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An anisotropic synchronous load test device and its application method

A technology of load test and fixed seat, which is applied in the direction of measuring device, test of mechanical parts, test of machine/structural parts, etc., to achieve the effect of accurate test of different direction loading

Active Publication Date: 2021-01-01
SHANGHAI AEROSPACE EQUIP MFG GENERAL FACTORY
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] In order to solve the problem of a different direction synchronous load test of a driving mechanism, the purpose of the present invention is to provide a different direction synchronous load test device to complete the different direction synchronous load test process of a certain driving mechanism

Method used

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  • An anisotropic synchronous load test device and its application method
  • An anisotropic synchronous load test device and its application method
  • An anisotropic synchronous load test device and its application method

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Embodiment Construction

[0025] The use of the present invention will be described below in conjunction with the accompanying drawings.

[0026] In the prior art, an anisotropic synchronous load test device is needed to complete an anisotropic synchronous load test process of a driving mechanism. In order to achieve the purpose of the above invention, the present invention provides an anisotropic synchronous load test device, including: a fixed base 1, a baffle plate 2, an upper pull rod assembly 3, a U-shaped piece 4, a positive pressure sensor system 5, a circular cover 6, Loading screw 7. The fixed seat 1 is a square box structure, with product installation holes and lightening rectangular holes on both sides, the rectangular holes can be used for hand handling; the bottom has product installation holes and tension machine interfaces. The baffle plate 2 is connected with the fixing seat by screws, and there are two symmetrical square holes on the baffle plate, and a circular sensor installation gr...

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Abstract

Provided is a different-direction synchronous load test device including a fixed seat, a baffle board, an upper pull rod assembly, a U-shaped member, a positive pressure sensor system, a round cover, and a load screw rod, the fixed seat is in a square box structure, the baffle board is connected with the fixed seat via a screw, two symmetrical square holes are arranged in the baffle board, the surface of one side is provided with a round sensor installing groove, the upper pull rod assembly is composed of a square block and a round rod, the round rod end is connected with a tensile machine chuck, threaded holes are arranged in the two sides of the square block for installing product bearing pins, the U-shaped member is a forked long-strip structure, the four edges of the two long strips are provided with chamfering, the U-shaped member passes through the symmetrical holes in the baffle board, through holes are arranged in the head parts of the long strips for installing product bearing rings, the positive pressure sensor system is composed of a positive pressure sensor and an amplification display, the positive pressure sensor is arranged in the round sensor installing groove in the surface of one side of the baffle board, the round cover is arranged on the other side of the positive pressure sensor to protect the sensor, and the load screw rod is cooperated with the threaded hole in the end face of the U-shaped member.

Description

technical field [0001] The invention relates to the technical field of tensile loading test, in particular to a different-direction synchronous load test device and its use method. Background technique [0002] combine Figure 8 The structure of a locking mechanism is shown, and its functional principle is to drive the guide rail through the output screw of the driving mechanism to realize the locking of the X-direction force-bearing ring and the locking of the Y-direction force-bearing pin. Design index requirements: synchronous loading is carried out through the passive end installation interface of this locking mechanism, and the loading capacity requirement is X direction: (4±0.2) kN, Y direction: (21±0.2) kN. [0003] Existing test equipment can only complete the one-way tension and compression load test, or complete the synchronous load test in different directions by hanging weights in the other direction. Although the method of hanging the weight is in the horizonta...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01M13/00
CPCG01M13/00
Inventor 徐清华王曙群赵杰琚龙汪万桥王闻杰俞忠
Owner SHANGHAI AEROSPACE EQUIP MFG GENERAL FACTORY