Stretcher support mechanism used under aviation condition

Abstract

The invention discloses a stretcher support mechanism used under the aviation condition, and relates to the technical field of aviation medical aid. The stretcher support mechanism comprises two standcolumns, an upper crossbeam, a lower crossbeam, two stretchers, supporting arms, lower supporting feet, a safety belt, a power box and a medical equipment rack, wherein the two stand columns are vertically and symmetrically placed; the upper crossbeam is fixedly installed at the top between the two stand columns; the lower crossbeam is fixedly installed in the middle between the two stand columns; the middles and the bottoms of the two stand columns all horizontally stretch out to form the supporting arms; one stretcher is fixedly installed at the upper end of the middle supporting arm; the other stretcher is fixedly installed at the upper end of the bottom supporting arm; the lower supporting feet are fixedly installed at the bottom of the stretcher fixedly installed at the bottom supporting arm; safety belts are arranged at the side walls of the stretchers; the medical equipment rack is fixedly installed at the side wall of the stand column at the inner side; the power box is fixedly installed in the middle of the medical equipment rack; the stretcher support mechanism can be rapidly disassembled, and the purposes of medical configuration conversion, standby and refitting modularization are achieved.

Description

technical field [0001] The invention relates to the technical field of aviation medical rescue, in particular to a stretcher support mechanism used under aviation conditions. Background technique [0002] The stretcher support mechanism applied under aviation conditions should generally have the following characteristics, meet the requirements of air transportation for 2 or more wounded and sick, and meet the requirements of extreme load, vibration, flame retardancy, electromagnetic compatibility, safety, ergonomics and other aviation-adaptive types. It can be installed and fixed on the plane reliably, with fast loading and unloading capabilities, and can meet the requirements of oxygen supply, power supply, medical equipment interface, casualty Fixed requirements. [0003] In the prior art, the stretcher support mechanism used under aviation conditions has the following problems: [0004] First, the integration is low, and it does not have independent oxygen supply, power...

AI Technical Summary

Problems solved by technology

[0004] First, the integration level is low, and it does not have independent oxygen supply, power supply, and equipment dressing storage capabilities;

[0005] Second, there are few medical equipment that can be equipped, which cannot meet the requirements for the airlift treatment of moderately ill patients;

[0006] Third, the man-machine function is poor and cannot fully meet the requirements of medical service use;

[0007] Fourth, it does not have the ability to quickly disassemble, and does not meet the modular requirements for standing and refitting

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