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Небесная энциклопедия

Космические корабли и станции, автоматические КА и методы их проектирования, бортовые комплексы управления, системы и средства жизнеобеспечения, особенности технологии производства ракетно-космических систем

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Мониторинг СМИ

Мониторинг СМИ и социальных сетей. Сканирование интернета, новостных сайтов, специализированных контентных площадок на базе мессенджеров. Гибкие настройки фильтров и первоначальных источников.

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Применить Всего найдено 9. Отображено 9.
05-08-2009 дата публикации

Clamper of cold upsetting tester used for titanium alloy wire materials

Номер: CN0101498634A
Принадлежит:

The invention relates to a clamp for a cold upsetting tester of titanium alloy wires, which comprises an upper clamp, a lower clamp and a material mechanical property tester connected with the upper clamp and the lower clamp through large-bore screw threads. The clamp is characterized in that the center positions of the support faces of the upper clamp and the lower clamp are provided with grooves with depths of 5mm, the grooves are used for placing and positioning support boards and preventing the support boards from protruding accidentally; upper support boards and lower support boards which are cylinders with the thicknesses of 10 mm are arranged in the grooves, and the diameters of the supports boards are smaller than those of the grooves. The invention has the advantages that the tester is simple and practical and convenient for assembly and disassembly and has efficient and safe testing process, is easy to accurately realize the cold upsetting test of titanium alloy wires with set ...

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08-09-2010 дата публикации

High strength and high full hardening titanium alloy

Номер: CN0101503771B
Принадлежит:

The invention relates to titanium alloy with high strength and high through hardening, namely Ti-5.5Al-4Mo-6V-2Nb-1Fe alloy. The alloy belongs to transitional alpha-beta titanium alloy, wherein the nominal aluminum equivalent is 5.5 and the molybdenum equivalent is approximately 11. The Ti-5.5Al-4Mo-6V-2Nb-1Fe alloy is characterized by comprising the following chemical compositions in percentage by mass: 5.0 to 6.2 percent of aluminum, 3.5 to 4.5 percent of molybdenum, 5.5 to 6.5 percent of vanadium, 1.5 to 2.5 percent of niobium, 0.5 to 1.5 percent of iron, less than or equal to 0.05 percentof carbon, less than or equal to 0.13 percent of oxygen, less than or equal to 0.05 percent of nitrogen, less than or equal to 0.015 percent of hydrogen, and the balance of titanium. The alloy has superior comprehensive properties of high strength, high through hardening, high toughness and high weldability. After complex duplex annealing of alloy forgings, the tensile strength index reaches 1,150 MPa ...

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22-09-2010 дата публикации

Post weld vacuum heat treatment process of TC18 titanium alloy welding component

Номер: CN0101838785A
Принадлежит:

The invention relates to a post weld vacuum heat treatment process of TC18 titanium alloy welding component. The method comprises the following steps of: (1) placing a clean high-intensity TC18 titanium alloy welding component and a furnace test sample into a vacuum heat treatment furnace, wherein the vacuum working pressure in the vacuum chamber is not greater than 6.7*10-2Pa; (2) heating the welding component with the temperature of the furnace to 810-850 DEC G via a step temperature increasing method, and maintaining the temperature for 1-2h; (3) cooling the TC18 titanium alloy welding component and the furnace test sample below 300 DEC G at the cooling speed of 0.3-5 DEG G/min, and taking the component and the sample out of the furnace to cool via air; and (4) carrying out the heat treatment on the component, and carrying out the tension performance test on the furnace test sample for testing the tension performances of the welding component substrate and the welding joint. The intensity ...

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12-08-2009 дата публикации

High strength and high full hardening titanium alloy

Номер: CN0101503771A
Принадлежит:

The invention relates to titanium alloy with high strength and high through hardening, namely Ti-5.5Al-4Mo-6V-2Nb-1Fe alloy. The alloy belongs to transitional alpha-beta titanium alloy, wherein the nominal aluminum equivalent is 5.5 and the molybdenum equivalent is approximately 11. The Ti-5.5Al-4Mo-6V-2Nb-1Fe alloy is characterized by comprising the following chemical compositions in percentage by mass: 5.0 to 6.2 percent of aluminum, 3.5 to 4.5 percent of molybdenum, 5.5 to 6.5 percent of vanadium, 1.5 to 2.5 percent of niobium, 0.5 to 1.5 percent of iron, less than or equal to 0.05 percent of carbon, less than or equal to 0.13 percent of oxygen, less than or equal to 0.05 percent of nitrogen, less than or equal to 0.015 percent of hydrogen, and the balance of titanium. The alloy has superior comprehensive properties of high strength, high through hardening, high toughness and high weldability. After complex duplex annealing of alloy forgings, the tensile strength index reaches 1,150 ...

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24-09-2008 дата публикации

Method for optimization of titanium alloy beta smithing technological parameter

Номер: CN0101270461A
Принадлежит:

The invention relates to a parameter optimizing method for the Beta forging technique of titanium alloy. The method proposes an empirical formula that Zeta is equal to one second Theta plus 8 Eta; in the formula, Zeta relates to the comprehensive parameters of the Beta forging, the physical meaning of Zeta refers to that the average diameter D of Beta crystal grains and Zeta are in a leaner relation, the Beta forging temperature is equal to subtracting T Beta from T, T relates to the heating temperature of a Beta area and T Beta relates to the temperature of a Beta phase transition point; a heating coefficient Eta is equal to t divided by Delta; wherein, t relates to the heating time of the Beta area and Delta relates to the thickness of a stock; under a certain deformation capacity, the comprehensive parameters of Beta forging, the section shrinkage factor Psi of a cast and the impact tenacity aKU of the cast are all in linear quantitative relations; Zeta and the cracking temper KIC of ...

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27-10-2010 дата публикации

Clamper of cold upsetting tester used for titanium alloy wire materials

Номер: CN0101498634B
Принадлежит:

The invention relates to a clamp for a cold upsetting tester of titanium alloy wires, which comprises an upper clamp, a lower clamp and a material mechanical property tester connected with the upper clamp and the lower clamp through large-bore screw threads. The clamp is characterized in that the center positions of the support faces of the upper clamp and the lower clamp are provided with grooves with depths of 5mm, the grooves are used for placing and positioning support boards and preventing the support boards from protruding accidentally; upper support boards and lower support boards which are cylinders with the thicknesses of 10 mm are arranged in the grooves, and the diameters of the supports boards are smaller than those of the grooves. The invention has the advantages that the tester is simple and practical and convenient for assembly and disassembly and has efficient and safe testing process, is easy to accurately realize the cold upsetting test of titanium alloy wires with set ...

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29-10-2008 дата публикации

Titanium alloy smithing technological parameter testing method

Номер: CN0101294265A
Принадлежит:

The invention relates to a test mode of a titanium alloy smithing technological parameter. The test mode has the steps that: (1) multi-forging various-direction smithing is performed on a titanium alloy steel bar to obtain an original structure which is as uniform as possible; (2) the steel bar after substituting forging is made into stocks under the temperature ranging from 30 to 50 DEG C below a Beta transformation point (TBeta); (3) the stocks are preheated for 1 to 2 hours under the temperature which is about 200 DEG C, and then are coated with special lubricant Ti-6 of a titanium alloy die forming; (4) the surface of a die is preheated until the temperature is more than 350 DEG C, the die forming is finished with 1 to 2 fire levels, and three different deformation amounts of 10 percent, 35 percent and 60 percent are obtained on a forgeable piece; (5) after the forgeable piece is processed through heat treatment, various types of mechanical property samples are get from the parts with ...

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21-12-2011 дата публикации

Post weld vacuum heat treatment process of TC18 titanium alloy welding component

Номер: CN0101838785B
Принадлежит:

The invention relates to a post weld vacuum heat treatment process of TC18 titanium alloy welding component. The method comprises the following steps of: (1) placing a clean high-intensity TC18 titanium alloy welding component and a furnace test sample into a vacuum heat treatment furnace, wherein the vacuum working pressure in the vacuum chamber is not greater than 6.7*10-2Pa; (2) heating the welding component with the temperature of the furnace to 810-850 DEC G via a step temperature increasing method, and maintaining the temperature for 1-2h; (3) cooling the TC18 titanium alloy welding component and the furnace test sample below 300 DEC G at the cooling speed of 0.3-5 DEG G/min, and taking the component and the sample out of the furnace to cool via air; and (4) carrying out the heat treatment on the component, and carrying out the tension performance test on the furnace test sample for testing the tension performances of the welding component substrate and the welding joint. The intensity ...

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27-01-2010 дата публикации

Titanium alloy forging technological parameter testing method

Номер: CN0100584987C
Принадлежит:

The invention relates to a test mode of a titanium alloy smithing technological parameter. The test mode has the steps that: (1) multi-forging various-direction smithing is performed on a titanium alloy steel bar to obtain an original structure which is as uniform as possible; (2) the steel bar after substituting forging is made into stocks under the temperature ranging from 30 to 50 DEG C below a Beta transformation point (TBeta); (3) the stocks are preheated for 1 to 2 hours under the temperature which is about 200 DEG C, and then are coated with special lubricant Ti-6 of a titanium alloy die forming; (4) the surface of a die is preheated until the temperature is more than 350 DEG C, the die forming is finished with 1 to 2 fire levels, and three different deformation amounts of 10 percent, 35 percent and 60 percent are obtained on a forgeable piece; (5) after the forgeable piece is processed through heat treatment, various types of mechanical property samples are get from the parts with ...

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