Method for inhibiting armature transition through reducing vortex based on empennage layering
An armature and tail technology, applied in the field of orbital electromagnetic launch, can solve the problems of reducing the total magnetic field, reducing the skin effect of the speed, etc., and achieve the effects of not easy to start arc, good suppression effect, and simple and easy method.
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[0014] The armature transition suppression method based on empennage layering to reduce eddy current of the present invention will be further described in detail with reference to the accompanying drawings.
[0015] The schematic diagram of the empennage layering of the present invention to reduce the internal eddy current of the armature is as follows: figure 1 shown. The present invention changes the armature tail into a layered structure 1 on the basis of the existing C-shaped armature, and the interlayer is an epoxy resin glass fiber material 2 resistant to high temperature and high pressure, and the epoxy resin glass fiber material 2 can block the eddy current 3 The path of the eddy current 3 is limited in the narrow area of the conductive layer, so that the intensity of the eddy current 3 is reduced, the reverse electromagnetic force caused by the eddy current 3 is reduced, the contact pressure drop speed of the armature tail and the track 4 is reduced, and the tail la...
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