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Rudder support bearing cover

A rudder and bearing cap technology, applied in the aviation field, can solve the problems of limited structural space, time-consuming and laborious, and achieve the effect of reducing workload and improving maintainability

Pending Publication Date: 2021-10-12
SHAANXI AIRCRAFT CORPORATION
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] In the daily in-situ grease injection of bearings, due to the limitation of structural space, the rudder must be hoisted, the bearing support must be removed, and the bearing cover 1 must be opened to perform grease injection, which is time-consuming and labor-intensive.

Method used

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Embodiment Construction

[0023] The rudder support bearing bearing cap provided by the present invention will be introduced below in conjunction with the accompanying drawings.

[0024] figure 2 The exploded schematic view of the rudder bearing bearing cap provided by the present invention, image 3 The installation schematic diagram of the rudder support bearing bearing cap provided by the present invention, Figure 4 The sectional view of the rudder support bearing cap provided for the present invention, as Figure 2-4 as shown,

[0025] The present invention provides a rudder support bearing bearing cover, including: a machined cover plate 10, a spring washer 20 and a grease nozzle 30; wherein,

[0026] 4 bosses are arranged on the surface away from the bearing of the machine-adding cover plate 10, and a step-shaped annular through hole is arranged inside the machine-adding cover plate 10, which is used to clamp the rudder rotating tube shaft; each boss is provided with an L-shaped Channel, th...

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Abstract

The invention provides a rudder support bearing cover. The rudder support bearing cover comprises a cover plate (10), spring washers (20) and an oil injection nozzle (30), wherein four bosses are arranged on the surface, away from a bearing, of the cover plate (10), a step-shaped annular through hole is formed in the cover plate (10) and used for clamping a rudder rotating pipe shaft, an L-shaped channel is formed in each boss, the axial direction of an inlet of each L-shaped channel is parallel to or forms an acute angle with the surface of the cover plate (10), an outlet of each L-shaped channel is formed in the step of the step-shaped annular through hole and used for injecting lubricating grease into a bearing ball of the rudder support bearing, an inlet of the L-shaped channel is in threaded connection with the oil injection nozzle (30), and the spring washers (20) are arranged between the inlet of the L-shaped channels and the oil injection nozzle (30).

Description

technical field [0001] The invention belongs to the technical field of aviation, and in particular relates to a rudder support bearing bearing cap. Background technique [0002] The connecting structure of the empennage rudder bearing block of the large rudder surface rudder of existing aircraft is as follows: figure 1 As shown, see the Chinese patent application number 201610217272.6. [0003] When the bearing is filled with grease in situ on a daily basis, due to the limitation of structural space, the rudder must be hoisted, the bearing support must be removed, and the bearing cover 1 can be opened to implement the grease injection, which is time-consuming and labor-intensive. Contents of the invention [0004] The invention provides a bearing cap of a rudder support bearing, which realizes in-situ injection of grease and facilitates daily lubrication of the rudder support bearing. [0005] The present invention provides a rudder support bearing bearing cover, includi...

Claims

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Application Information

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IPC IPC(8): F16C35/04F16C33/66
CPCF16C35/04F16C33/6659
Inventor 刘斌赵占军常鑫荣谭小辉欧宇张建波李锐周明杨梓英刘毅
Owner SHAANXI AIRCRAFT CORPORATION