CN104786171B - Contact gyromagnet substrate bonds positioning tool and localization method - Google Patents
Contact gyromagnet substrate bonds positioning tool and localization method Download PDFInfo
- Publication number
- CN104786171B CN104786171B CN201510211091.8A CN201510211091A CN104786171B CN 104786171 B CN104786171 B CN 104786171B CN 201510211091 A CN201510211091 A CN 201510211091A CN 104786171 B CN104786171 B CN 104786171B
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- Prior art keywords
- substrate
- frock
- disengagement zone
- gyromagnet
- frock body
- 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.)
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Links
- 239000000758 substrate Substances 0.000 title claims abstract description 118
- 238000000034 method Methods 0.000 title claims description 11
- 230000004807 localization Effects 0.000 title claims description 8
- 239000003292 glue Substances 0.000 claims abstract description 22
- 238000002271 resection Methods 0.000 claims abstract description 8
- 241000237509 Patinopecten sp. Species 0.000 claims description 41
- 235000020637 scallop Nutrition 0.000 claims description 41
- 230000006578 abscission Effects 0.000 claims description 4
- 230000009286 beneficial effect Effects 0.000 abstract description 2
- 230000000694 effects Effects 0.000 description 3
- 238000004519 manufacturing process Methods 0.000 description 2
- 238000009825 accumulation Methods 0.000 description 1
- 230000001154 acute effect Effects 0.000 description 1
- 239000000853 adhesive Substances 0.000 description 1
- 230000001070 adhesive effect Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 230000018109 developmental process Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000003014 reinforcing effect Effects 0.000 description 1
- 230000000007 visual effect Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B25—HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
- B25B—TOOLS OR BENCH DEVICES NOT OTHERWISE PROVIDED FOR, FOR FASTENING, CONNECTING, DISENGAGING OR HOLDING
- B25B11/00—Work holders not covered by any preceding group in the subclass, e.g. magnetic work holders, vacuum work holders
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
- F16B11/00—Connecting constructional elements or machine parts by sticking or pressing them together, e.g. cold pressure welding
- F16B11/006—Connecting constructional elements or machine parts by sticking or pressing them together, e.g. cold pressure welding by gluing
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Gyroscopes (AREA)
Abstract
The present invention relates to microwave device field, positioning tool, including frock body are bonded it discloses a kind of gyromagnet substrate, the frock body is provided with cavity locating surface（1）, substrate disengagement zone（2）, substrate locating surface（3）, glue disengagement zone（4）With frock disengagement zone（5）, the frock body is consistent with the broadside size of waveguide junction；Frock body carries out Partial Resection and forms substrate disengagement zone（2）.The beneficial effects of the invention are as follows：Avoid the position error of gap presence；The positioning of contact, reduces the operating time for finding accurate location, improves operating efficiency；Using larger disengagement zone, it is to avoid influencing each other for frock, glue and substrate, the position error that substrate position moving belt comes is reduced, more convenient operation is rapid.
Description
Technical field
The present invention relates to microwave device field, more particularly to a kind of contact gyromagnet substrate bonds positioning tool and positioning
Method.
Background technology
Gyromagnet substrate is the key componentses that waveguide junction circulator isolator realizes function, and the accuracy of its position is to product
Electrical property has extreme influence.With the development of radar, communication, electronic countermeasure, remote measuring and controlling and accurate guidance unit, to waveguide ring
The performance of row device isolator and production efficiency requirement more and more higher, requirement to gyromagnet substrate technique for sticking also more and more higher.
In existing gyromagnet substrate cemented in place, there are clearance-type positioning bonding frock and two kinds of techniques of microscope positioning bonding.Gap
The shortcoming of formula positioning bonding frock is：In order that positioning tool is put into waveguide junction and gyromagnet substrate is put into positioning tool,
Certain gap need to be reserved during design, the presence in gap is introduced into certain position error；Gap is excessive, and it is fixed to have a strong impact on
Level exactness；The too small then operating difficulties in gap, unnecessary bonded adhesives causes that frock bonds together with substrate, pole when taking out frock
Easily contact substrate, causes substrate to move, and loses locating effect；The rework rate of clearance-type positioning bonding is higher.Microscope positioning is viscous
It is the center that waveguide core knot position and gyromagnet substrate are caught by microscope to connect, and is realized in two by adjusting gyromagnet substrate position
The heart overlaps, and reaches locating effect.But there is the limitation in the visual field due to microscope, and waveguide boundary and gyromagnet substrate seamed edge not
It is easy to identify so that cemented in place efficiency is very low.
The content of the invention
In order to solve the problems of the prior art, positioning tool is bonded the invention provides a kind of contact gyromagnet substrate,
It is used to solve the problems, such as that locating effect is poor in the prior art.
The present invention solves the technical scheme that is used of prior art problem：Design and manufacture a kind of contact gyromagnet substrate
Bond positioning tool, including frock body, it is characterised in that:The frock body is provided with cavity locating surface（1）, substrate abscission zone
Domain（2）, substrate locating surface（3）, glue disengagement zone（4）With frock disengagement zone（5）, the width of the frock body and waveguide junction
Side size is consistent；Frock body carries out Partial Resection and forms substrate disengagement zone（2）With frock disengagement zone（5）.
As a further improvement on the present invention：The frock body central is provided with scallop hole；The scallop hole is divided into diameter
Smaller portions scallop hole and larger diameter portion scallop hole；The smaller-diameter portion scallop hole is substrate locating surface（3）；It is described
Larger diameter portion scallop hole is substrate disengagement zone（2）.
As a further improvement on the present invention：The obverse and reverse of the frock body is respectively equipped with circular counter bore, described
Circular counter bore is glue disengagement zone（4）.
As a further improvement on the present invention：The cavity locating surface（1）It is the outline of the frock body.
As a further improvement on the present invention：The frock body is provided with clear corner structure, and its seamed edge is provided with chamfering.
Localization method is bonded invention also provides a kind of contact gyromagnet substrate, is comprised the following steps：（A）Gyromagnet base
Piece is adhered to cavity（6）On；（B）Frock body is put into cavity（6）It is interior；（C）Remove frock body；The frock body is provided with chamber
Body locating surface（1）, substrate disengagement zone（2）, substrate locating surface（3）, glue disengagement zone（4）With frock disengagement zone（5）, institute
State frock body consistent with the broadside size of waveguide junction；Frock body carries out Partial Resection and forms substrate disengagement zone（2）.
As a further improvement on the present invention：The step（A）In, gyromagnet substrate is adhered to cavity（6）On, move back and forth
Gyromagnet substrate（7）, unnecessary glue is near operating personnel side, and make gyromagnet substrate off-center, it is slightly moved closer to operation
Personnel side.
As a further improvement on the present invention：The step（B）In, make substrate disengagement zone near operating personnel；To work
Dress body edges reinforcing, makes cavity locating surface be everywhere in close contact with cavity；Mobile gyromagnet substrate, adds to gyromagnet substrate edge
Power, makes gyromagnet substrate be in close contact with substrate locating surface；Frock body edges are exerted a force, make frock away from operating personnel side,
Even if gyromagnet substrate departs from frock body, in substrate disengagement zone.
As a further improvement on the present invention：The frock body central is provided with scallop hole；The scallop hole is divided into diameter
Smaller portions scallop hole and larger diameter portion scallop hole；The smaller-diameter portion scallop hole is substrate locating surface（3）；It is described
Larger diameter portion scallop hole is substrate disengagement zone（2）；The obverse and reverse of the frock body is respectively equipped with circular counter bore,
The circular counter bore is glue disengagement zone（4）.
The beneficial effects of the invention are as follows：Avoid the position error of gap presence；The positioning of contact, reduces searching accurate
The operating time of true position, improve operating efficiency；Using larger disengagement zone, it is to avoid frock, glue and substrate it is mutual
Influence, reduces the position error that substrate position moving belt comes, and more convenient operation is rapid.
Brief description of the drawings
Fig. 1 is that contact gyromagnet substrate of the present invention bonds positioning tool structural representation.
Fig. 2 is the positioning schematic diagram that contact gyromagnet substrate of the present invention bonds positioning tool.
Specific embodiment
The invention will be further described below in conjunction with the accompanying drawings.
A kind of contact gyromagnet substrate bonds positioning tool, including frock body, it is characterised in that:The frock body sets
There are cavity locating surface 1, substrate disengagement zone 2, substrate locating surface 3, glue disengagement zone 4 and frock disengagement zone 5, the frock
Body is consistent with the broadside size of waveguide junction；Frock body carries out Partial Resection and forms substrate disengagement zone 2 and frock abscission zone
Domain 5.
The frock body central is provided with scallop hole；The scallop hole is divided into smaller-diameter portion scallop hole and is relatively large in diameter
Partial sector hole；The smaller-diameter portion scallop hole is substrate locating surface 3；The larger diameter portion scallop hole is de- for substrate
From region 2.
The obverse and reverse of the frock body is respectively equipped with circular counter bore, and the circular counter bore is glue disengagement zone 4.
The cavity locating surface 1 is the outline of the frock body.
The frock body is provided with clear corner structure, and its seamed edge is provided with chamfering；The frock disengagement zone 5 is frock body
Cut-out is easy to frock to depart from cavity to reserve frock mobile space.
Localization method is bonded invention also provides a kind of contact gyromagnet substrate, is comprised the following steps：（A）Gyromagnet base
Piece is adhered on cavity 6；（B）Frock body is put into cavity 6；（C）Remove frock body；The frock body is provided with cavity to be determined
Plane 1, substrate disengagement zone 2, substrate locating surface 3, glue disengagement zone 4 and frock disengagement zone 5, the frock body and ripple
The broadside size for leading knot is consistent；Frock body carries out Partial Resection and forms substrate disengagement zone 2.
The step（A）In, gyromagnet substrate is adhered on cavity 6, moves back and forth gyromagnet substrate 7, is in unnecessary glue
Near operating personnel side, and make gyromagnet substrate off-center, be slightly moved closer to operating personnel side.
The step（B）In, make substrate disengagement zone near operating personnel；Frock body edges are reinforced, makes chamber everywhere
Body locating surface is in close contact with cavity；Mobile gyromagnet substrate, reinforces to gyromagnet substrate edge, makes gyromagnet substrate and substrate locating surface
It is in close contact；Frock body edges are exerted a force, makes frock away from operating personnel side, even if gyromagnet substrate takes off with frock body
From in substrate disengagement zone.
The frock body central is provided with scallop hole；The scallop hole is divided into smaller-diameter portion scallop hole and is relatively large in diameter
Partial sector hole；The smaller-diameter portion scallop hole is substrate locating surface 3；The larger diameter portion scallop hole is de- for substrate
From region 2；The obverse and reverse of the frock body is respectively equipped with circular counter bore, and the circular counter bore is glue disengagement zone 4.
In one embodiment, a kind of contact gyromagnet substrate bonds positioning tool includes cavity locating surface 1, substrate abscission zone
Domain 2, substrate locating surface 3, glue disengagement zone 4 and frock disengagement zone 5；The width of the gyromagnet substrate positioning tool and waveguide junction
Side size is consistent, while be also made up of three 120 ° of symmetric arms, to enable positioning tool to free in and out waveguide junction, to positioning tool
Partial Resection is carried out, substrate disengagement zone has been formed, has made positioning tool wherein four sides that positioning is contacted with cavity, while being easy to positioning
Frock is separated with cavity；Positioning tool center is a scallop hole, and wherein smaller-diameter portion is consistent with gyromagnet sizes of substrate, makes base
Piece can contact positioning with positioning tool, and wherein larger diameter portion is substrate disengagement zone, be easy to substrate enter position location with
Depart from positioning tool；The circular counter bore of positioning tool tow sides is glue disengagement zone, it is to avoid the glue of accumulation and positioning work
Attaching is touched；Positioning tool is processed using clear angle, it is to avoid frock interior angle is interfered with cavity seamed edge；Seamed edge uses chamfered, it is to avoid
Operating personnel are scratched by acute angle.
When carrying out positioning action, operated according to the following steps：Make a waveguide junction wherein arm towards operating personnel；Gyromagnet base
Piece is adhered on cavity 6, moves back and forth gyromagnet substrate 7, unnecessary glue is near operating personnel side, and make gyromagnet substrate
It is off-center, it is slightly moved closer to operating personnel side；Be put into contact gyromagnet substrate positioning tool 8, scallop hole be relatively large in diameter one
Side is towards operating personnel；Positioning tool edge is reinforced with hand, cavity locating surface everywhere is in close contact with cavity；With tweezers or
Other appropriate instrument movement gyromagnet substrates, reinforce to gyromagnet substrate edge, gyromagnet substrate is in close contact with substrate locating surface；First
The power to gyromagnet substrate is removed, then removes the power to positioning tool, stand 2 ~ 3min；Positioning tool edge is exerted a force, makes frock
Away from operating personnel side, even if gyromagnet substrate departs from positioning tool, in substrate disengagement zone；With tweezers or other are appropriate
Instrument removes positioning tool.
Above content is to combine specific preferred embodiment further description made for the present invention, it is impossible to assert
Specific implementation of the invention is confined to these explanations.For general technical staff of the technical field of the invention,
On the premise of not departing from present inventive concept, some simple deduction or replace can also be made, should be all considered as belonging to of the invention
Protection domain.
Claims (9)
1. a kind of contact gyromagnet substrate bonds positioning tool, including frock body, it is characterised in that:The frock body is provided with
Cavity locating surface（1）, substrate disengagement zone（2）, substrate locating surface（3）, glue disengagement zone（4）With frock disengagement zone（5）,
The frock body is consistent with the broadside size of waveguide junction；Frock body carries out Partial Resection and forms substrate disengagement zone（2）With
And frock disengagement zone（5）；The frock body central is provided with scallop hole；The scallop hole is divided into smaller-diameter portion scallop hole
With larger diameter portion scallop hole；The smaller-diameter portion scallop hole is substrate locating surface（3）；The larger diameter portion fan
Shape hole is substrate disengagement zone（2）.
2. contact gyromagnet substrate according to claim 1 bonds positioning tool, it is characterised in that：The frock body
Obverse and reverse is respectively equipped with circular counter bore, and the circular counter bore is glue disengagement zone（4）.
3. contact gyromagnet substrate according to claim 1 bonds positioning tool, it is characterised in that:The cavity positioning
Face（1）It is the outline of the frock body.
4. contact gyromagnet substrate according to claim 1 bonds positioning tool, it is characterised in that：The frock body sets
There is clear corner structure, its seamed edge is provided with chamfering.
5. contact gyromagnet substrate according to claim 1 bonds positioning tool, it is characterised in that：The frock abscission zone
Domain（5）Be the cut-out of frock body reserving frock mobile space, be easy to frock to depart from cavity.
6. a kind of contact gyromagnet substrate bonds localization method, it is characterised in that：Comprise the following steps：（A）Gyromagnet substrate is bonded
In cavity（6）On；（B）Frock body is put into cavity（6）It is interior；（C）Remove frock body；The frock body is provided with cavity positioning
Face（1）, substrate disengagement zone（2）, substrate locating surface（3）, glue disengagement zone（4）With frock disengagement zone（5）, the frock
Body is consistent with the broadside size of waveguide junction；Frock body carries out Partial Resection and forms substrate disengagement zone（2）；The frock sheet
Body center is provided with scallop hole；The scallop hole is divided into smaller-diameter portion scallop hole and larger diameter portion scallop hole；It is described straight
Footpath smaller portions scallop hole is substrate locating surface（3）；The larger diameter portion scallop hole is substrate disengagement zone（2）.
7. contact gyromagnet substrate according to claim 6 bonds localization method, it is characterised in that：The step（A）In,
Gyromagnet substrate is adhered to cavity（6）On, move back and forth gyromagnet substrate（7）, unnecessary glue is near operating personnel side, and
Make gyromagnet substrate off-center, be slightly moved closer to operating personnel side.
8. contact gyromagnet substrate according to claim 6 bonds localization method, it is characterised in that：The step（B）In,
Make substrate disengagement zone near operating personnel；Frock body edges are reinforced, cavity locating surface everywhere is in close contact with cavity；
Mobile gyromagnet substrate, reinforces to gyromagnet substrate edge, gyromagnet substrate is in close contact with substrate locating surface；To frock body edges
Force, makes frock away from operating personnel side, even if gyromagnet substrate departs from frock body, in substrate disengagement zone.
9. contact gyromagnet substrate according to claim 6 bonds localization method, it is characterised in that：In the frock body
The heart is provided with scallop hole；The scallop hole is divided into smaller-diameter portion scallop hole and larger diameter portion scallop hole；The diameter compared with
Fraction scallop hole is substrate locating surface（3）；The larger diameter portion scallop hole is substrate disengagement zone（2）；The frock
The obverse and reverse of body is respectively equipped with circular counter bore, and the circular counter bore is glue disengagement zone（4）.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510211091.8A CN104786171B (en) | 2015-04-29 | 2015-04-29 | Contact gyromagnet substrate bonds positioning tool and localization method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510211091.8A CN104786171B (en) | 2015-04-29 | 2015-04-29 | Contact gyromagnet substrate bonds positioning tool and localization method |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN104786171A CN104786171A (en) | 2015-07-22 |
| CN104786171B true CN104786171B (en) | 2017-06-09 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201510211091.8A Active CN104786171B (en) | 2015-04-29 | 2015-04-29 | Contact gyromagnet substrate bonds positioning tool and localization method |
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Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN204658249U (en) * | 2015-04-29 | 2015-09-23 | 西南应用磁学研究所 | Contact gyromagnet substrate bonding positioning tool |
Family Cites Families (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH10294607A (en) * | 1997-04-18 | 1998-11-04 | Fuji Elelctrochem Co Ltd | Jig for soldering and mounting isolator, production of isolator mount using the same and isolator mount produced by using the same |
| CN100563921C (en) * | 2007-05-22 | 2009-12-02 | 佛山普立华科技有限公司 | Fixing device of localization tool |
| CN201112534Y (en) * | 2007-09-18 | 2008-09-10 | 北京华大智宝电子系统有限公司 | High power annular equipment |
| FR2926949B1 (en) * | 2008-01-24 | 2010-04-02 | Chelton Telecom & Microwave | ELECTRONIC COMPONENT WITH SURFACE MOUNTING WITH ELECTRICAL CONNECTION POSITIONED WITH PRECISION. |
| CN201336345Y (en) * | 2009-01-08 | 2009-10-28 | 世达普(苏州)通信设备有限公司 | Isolator for junction circulator |
| CN101894998B (en) * | 2010-07-16 | 2014-01-22 | 中国兵器工业第二0六研究所 | Ultra-thin three-port waveguide junction circulator |
| CN102629706A (en) * | 2012-04-28 | 2012-08-08 | 成都泰格微波技术股份有限公司 | Circulator magnetic rotation piece positioning tooling |
| CN203192926U (en) * | 2013-04-25 | 2013-09-11 | 苏州工业园区凯艺精密科技有限公司 | Isolator assembly fixture |
| CN103490130B (en) * | 2013-08-30 | 2016-03-02 | 南京信息职业技术学院 | The manufacture method of a kind of waveguide junction circulator and match block thereof |
| CN203918833U (en) * | 2014-05-27 | 2014-11-05 | 安徽大地熊新材料股份有限公司 | A kind of isolator ndfeb magnet bonding jig |
-
2015
- 2015-04-29 CN CN201510211091.8A patent/CN104786171B/en active Active
Patent Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN204658249U (en) * | 2015-04-29 | 2015-09-23 | 西南应用磁学研究所 | Contact gyromagnet substrate bonding positioning tool |
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| CN104786171A (en) | 2015-07-22 |
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