A calibration device and calibration method for the relationship between pretightening force and pretightening torque

A calibration device and pre-tightening force technology, applied to measuring devices, force/torque/work measuring instruments, and measuring torque/torsion force during tightening, can solve problems such as wire breakage, calibration data, discontinuity, and easy entanglement of wires , to achieve the real effect of the calibration result

Active Publication Date: 2016-08-31
BEIJING INST OF ASTRONAUTICAL SYST ENG +1
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  • Abstract
  • Description
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  • Application Information

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Problems solved by technology

[0006] The purpose of the present invention is to provide a pre-tightening force to solve the problems in the prior art that holes need to be dug on the simulated connected structure, and the wires of the strain gauges are easily wound on the connecting bolt rods, causing the wires to break and the calibration data to be discontinuous. Calibration device and calibration method for relationship with preload torque

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  • A calibration device and calibration method for the relationship between pretightening force and pretightening torque
  • A calibration device and calibration method for the relationship between pretightening force and pretightening torque
  • A calibration device and calibration method for the relationship between pretightening force and pretightening torque

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Embodiment Construction

[0024] The technical solutions of the present invention will be further described below in conjunction with the accompanying drawings.

[0025] This embodiment provides a device for calibrating the relationship between pre-tightening force and pre-tightening torque, which is mainly used for calibrating the relationship between pre-tightening force and pre-tightening torque of separation nuts. Its structure is as follows: figure 1 As shown, it includes a device 1 capable of providing a torsional load, a torsional force sensor sleeve 4, a pressure sensor tooling 5, a separation nut sleeve 6 and a data processing device 10; the device 1 capable of providing a torsional load is an existing device, including The equipment body, the torsion end fixture 2 and the fixed end fixture 3, the equipment body includes a bottom plate and two side plates parallel to each other, the torsion end fixture 2 and the fixed end fixture 3 are respectively installed on the inner side of the two side pl...

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Abstract

The invention, which belongs to the field of the aircraft separating apparatus, particularly relates to a calibration apparatus for a relation between a pretightening force and a pretightening moment, and a calibration method thereof. The apparatus comprises a device capable of providing a torsion load, a torsional force sensor sleeve, a pressure sensor tool, a separating nut sleeve, and a data processing device. According to the method, a torsional force is applied to the separating apparatus; a torsional force sensor and a pressure sensor are used for reflecting a pretightening moment applied to the separating apparatus and a pretightening force generated by the separating apparatus in real time; and thus calibration of the relation between the pretightening force and the pretightening moment of the separating apparatus is completed. The method and the apparatus have the following beneficial effects: a curve of a relation between a pretightening force and a pretightening moment can be calibrated continuously and be drawn automatically; the separating nut and the connecting bolt are consistent with the motion state of the connected structure relatively when the pretightening moment is applied to the separating apparatus, so that the calibration result is more real. The strain gauge leads are arranged outside and twisting of the leads with the separating apparatus can be prevented.

Description

technical field [0001] The invention belongs to the field of aircraft separation devices, and in particular relates to a calibration device and a calibration method for the relationship between pre-tightening force and pre-tightening torque. Background technique [0002] Separation nut separation devices are widely used in the connection and separation of various sections of rockets, missiles and other aircraft or instruments and equipment due to their advantages of small separation impact, no pollution, and ground inspection. [0003] The separation nut separation device is generally composed of a separation nut, a connecting bolt and a catcher, and has the functions of connecting, carrying and unlocking. The separation device of the separation nut realizes its connection function by the thread pair between the separation nut and the connecting bolt, and applies a pretightening moment to the separation device at one end of the separation nut or the connection bolt according...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01L5/00G01L5/24
Inventor 于兵胡振兴陈岱松卢红立苏晗王帅张志峰
Owner BEIJING INST OF ASTRONAUTICAL SYST ENG
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