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Combined aircraft hoisting device

A hoisting device and aircraft technology, applied in the direction of transportation and packaging, load hanging components, etc., can solve the problems of high cost, large quantity, inconvenient storage and transportation, etc., and achieve the goals of reducing rescue costs, strong flexibility, and convenient maintenance and management Effect

Pending Publication Date: 2022-07-12
航大联合航空设备有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The current hoisting devices are multiple designed according to the existing aircraft models, the number is large, not only the cost is high, but also, it is extremely inconvenient for daily storage and transportation during rescue

Method used

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Examples

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Embodiment Construction

[0023] The present invention will be further described in detail below through specific examples. The following examples are only descriptive, not restrictive, and cannot limit the protection scope of the present invention.

[0024] A combined aircraft hoisting device is innovative in that it includes a main combined hanging beam, an auxiliary combined hanging beam and a hoisting belt 11. The suspending beam part 2 and the suspending belt connecting piece 4 are constituted. A 40 t main suspending beam part is installed in the middle of the 60 t main suspending beam part; A main sling is connected between the upper ends of the connecting pieces, and two auxiliary slings 5 ​​are connected to the lower ends of the two sling connecting pieces; the two auxiliary slings described on each side are connected to the auxiliary combined suspending beam;

[0025] The said auxiliary combined hanging beam includes a 60t auxiliary hanging beam mechanism 6 and a 40t auxiliary hanging beam mec...

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Abstract

The invention relates to a combined aircraft hoisting device which comprises a main combined hoisting beam, auxiliary combined hoisting beams and hoisting belts, the two sides of the upper end of the main combined hoisting beam are connected with the hoisting belts, the two sides of the lower end of the main combined hoisting beam are provided with the auxiliary combined hoisting beams, and the main combined hoisting beam is composed of a main hoisting belt, a 60t main hoisting beam component, a 40t main hoisting beam component and a hoisting belt connecting piece. The auxiliary combined hanging beam comprises a 60t auxiliary hanging beam mechanism and a 40t auxiliary hanging beam mechanism; and the 60t auxiliary hanging beam mechanism and the 40t auxiliary hanging beam mechanism are assembled by connecting a 60t auxiliary hanging beam component and a 40t auxiliary hanging beam component through screws. The hoisting device can be detached and combined, and the 150-ton hoisting device can be detached into a 40-ton hoisting device and a 60-ton hoisting device, so that the hoisting device can provide rescue for various different types of airplanes.

Description

technical field [0001] The invention belongs to the field of aircraft rescue devices, and relates to a hoisting device, in particular to a combined aircraft hoisting device. Background technique [0002] The hoisting device is a device used to hoist the aircraft during air rescue. It is mainly composed of the main hoisting beam, the auxiliary hoisting beam and the hoisting belt. Several U-shaped slings are connected between them, and the several U-shaped slings form a contact surface with a certain width. During rescue, depending on the model of the aircraft, a hoisting device with a corresponding number of hoisting straps should be selected, so that it has a contact surface suitable for the rescue aircraft. [0003] The current hoisting devices are designed according to the existing aircraft models, and the number is large, which not only costs high, but also is extremely inconvenient for daily storage and transportation during rescue. SUMMARY OF THE INVENTION [0004] ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B66C1/18
CPCB66C1/18
Inventor 何振华李新健冯闯
Owner 航大联合航空设备有限公司
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