Lubricating structure for transmission mechanism

A technology for lubricating structures and transmission mechanisms, applied to transmission parts, gear lubrication/cooling, mechanical equipment, etc., which can solve problems such as secondary wear, poor lubrication effect, and inability to discharge metal debris, so as to avoid secondary wear Effect

Active Publication Date: 2020-08-07
AECC HUNAN AVIATION POWERPLANT RES INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0006] A main purpose of the present invention is to provide a lubricating structure of a transmission mechanism to solve the problems of poor lubricating effect and secondary wear caused by metal debris in the prior art

Method used

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  • Lubricating structure for transmission mechanism
  • Lubricating structure for transmission mechanism
  • Lubricating structure for transmission mechanism

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0048] Such as figure 2 and image 3 as shown, figure 2 is a schematic diagram of a lubrication structure of a transmission mechanism shown according to an exemplary embodiment. image 3 It is a schematic diagram of another perspective of the lubricating structure of the transmission mechanism shown according to an exemplary embodiment. In an exemplary embodiment, the transmission mechanism includes an input shaft 100 , an output shaft 200 and a rotating shaft 400 , the input shaft 100 is linked to the output shaft 200 , and the output shaft 200 is linked to the rotating shaft 400 .

[0049] Such as figure 2 and image 3As shown, in some embodiments, both the input shaft 100 and the output shaft 200 are hollow structures, and the output shaft 200 is sleeved outside the input shaft 100, between the inner side wall of the output shaft 200 and the outer side wall of the input shaft 100 A keyed connection, such as a spline pair 700 , is formed to transmit power from the in...

Embodiment 2

[0060] In some embodiments, the in-out relationship of the input and output shafts can be reversed. Specifically, the input shaft can be sheathed outside the output shaft, and the rotating shaft can be linked to the input shaft or the output shaft. The oil collecting tube is fixedly connected to the inside of the output shaft, and other structures and beneficial effects are basically the same as those of the first embodiment above, and will not be repeated here.

Embodiment 3

[0062] An embodiment of the present invention provides a lubrication structure for a transmission mechanism. The transmission mechanism of this embodiment includes an input shaft, an output shaft and a rotating shaft. The output shaft is sleeved outside the input shaft, and the input shaft and the output shaft are connected by a key. , the rotating shaft is linked to the input shaft or output shaft. The structures and connections of the input shaft, the output shaft and the rotating shaft are basically the same as those of the first and second embodiments above, and will not be repeated here. The difference between embodiment three and above embodiment one and embodiment two is:

[0063] The lubricating structure of this embodiment includes an oil inlet channel, an oil return channel, and a plurality of first oil holes. The oil inlet channel is formed inside the input shaft and runs through the end face of the input shaft, so that the oil is thrown off by the oil rejection str...

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Abstract

The invention provides a lubricating structure for a transmission mechanism. The transmission mechanism comprises an inner transmission shaft, an outer transmission shaft sleeved on the outside of theinner transmission shaft, and a rotating shaft, wherein the inner transmission shaft and the outer transmission shaft are connected by a key, and the rotating shaft is linked to the inner transmission shaft or the outer transmission shaft; the lubricating structure comprises an oil collecting cylinder, an oil return channel, a first oil hole and a second oil hole; the oil collecting cylinder is arranged in the inner transmission shaft and has an oil inlet channel, and the oil inlet channel has an inner conical surface; the oil return channel is arranged between the inner transmission shaft and the outer transmission shaft, and the key is located on the path of the oil return channel; the first oil hole is arranged on the inner transmission shaft and connected to the oil return channel; the second oil hole is arranged on the oil collecting cylinder and connected to the oil inlet channel, an oil collecting groove is formed between the outer side wall of the oil collecting cylinder and the inner side wall of the inner transmission shaft, and the oil collecting groove is respectively connected to the first oil hole and the second oil hole; an oil throwing structure, which can throw the lubricating oil in the oil pool into the oil inlet channel, is provided on the outside of the rotating shaft.

Description

technical field [0001] The present invention generally relates to the technical field of lubrication, and specifically relates to a lubrication structure of a transmission mechanism. Background technique [0002] Helicopter tail reducers generally use the "splash lubrication" method to achieve lubrication and cooling, that is, during the high-speed rotation of the gear, the gear teeth throw the lubricating oil in the oil pool to the inner cavity wall of the casing, and the oil collecting pocket on the inner cavity wall of the casing After the lubricating oil is collected, the lubricating oil is transported along the oil passage on the casing wall to each component that needs lubrication and cooling. However, for those areas located inside the components, since this area is far away from the casing wall, and it is difficult to connect with the oil circuit on the casing wall, this area cannot be lubricated and cooled. [0003] In order to solve the above problems, the prior a...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F16H57/04B08B15/04
CPCB08B15/04F16H57/043F16H57/0434
Inventor 阳新元陈金张川苏新生
Owner AECC HUNAN AVIATION POWERPLANT RES INST
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