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Secondary unlocking type helicopter emergency floating bag

A technology for helicopters and floating sacs, applied in the direction of floats, etc., to solve the complex installation environment and solve the effect of easy overturning of water

Pending Publication Date: 2021-11-26
AEROSPACE LIFE SUPPORT IND LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The technical problem to be solved by the present invention is to provide a two-stage unlocked helicopter emergency buoyant bag for the above-mentioned defects in the prior art, which can automatically raise the buoyancy center of the buoy when it hits water without adding traction to the fuselage At the same time, it can meet the complex installation requirements of helicopters, effectively solving the technical problems of helicopters being forced to land on water, easy to overturn and complex installation environment

Method used

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  • Secondary unlocking type helicopter emergency floating bag
  • Secondary unlocking type helicopter emergency floating bag
  • Secondary unlocking type helicopter emergency floating bag

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Embodiment Construction

[0029] The present invention will be described in detail below in conjunction with the accompanying drawings and embodiments.

[0030] refer to Figure 1 to Figure 8 As shown, the secondary unlocking helicopter emergency floating bag in an embodiment provided by the present invention includes a floating bag main body 9, an upper connection belt 10, a secondary expansion belt 11 and a lower connecting belt 12, and the floating bag main body 9 is arranged on the helicopter On one side of the hanging point, the two ends of the upper connecting belt 10 are connected with the upper end of the helicopter hanging point and the buoyant bag main body 9 respectively, and the two ends of the secondary deployment belt 11 and the lower connecting belt 12 are connected side by side, and are connected with the helicopter hanging point and the floating bag respectively. The lower end of the bag main body 9 is connected, and the lower connection belt 12 is provided with an unlocking mechanism;...

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Abstract

The invention discloses a secondary unlocking type helicopter emergency floating bag which comprises a floating bag body, an upper connecting belt, a secondary unfolding belt and a lower connecting belt, the floating bag body is arranged on one side of a hanging point of a helicopter, the two ends of the upper connecting belt are connected with the hanging point of the helicopter and the upper end of the floating bag body respectively, and the two ends of the secondary unfolding belt and the two ends of the lower connecting belt are connected side by side; the two ends of the secondary unfolding belt and the two ends of the lower connecting belt are connected with the helicopter hanging point and the lower end of the floating bag body, and the lower connecting belt is provided with an unlocking mechanism. According to the secondary unlocking type helicopter emergency floating bag, the buoyancy center of the buoy can be automatically raised during landing without adding a traction mechanism on the fuselage, and meanwhile, the complex mounting requirements of the helicopter can be met, so that the technical problems that the helicopter is easy to overturn during landing and the mounting environment is complex are effectively solved.

Description

technical field [0001] The invention specifically relates to a two-stage unlocking helicopter emergency floating bag. Background technique [0002] When the helicopter is flying in the sea, if there is a failure and the emergency landing is required, the emergency airbag is required to provide buoyancy for the helicopter, thereby providing sufficient escape time for the pilot, thereby improving the efficiency of rescue. [0003] The emergency airbag is installed in the exposed area of ​​the helicopter, which is often unable to provide sufficient righting moment due to the limitations of the fuselage frame structure, weapon pylon, radar antenna and other factors. Therefore be badly in need of a kind of two-stage unlocking mechanism, can satisfy the complex installation of helicopter and use requirement, can realize the safe landing of helicopter again without overturning. Contents of the invention [0004] The technical problem to be solved by the present invention is to p...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C25/56
CPCB64C25/56
Inventor 任健何帆杨力王晓强朱元春刘畅杨娇
Owner AEROSPACE LIFE SUPPORT IND LTD
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