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A high-voltage driving tool for cold start of aero-engine

An aero-engine, high-pressure drive technology, applied in the direction of machines/engines, mechanical equipment, gas turbine devices, etc., can solve the problems of long operation time, unfavorable rapid maneuvering, large workload, etc., to achieve simple operation, improve service life, reduce The effect of workload

Active Publication Date: 2019-08-20
成都航利装备科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The method of using a ratchet wrench to achieve a cold start must open the lower skin of the belly, which requires a lot of work and takes a long time to operate, which is not conducive to rapid maneuvering

Method used

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  • A high-voltage driving tool for cold start of aero-engine
  • A high-voltage driving tool for cold start of aero-engine

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Embodiment Construction

[0017] The present invention will be further described below in conjunction with accompanying drawing, protection scope of the present invention is not limited to the following:

[0018] Such as figure 1 and figure 2 As shown, a high-pressure driving tool for cold start of an aero-engine includes a rotating shaft 1, an input shaft 2, a connecting rod 3, a connecting bush 4 and a working elbow 5, the right end of the rotating shaft 1 is provided with a handle 6, and the left end of the rotating shaft 1 is installed On the planetary reducer 7, the input shaft 2 is installed on the left end of the planetary reducer 7, the left end of the input shaft 2 is fixedly connected with the connecting rod 3, the left end of the connecting rod 3 is installed on the connecting bush 4, and the left end of the connecting bush 4 is set There are working elbows 5;

[0019] The middle position of the connecting rod 3 is installed through the bearing and the upper end of the fixed seat 8, and t...

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Abstract

The invention discloses a cold-start high-pressure driving tool for an aircraft engine. The tool comprises a rotating shaft, an input shaft, a connecting rod, a connecting bushing and a working bend,wherein the right end of the rotating shaft is sleeved with a handle, the left end of the rotating shaft is mounted on a planetary reducer, the input shaft is mounted at the left end of the planetaryreducer, the left end of the input shaft is fixedly connected with the connecting rod, the left end of the connecting rod is mounted on the connecting bushing, and the working bend is arranged at theleft end of the connecting bushing; the outer side of the middle of the connecting rod is matched with the upper end of a fixing seat through a bearing, and the lower end of the fixing seat is fixed on a rack through a clamping mechanism; a driving rod is mounted in the connecting bushing through a bearing and fixedly connected with the left end of the connecting rod, and the left end of the driving rod extends into the working bend; the working bend is L-shaped, a bevel gear set is arranged in the working bend, and a switching sleeve is also arranged in the working bend. The cold-start high-pressure driving tool has the benefits as follows: the tool is simple to operate, rapid to start and convenient to maintain and the workload is reduced.

Description

technical field [0001] The invention relates to the technical field of aero-engine drive and maintenance, in particular to an aero-engine cold-start high-voltage drive tool. Background technique [0002] At present, when the engine is installed and needs to be cold started, it is usually completed by ignition of the turbine starter on the aircraft, and there is no tool specially used for the cold start of the aircraft engine. During the ground maintenance test run, the aircraft skin is usually opened, and a ratchet wrench is used to drive the high-pressure rotor to complete the cold start of the engine. Since the number of ignitions of the turbine starter is strictly regulated, there is a requirement for ignition life. Turbine starters are expensive, and frequent use of turbine starters reduces the working life of turbine starters and greatly reduces the number of times an aircraft can fly. the cost is too high. The method of using the ratchet wrench to realize the cold s...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F02C7/275
Inventor 刘华平徐灵王军蔡远思古云祥董子刚杨林
Owner 成都航利装备科技有限公司
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