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Stretcher system for aviation

A stretcher and aviation technology, applied in stretchers, respirators, vehicle rescue and other directions, can solve the problems of installation method, lack of universality and safety of carrying capacity, and achieve flexible installation layout, good versatility and strong carrying capacity. Effect

Inactive Publication Date: 2017-04-26
CHINA AVIATION LIFESAVING INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

In order to overcome the shortcomings of the existing stretcher system in terms of installation method, carrying capacity, versatility and safety, etc., a stretcher system with a new structure is required

Method used

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  • Stretcher system for aviation
  • Stretcher system for aviation
  • Stretcher system for aviation

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Experimental program
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Embodiment Construction

[0022] The present invention will be further described below in conjunction with the accompanying drawings and embodiments.

[0023] The stretcher system mainly includes two parts: the main body of the stretcher system and the oxygen supply and calling equipment. Unloading pin 11, quick release point locking pin 8, guide rail locking assembly 9, etc.

[0024] The support arm assembly includes a support arm 101, a support arm buckle 102, a pin shaft 103, a latch, a latch handle 104, a preload block 106, a pressure block 107, and a button 105. The support arm assembly plays the role of carrying and fixing the stretcher. Each stretcher The system can be equipped with four pairs of support arm assemblies. The support arm is installed on the column to carry the stretcher. The arm buckle 102 cooperates with the latch to fix the special stretcher or the GJB831 stretcher of different manufacturers. The latch handle can control the latch to lock and unlock the arm buckle. The button ...

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Abstract

The invention relates to a stretcher system for aviation. The stretcher system is generally mounted on large aircrafts like transport aircrafts and used for the aircrafts to transport the sick and wounded. The stretcher system is composed of supporting arm components, oxygen supply and calling equipment, uprights, a transverse stay bar, inclined stay bars, a fork-shaped joint, a base and quick-demounting pins, and the stretcher system is used for the aircrafts to transport the sick and wounded and can meet oxygen supply and calling needs of the sick and wounded. Mounting of the stretcher system on an aircraft does not depend on the cabin wall and the top of the aircraft, and the stretcher system is directly connected with an aircraft floor through quick-demounting point locking pins and guide rail locking components, so that the stretcher system is convenient to mount and demount, flexible in installation layout and stable in structure, meets airworthiness standards and has obvious advantages in the aspects of carrying capacity, mounting mode, functional expansion and universality when compared with existing products.

Description

technical field [0001] The invention relates to an aviation stretcher system, which is generally installed in large-scale aircraft such as transport planes, and is used when the aircraft transports the sick and wounded by air. Background technique [0002] At present, the stretcher system used for transporting the wounded on the helicopter generally benefits from the small helicopter cabin, which makes the bottom and top of the stretcher system have load-bearing parts that can be connected to the aircraft structure, but is also limited by the size of the helicopter cabin to transport the wounded. Can't realize the bulk transportation to the lying position wounded. However, the equipment used by domestic transport aircraft to transport the wounded is relatively simple, and it is basically a zero-time modification equipment. Connection points must be set on the aircraft bulkhead. The installation position of the equipment in the cabin is not flexible enough, and the overall eq...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): A61G1/00A61G1/04A61M16/00
CPCA61G1/00A61G1/04A61G2203/70A61G2220/10A61M16/00
Inventor 熊彬贺振郗文
Owner CHINA AVIATION LIFESAVING INST
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