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A double-channel cable mechanism and an aircraft landing gear hatch with the same

A dual-channel, steel cable technology, applied in the chassis and other directions, can solve problems such as increasing the difficulty of finished product design, and achieve the effect of reducing design difficulty and development risk, rational structure layout, and non-interference.

Active Publication Date: 2020-10-09
XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

For products with compact and complex structures, it is often impossible to realize, which puts forward higher requirements for the design of the finished product and increases the difficulty of the design of the finished product

Method used

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  • A double-channel cable mechanism and an aircraft landing gear hatch with the same
  • A double-channel cable mechanism and an aircraft landing gear hatch with the same
  • A double-channel cable mechanism and an aircraft landing gear hatch with the same

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Embodiment Construction

[0036] In order to make the objectives, technical solutions and advantages of the present invention clearer, the technical solutions in the embodiments of the present invention will be described in more detail below in conjunction with the drawings in the embodiments of the present invention. In the drawings, the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The described embodiments are some, but not all, embodiments of the invention. The embodiments described below by referring to the figures are exemplary and are intended to explain the present invention and should not be construed as limiting the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention. Embodiments of the present invention will be described in detail below ...

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Abstract

The invention discloses a dual-channel steel rope overrun mechanism and an aircraft landing gear hatch with the same. The dual-channel steel rope overrun mechanism comprises a bracket, a splined shaft, a first fan-shaped assembly, a second fan-shaped assembly, a first steel rope, a second steel rope, a lever, a first pre-tightening torsional spring, a second pre-tightening torsional spring and a third pre-tightening torsional spring, wherein the bracket comprises a connecting part, a first cylinder shaft and a second cylinder shaft; the splined shaft is arranged in a manner of penetrating through the first cylinder shaft and the second cylinder shaft; the first fan-shaped assembly is arranged on the first cylinder shaft; the second fan-shaped assembly is arranged on the second cylinder shaft; one end of the first steel rope is arranged on the first fan-shaped assembly; one end of the second steel rope is arranged on the second fan-shaped assembly; the lever is arranged between the first fan-shaped assembly and the second fan-shaped assembly, is connected with the splined shaft, and is provided with a first boss and a second boss; the first pre-tightening torsional spring is arranged on the first cylinder shaft or the splined shaft; the second pre-tightening torsional spring is arranged on the first cylinder shaft or the splined shaft; and the third pre-tightening torsional spring is arranged on the second cylinder shaft or the splined shaft. The dual-channel steel rope overrun mechanism disclosed by the invention is reasonable in structural configuration and convenient to mount; and the problem that a ground handle and an emergency handle in a cabin are in mutual non-interference is solved.

Description

technical field [0001] The invention relates to the technical field of aircraft structures, in particular to a double-channel steel cable mechanism and an aircraft landing gear hatch provided therewith. Background technique [0002] For products with only one external control structure, it needs to be driven by a set of mechanisms and using two different control modes, which puts higher requirements on the cable control mechanism. The two manipulation modes correspond to two different cable paths, and the manipulation of one mode has no influence on the mechanism of the other cable path. [0003] In general, when two different cable paths are used to complete the same manipulation task of the same product, it is often required that the driven product has two independent mechanical interfaces, which are connected to two cable systems to achieve two different operations. A cable-driven approach to task realization. For products with compact and complex structures, it is ofte...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C25/16B64C25/20
CPCB64C25/16B64C25/20
Inventor 贾锦张万民孙卫华柳刚
Owner XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA