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Hydraulic actuation system

A hydraulic actuation and hydraulic system technology, which is applied in the direction of fluid pressure actuation system components, fluid pressure actuation devices, servo motors, etc., can solve the problems of slow boosting speed and cannot meet the needs of use, so as to improve work efficiency, Reasonable structural design and simple operation

Pending Publication Date: 2017-12-19
辽宁港泰航空科技有限公司
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  • Abstract
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AI Technical Summary

Problems solved by technology

[0002] In the civil aviation airport's hydraulic maintenance field where the aircraft reverse thrust cover is opened during maintenance of the engine, the existing hydraulic actuation system is originally equipped with an electric cylinder manual booster method, which requires manual operation. , and the pressurization speed is slow, there is no oil filter, and it cannot meet the needs of modern use. Therefore, a system to replace the manual manual hydraulic pressurization device to open the aircraft thrust reverser cover is studied.

Method used

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Embodiment Construction

[0011] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0012] see Figure 1-3 , the present invention provides a technical solution: a hydraulic actuation system includes a vehicle body 1, a universal wheel 2, a steering wheel 3, a side door 4, an upper cover door 5, a push-pull rod 6, an electric control system and a hydraulic system. The bottom of the body 1 is provided with a universal wheel 3 and two direction wheels 2, the front side of the car body 1 is provided with a side door 4, the top of the car body 1 ...

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Abstract

The invention discloses a hydraulic actuation system and relates to the technical field of hydraulic control equipment. A universal wheel and two direction wheels are arranged at the bottom of a vehicle body; a side door is arranged on the front side of the vehicle body; an upper closing cover is arranged at the upper part of the vehicle body; the rear side of the vehicle body is connected with a push-pull rod; a control panel is arranged in the vehicle body and is in control connection with an electric control system; a hydraulic system is arranged in the vehicle body. The hydraulic actuation system has the advantages of reasonable structure design, easier operation and high degree of modernization; by adopting electricity to replace manual hand cranking for hydraulic boosting opening, the human and material resources are saved, and the working efficiency is greatly improved.

Description

technical field [0001] The invention relates to a hydraulic actuation system, in particular to a hydraulic maintenance system for opening an aircraft reverse thrust cover during engine maintenance in civil aviation airports. Background technique [0002] In the civil aviation airport's hydraulic maintenance field where the aircraft reverse thrust cover is opened during maintenance of the engine, the existing hydraulic actuation system is originally equipped with an electric cylinder manual booster method, which requires manual operation. , and the pressurization speed is slow, there is no oil filter, and it cannot meet the needs of modern use. Therefore, a system to replace the manual manual hydraulic pressurization device to open the aircraft thrust reverser cover is studied. Contents of the invention [0003] The purpose of the present invention is to provide a hydraulic actuation system to solve the problems in the above-mentioned background technology. [0004] In ord...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C25/22B64C25/34F15B13/02F15B11/17F15B21/04
CPCF15B11/17F15B13/023F15B21/041B64C25/22B64C25/34
Inventor 王媛媛
Owner 辽宁港泰航空科技有限公司
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