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Output bearing oil delivery mechanism, intermediate reducer and helicopter

A technology for output bearings and reducers, which is applied in mechanical equipment, gear lubrication/cooling, belts/chains/gears, etc. It can solve problems such as troublesome assembly, complex structural design of casing and end cover, and increased weight of intermediate reducers. Achieve the effect of reducing weight, simple structure and increasing weight

Active Publication Date: 2022-06-21
AECC HUNAN AVIATION POWERPLANT RES INST
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The invention provides an output bearing oil delivery mechanism, an intermediate speed reducer and a helicopter, in order to solve the complicated structure design of the casing and the end cover and the troublesome assembly between the components in the existing oil supply mode of the bearing in the intermediate speed reducer And the technical problem of increasing the weight of the intermediate reducer

Method used

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  • Output bearing oil delivery mechanism, intermediate reducer and helicopter
  • Output bearing oil delivery mechanism, intermediate reducer and helicopter

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Embodiment Construction

[0024] The embodiments of the present invention will be described in detail below with reference to the accompanying drawings, but the present invention can be implemented in many different ways as defined and covered below.

[0025] figure 1 It is a schematic structural diagram of the output bearing oil feeding mechanism according to the preferred embodiment of the present invention; figure 2 It is a schematic structural diagram of the oil collecting device of the output bearing oil feeding mechanism according to the preferred embodiment of the present invention.

[0026] like figure 1 and figure 2 As shown, the output bearing oil feeding mechanism of this embodiment is used for the lubrication of the output bearing of the intermediate reducer of the helicopter, and includes a casing 1, a gear shaft 2, a bearing 5 and an end cover 6. The casing 1 is connected with the end cover 6, and the gear The shaft 2 is arranged in the casing 1 and is rotatably connected to the end ...

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Abstract

The invention discloses an oil delivery mechanism for an output bearing. The lubricating oil is stored in the casing oil pool of the casing. The input shaft of the intermediate reducer of the helicopter meshes and drives the gear to rotate to drive the lubricating oil in the casing oil pool to splash, and the oil collecting device collects the lubricating oil. The lubricating oil splashed with the gears is introduced into the oil guide structure, and the lubricating oil in the oil guide structure guides the lubricating oil to the oil groove of the end cover under the action of the centrifugal force formed by the high-speed rotation of the gear shaft, and then the lubricating oil enters the bearing to clean the bearing Lubricates and returns to the case sump. The components of this application have simple structure, very reliable assembly and good casting process. While rationally utilizing the space, they also play a role in reducing weight; making full use of the centrifugal force brought by the rotation of the output bearing, so that the lubricating oil flows along a specific direction, Good lubricating effect: the oil delivery structure is located inside the output shaft, correspondingly shortening the length of the output gear shaft and reducing the weight of the intermediate reducer. The invention also discloses an intermediate reducer and a helicopter.

Description

technical field [0001] The present invention relates to the technical field of bearing lubrication, in particular, to an output bearing oil feeding mechanism. In addition, the present invention also relates to an intermediate speed reducer and a helicopter comprising the above-mentioned output bearing oil feeding mechanism. Background technique [0002] The angle between the input axis and the output axis of the intermediate reducer of a helicopter is usually an obtuse angle, the output end is upturned, the output bearing position is high, and lubrication is difficult, but the output bearing is the key component of the helicopter intermediate reducer, and its performance is very high. Quality directly affects the service life and reliability of the intermediate reducer, and excellent lubrication design is an important guarantee for improving the service life and reliability of the bearing, and also affects the number of intermediate reducer parts, the weight of the whole mac...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F16H57/023F16H57/021F16H57/04F16H57/029
CPCF16H57/023F16H57/021F16H57/043F16H57/045F16H57/029
Inventor 宋益明朱卓宇
Owner AECC HUNAN AVIATION POWERPLANT RES INST
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