A Transient Detonation Pulse Engine and Radial Multipulse Thrust Vectoring Device
An engine and detonation technology, applied in the field of high-speed rotating aircraft, can solve the problems affecting the landing accuracy of the flying body and the low control accuracy of the radial attitude of the flying rotating body.
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[0020] Such as figure 2 Shown, a kind of transient detonation pulse engine of the present invention is made of engine body 20, reinforcing sleeve 20-1, plasma ignition tool 20-2, insulator 20-3, mixed ignition powder 20-4, strong explosive 20-5 , The spout sealing body 20-6, the head body 20-7, the electrode A, and the electrode B are composed.
[0021] A reinforcement sleeve 20-1 is installed in the engine body 20, and a strong explosive 20-5 is filled in the reinforcement sleeve 20-1; a plasma igniter 20-2, a mixed ignition powder 20-4, and a plasma ignition device are installed in the insulator 20-3. The tool 20-2 is connected with electrode A and electrode B.
[0022] The plasma igniter 20-2 and the mixed ignition powder 20-4 constitute a micron-scale bridge foil energy-containing plasma igniter device; the plasma igniter 20-2 adopts a vacuum sputtering metal coating process or adopts Ion ignition devices made by printed circuit board technology, see image 3 As shown,...
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