Tubular launching device for aircraft launching and missile support mechanism of tubular launching device

A technology for launching devices and aircraft, applied in the direction of launching/dragging transmissions, aircraft, unmanned aircraft, etc., can solve the problems of complex structure and inconvenient operation, and achieve a simple and compact structure, complete functions, and many applicable models Effect

Active Publication Date: 2017-03-22
北京华信宇航科技有限公司
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

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

Method used

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  • Tubular launching device for aircraft launching and missile support mechanism of tubular launching device
  • Tubular launching device for aircraft launching and missile support mechanism of tubular launching device
  • Tubular launching device for aircraft launching and missile support mechanism of tubular launching device

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Embodiment Construction

[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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Abstract

The invention provides a tubular launching device for aircraft launching and a missile support mechanism of the tubular launching device. The missile support mechanism is arranged in a launching barrel of the tubular aircraft launching device, and in the aircraft launching process, the missile support mechanism is used for supporting and fixing an aircraft in the launching barrel. The missile support mechanism comprises a connection seat, an electrical connector missile support, a fixing pin missile support and two spring pin missile supports, wherein the electrical connector missile support, the fixing pin missile support and the two spring pin missile supports are fixedly connected with the connection seat, the two spring pin missile supports are arranged oppositely, and the electrical connector missile support and the fixing pin missile support are arranged oppositely so that the aircraft can be supported and fixed from four positions on the periphery of the tailcone of the aircraft. Compared with the prior art, the missile support mechanism has the advantages that the structure is simple and compact, the missile support mechanism is suitable for aircrafts of a large number of types, and the missile supports have 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...

Claims

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Application Information

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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
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