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Supporting structure for mounting stretcher on helicopter

A technology of supporting structure and helicopter, applied in the field of aviation medical rescue equipment, can solve the problems of low reliability of stretchers, inability to realize quick disassembly and assembly of stretchers, poor appearance effect, etc.

Inactive Publication Date: 2014-10-29
HARBIN
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] At present, the stretcher installation on the helicopter mainly uses positioning brackets and straps for fixing, which cannot realize the quick disassembly and assembly of the stretcher, and the appearance effect is poor; at the same time, because the strap itself is a non-rigid part, the reliability of fixing the stretcher is not high.

Method used

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  • Supporting structure for mounting stretcher on helicopter
  • Supporting structure for mounting stretcher on helicopter
  • Supporting structure for mounting stretcher on helicopter

Examples

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Embodiment Construction

[0010] The specific embodiments of the present invention will be further described below in conjunction with the accompanying drawings.

[0011] see figure 1 , figure 2 , image 3 , a support structure for installing a stretcher on a helicopter, consisting of a front support structure 1 and a rear support structure 2: the front support structure 1 includes a front support frame 3, left and right supports 4, left and right cover plates 5 and left and right locks 6. The support 4 is located on the front support frame 3, and the front support frame 3 and the support 4 are fixedly connected by bolts; the upper plane of the support 4 has a semicircular depression, and its shape and position are matched with the stretcher pole; the support 4 is a The side is connected with the cover plate 5 through a shaft, and the lower plane of the cover plate 5 has a semicircular depression, and its shape matches the stretcher support rod; the cover plate 5 and the lock catch 6 are connected t...

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Abstract

The invention belongs to the field of aviation medical aid devices, and relates to a supporting structure for mounting a stretcher on a helicopter. The supporting structure comprises a front supporting structure body (1) and a rear supporting structure body (2). The front supporting structure body (1) comprises a front supporting frame (3), a left support (4), a right support (4), a left cover plate (5), a right cover plate (5), a left lock catch (6) and a right lock catch (6). The rear supporting structure body (2) comprises a rear supporting frame (8), a left lower support (7), a right lower support (7), a left upper support (9) and a right upper support (9). According to the supporting structure, through the quick releasing structures, the stretcher can be quickly dismounted and mounted, stability and reliability of the stretcher are guaranteed, and the functions of the rescue stretcher are given to full play.

Description

technical field [0001] The invention belongs to the field of aviation medical rescue equipment, and relates to a support structure for installing a stretcher on a helicopter. Background technique [0002] At present, the stretcher installation on the helicopter mainly uses positioning brackets and straps for fixing, which cannot realize the quick disassembly and assembly of the stretcher, and the appearance effect is poor; at the same time, because the strap itself is a non-rigid part, the reliability of fixing the stretcher is not high. . Contents of the invention [0003] The technical problem to be solved by the present invention is to provide a safe and reliable support structure for installing a stretcher on a helicopter. [0004] The technical solution of the present invention is: a support structure for installing a stretcher on a helicopter, characterized in that: the support structure includes a front support structure 1 and a rear support structure 2; the front ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D47/00
Inventor 鹿文宝林大威武金祥付东刘亮庞茂江
Owner HARBIN
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