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Carrying device under high overload resistance configuration of bearing and characteristic evaluation method

A bearing device and bearing technology, which is applied to the rigid bracket of bearing components, bearing assembly, bearing components, etc., can solve the problems of not proposed steering gear bearing configuration and bearing characteristic evaluation method, etc., to shorten the trial production period, reduce the complexity, Solve the effect of aligning

Active Publication Date: 2021-04-02
SHANGHAI AEROSPACE CONTROL TECH INST
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  • Description
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  • Application Information

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Problems solved by technology

"Based on the elastoplastic Hertz theory, Palmgren's formula, and Mises criterion, the paper deduced the relationship between the total deformation of the roller and the raceway in contact with the load, but the verification test shows that this relationship is only applicable to low overload conditions.
[0009] In summary, the prior art has not yet proposed a configuration and load-carrying characteristic evaluation method for steering gear bearings against high overload, especially the evaluation method for steering gear bearing load-carrying characteristics applied to short-term high-overload steering gears.

Method used

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  • Carrying device under high overload resistance configuration of bearing and characteristic evaluation method
  • Carrying device under high overload resistance configuration of bearing and characteristic evaluation method
  • Carrying device under high overload resistance configuration of bearing and characteristic evaluation method

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Embodiment Construction

[0061]Combined with the drawings, such asFigure 1 ~ 2As shown in Figure: 1. Frame, 2. Rudder axis, 3. First Bearing, 4. Locking nut, 5. Connecting pin, 6. Second Bear, 7. Positioning screw, 8. Bar ribor assembly, 9. Third bearing. Bearing characteristic evaluation method under high overload configuration, including frame 1, rudder shaft 2, first bearing 3, lock nut 4, connect pin 5, second bearing 6, positioning screw 7, ball rib bar assembly 8, Three-bearing 9;

[0062]The outer diameter of the rudder shaft 2 is inner diameter of the first bearing 3, the second bearing 6 inner diameter shaft hole, the locking nut 4 is mounted on the outer diameter of the rudder shaft 2 by the connecting pin 5, and the lock nut 4 is each and the first Bearings 3, the second bearing 6 end surface axial positioning, the positioning screw 7 is attached to the rear end of the rudder shaft 2, and is positioned with the second bearing 6; the outer diameter of the first bearing 3, the outer diameter of the se...

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Abstract

The invention discloses a carrying device under high overload resistance configuration of a bearing and a characteristic evaluation method. The carrying characteristic evaluation method under the highoverload resistance configuration of the bearing comprises the following steps that firstly, a configuration method of radial high overload resistance of a cylindrical roller bearing and a centripetal knuckle bearing and axial high overload resistance of a double-row full-complement angular contact ball bearing is proposed; the cylindrical roller bearing and the centripetal knuckle bearing are installed at the two ends of a rudder shaft so as to solve the problem about aligning performance of the centripetal knuckle bearing; and the centripetal knuckle bearing is used for enabling the ruddershaft to bear certain Y-direction overload. Secondly, taking the cylindrical roller bearing as an example, in order to characterize the carrying characteristic of high overload resistance of the bearing, a bearing maximum radial static load concept and a checking method are proposed. The engineering realization is simple, scientific and effective, and the complexity of a steering engine structureis effectively reduced; the bearing maximum radial static load concept and the checking method are proposed, and a certain engineering basic theoretical depth is achieved; and the method has wide applicability and can be applied to various high-overload working conditions such as precision guided weapons.

Description

Technical field[0001]The present invention belongs to the field of precisely guided weapon flight control, and is specifically involved in a bearing device and a characteristic evaluation method under high overload configuration.Background technique[0002]In recent years, the development of precision missile drugs has been greatly improved, and it has the ability to scratch and high-efficiency and high-efficiency damage, which has become a high-tech and information warfare. By increasing precise guidance assemblies in the shell, a ballistic correction can be realized to effectively improve the hit accuracy of ammunition.[0003]However, the ammunition is in the launch process, the shells must experience huge overloads to accelerate the initial speed of the expected emission, the amplitude peak of the overload can reach more than 2000G (G is the gravity acceleration, the same), the action time is tens of milliseconds Within. For example, the maximum overload pulse generated by 155mm gre...

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Application Information

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IPC IPC(8): F16C41/00F16C35/07G01M13/04
CPCF16C41/00F16C35/07G01M13/04
Inventor 陈辉徐志伟唐德佳王厚浩刘旭张伟潘强严铖伏宜永杨灏
Owner SHANGHAI AEROSPACE CONTROL TECH INST