Dragging type vacuum launching tube multimode hybrid heavy-load electromagnetic launching device
A technology of vacuum launch and launch device, which is applied to electromagnetic launchers, weapons without explosives, offensive equipment, etc., can solve the problems of high design cost, large air resistance, and large size of the device, so as to reduce design cost and reduce air resistance. , the effect of small size of the device
Inactive Publication Date: 2022-08-05
广东先进动力科技有限公司
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Problems solved by technology
[0003] However, the electromagnetic orbital launch of the traditional electromagnetic launch device requires long-distance acceleration and large air resistance, which will also lead to a large device size and high design cost
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[0020] see Figure 1-4 , The present invention discloses a multi-mode hybrid heavy-duty electromagnetic launch device of a pulling type vacuum launch tube, comprising a vacuum launch tube 10, an airborne object 11, an electromagnetic track 12, an electromagnet 13, a sleeve 14, a launch object 15, and a vacuum pump 16 and pulse power supply 17.
[0021] The aerial object 11 is connected to the vacuum launch tube 10 for fixing the vacuum launch tube 10 .
[0022] Preferably, the aerial object 11 is used for arranging the vacuum launch tube 10 in a vertical direction.
[0023] In this embodiment, the flying object 11 includes a motorboat or a hot air balloon, and the motorboat or the hot air balloon is connected to the vacuum launch tube 10 through a carbon fiber material pull rope. That is to say, the vacuum launch tube 10 is fixed by pulling a motorboat or a hot air balloon, which effectively reduces the construction cost.
[0024] It should be understood that there are mult...
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The invention discloses a multi-mode hybrid heavy-load electromagnetic launching device with a pull type vacuum launching tube. The multi-mode hybrid heavy-load electromagnetic launching device comprises the vacuum launching tube; the air flyer is connected with the vacuum launching tube and used for fixing the vacuum launching tube; the electromagnetic track is arranged in the vacuum launching tube; the electromagnet is arranged in the vacuum transmitting tube, and a first coil is arranged outside the electromagnet in a surrounding manner; the sleeve is arranged outside the electromagnet in a sleeving mode, and a second coil is arranged outside the sleeve in a surrounding mode; the launching object is contained in the vacuum launching tube and is connected with the sleeve through a detachable part; the vacuum pump is used for vacuumizing the vacuum transmitting tube; the pulse power supply is used for synchronously or asynchronously supplying power to the first coil and the electromagnetic track; wherein the electromagnetic track comprises a positive pole electromagnetic track and a negative pole electromagnetic track, one end of the second coil is arranged in the positive pole electromagnetic track in a sliding mode, and the other end of the second coil is arranged in the negative pole electromagnetic track in a sliding mode. In this way, short-distance launching can be achieved, the air resistance is small, the device size is small, the influence caused by shaking of the launching tube is reduced, and the design cost is effectively reduced.
Description
technical field [0001] The invention relates to the technical field of electromagnetic launch, in particular to a multi-mode hybrid heavy-duty electromagnetic launch device of a pulling type vacuum launch tube. Background technique [0002] Electromagnetic launch technology is a new launch technology that converts electromagnetic energy into kinetic energy, thereby enabling the launch object to obtain high acceleration and high-speed new launch technology. Moreover, the time required for electromagnetic emission technology is very short, generally from a few milliseconds to more than ten milliseconds. Compared with traditional chemical energy and mechanical energy emission technologies, electromagnetic emission technology has the advantages of fast emission speed, good controllability, excellent performance, and emission efficiency. Advanced series of advantages. [0003] However, the electromagnetic orbital launch of the traditional electromagnetic launch device requires l...
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IPC IPC(8): F41B6/00
CPCF41B6/006F41B6/003
Inventor 孙志强
Owner 广东先进动力科技有限公司