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Accelerator console control mechanism

A control mechanism and accelerator platform technology, which is applied to aircraft parts, aircraft power units, transportation and packaging, etc., can solve the problems of time-consuming and labor-intensive, prone to fatigue, low comfort of operating the throttle handle, etc.

Inactive Publication Date: 2016-03-23
GUIZHOU HUAYANG ELECTRICAL
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

This arrangement leads to the following problems: pilots are less comfortable to manipulate the throttle handle, time-consuming and labor-intensive, prone to fatigue, and lower work efficiency

Method used

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  • Accelerator console control mechanism

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Embodiment Construction

[0014] Below in conjunction with the accompanying drawings and preferred embodiments, the specific implementation, structure, features and functions of the throttle platform operating mechanism proposed according to the present invention will be described in detail as follows.

[0015] see figure 1 , the throttle platform operating mechanism of the present invention includes a throttle handle 1 and a flexible shaft joint 9, wherein: a throttle lever 2 is fixedly installed under the throttle lever 1, and a slider A3 is fixedly connected to the lower part of the throttle lever 2, and the slider A3 is slidably set On the guide rail A4, the slider B5 is fixedly connected under the slider A3, the slider B5 is slidably set on the guide rail B6, the lower part of the guide rail B6 is fixedly connected with the slider C7, and the slider C7 is slidably set on the guide rail C8, A flexible shaft joint 9 is fixedly connected to the slide block C7. The centerlines of guide rail A4 and gu...

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PUM

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Abstract

The invention discloses an accelerator console control mechanism. The accelerator console control mechanism comprises an accelerator handle (1) and a flexible shaft connector (9). The accelerator console control mechanism is characterized in that an accelerator lever (2) is fixedly mounted under the accelerator handle (1), a sliding block A(3) is fixedly connected to the lower part of the accelerator lever (2), and the sliding block A(3) can be mounted on a guide rail A(4) in a sliding and sleeving manner; a sliding block B(5) is fixedly connected to a position under the sliding block A(3), and can be mounted on a guide rail B(6) in a sliding and sleeving manner; a sliding block C(7) is fixedly connected to the lower part of the guide rail B(6), and can be mounted on a guide rail C(8) in a sliding and sleeving manner; the flexible shaft connector (9) is fixedly connected to the sliding block C(7); the center line of the guide rail A(4) and the center line of the guide rail C(8) are straight lines on different surfaces. The accelerator console control mechanism disclosed by the invention is simple in structure, high in efficiency, comfortable, convenient to operate, time-saving and labor-saving, and is suitable for an accelerator handle to manipulate and control the state of an aircraft engine.

Description

technical field [0001] The invention belongs to the technical field of aerodynamic control devices, and in particular relates to an accelerator platform control mechanism. Background technique [0002] For aircraft, the control of the throttle console is an essential link. In the prior art, since the throttle handle needs to control the engine through the flexible shaft (cable), affected by the arrangement and movement of the flexible shaft (cable), the control direction of the throttle handle in the flat-push throttle platform moves with the flexible shaft (cable) The directions are the same, that is, they are arranged along the direction of the aircraft. This arrangement leads to the following problems: the pilot's manipulation of the throttle handle is less comfortable, time-consuming and labor-intensive, prone to fatigue, and lower work efficiency. Contents of the invention [0003] The object of the present invention is to overcome the above-mentioned shortcomings a...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D31/04B64D31/14
CPCB64D31/04B64D31/14
Inventor 杨俊
Owner GUIZHOU HUAYANG ELECTRICAL
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