Barrel-type launching device and its bullet-retaining mechanism for aircraft launching
A launcher and aircraft technology, applied in launch/drag transmissions, aircraft, unmanned aircraft, etc., can solve problems such as inconvenient operation and complex structure, and achieve a simple and compact structure, multiple applicable models, and complete functions Effect
Active Publication Date: 2019-01-11
北京华信宇航科技有限公司
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Problems solved by technology
[0005] Embodiments of the present invention provide a barrel-type launching device for aircraft launching and its flip-back mechanism, so as to solve the technical problems of complex structure and inconvenient operation existing in aircraft launching equipment in the prior art
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[0027] The present invention will be described in further detail below in conjunction with the accompanying drawings and embodiments. In particular, the following examples are only used to illustrate the present invention, but not to limit the scope of the present invention. Likewise, the following embodiments are only some but not all embodiments of the present invention, and all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention.
[0028] Please also refer to figure 1 and figure 2 , figure 1 It is a structural schematic diagram of a preferred embodiment of the bullet rest mechanism used in the aircraft barrel launcher of the present invention, figure 2 yes figure 1 Schematic diagram of the bottom structure of the flick mechanism in the embodiment. The bullet rest mechanism is located in the launch tube (not shown) of the barrel-type launching aircraft device. During the ...
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The invention provides a barrel-type launching device for launching an aircraft and a bullet holder mechanism thereof. The aircraft is supported and fixed in the barrel; the bullet holder mechanism includes a connecting seat, an electrical interface bullet holder, a fixed pin bullet holder and two spring pin bullet holders; wherein, the electrical interface bullet holder, the fixed pin bullet holder and two The spring pin bullet holders are respectively fixedly connected with the connecting seat, and the two spring pin bullet holders are arranged oppositely, and the electric interface bullet holder and the fixed pin bullet holder are arranged oppositely, so as to support and fix the aircraft from four positions around the tail cone ring of the aircraft. Compared with the prior art, the advantages of the flip support mechanism are that the structure is simple and compact, the applicable models are many, and the flip support realizes complete functions.
Description
technical field [0001] The invention relates to the technical field of aircraft launching equipment, in particular to a barrel-type launching device for aircraft launching and a bullet holder mechanism thereof. Background technique [0002] Commonly used aircraft launch equipment in the prior art includes catapult launch equipment and towed launch equipment. [0003] Catapult launch equipment mainly tightens the rubber band through the motor, and releases the rubber band when launching, thereby converting the potential energy of the rubber band into the kinetic energy of the aircraft, so that the aircraft reaches the take-off speed. However, this technical solution is suitable for limited types of aircraft wings, and the attainable flight speed is related to the energy storage and energy release speed of the rubber band, thus limiting the maximum take-off speed that the aircraft can achieve. Generally, the take-off speed can only reach 20m / s -30m / s, which limits the scope o...
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IPC IPC(8): B64F1/06
CPCB64F1/06B64U70/70
Inventor 陈波李佐政刘玖
Owner 北京华信宇航科技有限公司