CN201569540U - Novel torque loading calibrating device - Google Patents

Novel torque loading calibrating device Download PDF

Info

Publication number
CN201569540U
CN201569540U CN2009202711426U CN200920271142U CN201569540U CN 201569540 U CN201569540 U CN 201569540U CN 2009202711426 U CN2009202711426 U CN 2009202711426U CN 200920271142 U CN200920271142 U CN 200920271142U CN 201569540 U CN201569540 U CN 201569540U
Authority
CN
China
Prior art keywords
torque sensor
pull pressure
calibrating
cross
frame
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
CN2009202711426U
Other languages
Chinese (zh)
Inventor
吴双金
王亦明
龙贵华
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
China Helicopter Research and Development Institute
Original Assignee
China Helicopter Research and Development Institute
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by China Helicopter Research and Development Institute filed Critical China Helicopter Research and Development Institute
Priority to CN2009202711426U priority Critical patent/CN201569540U/en
Application granted granted Critical
Publication of CN201569540U publication Critical patent/CN201569540U/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Abstract

The utility model relates to a novel torque loading calibrating device which belongs to the technology of calibrating test. The calibrating device comprises a cross calibrating rack, hydraulic power assisting cylinders, pull pressure sensors, an upper end shaft, a lower end shaft and a horizontal rack, wherein the center of the cross calibrating rack is fixed on the upper end shaft; the four top ends of the cross calibrating rack are respectively connected with the pull pressure sensors through universal joints; each pull pressure sensor is connected with one hydraulic power assisting cylinder through a bolt; the four hydraulic power assisting cylinders are respectively fixed on the four support bases of the horizontal rack; and a calibrated torque sensor is mounted between the upper and the lower end shafts. In the utility model, by adopting the loading mode, the loading can be uniformly conducted through four power assisting cylinders, the torque sensor can be calibrated without needing to be dismounted from the rotary wing of a helicopter, and therefore, the difficulties that the calibration of the torque sensor with large range is inconvenient, and the torque sensor cannot be calibrated on the spot are solved, and the accurate load of the torque sensor in the operation of the system is reflected.

Description

A kind of novel moment of torsion loads caliberating device
Technical field
The utility model belongs to the rating test technology, relates to a kind of novel moment of torsion and loads caliberating device.
Background technology
When carrying out lifting airscrew torque sensor rating test, the scaling method of employing is to carry out rating test with being loaded weights on ground by calibration element mostly, then, calibration element is reinstalled returned to original position again.In the lifting airscrew tower, because torque sensor is installed in 15 meters high positions, volume is bigger, and dismounting is difficulty, and the load range owing to torque sensor loads than carrying out full and down again, then needs a large amount of counterweights, loads and demarcates inconvenience.
Summary of the invention
The purpose of this utility model is: a kind of carried convenient that adds is provided, and loading wide ranges, a kind of novel moment of torsion that stated accuracy is high load caliberating device.Technical solution of the present utility model is that caliberating device comprises cross demarcation frame, hydraulic booster tube, pull pressure sensor, upper shaft, lower end axle, level frame; Cross is demarcated the center fixation of frame on upper shaft, four tops that frame demarcated in cross connect pull pressure sensor by universal joint respectively, each pull pressure sensor links to each other with the hydraulic booster tube by bolt, four hydraulic booster tubes are separately fixed on four supporting seats on the level frame, and the torque sensor of being demarcated is installed between upper shaft and the lower end axle.Advantage that the utlity model has and beneficial effect, the utility model adopts by novel load mode, can evenly load by 4 power-assisted tubes, need not torque sensor is pulled down just and can be demarcated it from lifting airscrew, solve the wide range torque sensor and demarcated inconvenient problem, and the difficult point that can't demarcate at the scene torque sensor, the real definite coefficient of reaction torque sensor when system works improved the precision of transducer calibration.
Description of drawings
Fig. 1 is a structural representation of the present utility model;
Fig. 2 is that frame and hydraulic booster tube and pull pressure sensor connection diagram demarcated in the utility model cross.
Embodiment
Below the utility model is described in further details.Caliberating device comprises cross demarcation frame 1, hydraulic booster tube 2, pull pressure sensor 3, upper shaft 5, lower end axle 6, level frame 7; Cross is demarcated the center fixation of frame 1 on upper shaft 5, four tops that frame 1 demarcated in cross connect pull pressure sensor 3 by universal joint 11 respectively, each pull pressure sensor 3 links to each other with hydraulic booster tube 2 by bolt, four hydraulic booster tubes 2 are separately fixed on four supporting seats 14 on the level frame 7, and the torque sensor of being demarcated 4 is installed between upper shaft 5 and the lower end axle 6.
The utility model moment of torsion loads caliberating device and will demarcate on the frame 1 to cross by 4 hydraulic booster tube 2 loading forces, and then, the strong and arm of force has just loaded moment of torsion on upper shaft 5, make the load that has been subjected to moment of torsion by calibration element torque sensor 4; When hydraulic booster tube 2 loads, just can know the load of loading by pull pressure sensor 3, just can calculate the actual torque of the torque sensor that is loaded into 4 again by the load and the arm of force, just can obtain the load of torque sensor by the signal of actual value and torque sensor 4.
When carrying out rating test, lower end axle 6 has bolt 12 to be fixed on down on the transverse plane 13, the lower end of torque sensor 4 is installed in the upper end of lower end axle 6 with bolt 8, the upper end of torque sensor 4 is installed in the bottom of upper shaft 5 by bolt 9, it is fixing that frame 1 is demarcated by bolt 10 and cross in the top of upper shaft 5,4 tops that frame 1 demarcated in cross connect pull pressure sensor 3 by universal joint 11 respectively, pull pressure sensor 3 links to each other with hydraulic booster tube 2 by bolt, hydraulic booster tube 2 is by on the supporting seat 14 on the bolt level frame 7, acting force by hydrostatic control power-assisted tube 2 during use, and the arm of force calculates the size of the load that is loaded.The utility model can effectively improve easy to use at the high pulling torque sensor, has improved loading accuracy, and has realized that the torque sensor of wide range can load at the scene.

Claims (1)

1. a novel moment of torsion loads caliberating device, it is characterized in that, caliberating device comprises cross demarcation frame [1], hydraulic booster tube [2], pull pressure sensor [3], upper shaft [5], lower end axle [6], level frame [7]; Cross is demarcated the center fixation of frame [1] on upper shaft [5], four tops that frame [1] demarcated in cross connect pull pressure sensor [3] by universal joint [11] respectively, each pull pressure sensor [3] links to each other with hydraulic booster tube [2] by bolt, four hydraulic booster tubes [2] are separately fixed on four supporting seats [14] on the level frame [7], and the torque sensor of being demarcated [4] is installed between upper shaft [5] and the lower end axle [6].
CN2009202711426U 2009-11-27 2009-11-27 Novel torque loading calibrating device Expired - Lifetime CN201569540U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2009202711426U CN201569540U (en) 2009-11-27 2009-11-27 Novel torque loading calibrating device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2009202711426U CN201569540U (en) 2009-11-27 2009-11-27 Novel torque loading calibrating device

Publications (1)

Publication Number Publication Date
CN201569540U true CN201569540U (en) 2010-09-01

Family

ID=42661833

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2009202711426U Expired - Lifetime CN201569540U (en) 2009-11-27 2009-11-27 Novel torque loading calibrating device

Country Status (1)

Country Link
CN (1) CN201569540U (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101865750A (en) * 2010-06-22 2010-10-20 胡卓林 Portable calibrating device for pull pressure sensor
CN101961559A (en) * 2010-10-21 2011-02-02 哈尔滨工程大学 Rotor wing supporting device of model helicopter
CN102494839A (en) * 2011-12-08 2012-06-13 中国航天空气动力技术研究院 Self-balancing large range torque calibrating device
CN102798494A (en) * 2012-09-04 2012-11-28 德州联合石油机械有限公司 High-precision torque measurement device and method for petroleum pipeline dismounting frame
CN103852211A (en) * 2012-11-28 2014-06-11 江苏金风科技有限公司 Bending moment sensor calibration device and calibration method
CN114235393A (en) * 2021-12-09 2022-03-25 中国船舶重工集团公司第七0三研究所 Helicopter main reducer rotor torque static calibration method

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101865750A (en) * 2010-06-22 2010-10-20 胡卓林 Portable calibrating device for pull pressure sensor
CN101865750B (en) * 2010-06-22 2013-10-30 胡卓林 Portable calibrating device for pull pressure sensor
CN101961559A (en) * 2010-10-21 2011-02-02 哈尔滨工程大学 Rotor wing supporting device of model helicopter
CN101961559B (en) * 2010-10-21 2012-02-01 哈尔滨工程大学 Rotor wing supporting device of model helicopter
CN102494839A (en) * 2011-12-08 2012-06-13 中国航天空气动力技术研究院 Self-balancing large range torque calibrating device
CN102494839B (en) * 2011-12-08 2013-10-30 中国航天空气动力技术研究院 Self-balancing large range torque calibrating device
CN102798494A (en) * 2012-09-04 2012-11-28 德州联合石油机械有限公司 High-precision torque measurement device and method for petroleum pipeline dismounting frame
CN103852211A (en) * 2012-11-28 2014-06-11 江苏金风科技有限公司 Bending moment sensor calibration device and calibration method
CN103852211B (en) * 2012-11-28 2016-08-03 江苏金风科技有限公司 Moment of flexure sensor calibration apparatus and scaling method
CN114235393A (en) * 2021-12-09 2022-03-25 中国船舶重工集团公司第七0三研究所 Helicopter main reducer rotor torque static calibration method

Similar Documents

Publication Publication Date Title
CN201569540U (en) Novel torque loading calibrating device
CN102494839B (en) Self-balancing large range torque calibrating device
CN103528752B (en) Wind tunnel lever and power and torque standard device
CN203772258U (en) Tower barrel comprehensive monitoring device for wind turbine generator
CN109580094B (en) Fan generator set axis of rotation moment balance calibration system
CN201255659Y (en) Balance detection cart for servo system
CN202522369U (en) Engineering vehicle torque sensor calibration device
CN101881679A (en) Airplane steering wheel multi-axis force measurement component and measurement method thereof
CN106706267A (en) Marine structure wave-current load experimental measuring device in actual marine environment
CN104390772A (en) Device and method for testing static and dynamic variable friction of telescopic mechanism
CN108844666B (en) Tractor hangs force measurement device
CN219121719U (en) Test tester convenient to dismouting
CN204831636U (en) Vehicle tie rod axial force transducer and axial force test system
CN207423355U (en) A kind of truck scale calibration electronic weight
CN207263368U (en) A kind of self-checking device of wireless work(figure test terminal
CN209230873U (en) A kind of wind turbine power generation unit rotation axis torque balance calibration system
CN109552666A (en) A kind of direct measuring method of propeller flight pulling force
CN202704827U (en) Wireless weighing device of crane hook
CN201653615U (en) Direct detection type moment signal measuring device
CN211576332U (en) Weighing sensor and truck
CN202956279U (en) Vehicle steering data acquisition device
CN203551057U (en) Weigh sensing module
CN208459028U (en) Control arm assembly sluggishness detection device
CN203299007U (en) Calibration tool for car suspension system
CN207423324U (en) The intelligent continuous calibration equipment of float level meter

Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
CX01 Expiry of patent term

Granted publication date: 20100901

CX01 Expiry of patent term