CN107907257A - A kind of compressor arm demarcates test device - Google Patents
A kind of compressor arm demarcates test device Download PDFInfo
- Publication number
- CN107907257A CN107907257A CN201711380411.8A CN201711380411A CN107907257A CN 107907257 A CN107907257 A CN 107907257A CN 201711380411 A CN201711380411 A CN 201711380411A CN 107907257 A CN107907257 A CN 107907257A
- Authority
- CN
- China
- Prior art keywords
- compressor arm
- loading
- arm
- test device
- computer
- 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.)
- Pending
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Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01L—MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
- G01L5/00—Apparatus for, or methods of, measuring force, work, mechanical power, or torque, specially adapted for specific purposes
- G01L5/0028—Force sensors associated with force applying means
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01L—MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
- G01L5/00—Apparatus for, or methods of, measuring force, work, mechanical power, or torque, specially adapted for specific purposes
- G01L5/24—Apparatus for, or methods of, measuring force, work, mechanical power, or torque, specially adapted for specific purposes for determining value of torque or twisting moment for tightening a nut or other member which is similarly stressed
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- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Chemical & Material Sciences (AREA)
- Analytical Chemistry (AREA)
- Control Of Positive-Displacement Pumps (AREA)
Abstract
A kind of compressor arm demarcates loading test device, it is to produce loading by computer motion control, and measuring each measuring point by strain transducer strains.The device is easy to operate automatic, is suitable for the calibration load test of various compressor arms.
Description
Technical field:
The present invention relates to a kind of compressor arm test device, specifically a kind of compressor arm calibration loading test device.
Background technology:
Structural member on space satellite, through carrying out structure connection frequently with compression release device, wherein on compressor arm
Pretightning force needs to demarcate, generally use spanner manual rotation clamp nut, obtains nut rotation angle pass corresponding with pretightning force
System, but manual loading easily produces deviation, uneven stress, when compared with big load nut is blocked with screw thread, causes to press
Tight bar failure, control accuracy and operating characteristics are poor.
The content of the invention:
The purpose of the present invention is to solve the shortcomings of the prior art and provide a kind of compressor arm calibration loading test device.Should
Device, which is adopted to computerized control, carries out loading measurement, high certainty of measurement, and the degree of automation is high, easy to operate.
Technical scheme:
Loaded by computer controlled motion control card, realized by motor and rotatably compress nut, pass through strain sensing
Device measures each measuring point stress, and computer automatically processes rating test result.
The beneficial effects of the invention are as follows:Compared with the prior art, the present invention is a kind of based on the control of computer controlled motion
Block the automatic testing equipment loaded, high certainty of measurement, the degree of automation is high, easy to operate.
Brief description of the drawings:
Fig. 1 is the structure diagram of the present invention.
Marked in figure:1 compressor arm holds end, 2 frames, 3 load sleeves, 4 compressor arms, 5 clamp nuts, on 6 pressed seats
Portion, 7 strain transducers, 8 pressed seat lower parts, 9 reverse loading arm, 10 motion control cards, 11 computers.
Embodiment:
A kind of as shown in Figure 1, compressor arm calibration loading test device.End, 2 frames, 3 loading sleeves are held including 1 compressor arm
Cylinder, 4 compressor arms, 5 clamp nuts, 6 pressed seat tops, 7 strain transducers, 8 pressed seat lower parts, 9 reverse loading arm, 10 movements
Control card, 11 computers.
The pressed seat top 6, pressed seat lower part 8 are fixed on loading frame 2 after being connected by compressor arm 4, are compressed
4 upper end of bar holds end 1 by compressor arm and clamps;Reverse loading arm 9 and apply moment of torsion generation pressure to clamp nut 5 by load sleeve 3
Tight effect;Controlled by computer 11 by motion control card 10 and reverse loading arm 9;Strain transducer 7 is connected to computer 11;Meter
The processing of calculation machine 11 obtains the thrust of compressor arm 4.
The compressor arm demarcates loading test device operation principle:Motion control card drives torsion under the control of the computer
Turn loading arm, compression rating test can be carried out according to measurement needs, strain transducer result of the test is automatically saved to computer
In.
Claims (1)
1. a kind of compressor arm demarcates loading test device, it is characterized in that:Pressed seat top (6), pressed seat lower part (8) pass through compression
It is fixed on after bar (4) series connection on loading frame (2), compressor arm (4) upper end holds end (1) by compressor arm and clamps;Reverse loading arm
(9) moment of torsion is applied to clamp nut (5) by load sleeve (3) and produces pressuring action;Motion control is passed through by computer (11)
Block (10) control and reverse loading arm (9);Strain transducer (7) is connected to computer (11);Computer (11) processing is compressed
The thrust of bar 4.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201711380411.8A CN107907257A (en) | 2017-12-20 | 2017-12-20 | A kind of compressor arm demarcates test device |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201711380411.8A CN107907257A (en) | 2017-12-20 | 2017-12-20 | A kind of compressor arm demarcates test device |
Publications (1)
Publication Number | Publication Date |
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CN107907257A true CN107907257A (en) | 2018-04-13 |
Family
ID=61869378
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201711380411.8A Pending CN107907257A (en) | 2017-12-20 | 2017-12-20 | A kind of compressor arm demarcates test device |
Country Status (1)
Country | Link |
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CN (1) | CN107907257A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109827689A (en) * | 2019-02-14 | 2019-05-31 | 上海卫星工程研究所 | Measuring device is loaded for spaceborne radar antenna pressing force |
CN110441042A (en) * | 2019-08-12 | 2019-11-12 | 中国科学院高能物理研究所 | A kind of HEPS-TF high-precision bracket coupling mechanism force calibration system and method |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101403646A (en) * | 2007-11-21 | 2009-04-08 | 奇瑞汽车股份有限公司 | Wiper pressing force test device and method |
CN105659838B (en) * | 2012-04-01 | 2014-08-13 | 北京空间飞行器总体设计部 | A kind of rod-type hold-down mechanism preload applying method |
CN105149930A (en) * | 2015-10-12 | 2015-12-16 | 沈阳航天新光集团有限公司 | Pre-tightening force loading device |
CN105253331A (en) * | 2015-09-10 | 2016-01-20 | 北京空间飞行器总体设计部 | Force-limited compaction releasing mechanism |
CN106546365A (en) * | 2016-09-22 | 2017-03-29 | 北京空间飞行器总体设计部 | A kind of sun blanket pressure calibration method of flexible solar wing |
CN206709995U (en) * | 2017-04-06 | 2017-12-05 | 武汉凡谷电子技术股份有限公司 | A kind of intelligent pressure detection assembly tool |
-
2017
- 2017-12-20 CN CN201711380411.8A patent/CN107907257A/en active Pending
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101403646A (en) * | 2007-11-21 | 2009-04-08 | 奇瑞汽车股份有限公司 | Wiper pressing force test device and method |
CN105659838B (en) * | 2012-04-01 | 2014-08-13 | 北京空间飞行器总体设计部 | A kind of rod-type hold-down mechanism preload applying method |
CN105253331A (en) * | 2015-09-10 | 2016-01-20 | 北京空间飞行器总体设计部 | Force-limited compaction releasing mechanism |
CN105149930A (en) * | 2015-10-12 | 2015-12-16 | 沈阳航天新光集团有限公司 | Pre-tightening force loading device |
CN106546365A (en) * | 2016-09-22 | 2017-03-29 | 北京空间飞行器总体设计部 | A kind of sun blanket pressure calibration method of flexible solar wing |
CN206709995U (en) * | 2017-04-06 | 2017-12-05 | 武汉凡谷电子技术股份有限公司 | A kind of intelligent pressure detection assembly tool |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109827689A (en) * | 2019-02-14 | 2019-05-31 | 上海卫星工程研究所 | Measuring device is loaded for spaceborne radar antenna pressing force |
CN109827689B (en) * | 2019-02-14 | 2020-12-11 | 上海卫星工程研究所 | Be used for satellite-borne radar antenna packing force loading measuring device |
CN110441042A (en) * | 2019-08-12 | 2019-11-12 | 中国科学院高能物理研究所 | A kind of HEPS-TF high-precision bracket coupling mechanism force calibration system and method |
CN110441042B (en) * | 2019-08-12 | 2020-10-20 | 中国科学院高能物理研究所 | System and method for calibrating locking force of HEPS-TF high-precision support |
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WD01 | Invention patent application deemed withdrawn after publication | ||
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Application publication date: 20180413 |