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Aero engine gearbox and aero engine

An aero-engine and gear box technology, applied in belts/chains/gears, mechanical equipment, transmission parts, etc., can solve problems such as difficulty in keeping the thermal expansion coefficient consistent, gear shaft failure, and small axial movement of the gear shaft. Avoid stuck failure, improve stability, and ensure the effect of stability

Active Publication Date: 2021-04-30
AECC HUNAN AVIATION POWERPLANT RES INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

These two support methods make the axial movement of the gear shaft very small or impossible, which not only limits the application conditions of the gear shaft, but also the gear shaft is easy to get stuck when subjected to axial load
For example, when the gear shaft expands with heat and contracts with cold, because the thermal expansion coefficients of the gear shaft and other components in the aero-engine accessory transmission gearbox are difficult to keep consistent, and the axial movement of the gear shaft is extremely small, the gear shaft It is difficult to achieve effective expansion and contraction, resulting in changes in internal stress and forces with other components, and in severe cases, it will lead to failure of the gear shaft

Method used

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  • Aero engine gearbox and aero engine
  • Aero engine gearbox and aero engine
  • Aero engine gearbox and aero engine

Examples

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Embodiment Construction

[0033] Example embodiments will now be described more fully with reference to the accompanying drawings. Example embodiments may, however, be embodied in many forms and should not be construed as limited to the examples set forth herein; rather, these embodiments are provided so that this disclosure will be thorough and complete, and will fully convey the concept of example embodiments to those skilled in the art. The described features, structures, or characteristics may be combined in any suitable manner in one or more embodiments. In the following description, numerous specific details are provided in order to give a thorough understanding of embodiments of the present disclosure.

[0034] The terms "a", "an" and "the" are used to indicate the presence of one or more elements / components / etc; Additional elements / components / etc. may be present in addition to the listed elements / components / etc. The words "first" and "second" etc. are used only as marks, not to limit the num...

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PUM

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Abstract

The disclosure provides an aero-engine gearbox and an aero-engine, which belong to the technical field of aero-engines. The aero-engine gearbox includes a box body, a gear shaft, a gear, a first bearing and a second bearing; the first bearing and the second bearing realize the floating support of both ends of the gear shaft, so that the gear shaft can be bidirectional in the axial direction Movement: a first boss and a second boss are arranged on the gear shaft, and the first boss and the second boss cooperate with the first bearing and the second bearing respectively to limit the amount of movement of the gear shaft in the axial direction. The aero-engine gearbox has higher stability.

Description

technical field [0001] The present disclosure relates to the technical field of aero-engines, in particular to an aero-engine gearbox and an aero-engine. Background technique [0002] At present, the axial fixing methods adopted by the aero-engine accessory transmission gearbox are mainly divided into two-point one-way fixed type (both ends fixed) or single-point two-way fixed (one end fixed, one end swimming type). These two support methods make the axial movement of the gear shaft extremely small or impossible, which not only limits the application conditions of the gear shaft, but also easily blocks the gear shaft when subjected to an axial load. For example, when the gear shaft expands with heat and contracts with cold, because the thermal expansion coefficients of the gear shaft and other components in the aero-engine accessory transmission gearbox are difficult to keep consistent, and the axial movement of the gear shaft is extremely small, the gear shaft It is diffic...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F16H57/022
CPCF16H57/022F16H2057/02039F16H2057/0221
Inventor 李陆俊江平肖根升李超罗敏王帅
Owner AECC HUNAN AVIATION POWERPLANT RES INST
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