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Vibration-acceleration coupled environmental test system for spacecraft dynamics test

An environmental testing and acceleration technology, applied in vibration testing, machine/structural component testing, measuring devices, etc., can solve problems such as insufficient exposure of product design and manufacturing defects, insufficient assessment of aerospace products, etc. Reliable, easy-to-manage effects

Active Publication Date: 2019-08-06
BEIJING INST OF SPACECRAFT ENVIRONMENT ENG
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0004] In order to meet the development needs of aerospace product mission reliability measurement, avoid insufficient assessment of aerospace products during the test process, and fail to fully expose product design and manufacturing defects, it is very necessary to develop a test system that can perform vibration-acceleration coupling environmental tests

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  • Vibration-acceleration coupled environmental test system for spacecraft dynamics test
  • Vibration-acceleration coupled environmental test system for spacecraft dynamics test
  • Vibration-acceleration coupled environmental test system for spacecraft dynamics test

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Embodiment Construction

[0028] A vibration-acceleration coupled environmental test system for spacecraft dynamic tests of the present invention will be described in detail below in conjunction with the accompanying drawings. The specific implementation is only for the purpose of illustration and is not intended to limit the protection scope of the present invention.

[0029] refer to Figure 1-2 , Figure 1-2 A front view and a top view of a vibration-acceleration coupled environmental test system for spacecraft dynamic tests of the present invention are respectively shown. According to the accompanying drawings, it can be known that the vibration-acceleration coupling environment test system of the present invention includes a support 1; a motor 2; a speed measuring device 3; a shaft coupling 4; a reducer casing 5; Flow ring 8; counterweight 9; electrical control system wiring panel 10; fan 11; electromagnetic vibrating table suspension ring 12; electromagnetic vibrating table 13; steel bracket 14;...

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Abstract

The invention discloses a vibration-acceleration coupling environment test system used for a spacecraft dynamic test. The system comprises an acceleration environment test system and a vibration environment test system. The acceleration environment test system is used for providing constant linear acceleration environment stress through jib rotation and mainly comprises a base, a motor, a transmission system, a speed measurement device, a working jib, a current collecting ring and an electronic control system. The vibration environment test system is used for providing vibration excitation and mainly comprises an electromagnetic vibration table body, a forced air cooling system and an image photographing system. The electromagnetic vibration table body, the forced air cooling system and the image photographing system are fixed on a centrifuge jib through bolts. The environment test system has the advantages of being simple in structure and easy to control and can be used for providing the vibration-acceleration coupling dynamic test for the spaceflight product.

Description

technical field [0001] The invention belongs to the technical field of spacecraft dynamics test, in particular, the invention relates to a vibration-acceleration coupled environmental test equipment. Background technique [0002] In the national defense industry, aerospace products generally work in a coupled dynamic environment where vibration and linear acceleration act simultaneously, such as when a spacecraft is in the launch phase, when an aircraft is climbing, diving, and circling, when a strategic missile is in the active section and through the reentry section At the same time, its equipment and devices are subject to the coupling effect of acceleration overload and engine vibration. However, in the current mechanical environment test, due to the lack of coupling test equipment, the vibration test and the centrifugal test are generally carried out separately in time, and the product's tolerance to vibration or linear acceleration single stress is assessed on the vibr...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01M7/02
Inventor 宋超周原冯咬齐刘闯吴儒亮唐学伟郎冠卿
Owner BEIJING INST OF SPACECRAFT ENVIRONMENT ENG