Synchronous detonation device for hypersonic aircraft component separation wind tunnel experiment
An aircraft component, hypersonic technology, which is applied in the testing, measuring devices, instruments, etc. of machine/structural components, can solve the problems of detonation process monitoring, time synchronization, false initiation, etc., so as to avoid false initiation and reduce development cost and cycle. Effect
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[0017] Embodiment 1: see figure 1 , figure 2 , a hypersonic vehicle component separation wind tunnel experiment synchronous detonation device, comprising: synchronous trigger unit 1, detonation control unit 2, constant current unit 3;
[0018] The synchronous triggering unit 1 receives the resident gas formation signal sent by the pressure sensor installed in the wind tunnel resident room, and determines the time delay of the synchronous triggering unit 1 according to the start time of the wind tunnel nozzle of the hypersonic vehicle component separation experiment, Then send a detonation start signal to the detonation control unit 2, so that the detonation bolts are detonated while the flow field of the hypersonic vehicle component separation experiment wind tunnel is established;
[0019] After the detonation control unit 2 receives the detonation signal sent by the synchronous trigger unit 1, it connects the constant current unit 3, and loads the detonation current to bot...
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