CN105651687A - A tool for testing bobbin coil binding power and a method therefor - Google Patents

A tool for testing bobbin coil binding power and a method therefor Download PDF

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Publication number
CN105651687A
CN105651687A CN201410649446.7A CN201410649446A CN105651687A CN 105651687 A CN105651687 A CN 105651687A CN 201410649446 A CN201410649446 A CN 201410649446A CN 105651687 A CN105651687 A CN 105651687A
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China
Prior art keywords
shaped framework
coil
load
framework coil
cantilever lever
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CN201410649446.7A
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CN105651687B (en
Inventor
樊正云
姚远
林莉
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No 618 Research Institute of China Aviation Industry
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No 618 Research Institute of China Aviation Industry
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Publication of CN105651687B publication Critical patent/CN105651687B/en
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Abstract

The invention relates to a tool for testing bobbin coil binding power and a method therefor. The tool comprises a guide rail base (1), a first suspended rod (2), a first lock screw (3), a load (4), a bobbin coil (5), a central spindle (6), a second lock screw (7) and a second suspended rod (8). At the tangential direction of the outmost coil layer of the bobbin coil (5), the load (4) is hung on a self-adhesive varnished wire at an end of the bobbin coil (5), the weight of the load (4) is increased gradually until the self-adhesive varnished wire on which the load (4) is hung is separated from the bobbin coil (5), and then the weight of the load (4) is a binding power value of the outmost coil layer of the bobbin coil (5). Through results of coil binding power testing, heating temperature and heating time in heat bonding process parameters can be adjusted, and therefore binding power values of bobbin coils can be quantified and controlled.

Description

A kind of shaped framework coil cohesive force test fixture and method
Technical field
The present invention relates to a kind of shaped framework coil cohesive force test fixture and method.
Background technology
Current aviation field is increasingly employed fly-by-wire flight control system to control the flight of aircraft, and the parts that electromagnetic sensor, motor, transformator, electromagnetic valve etc. comprise various electromagnetic component are the important component parts constituting system feedback. Generally, the coil of these components interior can adopt general enamel-covered wire, through operations such as preliminary drying, dipping lacquer, drip-dry, drying after processing, several hours consuming time even tens hourly workers time, need supporting special impregnating equipment, leaching can produce to be pungent when drying, harmful gas. Along with the development of China's basic industries, a kind of outer layer is covered with the self-binding enamel wire of self-adhesion paint and receives the concern of aviation and introduced gradually. At present, self-binding enamel wire coil adopts the bonding method of blowing hot-air limit, limit coiling, and all process steps can complete within a few minutes to dozens of minutes, and above-mentioned leaching can be avoided to dry the weak point of mode, embodies obvious advantage. It is firm by being mutually bonded between coil and coil that this kind of coil requires by heating, loose wire is there is not under working environment, and great majority are needed to adjust the shaped framework coil of electrical property, control if the force value that bonds between coil is not done, when adjusting electrical property and need to remove some circle coils, the insullac of enamel-covered wire internal layer may be made to be stripped because cohesive force between coil is excessive, thus causing shaped framework coil that Insulation Problems occurs. Therefore in the urgent need to designing a kind of shaped framework coil cohesive force test fixture and method.
Summary of the invention
The purpose of the present invention is to propose to a kind of shaped framework coil cohesive force test fixture and method.
The technical scheme is that
A kind of shaped framework coil cohesive force test fixture, is made up of guiderail base the 1, first cantilever lever the 2, first lock-screw 3, load 4, shaped framework coil 5, mandrel the 6, second lock-screw 7 and the second cantilever lever 8; Guiderail base 1 is the base plate with guide-track groove; First cantilever lever 2 and the second cantilever lever 8 are placed in parallel in the guide-track groove of guiderail base 1, and may move the spacing of adjustment, one end of first cantilever lever 2 and the second cantilever lever 8 is equipped with the installing hole that can place mandrel 6, and on installing hole, it is respectively equipped with the first lock-screw 3 and the second lock-screw 7 of fixed central spindle 6, mandrel 6 is that two ends match with the installing hole of the first cantilever lever 3 and the second cantilever lever 8 respectively, the middle axle matched with shaped framework coil 5 endoporus, mandrel 6 can flexible rotating between shaped framework coil 5 endoporus.
A kind of shaped framework coil cohesive force method of testing, its operating procedure is as follows:
Step 1: self-binding enamel wire is wound on skeleton and forms shaped framework coil 5 to be tested through heat bonding, gets out shaped framework coil cohesive force test fixture as above;
Step 2: be enclosed within mandrel 6 by shaped framework coil 5, first puts in the installing hole of the first cantilever lever 3 and screws the first lock-screw 3, and then mobile second cantilever lever 8 that adjusts makes mandrel 6 penetrate in its installing hole and screws the second lock-screw 7;
Step 3: in the tangential direction of the outermost layer coil of shaped framework coil 5, load 4 is hung on the self-binding enamel wire of shaped framework coil 5 termination, it is stepped up the weight of load 4, until the self-binding enamel wire of hanging load 4 is just peeled off with shaped framework coil 5, now the weight of load 4 is the bonding force value of shaped framework coil 5 outermost layer coil.
The present invention has the advantage that and beneficial effect: self-binding enamel wire is wound on skeleton and puts the enterprising line circle cohesive force test of test fixture in the present invention through the shaped framework coil of heat bonding, heating-up temperature in thermal bonding technology parameter and heat time heating time can be adjusted by coil cohesive force test result, so that shaped framework coil cohesive force value is quantified and controls. I is had tens kinds of type products and is used the coil cohesive force test fixture in the present invention and method at present, shaped framework coil cohesive force value is not only made to obtain effective control, and the adjustment of shaped framework coil performance to its insulating properties without any harmful effect, thus ensure that product quality, it was demonstrated that respond well.
Accompanying drawing explanation
The shaped framework coil cohesive force test fixture that Fig. 1 is the present invention constitutes schematic diagram.
Wherein, 1-guiderail base, 2-the first cantilever lever, 3-the first lock-screw, 4-load, 5-shaped framework coil, 6-mandrel, 7-the second lock-screw, 8-the second cantilever lever.
Detailed description of the invention
Below in conjunction with Figure of description, the present invention is elaborated.
Referring to Fig. 1, a kind of shaped framework coil cohesive force test fixture, it is made up of guiderail base the 1, first cantilever lever the 2, first lock-screw 3, load 4, shaped framework coil 5, mandrel the 6, second lock-screw 7 and the second cantilever lever 8; Guiderail base 1 is the base plate with guide-track groove; First cantilever lever 2 and the second cantilever lever 8 are placed in parallel in the guide-track groove of guiderail base 1, and may move the spacing of adjustment, one end of first cantilever lever 2 and the second cantilever lever 8 is equipped with the installing hole that can place mandrel 6, and on installing hole, it is respectively equipped with the first lock-screw 3 and the second lock-screw 7 of fixed central spindle 6, mandrel 6 is that two ends match with the installing hole of the first cantilever lever 3 and the second cantilever lever 8 respectively, the middle axle matched with shaped framework coil 5 endoporus, mandrel 6 can flexible rotating between shaped framework coil 5 endoporus. Described mandrel 6 is that two ends match with the installing hole of the first cantilever lever 3 and the second cantilever lever 8 respectively, and the middle axle matched with shaped framework coil 5 endoporus, mandrel 6 can flexible rotating between shaped framework coil 5 endoporus.
A kind of shaped framework coil cohesive force method of testing, specifically comprises the following steps that
Step 1: self-binding enamel wire is wound on skeleton and forms shaped framework coil 5 to be tested through heat bonding, gets out shaped framework coil cohesive force test fixture as above;
Step 2: be enclosed within mandrel 6 by shaped framework coil 5, first puts in the installing hole of the first cantilever lever 3 and screws the first lock-screw 3, and then mobile second cantilever lever 8 that adjusts makes mandrel 6 penetrate in its installing hole and screws the second lock-screw 7;
Step 3: in the tangential direction of the outermost layer coil of shaped framework coil 5, load 4 is hung on the self-binding enamel wire of shaped framework coil 5 termination, is stepped up the weight of load 4, it is desirable to the applying mode of load 4 is for handling with care, it is to avoid any additional impact; Apply the weight of load 4 from 5 grams, increase weight every time and be 5-10 gram, the interval that twice increases load 4 is not less than the 20-30 second, until the self-binding enamel wire of hanging load 4 is just peeled off with shaped framework coil 5, now the weight of load 4 is the bonding force value of shaped framework coil 5 outermost layer coil.

Claims (6)

1. a shaped framework coil cohesive force test fixture, it is characterised in that: described test fixture is made up of guiderail base (1), the first cantilever lever (2), the first lock-screw (3), load (4), shaped framework coil (5), mandrel (6), the second lock-screw (7) and the second cantilever lever (8); Guiderail base (1) is the base plate with guide-track groove; First cantilever lever (2) and the second cantilever lever (8) are placed in parallel in the guide-track groove of guiderail base (1), and may move the spacing of adjustment, one end of first cantilever lever (2) and the second cantilever lever (8) is equipped with the installing hole that can place mandrel (6), and is respectively equipped with the first lock-screw (3) and second lock-screw (7) of fixed central spindle (6) on installing hole.
2. shaped framework coil cohesive force test fixture as claimed in claim 1, it is characterized in that: described mandrel (6) is that two ends match with the installing hole of the first cantilever lever (3) and the second cantilever lever (8) respectively, the middle axle matched with shaped framework coil (5) endoporus, mandrel (6) can flexible rotating between shaped framework coil (5) endoporus.
3. a shaped framework coil cohesive force method of testing, it is characterised in that:
Step 1: self-binding enamel wire is wound on skeleton and forms shaped framework coil (5) to be tested through heat bonding, gets out shaped framework coil cohesive force test fixture as claimed in claim 1;
Step 2: shaped framework coil (5) is enclosed within mandrel (6), first putting in the installing hole of the first cantilever lever (3) and screw the first lock-screw (3), then mobile the second cantilever lever (8) that adjusts makes mandrel (6) penetrate in its installing hole and screw the second lock-screw (7);
Step 3: in the tangential direction of the outermost layer coil of shaped framework coil (5), load (4) is hung on the self-binding enamel wire of shaped framework coil (5) termination, it is stepped up the weight of load (4), until the self-binding enamel wire of hanging load (4) is just peeled off with shaped framework coil (5), now the weight of load (4) is the bonding force value of shaped framework coil (5) outermost layer coil.
4. a kind of shaped framework coil cohesive force method of testing as claimed in claim 3, it is characterised in that: apply the weight of load (4) from 5 grams, increase weight every time and be 5-10 gram.
5. a kind of shaped framework coil cohesive force method of testing as claimed in claim 3, it is characterised in that: the interval that twice increases load (4) is not less than the 20-30 second.
6. a kind of shaped framework coil cohesive force method of testing as claimed in claim 3, it is characterised in that: the applying mode of load (4) should be handles with care, it is to avoid any additional impact; Avoid load (4) to swing, rotate.
CN201410649446.7A 2014-11-14 2014-11-14 A kind of shaped framework coil cohesive force test fixture and method Active CN105651687B (en)

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Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107505262A (en) * 2017-09-30 2017-12-22 中国工程物理研究院电子工程研究所 One kind is used for exoskeletal self-binding enamel wire cohesive force test fixture and method
CN109632635A (en) * 2019-02-28 2019-04-16 常州工学院 A kind of bone-free coil bonding force automatic testing equipment
CN109632516A (en) * 2019-01-07 2019-04-16 常州工学院 A kind of bone-free coil mechanics test device
CN110879172A (en) * 2019-08-14 2020-03-13 河南工程学院 Suspensible test method for knitted portrait and landscape artistic calligraphy and painting product
CN112577894A (en) * 2020-12-08 2021-03-30 铜陵精达里亚特种漆包线有限公司 Enameled wire impregnating varnish adhesion testing device and testing method
CN114034637A (en) * 2022-01-10 2022-02-11 中国空气动力研究与发展中心低速空气动力研究所 Device and method for in-situ measurement of icing adhesion

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2372093A (en) * 1942-12-03 1945-03-20 Westinghouse Electric & Mfg Co Apparatus for testing enameled wire
US5374808A (en) * 1993-06-23 1994-12-20 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Method and device for determining bond separation strength using induction heating
CN101113948A (en) * 2006-07-25 2008-01-30 三得利株式会社 Adhesion inspection apparatus and adhesion inspection method using the same
CN101216413A (en) * 2007-12-28 2008-07-09 保定天威集团有限公司 Heat bonding enamelling wire high-temperature bond strength experimental method and device
CN101724339A (en) * 2008-10-22 2010-06-09 上海川叶电子科技有限公司 Heat resistant alcohol-soluble self-bonding paint used for self-bonding insulated winding wire and manufacturing method thereof
CN201560012U (en) * 2009-11-12 2010-08-25 芜湖国睿兆伏电子股份有限公司 Fixing tool for enameled wires
CN201844966U (en) * 2010-11-02 2011-05-25 浙江师范大学 Magnetorheological fluid press shearing yield strength test device
CN102323208A (en) * 2011-08-25 2012-01-18 江苏宝杰隆电磁线有限公司 Method for testing adhesion stress of self-adhesive enameled lenticular wire
CN102866109A (en) * 2012-09-29 2013-01-09 珠海松田电工有限公司 Adhesive force test method for ultra-miniature self-adhesive enameled wire

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2372093A (en) * 1942-12-03 1945-03-20 Westinghouse Electric & Mfg Co Apparatus for testing enameled wire
US5374808A (en) * 1993-06-23 1994-12-20 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Method and device for determining bond separation strength using induction heating
CN101113948A (en) * 2006-07-25 2008-01-30 三得利株式会社 Adhesion inspection apparatus and adhesion inspection method using the same
CN101216413A (en) * 2007-12-28 2008-07-09 保定天威集团有限公司 Heat bonding enamelling wire high-temperature bond strength experimental method and device
CN101724339A (en) * 2008-10-22 2010-06-09 上海川叶电子科技有限公司 Heat resistant alcohol-soluble self-bonding paint used for self-bonding insulated winding wire and manufacturing method thereof
CN201560012U (en) * 2009-11-12 2010-08-25 芜湖国睿兆伏电子股份有限公司 Fixing tool for enameled wires
CN201844966U (en) * 2010-11-02 2011-05-25 浙江师范大学 Magnetorheological fluid press shearing yield strength test device
CN102323208A (en) * 2011-08-25 2012-01-18 江苏宝杰隆电磁线有限公司 Method for testing adhesion stress of self-adhesive enameled lenticular wire
CN102866109A (en) * 2012-09-29 2013-01-09 珠海松田电工有限公司 Adhesive force test method for ultra-miniature self-adhesive enameled wire

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
W.马丁: "热固性自粘性漆包线", 《电线电缆》 *
中华人民共和国国家质量监督检验检疫总局中国国家标准化管理委员会: "绕组线试验方法-第3部分:机械性能", 《中华人民共和国国家标准GB/T4074.3-2008/IEC60851-3:1997》 *

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107505262A (en) * 2017-09-30 2017-12-22 中国工程物理研究院电子工程研究所 One kind is used for exoskeletal self-binding enamel wire cohesive force test fixture and method
CN107505262B (en) * 2017-09-30 2024-01-12 中国工程物理研究院电子工程研究所 Bonding force testing tool and method for skeleton-free self-adhesive enameled wire
CN109632516A (en) * 2019-01-07 2019-04-16 常州工学院 A kind of bone-free coil mechanics test device
CN109632635A (en) * 2019-02-28 2019-04-16 常州工学院 A kind of bone-free coil bonding force automatic testing equipment
CN109632635B (en) * 2019-02-28 2021-06-22 常州工学院 Boneless coil bonding force automatic testing device
CN110879172A (en) * 2019-08-14 2020-03-13 河南工程学院 Suspensible test method for knitted portrait and landscape artistic calligraphy and painting product
CN112577894A (en) * 2020-12-08 2021-03-30 铜陵精达里亚特种漆包线有限公司 Enameled wire impregnating varnish adhesion testing device and testing method
CN114034637A (en) * 2022-01-10 2022-02-11 中国空气动力研究与发展中心低速空气动力研究所 Device and method for in-situ measurement of icing adhesion

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