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Reciprocating seal experiment table for measuring friction feature of single seal ring

A sealing ring and friction technology, applied in the field of reciprocating sealing test benches, can solve the problems of no friction distinction, difficulty in simulating aviation actuator application conditions, and inability to realize high pressure and high speed.

Inactive Publication Date: 2015-04-22
TSINGHUA UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The existing reciprocating seal test benches do not strictly distinguish the friction force of the inner and outer strokes of a single seal ring when measuring the friction force of the seal ring
In addition, the existing reciprocating sealing test bench cannot realize high-pressure and high-speed working conditions, and it is difficult to simulate the application conditions of aviation actuators

Method used

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  • Reciprocating seal experiment table for measuring friction feature of single seal ring
  • Reciprocating seal experiment table for measuring friction feature of single seal ring
  • Reciprocating seal experiment table for measuring friction feature of single seal ring

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Embodiment Construction

[0023] The present invention will be described in further detail below in conjunction with the accompanying drawings and specific embodiments.

[0024] Such as figure 1 As shown, the present invention is a reciprocating seal test bench for measuring the friction characteristics of a single sealing ring, which consists of three parts: an experimental cylinder 100, a high-pressure simulation system 200 connected to the experimental cylinder 100, a high-speed drive cylinder and its hydraulic system 300.

[0025] Such as figure 2 , image 3 and Figure 4As shown, the experimental cylinder 100 includes a workbench 102, a mounting base 101 fixed at one end of the workbench 102, a linear guide rail 103 fixed on the workbench 102, two slide blocks 106 installed on the linear guide rail 103, two The left cylinder base 131 and the right cylinder base 122 are installed respectively on the slide block 106, and the cylinder barrel 124 is installed between the left cylinder base 131 and...

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Abstract

The invention discloses a reciprocating seal experiment table for measuring a friction feature of a single seal ring. The experiment table is composed of an experiment cylinder, a high-pressure simulation system, a high-speed drive oil cylinder and a hydraulic system of the experiment table, wherein the high-pressure simulation system and the high-speed drive oil cylinder are connected with the experiment cylinder. A cylinder body of the experiment oil cylinder is installed on a work table through a linear guide rail, the high-speed drive oil cylinder drives the experiment cylinder to reciprocate through a connecting flange, a piston rod of the experiment cylinder is fixed and is divided into two halves, the two halves are connected through a pull pressure sensor and are fixed to the work table. A bushing, used for installation of the seal ring, of the experiment cylinder can be replaced, and therefore seal rings with different pre-compression amounts and different section shapes can be measured conveniently. A high-pressure oil supply system provides a high-pressure working simulation environment inside the experiment cylinder, and the experiment table can adjust the reciprocating speed, strokes and in-cylinder pressure of the drive oil cylinder. The experiment table can measurement the friction feature of the inner stroke and the outer stroke of the single seal ring, the leakage amount and the medium temperature after reciprocating for several times .

Description

technical field [0001] The invention belongs to the technical field of rubber and plastic reciprocating seals, and in particular relates to a reciprocating seal test bench for measuring the friction characteristics of a single sealing ring. Background technique [0002] Aviation actuators are key components of large aircraft, mainly used in aircraft wings and landing gear, and play a very important role in the process of aircraft takeoff, landing and attitude adjustment. At present, the research and development of large passenger aircraft has been listed as a major national project, but its actuation system is monopolized by foreign companies. In the actuation system, the aero actuator plays a very important role as the executive component. At present, the pressure system of large passenger aircraft is spanning from 21Mpa to 35Mpa, and is developing towards a higher direction. The actuator moves very quickly during the execution of the action. Therefore, whether the opera...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01L5/00
Inventor 吴长贵索双富高志迪力夏提·艾海提黄首清赵嵩阳武佩君张志强
Owner TSINGHUA UNIV
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