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Canopy jettison experiment device and system and canopy

A test device and test system technology, applied in the field of aircraft test, can solve problems such as multiple uncertain factors, long cycle of adjusting life-saving system design scheme, high test cost, etc., and achieve the effect of reducing the demand for progress and funds

Active Publication Date: 2017-05-31
SHENYANG AIRCRAFT DESIGN INST AVIATION IND CORP OF CHINA
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Therefore there are the following two problems: a, high cost of testing
Because it is impossible to verify the key design parameters and actual working effects before the detailed design of the system is carried out, the life-saving system under test has a low technical maturity, which makes the test process have many uncertain factors. Adjust the life-saving system design plan and The cycle of repeated test verification is longer

Method used

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  • Canopy jettison experiment device and system and canopy
  • Canopy jettison experiment device and system and canopy
  • Canopy jettison experiment device and system and canopy

Examples

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Embodiment Construction

[0027] In order to make the objectives, technical solutions and advantages of the present invention clearer, the technical solutions in the embodiments of the present invention will be described in more detail below in conjunction with the drawings in the embodiments of the present invention. In the drawings, the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The described embodiments are some, but not all, embodiments of the invention. The embodiments described below by referring to the figures are exemplary and are intended to explain the present invention and should not be construed as limiting the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention. Embodiments of the present invention will be described in detail below ...

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Abstract

The invention discloses a canopy jettison experiment device and system and a canopy. The canopy jettison experiment device comprises a mounting platform, a folding corn control component, a supporting component, a release device and a jettison power device, the folding corner control component is arranged on a mounting face and used for containing one end of the canopy, the canopy can rotate around the folding corner control component, the supporting component is arranged on the mounting face and supports the canopy, and the release device is arranged on the mounting platform; the jettison power device comprises a power member, one end of the power member is fixed while the other end of the same is connected with the release device, the power member can be in a fixed state and in a moving stage, and the power member has preset force and is stationary in the fixed state and release the preset force and is driven by the preset force to move in the moving state. By adopting the canopy jettison experiment device, an existing experiment verification means can be replaced at a scheme design stage before specific design work is conducted to perform preliminary experiment verification on performance of newly-developed life-saving system jettison canopies.

Description

technical field [0001] The invention relates to the technical field of aircraft testing, in particular to a canopy throwing test device, a canopy throwing test system and a canopy. Background technique [0002] There are two main ways to test and verify the performance of the existing aircraft lifesaving system by throwing the canopy to clear the ejection channel: one is to use a test bench that simulates the structure of the aircraft cockpit, install the canopy throwing system, and throw the real canopy or A simulated canopy with the same weight and center of gravity as the real canopy; the second is to directly use the real aircraft fuselage structure and throwing system to throw the real canopy. Both methods require the manufacture of corresponding test systems and equipment before they can start Test verification. According to the requirements of the "dumping test", the ground static test needs to be carried out 10 to 14 times during the development of the ditching syst...

Claims

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Application Information

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IPC IPC(8): B64F5/60B64C1/14B64D25/12
CPCB64C1/1476B64D25/12
Inventor 崔文博赵钢刘亮亮张书晔姜国纯
Owner SHENYANG AIRCRAFT DESIGN INST AVIATION IND CORP OF CHINA
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