (1) by a known computer (101) and is installed in said computer is applied to the full optical fiber digital inclinometer of strapdown inertial combined measurement of the control device, which is suitable for the and shaft prospecting tube (10) position setting initial aligning device; the inertia states Strapdown combined measuring control device comprises a strapdown inertial measurement unit (102), magnetic flux gate measuring unit (103), the optical cable running speed measuring unit (104), the Kalman filtering processing unit (105), information comparison A unit (106), information comparison B unit (107) and information comparison C unit (108) and zero speed correcting unit; the initial alignment device is through the two positions of the lower state shaft prospecting tube (10) on the parameters of sensing device outputs of the different coordinate parameter difference comparison, shaft prospecting tube to obtain the (10) to the azimuth ψ, φ cross roll angle, tilt angle θ.

The central processor (1) in the inertial measurement unit states Strapdown (102) first receives the A) optical fiber gyro output of the coordinate system of the organism shaft prospecting tube Ob Xb Yb Zb the angular speed information; and B) an accelerometer to output the coordinate system of the organism shaft prospecting tube Ob Xb Yb Zb of the specific information; and then the the angular velocity information and the states compared to the strength information after processing by track projections, output C) of the speed information for the shaft prospecting tube Vx, Vy, Vz; and D) under the azimuth attitude information shaft prospecting tube ψ, φ cross roll angle, tilt angle θ; finally the E) speed information Vx, Vy, Vz output to the information comparison B unit (107) and information comparison C unit (108); the F) the posture information is outputted to the information comparison A unit (106);

The measuring unit states the magnetic flux gate (103) first receives the A) flux gate assembly output of the coordinate system of the organism shaft prospecting tube Ob Xb Yb Zb geomagnetic under the component information; and B) an accelerometer to output the coordinate system of the organism shaft prospecting tube Ob Xb Yb Zb information specific under; then to the geomagnetic the component information and the calculated information is invisibly states compared to the strength , and sets the calculated relative to the magnetic north azimuth angle conversion with respect to true north azimuth angle of the ψc the rear, the output of the azimuth angle of the posture information shaft prospecting tube ψc, roll angle φc, inclination angle θc; finally the C) the posture information is outputted to the information comparison A unit (106);

The optical cable running speed measuring unit (104) is measured by using the counter of the cable length in unit time increment cable length shaft prospecting tube the operation of obtaining the coordinate system in the machine body Ob Xb Yb Zb information on the speed of the;

states Calman the filtering processing unit of the (105) receiving A) information comparison A unit (106) the output of the posture difference value ZKA=ψ-ψc[!theta!]-[!theta!]c[!phi!]-[!phi!]c,And B) information comparison B unit (107) the output speed difference ZKB=Vx-VxcVy-VycVz-VzcAnd C) information comparison C unit (108) the output speed difference ZKC=Vx-0Vy-0Vz-0,Discrete Kalman filter using the received information the state variable data fusion X= [δrx, δry, δrz, δvx, δvy, δvz, ηx, ηy, ηz, δfx, δfy, δfz, δωx, δωy, δωz] of the optimal estimation, according to the estimated state variable inertial measurement states Strapdown to the on-line error compensation, the output compensation of the posture information shaft prospecting tubeψ0[!theta!]0[!phi!]0=ψ-ηx[!theta!]-ηy[!phi!]-ηzTo the computer display interface; in the formula,

δ rx said local geographical coordinate system Ot Xt Yt Zt the X axis component of the position error,

δ ry said local geographical coordinate system Ot Xt Yt Zt the Y axis component of the position error,

δ rz said local geographical coordinate system Ot Xt Yt Zt the Z axis component of the position error,

δ vx said local geographical coordinate system Ot Xt Yt Zt the X axis component of the velocity error,

δ vy said local geographical coordinate system Ot Xt Yt Zt the Y axis component of the velocity error,

δ vz said local geographical coordinate system Ot Xt Yt Zt the Z axis component of the velocity error,

ηx ψ error of said azimuth angle,

ηy said error angle of incidence θ,

ηz said roll angle error φ,

ηz δ fx said X-axis accelerometer error,

δ fy said Y-axis accelerometer error,

δ fz said Z-axis accelerometer error,

δωx said X-axis optical fiber gyro error,

δωy said Y-axis optical fiber gyro error,

δωz said Z-axis optical fiber gyro error;

The information comparison A unit (106), used for finishing to the output of the inertial measurement states Strapdown under the azimuth attitude information shaft prospecting tube ψ, φ cross roll angle, an inclined angle θ with the magnetic measurement output of the azimuth angle of the posture information shaft prospecting tube ψc, roll angle φc, inclination angle θc subtraction output posture difference value ZKA=ψ-ψc[!theta!]-[!theta!]c[!phi!]-[!phi!]cThe Kalman filtering processing unit (105);

The information comparison B unit (107), for completion of the strapdown inertial measurement output of the information on the speed of shaft prospecting tube Vx, Vy, Vz sports speed measuring the optical information output speed Vxc, Vyc, Vzc subtraction output speed difference ZKB=Vx-VxcVy-VycVz-VzcThe Kalman filtering processing unit (105);

The information comparison C unit (108), for completion of the strapdown inertial measurement output of the information on the speed of shaft prospecting tube Vx, Vy, Vzshaft prospecting tubestatic quantity output of the zero-speed information subtracted output speed difference ZKC=Vx-0Vy-0Vz-0The Kalman filtering processing unit (105).

2, the whole optical fiber digital inclinometer according to Claim 1, characterized in that its strap-down inertial measurement unit with strapdown inertial measurement + 1st mode of the measuring work of length, strapdown inertial measurement + 2nd correction of the zero speed mode of the measuring work, strapdown inertial measurement + 3rd magnetic measurement mode of the measuring work, strapdown inertial measurement + length + + magnetic measurement of zero speed amendment 4th mode of the measuring work.

3, the whole optical fiber digital inclinometer according to Claim 1, characterized in that the signal processor (2) is used for realizing the downhole data receiving the decoding of the well and issuing control instructions and optical cable length encoding of the data and the transmission; a signal processor (2) by the FPGA logic processor (201), the power amplification circuit (202), and a photoelectric conversion circuit (203) form, FPGA logic processor (201) received by the central processor (1) output shaft prospecting tubewith under L length of the optical cable (10) running state command, and sends the information encoded in accordance with the Manchester encoded format is then output to the power amplifying circuit; power amplification circuit for amplifying the coding information, filtering processing is output to the photoelectric conversion circuit, the photoelectric conversion circuit for converting an electrical signal to an optical signal, the light intensity signal is coupled into the optical fiber cable through the cable coupler (8) be transferred to the lower shaft prospecting tube (10).

4, the whole optical fiber digital inclinometer according to Claim 1, characterized in that the lower shaft prospecting tube (10) mechanical frame by an upper connecting piece (102a), the lower connecting piece (106a), underground power frame and a sensor assembly skeleton,

The upper connector (102a) through joint (104a) and the sensor assembly framework of the pressure-proof shell (101a) is connected with one end of the, joint (104a) and the other is connected with one threaded end of a hook (103a), optical cable (8) is fixed on the hook (103a) is, and the via hole (105a) passes through the;

The lower connecting piece (106a) of the sensor assembly frame through the joint of the pressure-proof shell (101a) is connected with one end of another;

The sensor assembly of the skeleton plate 1st (1a) is connected to the 1st positioning cylinder (4a) one end of, the barrel positioning 1st (4a) to the rectangular cavity with the X axis (8a) Y is between the axial mounting table (7a) and X axial mounting table (6a), X axial rectangular cavity (8a) to the rectangular cavity with the Y shaft (9a) is between the 2nd fixed plate (2a), to the rectangular cavity Y shaft (9a) and the 2nd positioning cylinder (5a) is between 3rd fixed plate (3a); the 1st fixed plate (1a) is an annular end of the two ends of the frame (11a, 12a), is provided with a strip-shaped hole on the board surface (13a) and a convex hole (14), a convex hole (14) is arranged on the ring-shaped end frame (11a) of the inner side, an annular end frame (12a) is connected to the 1st positioning cylinder (4a) on; the 1st positioning cylinder (4a) is provided with a mounting surface (42), the plane (43) and wedge-shaped hole (41), which is used to install the outside groove flat cable (44); the mounting table in the Y axis (7a) of the mounting surface (71) is used for placing the sensor assembly is provided with a circular hole (72); to the mounting table in the X axis (6a) of the mounting surface (61) is used for placing the sensor assembly is provided with a circular hole (62); to the rectangular cavity in the X axis (8a) of the upper panel (81) and lower panel (82) and in parallel with the three-dimensional coordinate system X axis perpendicular, to the rectangular cavity X axis (8a) of the ring-shaped end frame (84) is symmetrically provided with a notch (83); the 2nd fixed plate (2a) is provided with a concave cavity (21), the cavity (21) with the center of a strip-shaped hole (22); to the rectangular cavity in the Y axis (9a) of the left face plate (91) and the right panel (92) and the three-dimensional coordinate system is parallel to Y axis vertical, right panel (92) is provided with a on walks the filament trough (96), to the rectangular cavity Y axis (9a) of the upper annular end frame (93) and the lower annular end frame (94) is provided with a notch (95); in the 3rd fixed plate (3a) is provided with a concave cavity (31), 3rd fixed plate (3a) and the 2nd positioning the barrel (5a) the joint provided with a strip-shaped groove (32); positioning the barrel in the 2nd (5a) is provided with a mounting surface (53), the mounting surface (53) is opened on the center of the is provided with a circular hole (52), which is used to install the outside groove flat cable (51);

The underground power frame is an integrated part, its 1st positioning plate (110) and the thermos bottle (107a) in threaded connection with one end of the, 2nd positioning plate (111) into the upper connector (102a) of the through hole (105a) in. 1st positioning plate (110) is an annular right end of the one end of the frame (112), is provided with a strip-shaped hole on the board surface (114), the mounting hole (115), 1st positioning plate (110) to transition the other end of the circular frame (116), transition circular frame (116) of the center hole (117), transition circular frame (116) and the annular the left end frame (113) there is between the front side plate (111), a rear side plate (118), the transformer 1st (119) and 2nd transformer (120) parallel and fixedly mounted on the front side plate (111) and a rear side plate (118) is.

5, the whole optical fiber digital inclinometer according to Claim 1, characterized in that the counter (3) selecting martin a generation of gram cable is long counter.

6, the whole optical fiber digital inclinometer initial alignment method according to Claim 1, characterized in that the central processor (1) initial aligning of the alignment step comprises the following:

1st step: after system power-on, detecting lower shaft prospecting tube (10) of the working state is normal;

2nd step: in normal working state, setting the lower shaft prospecting tube (10) where the position of the present position is 1st F, shaft prospecting tube set under (10) around its spindle ozb rotary 1800 in position after the S to 2nd position;

3rd step: shaft prospecting tube F current collecting 1st position (10) of the sensor assembly output of the X-axis optical fiber gyro data XFOG1, Y-axis optical fiber gyro data YFOG1, Z-axis optical fiber gyro data ZFOG1, X-axis accelerometer data XA1, Y-axis accelerometer data YA1, Z-axis accelerometer data ZA1, and the collected data is output to the full optical fiber digital inclinometer measuring the inertia of the system;

Nowadays S shaft prospecting tube collecting 2nd position (10) of the sensor assembly output of the X-axis optical fiber gyro data XFOG2, Y-axis optical fiber gyro data YFOG2, Z-axis optical fiber gyro data ZFOG2, X-axis accelerometer data XA2, Y-axis accelerometer data YA2, Z-axis accelerometer data ZA2, and the collected data is output to the full optical fiber digital inclinometer measuring the inertia of the system;

4th step: step of the above-mentioned 2nd and 3rd step of the sensory data to the central control processing unit for comparison between two positions, to obtain lower shaft prospecting tube (10) to the azimuth ψ, φ cross roll angle, inclination angle θ, thus obtaining lower shaft prospecting tube (10) body coordinate system Ob Xb Yb Zb with local geographical coordinate system Ot Xt Yt Zt the transformation matrix between the

Ctb=cosψcos[!phi!]+sinψsin[!theta!]sin[!phi!]-sinψcos[!phi!]+cosψsin[!theta!]sin[!phi!]-cos[!theta!]sin[!theta!]sinψcos[!theta!]cosψcos[!theta!]sin[!theta!]cosψsin[!theta!]-sinψsin[!theta!]cos[!phi!]-sinψsin[!phi!]-cosψsin[!theta!]cos[!phi!]cos[!theta!]cos[!phi!],

In the formula, b show the shaft prospecting tube (10) body coordinate system (12), said local geographical coordinate system t (13), T is to b is that of the conversion matrix, ψ said azimuth angle, φ said tool face angle, said well deviation angle θ.