Combined type thrust vector spraying pipe system and projectile body with system

A thrust vectoring and combined technology, which is applied in the direction of self-propelled bombs, jet propulsion devices, rocket motor devices, etc., can solve the problems of low reliability of thrust vectoring devices, increased engine weight, increased engine weight, etc., and achieve enhanced anti-ablation capacity, reduced carry capacity, and friction-reduced effects

Active Publication Date: 2021-02-26
HARBIN ENG UNIV
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  • Summary
  • Abstract
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  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

This method can produce thrust vectoring to a certain extent, but this method will increase the weight of the engine, and it will also increase the weight of the engine
At the same time, due to the complex mechanical structure of this method, the reliability of this kind of thrust vectoring device is low, and the cooling requirements are higher in high temperature and high pressure environments.

Method used

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  • Combined type thrust vector spraying pipe system and projectile body with system
  • Combined type thrust vector spraying pipe system and projectile body with system
  • Combined type thrust vector spraying pipe system and projectile body with system

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Embodiment 1

[0043] see Figure 1-Figure 3 , the invention provides a combined thrust vectoring nozzle system, comprising a supersonic separation line swinging nozzle (such as Figure 4-Figure 5 shown), liquid secondary injection system (such as Figure 6-Figure 8 shown) and the control system (such as Figure 9-Figure 12 shown).

[0044] The control system (such as Figure 9-Figure 12 shown) including the comprehensive lateral force control system (such as Figure 9 shown), the secondary injection control system (such as Figure 10 shown) (including electromagnetic flowmeter controller, liquid secondary injection controller, flow signal processing module), and supersonic separation line swing nozzle control system (such as Figure 11 shown).

[0045] The invention combines the supersonic separation line swing nozzle with the liquid secondary injection system, effectively increasing the reliability of the supersonic separation line swing nozzle. The present invention simultaneously ...

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PUM

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Abstract

The invention belongs to the technical field of power of aerospace aircraft, in particular to a combined type thrust vector spraying pipe system and a projectile body with the system. Two sub-systemsincluding a liquid secondary ejection system and a supersonic separation line swinging spraying pipe are organically combined, so that the advantages of both of the sub-systems are fully developed, and the liquid secondary ejection system mainly has the characteristics of quick response, high efficiency and light structural weight, and also can play a role in lubrication and cooling of a sprayingpipe, so that the aircraft has a larger thrust vector deflection angle and higher response speed. According to the combined type thrust vector spraying pipe system disclosed by the invention, the carrying amount and the box storage size of liquid injecting agent of the aircraft can be reduced, and the total weight of the thrust vector control system is effectively controlled. Due to injection of the injecting agent, heating of an internal molded surface of the spraying pipe can be alleviated, the ablation resistance capability of the spraying pipe is enhanced, and granule phase is prevented from entering a separation line gap to prevent the spraying pipe from being stuck. Because of lubrication components added in the injecting agent, friction of a sealing ring also can be reduced, and thereliability of the system is further improved.

Description

technical field [0001] The invention belongs to the technical field of aerospace vehicle power, and in particular relates to a combined thrust vectoring nozzle system and a projectile with the system. Background technique [0002] Thrust vectoring technology is closely related to the development of missiles, aircraft and other aerospace vehicle technologies, and is one of the core and key technologies of missiles and aerospace power. The development and application of thrust vector control technology can effectively improve the maneuverability of the aircraft, and play a pivotal role in reducing the resistance and weight of the aircraft, improving stealth performance, safety performance and survivability, and thus can significantly improve the combat effectiveness of the aircraft . Thrust vector control technology is the key to the wide application of solid rocket motors. It has developed into a specialized technology and there are many types of thrust vector control system...

Claims

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Application Information

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IPC IPC(8): F02K9/84F02K9/82F02K9/80F02K9/97F42B15/36
CPCF02K9/805F02K9/82F02K9/84F02K9/97F02K9/972F42B15/36
Inventor 王革李德坚何定鹏苏成志程靖懿朱宁杨海威关奔周凌
Owner HARBIN ENG UNIV
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