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Cylindrical roller bearing inner ring anti-rotation structure

A technology of cylindrical roller bearings and anti-rotation structures, applied in the field of aero-engines, can solve problems such as deformation of thin-walled rings, unfavorable disassembly, etc., achieve the effects of reducing circumferential stress, improving reliability, and preventing inner rings from rotating

Pending Publication Date: 2021-10-19
AECC HUNAN AVIATION POWERPLANT RES INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0010] Increasing the torque of the lock nut at the end face of the inner ring can prevent the inner ring of the bearing from rotating. Excessive locking torque at the end face of the inner ring will cause deformation of the thin-walled ring, and it is not conducive to disassembly during disassembly

Method used

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  • Cylindrical roller bearing inner ring anti-rotation structure
  • Cylindrical roller bearing inner ring anti-rotation structure
  • Cylindrical roller bearing inner ring anti-rotation structure

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Embodiment Construction

[0023] The technical solutions of the present invention will be clearly and completely described below in conjunction with the embodiments. Apparently, the described embodiments are only some of the embodiments of the present invention, not all of them. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention.

[0024] see Figure 1-3 As shown, a cylindrical roller bearing inner ring anti-rotation structure includes a bearing outer ring 1, a cage 4 is fixedly installed on the inner periphery of the bearing outer ring 1, and a bearing inner ring 3 is rotatably connected to the inner periphery of the cage 4. A cylindrical roller 2 is arranged between the cage 4 and the bearing inner ring 3; the cylindrical roller 2 is used to keep the relative rotation between the bearing inner ring 3 and the cage 4, and the end surface of the bearin...

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Abstract

The invention discloses a cylindrical roller bearing inner ring anti-rotation structure. The anti-rotation structure comprises a bearing outer ring, a retainer is fixedly mounted on the inner circumference of the bearing outer ring, a bearing inner ring is rotatably connected to the inner circumference of the retainer, and a cylindrical roller is arranged between the retainer and the bearing inner ring; and the cylindrical roller is used for keeping relative rotation between the bearing inner ring and the retainer, the end face of the bearing inner ring is provided with a plurality of sets of anti-rotation bosses and anti-rotation grooves, and the anti-rotation bosses and the anti-rotation grooves are used for being matched with connecting grooves and limiting protrusions which are correspondingly arranged on the connecting end face of a connecting shaft. According to the anti-rotation structure, the bearing structure is simple, assembly is convenient, relative rotation between the inner ring and a connecting shaft can be effectively prevented, and especially when the magnitude of interference between the bearing inner ring and the connecting shaft is insufficient due to changes of the working environment, the inner ring can be effectively prevented from rotating; and by using the structure, the magnitude of interference between the bearing inner ring and the connecting shaft can be properly reduced, so that the circumferential stress of a ferrule is reduced, and the use reliability of a product is improved.

Description

technical field [0001] The invention belongs to the technical field of aero-engines, and in particular relates to an anti-rotation structure for an inner ring of a cylindrical roller bearing. Background technique [0002] Usually, the inner ring of the rolling bearing and the shaft rotate together with an interference fit. Advanced turboshaft and turboprop engine rotors have the characteristics of high speed and high temperature in the bearing cavity, and the working environment of the bearing is harsh. The interference fit between the inner ring and the shaft will be affected by the centrifugal force of the rotor, the ambient temperature and the working load. Insufficient, when the relative rotation occurs between the inner ring and the shaft during the use of the bearing, it is not conducive to the normal operation of the bearing, and in severe cases it will cause the bearing to fail. Therefore, how to prevent the inner ring of the bearing from rotating relative to the sh...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F16C19/52F16C19/22F16C33/58
CPCF16C19/52F16C19/22F16C33/581F16C33/583F16C2360/23
Inventor 胡广存满维伟贺凤祥郝建军张翼梁志远
Owner AECC HUNAN AVIATION POWERPLANT RES INST