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
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[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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