RADICALLY CURABLE COMPOSITION AND CURED PRODUCT THEREOF

A radically curable composition includes 100 parts by weight of a (meth)acrylic polymer (I) with an average of at least 0.8 radically-crosslinkable groups, 0.01 to 10 parts by weight of a radical polymerization initiator (II), and 10 to 100 parts by weight of a (meth)acrylate compound (III) having a rosin ester group. 1. A radically curable composition comprising:100 parts by weight of a (meth)acrylic polymer (I) with an average of at least 0.8 radically-crosslinkable groups;0.01 to 10 parts by weight of a radical polymerization initiator (II); and10 to 100 parts by weight of a (meth)acrylate compound (III) having a rosin ester group.2. The radically curable composition according to claim 1 , wherein the (meth)acrylic polymer (I) is a (meth)acrylic polymer having a radically-crosslinkable carbon-carbon double bond at a molecular terminal.3. The radically curable composition according to claim 1 , wherein the (meth)acrylic polymer (I) is a (meth)acrylic polymer having a (meth)acryloyl group at a molecular terminal.4. The radically curable composition according to claim 1 , wherein the (meth)acrylic polymer (I) has a molecular weight distribution of less than 1.8.5. The radically curable composition according to claim 1 , wherein the (meth)acrylic polymer (I) is obtained by polymerization or copolymerization of an acrylic acid alkyl ester monomer containing a saturated hydrocarbon group having 4 to 22 carbon atoms.6. The radically curable composition according to claim 1 , wherein the radical polymerization initiator (II) is a radical photoinitiator.7. The radically curable composition according to claim 1 , wherein the (meth)acrylate compound (III) is 1-acrylic acid-3-dehydroabietic acid-2-hydroxypropyl.8. A cured product obtained from the radically curable composition according to .9. A vibration damping material composed of the cured product according to .10. A pressure-sensitive adhesive composed of the cured product according to .11. An impact absorbing material ...

SEISMIC ISOLATION APPARATUS

A seismic isolation apparatus includes a laminated body having alternately laminated rubber plates and steel plates; a hollow portion provided inside the laminated body in a hermetically closed manner and extending in a laminated direction; a lead plug filled densely in the hollow portion and adapted to damp the vibration in a shearing direction of the laminated body by absorbing vibrational energy in the shearing direction; and a lid member having a semispherical concave surface which comes into contact with one end portion in the laminated direction A of the lead plug in order to guide and assist the plastic flow of the lead plug at one end portion in the laminated direction of the hollow portion in the deformation in the shearing direction of the lead plug. 1. A seismic isolation apparatus comprising:a laminated body having alternately laminated elastic layers and rigid layers;a hollow portion provided in an interior of said laminated body in a hermetically closed manner and extending in a laminated direction;a vibration damping member which is densely filled in said hollow portion and is adapted to damp the vibration in a shearing direction of said laminated body by absorbing vibrational energy in the shearing direction of said laminated body; anda closure member which closes one end in the laminated direction of said hollow portion and has a flow guiding concave surface which comes into contact with one end portion in the laminated direction of said vibration damping member, in order to guide and assist the plastic flow of said vibration damping member at one end portion in the laminated direction of said hollow portion in the deformation of said vibration damping member due to the vibration in the shearing direction of said laminated body,said hollow portion being defined by inner peripheral surfaces of the elastic layers and the rigid layers and by the flow guiding concave surface.2. The seismic isolation apparatus according to claim 1 , wherein said hollow ...

Resin fuses and vehicles comprising the same

A vehicle seat assembly including a seat frame assembly including a seat base and a seat back pivotally connected to the seat base. The seat back includes at least one resin fuse arranged in the seat back to indicate structural loading in the vehicle seat assembly above a tolerance loading. The at least one resin fuse includes an aperture extending through the seat back and comprising a flange encircling the aperture and extending generally perpendicular to the seat back, and an indicator bar extending across a diameter of the aperture. The aperture is open on either side of the indicator bar.

POLYMERIC SHOCK ABSORBING ELEMENT FOR A VEHICLE AND LONGITUDINAL SIDE MEMBER

Polymeric shock absorbing element for a vehicle including a substantially honeycomb structure having a plurality of channels which has a lateral external surface extending from a first open frontal end to a second open rear end, the shock absorbing element insertable and securable within an internal lateral cavity of a chassis of said vehicle, the internal lateral cavity being defined by at least two metallic plates. The lateral external surface includes at least one substantially planar face positioned on one side of the polymeric shock absorbing element and the additionally includes at least one metallic fixing element having a central portion which in turn includes a first central wall which is made integral with a corresponding substantially planar face of the lateral external surface, the at least one metallic fixing element additionally includes a plurality of side stiffeners which are weldable or made integral with the two metallic sheets. 11020303020221214301012143030149830108585818281828022241010505153242250568182. Polymeric shock absorbing element () for a vehicle comprising a substantially honeycomb structure () having a plurality of channels () realized by moulding into a single piece with a polymeric material , each channel () is preferably equipped with a substantially hexagonal section , additionally said substantially honeycomb structure () has an lateral external surface () which extends from a first open frontal end () to a second open rear end () , said plurality of channels () extends internally to said shock absorbing element () starting from said first open frontal end () to said second open rear end () , additionally each channel () of said plurality of channels () being internally tapered towards said second open rear end () and preferably having an inner rake angle included between 0° and 1.5° measured with respect to a longitudinal extension axis () of each channel () , said shock absorbing element () being insertable and fixable within an ...

Shock Absorbers For Protective Body Gear

A shock absorber includes a bottom rim, a top wall comprising a raised central portion and a top rim, a side wall extending between the top and bottom rims, and a corrugation surrounding a periphery of the raised central portion that (i) connects the raised central portion to the top rim, (ii) descends to a depth below half a height of the side wall, and (iii) is separated by a distance from a surface. Impact forces imparted on the shock absorber are attenuated by a first amount in a first stage by resistive yielding of the side wall; by a second amount in a second stage by depression of the central portion and resistive yielding of the corrugation associated therewith; and by a third amount in a third stage by resistive yielding of the corrugation in response to a force applied to the top rim upon contact with the surface. 1. A shock absorber for attenuating impact forces imparted thereto in stages of differing attenuation , the shock absorber comprising:a top wall comprising a raised central portion and a top rim;a bottom rim;a side wall extending between the top and bottom rims; anda corrugation surrounding a periphery of the raised central portion that (i) connects the raised central portion to the top rim, (ii) descends to a depth below half a height of the side wall, and (iii) is separated by a distance from a surface,wherein the shock absorber is configured to attenuate impact forces imparted on the shock absorber by a first amount in a first stage by resistive yielding of the side wall, by a second amount in a second stage by depression of the central portion and resistive yielding of the corrugation associated therewith, and by a third amount in a third stage by resistive yielding of the corrugation.2. The shock absorber of claim 1 , wherein the first amount is less than the second amount.3. The shock absorber of claim 2 , wherein the second amount is less than the third amount.4. The shock absorber of claim 1 , wherein the side wall comprises a first ...

CRASH BOX AND ITS MANUFACTURING METHOD

A crash box capable of easily deforming into a bellows shape and absorbing impact energy more reliably, and its manufacturing method are provided. The present disclosure is applied to a crash box which is partly deformed in an axial direction to absorb impact energy when the crash box receives an impact in the axial direction. A first layer made of metal and a second layer made of metal containing a larger volume of bubbles than that of the first layer are alternately formed in the axial direction in the crash box according to the present disclosure. 1. A crash box configured so that a part of the crash box is deformed in an axial direction and thereby absorbs impact energy when the crash box receives an impact in the axial direction , whereina first layer made of metal and a second layer made of metal containing a larger volume of bubbles than that of the first layer are alternately formed in the axial direction.2. The crash box according to claim 1 , wherein the first layer and the second layer are integrally formed.3. The crash box according to claim 1 , whereinthe crash box is mounted on a front or rear part of a vehicle in such a position that its axial direction is parallel to a longitudinal direction of the vehicle, whereinthe second layer which is farther from a center of a vehicle contains a larger volume of bubbles than that of the second layer which is closer to the center of the vehicle.4. A manufacturing method of a crash box claim 1 , the crash box being configured so that a part of the crash box is deformed in an axial direction and thereby absorbs impact energy when the crash box receives an impact in the axial direction claim 1 , the manufacturing method including alternately performing:a first step of forming a first layer by irradiating a metal powder with a laser and thereby curing the metal powder; anda second step of forming a second layer by irradiating a metal powder with a laser and thereby curing the metal powder by using a smaller amount ...

Shock absorbing member

A shock absorbing member is provided having a sequential destruction capability and protection against electrolytic corrosion on fastening-fixing portions thereof to be fastened to a bumper reinforcement or a vehicle body. Embodiments include a shock absorbing member between a bumper reinforcement and a vehicle body, including a distal end portion fastened to the bumper reinforcement; a base end flange portion fastened to the vehicle body; and an absorbing member body extending in a vehicle front-rear direction and connecting the distal end portion and the base end flange portion. The absorbing member body includes a carbon fiber-glass reinforced plastic layer. Fastening-fixing portions of the distal end portion and the base end flange portion are composed of glass fiber reinforced plastic layers.

SHOCK ABSORBER SYSTEM COMPRISING A PRIMARY SHOCK ABSORBER DEVICE AND A SECONDARY SHOCK ABSORBER DEVICE OF DIFFERENT STIFFNESSES, ASSOCIATED STRUCTURE AND AIRCRAFT

To increase a compactness of damping systems intended to operate in the event of a dynamic landing of an aircraft, a damping system comprises a primary damper device and a secondary damper device. The primary damper device comprises at least one beam, each beam extending along a direction of a longitudinal axis. The damping system is configured so that at rest, the primary damper device has a stiffness greater than a stiffness of the secondary damper device in the direction of the longitudinal axis. When a force is applied to the damping system along the direction of the longitudinal axis, with a value less than a limit value, each beam remains in a compression state. When the force applied has a value greater than or equal to the limit value, each beam undergoes buckling and the secondary damper device undergoes elastic deformation. 1. A structure for aircraft comprising at least one damping system , each damping system extending along a longitudinal axis and comprising:a first base and a second base arranged at a distance from one another along the longitudinal axis;a primary damper device, the primary damper device comprising at least one beam, each beam extending along a direction parallel to the longitudinal axis, each beam comprising two opposite ends and being attached to the first base by one of its two ends and to the second base by another one of its two ends;a secondary damper device comprising two opposite ends, the secondary damper device being connected to the first base by the one of its two ends, and to the second base by another one of its two ends; at rest, the primary damper device has a stiffness, along the direction of the longitudinal axis, greater than a stiffness of the secondary damper device along the direction of the longitudinal axis;', 'when a force applied to the damping system for urging the first base towards the second base has a value less than a predetermined limit value, each beam remains in a state of compression; and', 'when the ...

FORCE DAMPER

A force damper arranged to progressively arrest a first force imparted by an object moving in a first direction, the force damper including a housing, a driving member and first and second resilient members. The housing includes a first end and a second end, the first end having a first surface, a second surface opposite the first surface and a first connection point secured to the first surface, and the second end having a through bore and a third surface opposingly disposed relative to the second surface. The driving member includes a first end, a second end and a shaft therebetween, the first end having a stop and the second end having a second connection point. At least one of the first and second resilient members is formed from a material that at least partially undergoes plastic deformation when the first force is arrested. The first and second resilient members are disposed between the stop and the third surface and impart a second force on the stop toward the second surface. 1. A force damper arranged to progressively arrest a first force imparted by an object moving in a first direction , the force damper comprising:a housing comprising a first end and a second end, the first end having a first surface, a second surface opposite the first surface and a first connection point secured to the first surface, and the second end having a through bore and a third surface opposingly disposed relative to the second surface;a driving member comprising a first end, a second end and a shaft therebetween, the first end comprises a stop and the second end comprises a second connection point; and,a resilient member formed from a material that at least partially undergoes plastic deformation when the first force is arrested, the resilient member is disposed between the stop and the third surface and imparts a second force on the stop toward the second surface.2. The force damper of wherein the housing encloses the resilient member.3. The force damper of wherein the second ...

Impact absorbing member

An impact absorbing member 10 able to secure absorption energy while lightening weight by absorbing the impact load applied in the axial direction by periodic buckling, wherein the impact absorbing member 10 is provided with a main body 20 comprised of metal sheet and having a polygonal shape in cross-section vertical to an axial direction and a center sheet 30 comprised of metal sheet and provided at a hollow part in the main body along the axial direction, the polygonal shape of the main body 20 includes a pair of long side ( 20 a, 20 b ) facing each other, the center sheet 30 is joined to each of the long sides ( 20 a, 20 b ) of the polygonal shape of the main body 20 , and the sheet thickness t 1 (mm) of the main body 20 and the sheet thickness t 2 (mm) of the center sheet 30 satisfy 1.3×t 1 ≦t 2.

IMPACT ABSORBER

An impact absorber to be mounted between a vehicular panel and a vehicular interior part covering the vehicular panel from a vehicular interior side includes an opposite wall to be opposite the vehicular panel, outer walls extending from edges of the opposite wall toward a vehicular interior side, and an extended wall extending from the opposite wall toward the vehicular interior side and having a side edge connected to the one outer wall, and the extended wall having a thickness that is increased from a vehicular interior end thereof toward a vehicular exterior end thereof, and the extended wall having a cutout hole that is open toward a vehicular exterior side. 1. An impact absorber to be mounted between a vehicular panel and a vehicular interior part covering the vehicular panel from a vehicular interior side , the impact absorber comprising:an opposite wall to be opposite the vehicular panel;outer walls extending from edges of the opposite wall toward a vehicular interior side; andan extended wall extending from the opposite wall toward the vehicular interior side and having a side edge connected to the one outer wall, and the extended wall having a thickness that is increased from a vehicular interior end thereof toward a vehicular exterior end thereof, and the extended wall having a cutout hole that is open toward a vehicular exterior side.2. The impact absorber according to claim 1 , wherein the cutout hole has an opening width that is increased toward the vehicular exterior side.3. The impact absorber according to claim 1 , whereinthe extended wall includes at least four ribs connected to each other in a form of a cross shape seen from the vehicular interior side, andthe cutout hole is at a connecting section of the at least four ribs.4. The impact absorber according to claim 1 , whereinthe extended wall includes ribs extending from a vehicular interior side surface of the opposite wall and each of the ribs has the cutout hole.5. The impact absorber ...

Damper member, damper mechanism, actuator, and damper member manufacturing method

A damper member may include a gel-like member and a first film joined to a first surface of the gel-like member in a thickness direction, in which a side surface of the gel-like member located between a second surface opposite to the first surface of the gel-like member in the thickness direction and the first surface is opened.

COMPOSITE ENERGY-ABSORBING ASSEMBLY HAVING DISCRETE ENERGY-ABSORBING ELEMENTS SUPPORTED BY A CARRIER PLATE

An energy-absorbing assembly for a vehicle includes a carrier plate and a plurality of discrete energy-absorbing elements. The carrier plate includes a first polymer and a first plurality of reinforcing fibers. The plurality of energy-absorbing elements each includes a second polymer and a second plurality of reinforcing fibers. The plurality of energy-absorbing elements is fixed to the carrier plate. Each energy-absorbing element of the first plurality of energy-absorbing elements includes an elongated hollow structure defining a longitudinal axis extending nonparallel to the carrier plate. Another energy-absorbing assembly includes a carrier plate and a plurality of discrete energy-absorbing elements. The carrier plate includes a first polymer and a first plurality of reinforcing fibers. The plurality of energy-absorbing elements each includes a second polymer and a second plurality of reinforcing fibers. Each energy-absorbing element includes a transverse wall and is fixed to the carrier plate. 1. An energy-absorbing assembly for a vehicle comprising:a carrier plate comprising a first polymer and a first plurality of reinforcing fibers; anda first plurality of discrete energy-absorbing elements each comprising a second polymer and a second plurality of reinforcing fibers, the first plurality of energy-absorbing elements being fixed to the carrier plate, each energy-absorbing element of the first plurality of energy-absorbing elements comprising a first elongated hollow structure defining a first longitudinal axis extending nonparallel to the carrier plate.2. The energy-absorbing assembly of claim 1 , wherein the carrier plate defines a plurality of apertures claim 1 , the first elongated hollow structure of each energy-absorbing element of the first plurality of energy-absorbing elements extending through a respective aperture of the plurality of apertures in the carrier plate.3. The energy-absorbing assembly of claim 1 , further comprising:a second plurality of ...

Shock Absorbers For Protective Body Gear

A shock absorber includes a bottom rim, a top wall comprising a raised central portion and a top rim, a side wall extending between the top and bottom rims, and a corrugation surrounding a periphery of the raised central portion that (i) connects the raised central portion to the top rim, (ii) descends to a depth below half a height of the side wall, and (iii) is separated by a distance from a surface. Impact forces imparted on the shock absorber are attenuated by a first amount in a first stage by resistive yielding of the side wall; by a second amount in a second stage by depression of the central portion and resistive yielding of the corrugation associated therewith; and by a third amount in a third stage by resistive yielding of the corrugation in response to a force applied to the top rim upon contact with the surface. 1. A shock absorber for attenuating impact forces imparted thereto in stages of differing attenuation , the shock absorber comprising:a top wall comprising a raised central portion and a top rim;a bottom rim;a side wall extending between the top and bottom rims; anda corrugation surrounding a periphery of the raised central portion that (i) connects the raised central portion to the top rim, (ii) descends to a depth below half a height of the side wall, and (iii) is separated by a distance from a surface,wherein the shock absorber is configured to attenuate impact forces imparted on the shock absorber by a first amount in a first stage by resistive yielding of the side wall, by a second amount in a second stage by depression of the central portion and resistive yielding of the corrugation associated therewith, and by a third amount in a third stage by resistive yielding of the corrugation.2. The shock absorber of claim 1 , wherein the first amount is less than the second amount.3. The shock absorber of claim 2 , wherein the second amount is less than the third amount.4. The shock absorber of claim 1 , wherein the side wall comprises a first ...

VEHICLE

A vehicle includes: a front room disposed at a front part of the vehicle in a longitudinal direction of the vehicle; a fuel cell stack disposed in the front room, the fuel cell stack including multiple cells stacked in the longitudinal direction; a bumper reinforcement disposed at a front part of the front room in the longitudinal direction; and a buffer member disposed between the fuel cell stack and the bumper reinforcement in the longitudinal direction. At least a part of the buffer member overlaps with the bumper reinforcement, as viewed from a direction along the longitudinal direction. 1. A vehicle comprising:a front room disposed at a front part of the vehicle in a longitudinal direction of the vehicle;a fuel cell stack disposed in the front room, the fuel cell stack including multiple cells stacked in the longitudinal direction;a bumper reinforcement disposed at a front part of the front room in the longitudinal direction; anda buffer member disposed between the fuel cell stack and the bumper reinforcement in the longitudinal direction, whereinat least a part of the buffer member overlaps with the bumper reinforcement, as viewed from a direction along the longitudinal direction.2. The vehicle according to claim 1 , further comprising:an auxiliary-device component disposed between the bumper reinforcement and the buffer member, whereinthe buffer member includes a first buffer portion and a second buffer portion having a lower durable load in the longitudinal direction than a durable load of the first buffer portion in the longitudinal direction,the first buffer portion and the second buffer portion are arranged adjacent to each other, andthe first buffer portion is disposed within a range corresponding to an outline of the bumper reinforcement, as viewed from the direction along the longitudinal direction.3. The vehicle according to claim 2 , whereinthe first buffer portion and the second buffer portion are arranged adjacent to each other in a height ...

ENERGY ABSORBER

An energy absorber comprises a base having a weakened portion, a mounting aperture, and a connecting aperture. An energy absorber assembly includes the energy absorber, an anchor member extending through the connecting aperture, a mounting bracket including an aperture, and a fastener extending through the aperture of the mounting bracket and the mounting aperture of the energy absorber. 1. An energy absorber , comprising:a base;a weakened portion in the base, the weakened portion being arranged in a spiral configuration;a mounting aperture in the base proximate an outer portion of the spiral configuration; anda connecting aperture in the base proximate a center of the spiral configuration.2. The energy absorber of claim 1 , wherein the base is a disk member.3. The energy absorber of claim 2 , wherein the disk member is round.4. The energy absorber of claim 1 , wherein the weakened portion includes a plurality of alternating connected portions and cuts extending through the base.5. The energy absorber of claim 4 , wherein the cuts are elongated.6. The energy absorber of claim 1 , wherein the weakened portion forms an elongating portion having an intermediate portion interconnecting a distal end and a proximal end claim 1 , the distal end being positioned proximate the center of the spiral configuration and the proximal end being positioned proximate the outer portion of the spiral configuration claim 1 , the distal end and the intermediate portion being configured to separation from the base and deform to absorb energy.7. The energy absorber of claim 1 , further comprising:an anchor member extending through the connecting aperture;a lifeline operatively connected to the anchor member;an anchorage structure; anda mounting bracket interconnecting the base and the anchorage structure.8. The energy absorber of claim 7 , wherein the anchorage structure is a stanchion.9. The energy absorber of claim 1 , further comprising:an anchor member extending through the connecting ...

LOAD ENERGY-ABSORBER

A fiber-reinforced resin load energy-absorber has: a multi-layer woven fabric or laminated woven fabric as a reinforcement base material; a resin as a matrix; slits; binding threads; and reinforcing members. The reinforcement base material has corners formed by bending said reinforcement base material. Slits are provided at least in the portions of the reinforcement base material that form the corners. The binding threads bind each of the woven fabric layers in the multi-layer woven fabric or laminated woven fabric. The binding threads are configured so as to bind each of the woven fabric layers when the multi-layer woven fabric or laminated woven fabric is divided in the thickness direction into at least two woven fabric layers. The reinforcing members are held inside the slits. 1. A load energy absorber formed by a fiber-reinforced resin , comprising:a multi-layer woven textile or a laminated woven textile serving as a reinforcement base material, wherein the reinforcement base material includes a corner formed by bending the reinforcement base material;a resin serving as a matrix;a slit arranged in the reinforcement base material at a portion where at least the corner is formed;a joining yarn that joins woven layers of the multi-layer woven textile or the laminated woven textile, wherein the joining yarn is configured to join the woven layers in a state in which the woven layers of the multi-layer woven textile or the laminated woven textile are divided into two or more in a thickness-wise direction; anda reinforcement member accommodated inside the slit.2. The load energy absorber according to claim 1 , wherein the reinforcement member is a reinforcement fiber.3. The load energy absorber according to claim 2 , wherein the reinforcement fiber is one of a plurality of reinforcement fibers claim 2 ,the reinforcement fibers are arranged so that fiber axis directions extend in a single direction, andthe main axis direction is a load input direction.4. The load energy ...

Impact absorbing member

The present impact absorbing member includes: a hat-shaped member having a hat top section; and a plate-shaped member facing the hat top section. A deformation guidance section is provided on a wall section of at least one of the hat top section and the plate-shaped member. The deformation guidance section includes: a first high strength section having relatively higher buckling resistance in the wall section; and a pair of low strength sections having relatively lower buckling resistance and arranged on both sides of the first high strength section therebetween in a view along the longitudinal direction. Furthermore, the impact absorbing member includes a pair of second high strength sections disposed on both sides of the deformation guidance section to be adjacent to the pair of low strength sections in a view along the longitudinal direction and having a higher buckling strength relative to the low strength sections.

Vibration dampening compositions

A curable precursor composition for making a vibration damping composition having a density of less than 0.9 g / cm < 3 >, wherein the precursor composition comprises (i) at least one rigid epoxy resin, and (ii) at least one flexible epoxy resin, (iii) a first set of hollow microspheres, (iv) a second set of hollow microspheres, wherein the first set of microspheres differ in composition from the second set of microspheres, and And a curing agent capable of crosslinking the rigid epoxy resin with the flexible epoxy resin. Also provided are vibration dampening compositions obtainable from precursor compositions and methods of making such vibration dampening compositions.

冲击吸收部件

一种能够确保吸收能量且轻量化的、通过周期性的压曲来吸收在轴向上负荷的冲击载荷的冲击吸收部件(10)，冲击吸收部件(10)具备：主体(20)，其由金属板构成，在与轴向垂直的截面中的形状为多边形状；和中板(30)，其由金属板构成，在主体内的中空部沿着轴向设置，主体(20)的多边形状具有互相相对的一对长边(20a、20b)，中板(30)与主体(20)的多边形状的各长边(20a、20b)接合，主体(20)的板厚t1和中板(30)的板厚t2满足1.3×t1≤t2，板厚t1和板厚t2的单位为mm。

Structural members and structural members for vehicles

구조 부재(10)는, 해트 부재(1)와, 클로징 플레이트(2)를 구비한다. 해트 부재(1)와 클로징 플레이트(2)에 의해 형성되는 관형상부의 길이(LY)는, 한 쌍의 측벽(11, 12)의 높이(H)의 6배 이상이다. 한 쌍의 측벽(11, 12)의 각각은, 고강도부(11A, 12A)와 저강도부(11B, 12B)를 포함한다. 고강도부의 항복 강도는, 500MPa 이상이다. 저강도부의 항복 강도는, 고강도부의 항복 강도의 60~85%이다. 고강도부는, 능선의 연장 방향에 있어서의 치수 (2/3)H 이상, 3H 이하의 부분이며 한 쌍의 측벽의 서로 대향하는 부분에 형성된다. 저강도부는, 고강도부의 양측에 배치된다.

Shock absorbing member

吸収エネルギーを確保しつつ軽量化できる、軸方向に負荷される衝撃荷重を周期的な座屈によって吸収する衝撃吸収部材１０あって、衝撃吸収部材１０は、金属板から構成され、軸方向と垂直な断面での形状が多角形状である本体２０と、金属板から構成され、本体内の中空部に軸方向に沿って設けられる中板３０とを備え、本体２０の多角形状は、互いに対向する一対の長辺（２０ａ、２０ｂ）を有し、中板３０は、本体２０の多角形状の各長辺（２０ａ、２０ｂ）に接合され、本体２０の板厚ｔ１（ｍｍ）および中板３０の板厚ｔ２（ｍｍ）が１．３×ｔ１≦ｔ２を満足する。 There is an impact absorbing member 10 that absorbs an impact load applied in the axial direction by periodic buckling, which can reduce the weight while securing the absorbed energy. The impact absorbing member 10 is made of a metal plate and is perpendicular to the axial direction. The main body 20 having a polygonal cross-sectional shape and a middle plate 30 that is formed of a metal plate and is provided along the axial direction in a hollow portion in the main body, the polygonal shapes of the main body 20 face each other. The middle plate 30 has a pair of long sides (20a, 20b), and is joined to each of the polygonal long sides (20a, 20b) of the main body 20, and the thickness t1 (mm) of the main body 20 and the middle plate 30 The plate thickness t2 (mm) satisfies 1.3 × t1 ≦ t2.

Polymeric shock absorbing element for a vehicle and longitudinal side member

Shock-absorbing element

FIELD: machine building.SUBSTANCE: invention relates to the field of transport engineering. Shock-absorbing element absorbing the shock load applied in the axial direction comprises a main body and a central sheet. Main body consists of a metal sheet and has a polygonal shape in cross-section, vertical with respect to the axial direction. Central sheet consists of a metal sheet and is located in the hollow part inside the main body along the axial direction. Polygonal shape of the main body includes a pair of long sides facing each other. Central sheet is connected to each of the long sides of the polygonal shape of the main body. Thickness of the sheet of the center sheet is greater than the thickness of the sheet of the main body.EFFECT: improved absorption of shock energy is achieved.9 cl, 10 dwg РОССИЙСКАЯ ФЕДЕРАЦИЯ (19) RU (11) (13) 2 664 857 C1 (51) МПК F16F 7/12 (2006.01) B60R 19/18 (2006.01) ФЕДЕРАЛЬНАЯ СЛУЖБА ПО ИНТЕЛЛЕКТУАЛЬНОЙ СОБСТВЕННОСТИ (12) ОПИСАНИЕ ИЗОБРЕТЕНИЯ К ПАТЕНТУ (52) СПК F16F 7/12 (2006.01); B60R 19/18 (2006.01) (21)(22) Заявка: 2017116981, 16.10.2015 (24) Дата начала отсчета срока действия патента: Дата регистрации: 23.08.2018 17.10.2014 JP 2014-212631 (56) Список документов, цитированных в отчете о поиске: JP 2007030778 A, 08.02.2007. WO (45) Опубликовано: 23.08.2018 Бюл. № 24 (85) Дата начала рассмотрения заявки PCT на национальной фазе: 17.05.2017 2012026578 A1, 01.03.2012. RU 2283256 C2, 10.09.2006. RU 2460655 C1, 10.09.2012. (86) Заявка PCT: 2 6 6 4 8 5 7 R U (87) Публикация заявки PCT: WO 2016/060255 (21.04.2016) C 1 C 1 JP 2015/079348 (16.10.2015) 2 6 6 4 8 5 7 (73) Патентообладатель(и): НИППОН СТИЛ ЭНД СУМИТОМО МЕТАЛ КОРПОРЕЙШН (JP) Приоритет(ы): (30) Конвенционный приоритет: R U 16.10.2015 (72) Автор(ы): САВА Ясунори (JP), НАКАДЗАВА Йосиаки (JP), ХАМАДА Коити (JP), ИТО Ясунори (JP), ЙОСИДА Хироси (JP) Адрес для переписки: 129090, Москва, ул. Б. Спасская, 25, стр. 3, ООО "Юридическая фирма Городисский и Партнеры" (54) ...

Impact absorption member

흡수 에너지를 확보하면서 경량화할 수 있는, 축 방향으로 부하되는 충격 하중을 주기적인 좌굴에 의하여 흡수하는 충격 흡수 부재(10)이며, 충격 흡수 부재(10)는, 금속판으로 구성되고, 축 방향과 수직인 단면에서의 형상이 다각 형상인 본체(20)와, 금속판으로 구성되고, 본체 내의 중공부에 축 방향을 따라 설치되는 중판(30)을 구비하고, 본체(20)의 다각 형상은, 서로 대향하는 1쌍의 긴 변(20a, 20b)을 갖고, 중판(30)은, 본체(20)의 다각 형상의 각 긴 변(20a, 20b)에 접합되고, 본체(20)의 판 두께 t1(㎜) 및 중판(30)의 판 두께 t2(㎜)가 1.3×t1≤t2를 만족시킨다.

Transmission equipment impact vibration isolator based on foamed aluminum crushing

本发明的目的在于提供一种基于泡沫铝压溃的传动设备冲击隔振器，包括活塞杆、密封罩、隔振器底座、基座，隔振器底座通过安装螺栓固定在基座上，密封罩通过连接螺栓固定在隔振器底座上，隔振器底座设置向上凸起的活塞结构，活塞杆的端部伸入至密封罩里并位于活塞结构内部与活塞结构相配合，活塞杆的端部与活塞结构底部的隔振器底座平面之间设置吸能材料。本发明中利用弹簧和阻尼垫片组成弹簧隔振系统，在受到振动载荷时，主要由弹簧阻尼器作用，减弱并衰减设备运行所产生的振动；弹簧阻尼器具有限位功能，可保证隔振的同时不会产生多大的位移，保证设备的正常运行。在受到冲击时，采用气腔和泡沫铝相结合的方式吸收冲击能量，以保证设备正常运行。

DAMPING SYSTEM COMPRISING A PRIMARY SHOCK ABSORBER DEVICE AND A SECONDARY SHOCK ABSORBER DEVICE OF DIFFERENT RAIDERS, STRUCTURE AND ASSOCIATED AIRCRAFT

Pour augmenter la compacité des systèmes d'amortissement notamment destinés à opérer en cas d'atterrissage dynamique, il est proposé un système d'amortissement (4) comportant un dispositif amortisseur primaire (12) et un dispositif amortisseur secondaire (14), le dispositif amortisseur primaire (12) comportant au moins une poutre (16), chaque poutre (16) s'étendant le long d'un axe longitudinal (X-X), le système d'amortissement (4) étant configuré de sorte que : - au repos, le dispositif amortisseur primaire (12) présente une raideur supérieure à la raideur du dispositif amortisseur secondaire (14) selon l'axe longitudinal (X-X) ; - lorsqu'un effort appliqué au système d'amortissement (4) suivant l'axe longitudinal (X-X) présente une valeur inférieure à une valeur limite, chaque poutre (16) demeure dans un état de compression ; et - lorsque l'effort présente une valeur supérieure ou égale à la valeur limite, chaque poutre (16) subit un flambage et le dispositif amortisseur secondaire (14) subit une déformation élastique. In order to increase the compactness of the damping systems intended in particular to operate in the event of a dynamic landing, it is proposed a damping system (4) comprising a primary damping device (12) and a secondary damping device (14), the device primary damper (12) comprising at least one beam (16), each beam (16) extending along a longitudinal axis (XX), the damping system (4) being configured so that: - at rest , the primary damping device (12) has a stiffness greater than the stiffness of the secondary damping device (14) along the longitudinal axis (XX); when a force applied to the damping system (4) along the longitudinal axis (X-X) has a value less than a limit value, each beam (16) remains in a compression state; and when the force has a value greater than or equal to the limit value, each beam (16) undergoes buckling and the secondary damping device (14) undergoes elastic deformation.

Torque rod

Fuel cell vehicle

The damping system of main damper device and secondary damper device including different-stiffness, dependency structure and aircraft

为了增加特别是意在在动态着陆的情况下操作的阻尼系统的紧凑性，提出了一种阻尼系统(4)，该阻尼系统包括主阻尼器装置(12)和副阻尼器装置(14)。主阻尼器装置(12)包括至少一个梁(16)，每个梁(16)沿着纵向轴线(X‑X)延伸，阻尼系统(4)构造成使得：在静止时，沿着纵向轴线(X‑X)主阻尼器装置(12)的刚度大于副阻尼器装置(14)的刚度；当沿着纵向轴线(X‑X)施加至阻尼系统(4)的力具有小于极限值的值时，每个梁(16)保持在压缩状态中；并且当力具有大于或等于极限值的值时，每个梁(16)经受屈曲并且副阻尼器装置(14)经受弹性变形。

Impact-resilient mounted table device

In a table device (100) with a tabletop (110), which is coupled to a support strut (120) for mounting on a wall for purposes of a support, a danger of injury to a person located in its vicinity during a sudden acceleration, especially in the direction of travel, is significantly reduced as compared to the known table devices (110) in that the tabletop (110) is fastened to a carrier platform (140) provided with mechanical damping elements (130, 131; 130′, 131′) and is indirectly connected to the support strut (120) across the mechanical damping elements (130, 131; 130′, 131′).

Break-away cradle or sub-frame mount and retainer washer assembly

An isolator assembly (20) such as a cradle mount or a body mount assembly incorporates break-away features. An insert (70, 70~) includes a thinned cross-sectional region (100) or a gap/interface (90) between insert portions (70a, 70b) that allow a bolt (24) to break-away under a predetermined load in a fore direction (80) and an aft direction (90). In addition, a retainer washer (50) may have an irregular configuration such as a tear-drop or clover-leaf configuration that cooperates with the insert (70, 70~) to allow the isolator assembly (20) to pull away in the negative z-direction under a predetermined load.

Crash box and its manufacturing method

A crash box capable of easily deforming into a bellows shape and absorbing impact energy more reliably, and its manufacturing method are provided. The present disclosure is applied to a crash box which is partly deformed in an axial direction to absorb impact energy when the crash box receives an impact in the axial direction. A first layer made of metal and a second layer made of metal containing a larger volume of bubbles than that of the first layer are alternately formed in the axial direction in the crash box according to the present disclosure.

Vibration dampening compositions

A curable precursor composition for preparing a vibration dampening composition having a density of less than 0.9 g/cm said precursor composition comprising (i) one or more rigid epoxy resin (ii) one or more flexible epoxy resin, (iii) a first set of hollow microspheres, (iv) a second set of hollow microspheres wherein the microspheres of the first set are different in composition from the microspheres of the second set and, a curing agent capable of cross-linking the rigid and flexible epoxy resins. Also provided are vibration dampening compositions obtainable from the precursor compositions and methods of preparing such vibration dampening compositions.

Sound insulating, shock absorbing and heat resisting ABS resin composition for automobile interior and preparation method of ABS resin composition

本发明涉及一种汽车内饰用隔音减震耐热ABS树脂组合物及其制备方法，所述树脂组合物包含以下组分和含量：ABS树脂100重量份，耐热剂5～30重量份，隔音减震聚合物5～20重量份，空心玻璃微珠1～5重量份，光稳定剂0.3～1.0重量份，助剂0.5～2.0重量份。将上述原材料在高速混合机内搅拌充分混合后，经计量装置送入双螺杆挤出机中，在螺杆的输送、剪切和混炼下，物料熔化、复合，再经挤出、拉条、冷却、切粒步骤，得到汽车内饰用隔音减震耐热ABS树脂组合物。本发明的方法简单易行，制备的树脂组合物不仅具有优异的隔音减震效果，同时机械性能良好，非常适合应用于汽车内饰领域。

Seismic isolation device

Break-away cradle or sub-frame mount and retainer washer assembly

An isolator assembly (20) such as a cradle mount or a body mount assembly incorporates break-away features. An insert (70, 70’) includes a thinned cross-sectional region (100) or a gap/interface (90) between insert portions (70a, 70b) that allow a bolt (24) to break-away under a predetermined load in a fore direction (80) and an aft direction (90). In addition, a retainer washer (50) may have an irregular configuration such as a tear-drop or clover-leaf configuration that cooperates with the insert (70, 70’) to allow the isolator assembly (20) to pull away in the negative z-direction under a predetermined load.

Seismic isolation device

A seismic isolation apparatus 1 includes a laminated body 7 having alternately laminated rubber plates 2 and steel plates 3; a hollow portion 8 provided inside the laminated body 7 in a hermetically closed manner and extending in a laminated direction A; a lead plug 9 filled densely in the hollow portion 8 and adapted to damp the vibration in a shearing direction B of the laminated body 7 by absorbing vibrational energy in the shearing direction B; and a lid member 14 having a semispherical concave surface 12 which comes into contact with one end portion 11 in the laminated direction A of the lead plug 9 in order to guide and assist the plastic flow of the lead plug 9 at one end portion 10 in the laminated direction A of the hollow portion 8 in the deformation in the shearing direction B of the lead plug 9.

SHOCK ABSORBING POLYMERIC ELEMENT FOR A VEHICLE, LONGITUDINAL SIDE LIMB AND VEHICLE

ELEMENTO POLIMÉRICO DE ABSORÇÃO DE CHOQUE PARA UM VEÍCULO, MEMBRO LATERAL LONGITUDINAL E VEÍCULO. Elemento polimérico de absorção de choque (10) para um veículo, compreendendo uma estrutura substancialmente alveolar tendo uma pluralidade de canais (30) possuindo uma superfície lateral externa (22) que se estende a partir de uma primeira extremidade frontal aberta (12) até uma segunda extremidade traseira aberta (14), com o elemento de absorção de choque (10) sendo inserível e fixável dentro de uma cavidade lateral interna (85) do chassis do referido veículo, e a referida cavidade lateral interna (85) sendo definida por pelo menos duas placas metálicas (81) e (82). A superfície lateral externa (22) compreende pelo menos uma face substancialmente plana (24) posicionada em um lado do elemento polimérico de absorção de choque (10), com o mesmo compreendendo adicionalmente pelo menos um elemento metálico de fixação (50) incluindo uma porção central (51), que por sua vez compreende uma primeira parede central (53) formada integralmente com uma face substancialmente plana (24) correspondente da referida superfície externa lateral (22), com pelo menos um elemento metálico de fixação (50) compreendendo adicionalmente uma pluralidade de reforços laterais (56) que são soldados ou formados integralmente com as duas placas metálicas (81) e (82). POLYMERIC SHOCK ABSORBING ELEMENT FOR A VEHICLE, LONGITUDINAL SIDE LIMB AND VEHICLE. A polymeric shock absorbing element (10) for a vehicle, comprising a substantially honeycomb structure having a plurality of channels (30) having an outer side surface (22) extending from a first open front end (12) to a second open rear end (14), with the shock absorbing element (10) being insertable and fixable within an inner side cavity (85) of the chassis of said vehicle, and said inner side cavity (85) being defined by at least least two metallic plates (81) and (82). The outer side surface (22) comprises at least one substantially flat face (24) ...

Seismic isolation device

면진 장치(1)는, 교대로 적층된 고무판(2) 및 강판(3)을 갖는 적층체(7)와, 적층체(7)의 내부에 밀폐되어 설치되어 있음과 아울러 적층 방향(A)으로 연장된 중공부(8)와, 중공부(8)에 조밀하게 충전되어 있음과 아울러 전단 방향(B)의 진동 에너지를 흡수하여 적층체(7)의 전단 방향(B)의 진동을 감쇠시키는 납 플러그(9)와, 납 플러그(9)의 전단 방향(B)의 변형에 있어서 중공부(8)의 적층 방향(A)의 일단부(10)에서의 납 플러그(9)의 소성 유동을 안내 보조하기 위해, 납 플러그(9)의 적층 방향(A)의 일단부(11)에 접촉하는 반오목구면(12)를 갖고 있는 덮개 부재(14)를 구비하고 있다. The seismic isolator 1 is a laminate 7 having a rubber plate 2 and a steel plate 3 laminated alternately, and is sealed and installed inside the laminate 7 in the lamination direction (A). Lead that is densely filled in the extended hollow portion (8) and the hollow portion (8) and absorbs vibration energy in the shear direction (B) to attenuate the vibration in the shear direction (B) of the laminate (7) In the deformation of the plug 9 and the shear direction B of the lead plug 9, the plastic flow of the lead plug 9 is guided at the one end 10 in the stacking direction A of the hollow part 8 In order to assist, a cover member 14 having a semi-concave spherical surface 12 contacting one end 11 in the stacking direction A of the lead plug 9 is provided.

Structural element for vehicle (embodiments)

FIELD: machine building. SUBSTANCE: group of inventions relates to the field of transport machine building. Embodiments of a structural element for a vehicle comprise a closing plate and a trough-shaped element. Trough-shaped element comprises an upper portion, two first ribs arranged at both edges of the upper portion, two flanges connected to the closing plate, two second ribs arranged on the edges of the two flanges, and two side walls located between the first rib and the second rib. Side walls include high-strength section and low strength sections. Sections of high strength of two side walls face each other and have yield point not less than 500 MPa. Sections of low strength have yield point making from 60 to 85 % of yield point of high strength section. Structural element for vehicle comprises said structural element installed on vehicle. EFFECT: reduced deformation of structural section as a result of impact. 19 cl, 35 dwg, 5 tbl

Impact force dampening and defusing structure

An impact force dampening and defusing structure includes a plurality of components arranged in a grid array. A component has a three-dimensional geometric shape that includes an impact receiving surface area and an impact defusing surface area. The impact defusing surface area is larger than, and a distance “d” from, the impact receiving surface area. The component includes a material composition and, when an impact force strikes the impact receiving surface area of the component and the impact force dampening and defusing structure is in position to protect a body part, the component contributes to reducing pressure on the body part based on the material composition, the distance “d”, the impact receiving surface area, and the impact defusing surface area.

Impact absorbing member

An impact absorbing member able to secure absorption energy while lightening weight by absorbing the impact load applied in the axial direction by periodic buckling, wherein the impact absorbing member is provided with a main body comprised of metal sheet and having a polygonal shape in cross-section vertical to an axial direction and a center sheet comprised of metal sheet and provided at a hollow part in the main body along the axial direction, the polygonal shape of the main body includes a pair of long side facing each other, the center sheet is joined to each of the long sides of the polygonal shape of the main body, and the sheet thickness t1 (mm) of the main body and the sheet thickness t2 (mm) of the center sheet satisfy 1.3xt1<=t2.

Torque rod

Vehicle

一种车辆，包括：前室，所述前室在车辆的纵向方向上被布置在车辆的前部处；燃料电池堆，所述燃料电池堆被布置在前室中，所述燃料电池堆包括在纵向方向堆叠上的多个电池；保险杠加强件，所述保险杠加强件在纵向方向上被布置在前室的前部处；和缓冲构件，所述缓冲构件在纵向方向上被布置在燃料电池堆和保险杠加强件之间。在从沿着纵向方向的方向观察时，缓冲构件的至少一部分与保险杠加强件重叠。

Energy absorber

An energy absorber comprises a base having a weakened portion, a mounting aperture, and a connecting aperture. An energy absorber assembly includes the energy absorber, an anchor member extending through the connecting aperture, a mounting bracket including an aperture, and a fastener extending through the aperture of the mounting bracket and the mounting aperture of the energy absorber.

Vibration dampening compositions

A curable precursor composition for preparing a vibration dampening composition having a density of less than 0.9 g/cm said precursor composition comprising (i) one or more rigid epoxy resin (ii) one or more flexible epoxy resin, (iii) a first set of hollow microspheres, (iv) a second set of hollow microspheres wherein the microspheres of the first set are different in composition from the microspheres of the second set and, a curing agent capable of cross-linking the rigid and flexible epoxy resins. Also provided are vibration dampening compositions obtainable from the precursor compositions and methods of preparing such vibration dampening compositions.

Torque rod

具有：第1环状部(11)，其与用于连结于动力单元的第1安装构件(14)弹性地连结在一起；第2环状部(12)，其与用于连结于车辆的第2安装构件(15)弹性地连结在一起；连结撑条部(13)，其从第2环状部(12)的外周部分向径向外侧延伸而与第1环状部(11)的外周部分相连，具有上股部(16)和弯曲强度设定得比上股部(16)的弯曲强度低的下股部(17)；壁部(20)，其与第1环状部(11)和连结撑条部(13)相连，形成空腔部(21)，第1环状部(11)的一部分暴露于空腔部(21)；以及突起部(23)，其从第1环状部(11)中的暴露于空腔部(21)的部位(22)沿着第1环状部(11)的轴向突出。

Force defusing structure

A force defusing structure includes first and second plurality of spherical shaped objects. A first spherical shaped object is proximally positioned to two or more second spherical shaped objects. When a force is applied to the first spherical shaped object, the first spherical shaped object collides with the two or more second spherical shaped objects to defuse the force based on a multi-dimensional collision between the first spherical shaped object and the two or more second spherical shaped objects.

Impact absorbing member

An impact absorbing member able to secure absorption energy while lightening weight by absorbing the impact load applied in the axial direction by periodic buckling, wherein the impact absorbing member is provided with a main body comprised of metal sheet and having a polygonal shape in cross-section vertical to an axial direction and a center sheet comprised of metal sheet and provided at a hollow part in the main body along the axial direction, the polygonal shape of the main body includes a pair of long side facing each other, the center sheet is joined to each of the long sides of the polygonal shape of the main body, and the sheet thickness t1 (mm) of the main body and the sheet thickness t2 (mm) of the center sheet satisfy 1.3xt1<=t2.

Polymer impact absorbing member for vehicle and longitudinal side member

车辆用聚合物冲击吸收部件(10)包括具有多个通道(30)的基本蜂巢状结构，所述基本蜂巢状结构具有从第一开口前端(12)延伸到第二开口后端(14)的横向外表面(22)，冲击吸收部件(10)可插入和固定在所述车辆的底盘的内部横腔(85)内，内部横腔(85)由至少两个金属板(81)和(82)限定。横向外表面(22)包括被定位在聚合物冲击吸收部件(10)的一侧的至少一个基本平面的面(24)，另外还包括至少一个金属固定部件(50)，金属固定部件(50)包括中心部分(51)，中心部分(51)又包括与横向外表面(22)的对应的基本平面的面(24)制成一体的第一中心壁(53)，所述至少一个金属固定部件(50)另外还包括可焊接的或者被与所述两个金属板(81)和(82)制成一体的多个横向加固件(56)。

Shock absorbing apparatus

避震装置(1)包括：层叠体(7)，所述层叠体(7)具有交替层叠的橡胶板(2)和钢板(3)；中空部(8)，所述中空部(8)密闭地设于层叠体(7)的内部，并且沿层叠方向(A)延伸；铅塞(9)，所述铅塞(9)紧密地填充于中空部(8)，并且对剪切方向(B)的振动能进行吸收，以使层叠体(7)的剪切方向(B)的振动衰减；以及盖构件(14)，所述盖构件(14)具有半凹球面(12)，所述半凹球面(12)与铅塞(9)的层叠方向(A)的一端部(11)接触，在铅塞(9)发生剪切方向(B)的变形的情况下，对中空部(8)的层叠方向(A)的一端部(10)中的铅塞(9)的塑性流动进行引导辅助。

衝撃吸収部材

この衝撃吸収部材は、ハット頂部を有するハット型部材と、前記ハット頂部に対向する板状部材とを有する。前記ハット頂部及び前記板状部材の少なくとも一方の壁部には、変形誘導部が設けられている。前記変形誘導部が、前記壁部において相対的に座屈耐力が高い第１高強度部と、相対的に座屈耐力が低くてかつ長手方向に沿って見た場合に前記第１高強度部を間に挟む両側に配置された一対の低強度部と、を有している。さらに、この衝撃吸収部材は、前記長手方向に沿って見た場合に、前記一対の低強度部のそれぞれに隣接するように前記変形誘導部の両側に配置され、前記低強度部に対して相対的に座屈強度が高い一対の第２高強度部を有する。

Miembro de absorcion de impacto.

El presente miembro de absorción de impacto incluye: un miembro en forma de sombrero que tiene una sección superior del sombrero; y un miembro en forma de placa que mira a la sección superior del sombrero. Una sección de guía de deformación se provee en una sección de pared de al menos una de la sección superior del sombrero y el miembro en forma de placa. La sección de guía de deformación incluye: una primera sección de alta resistencia que tiene una resistencia al pandeo relativamente mayor en la sección de pared; y un par de secciones de baja resistencia que tienen una resistencia al pandeo relativamente menor y dispuestas a ambos lados de la primera sección de alta resistencia entre ellas en una vista a lo largo de la dirección longitudinal. Además, el miembro de absorción de impacto incluye un par de segundas secciones de alta resistencia dispuestas en ambos lados de la sección de guía de deformación para ser adyacentes al par de secciones de baja resistencia en una vista a lo largo de la dirección longitudinal y que tienen una mayor resistencia al pandeo en relación con las secciones de baja resistencia.

冲击吸收构件

本发明目的在于提供一种冲击吸收构件，该冲击吸收构件能够构成带有逐次破坏功能的冲击吸收构件，且能够防止紧固结合固定部对保险杠加强件或车身的腐蚀（电蚀）。本发明是一种设于保险杠加强件和车身之间的冲击吸收构件（10），上述冲击吸收构件（10）具备：与保险杠加强件紧固结合的前端部（20）、与车身紧固结合的基端法兰部（30）、在车辆前后方向延伸并连结上述前端部（20）和上述基端法兰部（30）的吸收构件主体部（40），上述吸收构件主体部40具备碳纤维增强塑料层（40C），上述前端部（20）和上述基端法兰部30的紧固结合固定部位（A´，D´）由玻璃纤维增强塑料层（20G，30G）形成。

冲击吸收构件

本发明目的在于提供一种冲击吸收构件，该冲击吸收构件能够构成带有逐次破坏功能的冲击吸收构件，且能够防止紧固结合固定部对保险杠加强件或车身的腐蚀（电蚀）。本发明是一种设于保险杠加强件和车身之间的冲击吸收构件（10），上述冲击吸收构件（10）具备：与保险杠加强件紧固结合的前端部（20）、与车身紧固结合的基端法兰部（30）、在车辆前后方向延伸并连结上述前端部（20）和上述基端法兰部（30）的吸收构件主体部（40），上述吸收构件主体部40具备碳纤维增强塑料层（40C），上述前端部（20）和上述基端法兰部30的紧固结合固定部位（A´，D´）由玻璃纤维增强塑料层（20G，30G）形成。

Stossdämpfungselement

Die Erfindung umfasst ein Stoßdämpfungselement, das zwischen einer Stoßfängerverstärkung und einer Fahrzeugkarosserie vorgesehen ist, wobei das Stoßdämpfungselement enthält: einen distalen Endabschnitt, der an der Stoßfängerverstärkung befestigt ist; einen Basisendflanschabschnitt, der an der Fahrzeugkarosserie befestigt ist; und einen Dämpfungselementkörper, der sich in einer Fahrzeug-Vorne-Hinten-Richtung erstreckt und den distalen Endabschnitt und den Basisendflanschabschnitt verbindet, wobei der Dämpfungselementkörper so gebildet ist, dass er eine kohlenstofffaserverstärkte Kunststoffschicht enthält, und Befestigungs-/Fixier-Abschnitte des distalen Endabschnitts und des Basisendflanschabschnitts aus glasfaserverstärkten Kunststoffschichten gebildet sind.

衝撃吸収部材

Shock absorbing member

A shock absorbing member is provided having a sequential destruction capability and protection against electrolytic corrosion on fastening-fixing portions thereof to be fastened to a bumper reinforcement or a vehicle body. Embodiments include a shock absorbing member between a bumper reinforcement and a vehicle body, including a distal end portion fastened to the bumper reinforcement; a base end flange portion fastened to the vehicle body; and an absorbing member body extending in a vehicle front-rear direction and connecting the distal end portion and the base end flange portion. The absorbing member body includes a carbon fiber-glass reinforced plastic layer. Fastening-fixing portions of the distal end portion and the base end flange portion are composed of glass fiber reinforced plastic layers.

可重复缓冲减振与吸能耦合作用的负刚度巷道o型棚支护

一种可重复缓冲减振与吸能耦合作用的负刚度巷道O型棚支护，包括U型钢外圈支架、U型钢内圈支架及二维负刚度结构带；U型钢内外圈支架为同心分布，二维负刚度结构带设在U型钢内外圈支架间的环形空间内；U型钢内外圈支架均由四根U型钢首尾相接而成，U型钢外圈支架的相邻U型钢之间由缓冲吸能接头构件固连，U型钢内圈支架的相邻U型钢之间由卡子固连；二维负刚度结构带与U型钢内外圈支架间均由卡缆固接。本发明在巷道支护体系内引入了负刚度结构和吸能结构，对巷道支护系统的防冲和减震控制更加理想，充分利用负刚度结构可重复性，使巷道支护系统具有持续防冲、多次吸能及减震的能力，延长了巷道支护系统的使用寿命，提高了结构承载力。

可重复缓冲减振与吸能耦合作用的负刚度巷道o型棚支护

一种可重复缓冲减振与吸能耦合作用的负刚度巷道O型棚支护，包括U型钢外圈支架、U型钢内圈支架及二维负刚度结构带；U型钢内外圈支架为同心分布，二维负刚度结构带设在U型钢内外圈支架间的环形空间内；U型钢内外圈支架均由四根U型钢首尾相接而成，U型钢外圈支架的相邻U型钢之间由缓冲吸能接头构件固连，U型钢内圈支架的相邻U型钢之间由卡子固连；二维负刚度结构带与U型钢内外圈支架间均由卡缆固接。本发明在巷道支护体系内引入了负刚度结构和吸能结构，对巷道支护系统的防冲和减震控制更加理想，充分利用负刚度结构可重复性，使巷道支护系统具有持续防冲、多次吸能及减震的能力，延长了巷道支护系统的使用寿命，提高了结构承载力。

Landing gear and stiffening member

A landing gear includes a pair of skids, a cross tube and a stiffening portion. The pair of skids is arranged in parallel with a front-rear axis of an airframe of a rotary wing aircraft. The cross tube is attached to the airframe and coupling the pair of skids to each other. The cross tube includes curved portions located closer to end portions of the cross tube than to portions of the cross tube attached to the airframe. The stiffening portion suppresses flattening of the cross tube and is arranged in at least one of internal spaces of the curved portions or a stiffened portion located between a pair of curved portions. The stiffening portion includes an enlarged diameter portion which increases in diameter by an axial fastening power acting in an axial direction of the cross tube, and a fastening portion configured to generate the axial fastening power.

Use of thermoplastic polyurethane and impact resistant composite laminate

Provided are a use of a thermoplastic polyurethane for forming an impact resistant layer and an impact resistant composite laminate (1, 1', 1"). The thermoplastic polyurethane comprises a structural unit represented by Formula (I): wherein each R independently is an alkylene group having 2 to 8 carbon atoms or CH 2 CH 2 OCH 2 CH 2 ; n is a number from 2 to 13; and the structural unit has a Mn ranging from 700 g/mole to 2500 g/mole. In addition, the impact resistant layer has a thickness of larger than 1.5 mm. The impact resistant composite laminate (1, 1', 1") comprises a base layer (20) and the impact resistant layer disposed on the base layer (20).

Apparatuses, systems, and materials for stiffness and damping control including ribbed geometry, and associated methods

Embodiments described herein relate generally to apparatus with ribbed structures or geometries for stiffness and damping control, and methods of producing the same. In some embodiments, an apparatus includes a ribbed structure having a set of ribs, configured to deform elastically under shock. In some embodiments, the set of ribs can have a sinusoidal wave shape. In some embodiments, the set of ribs can have a heterogeneous wave shape. In some embodiments, the set of ribs can have material properties that change along the length of the ribbed structure, such as wavelength, amplitude, wave shape, and material thickness.

ダンパ部材、ダンパ機構、アクチュエータおよびダンパ部材の製造方法

【課題】共振の抑制等にゲル状部材を利用した場合でも、取扱いが容易なダンパ部材、ダンパ機構、アクチュエータおよびダンパ部材の製造方法を提供すること。【解決手段】アクチュエータにおいて、第１部材と第２部材との間に構成されるダンパ機構のダンパ部材９は、ゲル状部材９５と、ゲル状部材９５の一方面９５１に接合された第１フィルム９１と、ゲル状部材９５の他方面９５２に接合された第２フィルム９２とを有しており、側面９５３は、開放状態にある。ダンパ部材９の一方面９５１の側は、第１フィルム９１を介して第１部材に接着剤によって固定され、ダンパ部材９の他方面９５２の側は、第２フィルム９２を介して第２部材に接着剤によって固定される。第１フィルム９１は、ゲル状部材９５の一方面９５１よりサイズが大きく、第１フィルム９１の端部は、全周にわたってゲル状部材９５の側面９５３から張り出している。【選択図】図６

一种内凹型负泊松比吸能结构

本发明涉及负泊松比超材料，能量吸收技术领域，尤其是涉及一种内凹型负泊松比吸能结构。内凹型负泊松比吸能结构包括多个单胞结构；所述单胞结构包括底部、顶部和肋板；所述底部和顶部为对称结构，底部和顶部位于同一侧的端部通过肋板连接，所述肋板、底部和顶部均为曲线结构。将传统内凹型结构与底部与顶部呈一定角度的直线肋部改成曲线结构，将原有的内凹型结构的顶部与底部也改成曲线结构。通过将肋部改成曲线肋，降低应力集中现象。

一种圆台形双稳态吸能阵列结构

本发明属于吸能材料技术领域，具体为一种圆台形双稳态吸能阵列结构。本发明阵列结构由若干胞元堆叠而成；胞元由16根螺旋形梁组成；其中8根螺旋形梁按顺时针方向均匀排布，另8根螺旋形梁按逆时针方向均匀排布，并与顺时针均匀排布的8根螺旋形梁交叉，围成一空间圆形锥台；梁上、下两端分别由两块块圆形板固接，形成空间网格式“圆台形状”；当胞元的上板受压时向下移动，梁结构逐渐内凹到达第二个稳态；将胞元的上板上拉则回到第一个稳态。可采用3D打印、采用焊接或切削方式制备。本发明阵列结构拉压性能可通过改变梁直径、形状进行调整改变，以满足多种不同场合的性能需求，可广泛应用于各类机械设备，实现诸如自锁、支撑、展开等功能。

結合された螺旋状圧縮ばね

【課題】広範な用途に対して十分な剛性を提供できる、軽量の圧縮ばねであり、疲労および腐食への耐性が改善されたばねを提供する。【解決手段】結合された螺旋状圧縮ばね１０。このばねは、連続した波形の山部１４および谷部１６を有する複数の層１２を含む。第１層の第１山部および第１谷部は、隣接する第２層の第２谷部および第２山部とそれぞれ位置合わせされるとともに、隣接する第３層の第３谷部および第３山部とそれぞれ位置合わせされる。第１層の第１山部は、隣接する第２層の第２谷部に結合され、第１層の第１谷部は、隣接する第３層の第３山部に結合される。隣接する層の山部および谷部は互いに結合され、山部と谷部との間の摩擦は排除される。【選択図】図１

Landing device and stiffened member

A landing gear (10) includes: a pair of skids (20) arranged in parallel with a front-rear axis of an airframe (12) of a rotary wing aircraft (11); a cross tube (30) attached to the airframe and coupling the pair of skids to each other, the cross tube (30) including an internal space; and a stiffening portion (40) configured to suppress flattening of the cross tube. The cross tube includes: curved pipe parts (37) located closer to corresponding end portions (31) of the cross tube than corresponding attached portions (35) of the cross tube, the attached portions being attached to the airframe; and a middle portion (32) located at opposite sides of the curved pipe parts (37) across the attached portions. The stiffening portion is arranged in at least one of internal spaces of pipe parts that are the curved pipe parts (37) and a pipe part located between the pair of curved pipe parts (37).

Landing gear and stiffening member

A landing device (10) comprises: a pair of skids (20) arranged parallel to a longitudinal axis of an airframe (12) of a rotary wing aircraft (11); a cross tube (30) that is mounted to the airframe, that links the pair of skids, and that has an internal space; and a stiffened part (40) that minimizes flattening of the cross tube. The cross tube has a curved tube portion (37) nearer to an end part (31) than a part (35) mounted with the airframe, and a center part (32) nearer to the side opposite the curved tube portion (37) than the mounted part. The stiffened part is arranged in the internal space of at least one pipe portion among the curved tube portion (37) and the pair of curved tube portions (37).

降着装置及び補剛部材

【課題】大きな着陸エネルギを吸収しつつ、地上共振を回避することができる降着装置を提供する。【解決手段】降着装置１０は、回転翼航空機１１の機体１２の前後軸に平行に配置される一対のスキッド２０と、前記機体に装着され、一対の前記スキッドを連結し、且つ、内部空間を有するクロスチューブ３０と、前記クロスチューブの扁平化を抑制する補剛部４０と、を備え、前記クロスチューブは、前記機体との装着部３５よりも端部３１側に湾曲管部分３７、及び、前記装着部よりも前記湾曲管部分３７側と反対側の中央部３２を有し、前記補剛部は、前記湾曲管部分３７及び一対の前記湾曲管部分３７の間のうちの少なくともいずれかの管部分の内部空間に配置されている。【選択図】図３

Landing gear and stiffening member

A landing gear includes a pair of skids, a cross tube and a stiffening portion. The pair of skids is arranged in parallel with a front-rear axis of an airframe of a rotary wing aircraft. The cross tube is attached to the airframe and coupling the pair of skids to each other. The cross tube includes curved portions located closer to end portions of the cross tube than to portions of the cross tube attached to the airframe. The stiffening portion suppresses flattening of the cross tube and is arranged in at least one of internal spaces of the curved portions or a stiffened portion located between a pair of curved portions. The stiffening portion includes an enlarged diameter portion which increases in diameter by an axial fastening power acting in an axial direction of the cross tube, and a fastening portion configured to generate the axial fastening power.

组合式复合金属能量吸收器

一种组合式复合金属能量吸收器，包括复合结构以及具有第一部分和第二部分的第一金属管，第一部分连结到复合结构。复合结构和第一金属管具有定制挤压曲线，以避免复合结构和第一金属管中任一个的过早压坏。

二级缓冲吸能薄壁管结构及其制作方法

本发明公开了一种二级缓冲吸能薄壁管结构及其制作方法，包括竖直设置的鼓形管、同轴设置在鼓形管内且两端超出鼓形管的喇叭内管、用于密封鼓形管上端的上外封盖、用于密封鼓形管下端的下外封盖、与上外封盖平齐且用于密封喇叭内管上端的上内封盖以及与下外封盖平齐且用于密封喇叭内管下端的下内封盖。本发明采用鼓形管与喇叭内管组合且喇叭内管上下高出鼓形管；当薄壁管结构受到轴向冲击时，首先接触到喇叭内管的上端突出部分，喇叭内管率先结构变形，在一级吸能阶段由于喇叭形状可以有效地诱导结构变形，从而有效降低冲击中的初始峰值力；在二级吸能阶段鼓形管的结构使得在受到轴向载荷时易按照预设的路径形式发生变形，进一步提高吸能效率。

二级缓冲吸能薄壁管结构及其制作方法

本发明公开了一种二级缓冲吸能薄壁管结构及其制作方法，包括竖直设置的鼓形管、同轴设置在鼓形管内且两端超出鼓形管的喇叭内管、用于密封鼓形管上端的上外封盖、用于密封鼓形管下端的下外封盖、与上外封盖平齐且用于密封喇叭内管上端的上内封盖以及与下外封盖平齐且用于密封喇叭内管下端的下内封盖。本发明采用鼓形管与喇叭内管组合且喇叭内管上下高出鼓形管；当薄壁管结构受到轴向冲击时，首先接触到喇叭内管的上端突出部分，喇叭内管率先结构变形，在一级吸能阶段由于喇叭形状可以有效地诱导结构变形，从而有效降低冲击中的初始峰值力；在二级吸能阶段鼓形管的结构使得在受到轴向载荷时易按照预设的路径形式发生变形，进一步提高吸能效率。

衝撃吸収体

【課題】ドアトリムの背面に設ける衝撃吸収体の衝撃吸収特性の安定性を向上させる。【解決手段】衝撃吸収体２２は、ドアトリム１２の背面に取り付けられ、ドアに加わる衝撃を吸収する。衝撃吸収体２２の四角筒体２８、４８は、筒先端面に端板３８を備え、ドアトリム１２の背面と対面している。四角筒体２８は、上板３０、下板３４と、前側板によって三側面が閉じられているが、残る一側面は開放されており、略コの字の形状からなる。【選択図】図４

仿蒲草缓冲吸能薄壁复合结构

本发明公开了一种仿蒲草缓冲吸能薄壁复合结构，包括由若干个仿蒲草月牙结构对称组合而成的仿生结构，仿蒲草月牙结构包括外弧板、内弧板、用于连接外弧板和内弧板侧边的连接平板以及均布于外弧板和内弧板之间的若干个肋板。本发明的仿生结构是由仿蒲草月牙结构组合而成，从蒲草内部特征衍生设计，整个仿生结构包含多级形态能够有效的促进仿生结构在受轴向冲击时将冲击能分散到不同的结构层次中从而缓冲作用在结构表面的冲击力；在冲击过程中，月牙外侧所受的应力大于内侧应力，导致月牙结构受力不均匀，有效防止结构失稳以及增强结构的抗冲击性能；因此整个仿生结构能够有效提高承载能力和缓冲吸能特性，保证了具有一定的初始峰值力和总吸能。

Kombinierter verbundwerkstoff- und metall-energieabsorber

Ein kombinierter Verbundwerkstoff- und Metall-Energieabsorber beinhaltet eine Verbundstruktur und ein erstes metallisches Rohr mit einem ersten Abschnitt und einem zweiten Abschnitt, wobei der erste Abschnitt mit der Verbundstruktur verbunden ist. Die Verbundstruktur und das erste metallische Rohr weisen ein maßgeschneidertes Quetsch-Profil auf, um ein vorzeitiges Quetschen der Verbundstruktur und des ersten metallischen Rohres zu vermeiden.

荷重エネルギ吸収材

【課題】コスト及び質量の増加を必要最小限に抑えつつ、コーナの強度を確保できる荷重エネルギ吸収材を提供すること。 【解決手段】クラッシュボックス２０は、多層織物４０における底側コーナ２４を形成する部分に、多層織物４０の各織物層４４を結合する経糸が、多層織物４０をそれぞれ厚さ方向において２つに分割する状態で結合することにより分割された織物層４４の間にスリット４０ｂを備える。クラッシュボックス２０は、スリット４０ｂの内部に強化部材２９が収容されている。 【選択図】図３

一种用于航天器部件连接的3d打印多模态隔振结构

本发明公开了一种用于航天器部件连接的3D打印多模态隔振结构，涉及三维打印结构技术领域。该结构可以优化航天器减振隔振性能，提高航天器传感器工作性能，相对于传统方法制造的零部件结构相对简单紧凑。所述多模态隔振结构包括为多层结构，每层包括呈阵列分布的若干形状形同的晶格单元；所述晶格单元包括承力基座以及三个弹性网络，三个弹性网络由内到外相互嵌套，并且三个弹性网络与承力基座保持固定连接。提高了航天器隔振零部件的工作性能，扩充了增材制造在航空航天领域的应用。

一种油气、扩径复合式耐坠毁缓冲器

一种油气、扩径复合式耐坠毁缓冲器。本发明涉及飞行器起降装置耐坠毁缓冲器领域。提出了一种可在工作状态下同时发挥金属扩径缓冲器和油气缓冲器的效能，从而有效提高了缓冲效率的油气、扩径复合式耐坠毁缓冲器。该缓冲器可运用在一次性耐坠毁缓冲任务环境中，也可与其他缓冲器串联，作为耐坠毁子级。包括活塞杆和金属胀筒；所述金属胀筒内容置有油，使得活塞杆内部形成气腔、且金属胀筒内形成油腔。本发明的有益效果为：能充分利用缓冲行程的同时有效提高了缓冲效率。利于控制过载保护飞行员或相关机载设备。使用方便，应用范围广。

冲击吸收体

本发明提供一种冲击吸收体，以提高被安装于车门装饰部的背面的冲击吸收体的冲击吸收特性的稳定性。冲击吸收体被安装在车门装饰部的背面，对被施加在车门上的冲击进行吸收。冲击吸收体的四棱筒体在筒顶端面具备端板，且面向车门装饰部的背面。四棱筒体由上板、下板和前侧板封闭三个侧面而剩余的一个侧面开放，从而成为大致匚字型的形状。

一种点阵缓冲吸能薄壁结构

本发明涉及一种点阵缓冲吸能薄壁结构，包括对称分布的两个承重板，两个承重板之间设置有缓冲吸能薄壁，每个缓冲吸能薄壁包括多个并列设置的缓冲吸能腿，缓冲吸能腿包括一个第二吸能腿、一个第三吸能腿和位于第二、第三吸能腿之间的多个串联连接的第一吸能腿；第一吸能腿包括第一连接部、第二连接部、第一平台、第二平台和连接臂。本发明的缓冲吸能薄壁结构连接稳定，结构设计合理精巧，采用薄壁空心结构，在实现缓冲吸能的同时能够极大地减轻自重，实现材料的利用率最大化，从而解决传统缓冲吸能结构应用场景单一、连接不合理导致吸能效果不佳、自重较大无法在航天等领域应用、使用的材料较昂贵无法在市场中推广普及等问题。

波纹型薄壁三层缓冲吸能结构及其制作方法

本发明公开了一种波纹型薄壁三层缓冲吸能结构及其制作方法，包括竖直设置的外波纹管、同轴设置的内波纹管、位于外波纹管和内波纹管之间的空腔内且沿竖直方向间隔环形填充的环状剪切增稠胶、位于内波纹管的内腔内的若干个弧形栏板、用于密封内波纹管和外波纹管上端的上封盖以及用于密封内波纹管和外波纹管下端的下封盖，其中弧形栏板的上下两端分别插入上封盖和下封盖内。本发明当受到轴向冲击碰撞时，内、外波纹管和先与弧形栏板一同受到冲击，在协同作用下开始弯曲变形，有效地吸收轴向冲击力；当冲击碰撞继续时，环状剪切增稠胶有效地诱导结构变形吸能，多层、间隔布置可促进结构平稳变形，提高整体的吸能特性，起到缓冲保护的作用。

波纹型薄壁三层缓冲吸能结构及其制作方法

本发明公开了一种波纹型薄壁三层缓冲吸能结构及其制作方法，包括竖直设置的外波纹管、同轴设置的内波纹管、位于外波纹管和内波纹管之间的空腔内且沿竖直方向间隔环形填充的环状剪切增稠胶、位于内波纹管的内腔内的若干个弧形栏板、用于密封内波纹管和外波纹管上端的上封盖以及用于密封内波纹管和外波纹管下端的下封盖，其中弧形栏板的上下两端分别插入上封盖和下封盖内。本发明当受到轴向冲击碰撞时，内、外波纹管和先与弧形栏板一同受到冲击，在协同作用下开始弯曲变形，有效地吸收轴向冲击力；当冲击碰撞继续时，环状剪切增稠胶有效地诱导结构变形吸能，多层、间隔布置可促进结构平稳变形，提高整体的吸能特性，起到缓冲保护的作用。

冲击吸收部件

本发明提供一种冲击吸收部件。该冲击吸收部件具有：具有帽顶部的帽型部件；以及与上述帽顶部对置的板状部件。在上述帽顶部以及上述板状部件中的至少一方的壁部设置有变形引导部。上述变形引导部具有：第1高强度部，在上述壁部中压曲屈服强度相对高；以及一对低强度部，压曲屈服强度相对低，且在沿着长度方向观察时将上述第1高强度部夹在之间而配置在两侧。进而，该冲击吸收部件具有一对第2高强度部，该一对第2高强度部的压曲强度比上述低强度部的压曲强度高，在沿着上述长度方向观察时，该一对第2高强度部以与上述一对低强度部分别邻接的方式配置在上述变形引导部的两侧。

硅酮自由扭簧铰链阻尼器

本公开内容提供了一种具有压缩限制器、第一盘、和第二盘的扭簧阻尼器。该第一盘布置在该压缩限制器的第一端处，并且该第二盘布置在该压缩限制器的第二端处，其中，该第二端与该第一端相对。该扭簧阻尼器还具有拉伸构件。该拉伸构件连接至该第一盘和该第二盘。该拉伸构件由嵌段共聚物构成。

Silikonfreier drehfeder-gelenkdämpfer

Die vorliegende Offenbarung sieht einen Drehfederdämpfer vor, der einen Kompressionsbegrenzer, eine erste Scheibe und eine zweite Scheibe aufweist. Die erste Scheibe ist an einem ersten Ende des Kompressionsbegrenzers angeordnet und die zweite Scheibe ist an einem zweiten Ende des Kompressionsbegrenzers angeordnet, wobei das zweite Ende dem ersten Ende gegenüber liegt. Der Drehfederdämpfer weist ebenfalls ein Zugelement auf. Das Zugelement ist mit der ersten Scheibe und der zweiten Scheibe verbunden. Das Zugelement besteht aus einem Blockcopolymer.

冲击吸收体

本发明提供一种冲击吸收体，以提高被安装于车门装饰部的背面的冲击吸收体的冲击吸收特性的稳定性。冲击吸收体被安装在车门装饰部的背面，对被施加在车门上的冲击进行吸收。冲击吸收体的四棱筒体在筒顶端面具备端板，且面向车门装饰部的背面。四棱筒体由上板、下板和前侧板封闭三个侧面而剩余的一个侧面开放，从而成为大致匚字型的形状。

一种具有负泊松比效应的金属吸能薄壁管及其设计方法

本发明提供了一种具有负泊松比效应的金属吸能薄壁管及其设计方法，包括薄壁管本体，薄壁管本体由多个自上而下依次首尾固定连接的单元体组成，每个所述单元体均包括固定连接的管和节，所述节固定在所述管的底部，所述管的壁厚大于所述节的壁厚。本发明技术方案金属管和相连接的节的厚度上不一致，金属管的厚度要大于连接的节的厚度，能够做到在受到弯曲载荷的时候相比于传统的相同厚度的金属管具有更好的抗弯强度，在受到相同载荷时不易变形弯曲，而且此结构在受到压缩时具有负泊松比效应，能够在受到压缩载荷的时候金属管纵向变短的同时横向也发生收缩，也更加容易发生致密化，相比于平常的金属管具有更好吸能效果。

一种鸟巢型布局的交叉薄板吸能结构

本发明涉及一种鸟巢型布局的交叉薄板吸能结构，包括设置在所述外壳内部鸟巢型布局的交叉薄板进行吸能的中央防护单元；以及设置在所述中央防护单元两端的端部防护单元；外壳为圆柱形；中央防护单元为多个薄板交叉组成，对称分布，截面形状鸟巢型布局；端部防护单元形状与外壳一致，为圆柱形，层级式布局；端部防护单元形状与外壳的半径相等。对比传统防护结构，本发明能够吸收更多的冲击能量，薄板拼装留下的空腔让结构更为轻量化，优化设计更是为不同设计需求、不同工程情况提供了设计思路及仿真方法。

一种点阵缓冲吸能薄壁结构

本发明涉及一种点阵缓冲吸能薄壁结构，包括对称分布的两个承重板，两个承重板之间设置有缓冲吸能薄壁，每个缓冲吸能薄壁包括多个并列设置的缓冲吸能腿，缓冲吸能腿包括一个第二吸能腿、一个第三吸能腿和位于第二、第三吸能腿之间的多个串联连接的第一吸能腿；第一吸能腿包括第一连接部、第二连接部、第一平台、第二平台和连接臂。本发明的缓冲吸能薄壁结构连接稳定，结构设计合理精巧，采用薄壁空心结构，在实现缓冲吸能的同时能够极大地减轻自重，实现材料的利用率最大化，从而解决传统缓冲吸能结构应用场景单一、连接不合理导致吸能效果不佳、自重较大无法在航天等领域应用、使用的材料较昂贵无法在市场中推广普及等问题。

仿蒲草缓冲吸能薄壁复合结构

本发明公开了一种仿蒲草缓冲吸能薄壁复合结构，包括由若干个仿蒲草月牙结构对称组合而成的仿生结构，仿蒲草月牙结构包括外弧板、内弧板、用于连接外弧板和内弧板侧边的连接平板以及均布于外弧板和内弧板之间的若干个肋板。本发明的仿生结构是由仿蒲草月牙结构组合而成，从蒲草内部特征衍生设计，整个仿生结构包含多级形态能够有效的促进仿生结构在受轴向冲击时将冲击能分散到不同的结构层次中从而缓冲作用在结构表面的冲击力；在冲击过程中，月牙外侧所受的应力大于内侧应力，导致月牙结构受力不均匀，有效防止结构失稳以及增强结构的抗冲击性能；因此整个仿生结构能够有效提高承载能力和缓冲吸能特性，保证了具有一定的初始峰值力和总吸能。

一种内凹型负泊松比吸能结构

本发明涉及负泊松比超材料，能量吸收技术领域，尤其是涉及一种内凹型负泊松比吸能结构。内凹型负泊松比吸能结构包括多个单胞结构；所述单胞结构包括底部、顶部和肋板；所述底部和顶部为对称结构，底部和顶部位于同一侧的端部通过肋板连接，所述肋板、底部和顶部均为曲线结构。将传统内凹型结构与底部与顶部呈一定角度的直线肋部改成曲线结构，将原有的内凹型结构的顶部与底部也改成曲线结构。通过将肋部改成曲线肋，降低应力集中现象。

一种具有负泊松比效应的金属吸能薄壁管及其设计方法

本发明提供了一种具有负泊松比效应的金属吸能薄壁管及其设计方法，包括薄壁管本体，薄壁管本体由多个自上而下依次首尾固定连接的单元体组成，每个所述单元体均包括固定连接的管和节，所述节固定在所述管的底部，所述管的壁厚大于所述节的壁厚。本发明技术方案金属管和相连接的节的厚度上不一致，金属管的厚度要大于连接的节的厚度，能够做到在受到弯曲载荷的时候相比于传统的相同厚度的金属管具有更好的抗弯强度，在受到相同载荷时不易变形弯曲，而且此结构在受到压缩时具有负泊松比效应，能够在受到压缩载荷的时候金属管纵向变短的同时横向也发生收缩，也更加容易发生致密化，相比于平常的金属管具有更好吸能效果。

波纹型薄壁三层缓冲吸能结构及其制作方法

本发明公开了一种波纹型薄壁三层缓冲吸能结构及其制作方法，包括竖直设置的外波纹管、同轴设置的内波纹管、位于外波纹管和内波纹管之间的空腔内且沿竖直方向间隔环形填充的环状剪切增稠胶、位于内波纹管的内腔内的若干个弧形栏板、用于密封内波纹管和外波纹管上端的上封盖以及用于密封内波纹管和外波纹管下端的下封盖，其中弧形栏板的上下两端分别插入上封盖和下封盖内。本发明当受到轴向冲击碰撞时，内、外波纹管和先与弧形栏板一同受到冲击，在协同作用下开始弯曲变形，有效地吸收轴向冲击力；当冲击碰撞继续时，环状剪切增稠胶有效地诱导结构变形吸能，多层、间隔布置可促进结构平稳变形，提高整体的吸能特性，起到缓冲保护的作用。