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Tractive connection device between aircraft carrier catapult and carrier-based aircraft

A technology of connecting devices and ejection devices, which is applied in the direction of launching/dragging transmission devices, etc., can solve the problems of increasing the weight and space occupation of carrier-based aircraft, increasing the structural weight and space occupation of carrier-based aircraft, and achieving the elimination of weight and space occupation , simple structure, the effect of simplifying the structure

Inactive Publication Date: 2017-11-28
董兰田
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

This structural form has the following problems and defects: 1. The pull rod and related supporting devices for retracting and retracting are arranged on the carrier-based aircraft, which increases the structural weight and space occupation of the carrier-based aircraft.
2. The powerful impact ejection power is transmitted to the carrier-based aircraft through the pull rod and the front landing gear bracket, which will inevitably require a stronger and more complex front landing gear system support, which also increases the weight and space occupation of the carrier-based aircraft

Method used

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  • Tractive connection device between aircraft carrier catapult and carrier-based aircraft
  • Tractive connection device between aircraft carrier catapult and carrier-based aircraft
  • Tractive connection device between aircraft carrier catapult and carrier-based aircraft

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Embodiment Construction

[0018] Below in conjunction with accompanying drawing of description, the present invention is described in further detail:

[0019] Such as figure 1 As shown, the traction connecting device between the aircraft carrier ejection device of the present invention and the carrier-based aircraft comprises an ejection shuttle 1, a draw bar 2, a damping buffer bar 3, a hook 4 and a hanging nose 5, and its ejection shuttle 1 and draw bar 2 and The damping buffer rods 3 are combined into a triangle through a hinge connection mode, and a hook 4 is arranged at the upper corner, and a hanging nose 5 matching the hook 4 is arranged at the lower end of the bracket in the middle of the front landing gear of the carrier aircraft.

[0020] figure 2 As shown, it is a schematic illustration of a scheme in which the nose 5 is arranged on the front or rear belly of the carrier aircraft nose landing gear.

[0021] image 3 As shown, the structural form of the inverted Y-shaped tow bar 2 adopted...

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PUM

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Abstract

The invention discloses a tractive connection device between an aircraft carrier catapult and a carrier-based aircraft. The device comprises a catapult gliding shuttle, a traction rod, a damping buffer rod, a hook and a hanging nose and is characterized in that the traction rod, the damping buffer rod and the hook are arranged on the catapult gliding shuttle, and the carrier-based aircraft is only provided with the hanging nose matched with the carrier-based aircraft. Compared with the prior art, the device has the beneficial effects of being simple in structure, firm, reliable, easy to manufacture, convenient to use and the like, the advantages of reducing the heavy and the space occupying of the catapult type carrier-based aircraft, reducing the manufacturing difficulty, the operation difficulty and maintaining difficulty of the carrier-based aircraft and the like are achieved, and the good popularization and application value is achieved.

Description

1. Technical field: [0001] The invention provides a traction connection device between an aircraft carrier ejection device and a carrier-based aircraft, which belongs to an aircraft carrier for ejecting carrier-based aircraft to take off. 2. Background technology: [0002] The aircraft carrier that accelerates the launch of the carrier-based aircraft through the ejection method uses a hinged pull rod that protrudes forward and downward from the front landing gear bracket of the side-by-side double wheels of the carrier-based aircraft, and is connected to the ejection shuttle of the catapult to complete the force. The transmission is realized. There are following problems and defects in this structural form: 1. The pull rod and the relevant supporting devices for retracting and unfolding are arranged on the carrier-based aircraft, which increases the structural weight and space occupation of the carrier-based aircraft. 2. The powerful impact ejection power is transmitted to ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64F1/06
CPCB64F1/06
Inventor 金函文董晖董兰田张峰
Owner 董兰田
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