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Multi-component simulative engine applied to vacuum plume effect experimental research and ignition scheme thereof

A plume effect, experimental research technology, applied in the direction of machines/engines, rocket engine devices, mechanical equipment, etc., can solve the problems of expensive, complex thermal protection methods, etc., to achieve simple schemes, simple thermal protection schemes, and obvious effects Effect

Inactive Publication Date: 2014-03-19
BEIHANG UNIV
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Real engines generally use expensive metal materials with high melting points for processing, and use methods such as ablation and cooling for thermal protection. The thermal protection method is more complicated

Method used

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  • Multi-component simulative engine applied to vacuum plume effect experimental research and ignition scheme thereof
  • Multi-component simulative engine applied to vacuum plume effect experimental research and ignition scheme thereof
  • Multi-component simulative engine applied to vacuum plume effect experimental research and ignition scheme thereof

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Embodiment Construction

[0045] The present invention will be further described in detail below with reference to the drawings and embodiments.

[0046] The invention is a multi-component simulation engine and its ignition scheme applied to the experimental study of the vacuum plume effect.

[0047] The multi-component simulation engine used in the experimental study of the vacuum plume effect such as figure 1 As shown, it includes a pre-combustion chamber head 1, a pre-combustion supplementary oxygen chamber 2, a thrust chamber head 3, and a thrust chamber body 4;

[0048] Such as figure 1 with figure 2 As shown, the pre-combustion chamber head 1 and the pre-combustion oxygen supplement chamber 2 are sealed by an expanded graphite sealing gasket 8 and are fastened with a threaded structure (screw). The pre-combustion oxygen supplement chamber 2, the thrust chamber head 3 and the thrust The chamber body 4 is fastened with a threaded structure (screw). The pre-combustion oxygen chamber 2 and the thrust cha...

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Abstract

The invention discloses a multi-component simulative engine applied to vacuum plume effect experimental research and an ignition scheme thereof. The multi-component simulative engine comprises a pre-combustion chamber head part, a pre-combustion oxygen supplementation chamber, a thrust chamber head part and a thrust chamber body part, wherein the pre-combustion chamber head part is tightly connected with the pre-combustion oxygen supplementation chamber, and the pre-combustion oxygen supplementation chamber, the thrust chamber head part and the thrust chamber body part are connected tightly and sequentially. The ignition scheme comprises working medium input, ignition time sequence and pre-combustion chamber capacity design. According to the invention, a propellant working medium is input through an ignition incendiary agent welding nozzle, an ignition oxidant welding nozzle and an oxygenating agent welding nozzle, and simulation of combustion products of different real engines can be realized by matching different incendiary agents, oxidants and other gases.

Description

Technical field [0001] The invention relates to a multi-component simulation engine applied to the experimental research of vacuum plume effect and its ignition scheme, belonging to the technical field of engine design. Background technique [0002] When a space chemical propulsion engine is ignited in a vacuum environment, it will produce a feather-like high-temperature and high-speed jet, called a plume. The plume will produce aerodynamic effects, aerothermal effects, pollution effects, electromagnetic effects, etc., collectively referred to as the vacuum plume effect, which will bring adverse consequences to the normal operation of the spacecraft. Therefore, it is necessary to study the vacuum plume effect, and then optimize the plan and rational layout in the design process of the spacecraft, so as to reduce the negative impact of the vacuum plume effect on the spacecraft. [0003] The research of vacuum plume effect includes numerical simulation and experimental research. Al...

Claims

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Application Information

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IPC IPC(8): F02K9/00F02K9/95
Inventor 贺碧蛟吴靖蔡国飙王文龙
Owner BEIHANG UNIV
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