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Anti-collision mechanism for aircraft fuel tank

A technology of aircraft fuel tanks and anti-collision mechanisms, applied in the direction of fuel tank safety measures, etc., can solve problems such as poor anti-collision performance, and achieve the effects of improving safety, improving stability, and moving smoothly

Active Publication Date: 2019-08-16
晨龙飞机(荆门)有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The purpose of the present invention is to make up for the deficiencies in the prior art, and to provide an anti-collision mechanism for aircraft fuel tanks, which has the advantages of good anti-collision performance and solves the problem of poor anti-collision performance of existing aircraft fuel tanks

Method used

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  • Anti-collision mechanism for aircraft fuel tank
  • Anti-collision mechanism for aircraft fuel tank
  • Anti-collision mechanism for aircraft fuel tank

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Embodiment Construction

[0033] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0034] see Figure 1-5 , the present invention provides a technical solution: an anti-collision mechanism for an aircraft fuel tank, comprising an aircraft fuel tank body 3, a fixing mechanism 2 is fixedly installed on the right side of the aircraft fuel tank body 3, and a buffer is fixedly installed on the right side of the fixing mechanism 2 Institution 1.

[0035]The buffer mechanism 1 includes a buffer block 101, a first slider 102, a base 103, a position...

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Abstract

The invention discloses an anti-collision mechanism of an aircraft fuel tank, relating to the technical field of the aircraft fuel tank, comprising an aircraft fuel tank body, wherein a fixing mechanism is fixedly installed on the right side surface of the aircraft fuel tank body, and a cushioning mechanism is fixedly installed on the right side surface of the fixing mechanism. The collision avoidance mechanism of the aircraft fuel tank, because the first slide rod is provided and usedin conjunction with that first slide rord, the second slider can move more conveniently, avoiding the problemof catching the second slider in motion, however, by provide with a baffle, the second slide rod can be effectively prevented from slipping off the second slide ring, The movable plate move more smoothly, so that that cushion mechanism is provide, The external store auxiliary fuel tank is prevented from bee damaged by bird impact, fuel leakage and other conditions that affect the safety of the aircraft, the safety performance of the device is improved, and through the fixing mechanism, the buff mechanism can be disassembled and inspected more conveniently, the buffer mechanism can be preventedfrom being damaged, and the safety hidden danger of the device can be avoided.

Description

technical field [0001] The invention relates to the technical field of aircraft fuel tanks, in particular to an anti-collision mechanism for aircraft fuel tanks. Background technique [0002] The auxiliary fuel tank refers to the fuel tank that is thick in the middle and streamlined at both ends hanging under the fuselage or wing. Hanging the auxiliary fuel tank can increase the flight range and endurance time of the aircraft, and the aircraft can throw away the auxiliary fuel tank when necessary in air combat, and enter the battle with better maneuverability. The installation type of the auxiliary fuel tank can be divided into two categories: non-disposable and disposable, Except for the non-disposable auxiliary fuel tank designed to match the shape of the fuselage in the early stage, the main design direction of the exterior design is streamlined, in order to reduce the drag generated, which has a negative impact on the aircraft's mobility and stability. Reduce the impact...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64D37/32
CPCB64D37/32
Inventor 梁定璿陈伟忠
Owner 晨龙飞机(荆门)有限公司
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