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Mobile test platform for low-thrust rocket engines

A rocket engine and test platform technology, applied in jet engine testing, gas turbine engine testing, etc., can solve the problems of poor portability, versatility, and complexity, and achieve the effects of good versatility, high precision, and high stability

Active Publication Date: 2013-08-07
BEIHANG UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The current rocket engine test bench system is relatively complicated and needs to be tested in a specific place, which is poor in portability and versatility

Method used

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  • Mobile test platform for low-thrust rocket engines
  • Mobile test platform for low-thrust rocket engines

Examples

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Embodiment Construction

[0037] The present invention will be further described in detail with reference to the accompanying drawings and embodiments.

[0038] The present invention is a kind of small-thrust rocket engine mobile test platform, such as figure 1 As shown, it includes a mobile platform 1 , a test frame 2 , a propellant supply system 3 and a gas distribution system 4 .

[0039] The test frame 2, the propellant supply system 3 and the gas distribution system 4 are all integrated and installed on the mobile platform 1, which has the advantages of miniaturization and good portability.

[0040] The mobile platform 1 includes a test frame installation structure 101 , wheels 102 , a load-bearing structure 103 , an inner cavity 104 and a gas distribution panel 105 .

[0041] The test rack installation structure 101 is welded by channel steel, and is used for installing the engine test rack 2 .

[0042] The wheels 102 are universal wheels with braking devices. The four wheels 102 are fixed on t...

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Abstract

The invention discloses a mobile test platform for low-thrust rocket engines. The mobile test platform comprises a mobile platform, a running support, a propellant feeding system and a gas distribution system. The running support, the propellant feeding system and the gas distribution system are integrally mounted on the mobile platform. The mobile platform comprises a testing rack mounting structure, wheels, a load-carrying structure, an inner cavity and a gas distribution panel. The testing rack comprises a motionless support, plate springs, a movable support, an engine support, a thrust support and a thrust sensor. The propellant feeding system comprises a fuel supply system and an oxidant supply system. The gas distribution system comprises a high-pressure gas tank, a pressurizing gas pipeline and a blowdown gas pipeline. All system components are integrated on one mobile platform, so that the mobile test platform has the advantages of miniaturization, portability and the like.

Description

technical field [0001] The invention relates to a small-thrust rocket engine mobile test platform, which belongs to the technical field of liquid rocket engines. Background technique [0002] The power system of space vehicles such as artificial satellites and spacecraft generally needs to complete tasks such as orbit change, orbit maintenance, rendezvous and docking, attitude control box and precise positioning. Small-thrust rocket engines could power these missions. The small-thrust rocket engine is also used in the start-up guarantee system of the main engine, the protection spacecraft system in case of an accident when the rocket takes off, and the soft landing system. Therefore, experimental research on small-thrust rocket engines is being carried out extensively. [0003] Engine test is an important part of engine development, also known as engine test run. The test run is carried out on a variety of specially built test benches, that is, the engine or its assembly ...

Claims

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Application Information

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IPC IPC(8): G01M15/14
Inventor 俞南嘉田辉曾鹏李君海蔡国飙
Owner BEIHANG UNIV
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