CN106925816A - A kind of novel supporting plate nut drill jig - Google Patents
A kind of novel supporting plate nut drill jig Download PDFInfo
- Publication number
- CN106925816A CN106925816A CN201710285559.7A CN201710285559A CN106925816A CN 106925816 A CN106925816 A CN 106925816A CN 201710285559 A CN201710285559 A CN 201710285559A CN 106925816 A CN106925816 A CN 106925816A
- Authority
- CN
- China
- Prior art keywords
- alignment pin
- hole alignment
- drill jig
- bushing plate
- rivet hole
- 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.)
- Granted
Links
- 238000005553 drilling Methods 0.000 claims abstract description 5
- 238000003466 welding Methods 0.000 claims abstract description 4
- 238000000034 method Methods 0.000 claims abstract description 3
- 229910000831 Steel Inorganic materials 0.000 claims description 3
- 239000000463 material Substances 0.000 claims description 3
- 239000010959 steel Substances 0.000 claims description 3
- 230000003746 surface roughness Effects 0.000 claims description 3
- 230000008602 contraction Effects 0.000 claims description 2
- 230000003647 oxidation Effects 0.000 claims 1
- 238000007254 oxidation reaction Methods 0.000 claims 1
- 238000004519 manufacturing process Methods 0.000 abstract description 6
- 241001074085 Scophthalmus aquosus Species 0.000 description 2
- 238000010301 surface-oxidation reaction Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 238000010791 quenching Methods 0.000 description 1
- 230000000171 quenching effect Effects 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23B—TURNING; BORING
- B23B47/00—Constructional features of components specially designed for boring or drilling machines; Accessories therefor
- B23B47/28—Drill jigs for workpieces
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Drilling And Boring (AREA)
- Insertion Pins And Rivets (AREA)
Abstract
A kind of novel supporting plate nut drill jig, belongs to aircraft assembling manufacturing technical field, and two drill jig holes are set on the bushing plate on novel supporting plate nut drill jig, drills two rivet holes in order respectively.Bolt hole alignment pin is used to realize the positioning of bolt hole, for small―gap suture coordinates between bolt hole alignment pin and the bolt hole of plate nut, is connected by jump ring between bolt hole alignment pin and bushing plate.Rivet hole alignment pin is used to realize first positioning of rivet hole, for small―gap suture coordinates between rivet hole alignment pin and the rivet hole of plate nut；For gap coordinates between rivet hole alignment pin and bushing plate, it is ensured that rivet hole alignment pin can be rotated freely.Spring is arranged between rivet hole alignment pin and bushing plate.Handle is connected with bushing plate using welding method, increases holding dynamics.Simple structure of the present invention, with low cost, the plate nut rivet hole that disclosure satisfy that in small space is drilled, it is ensured that borehole accuracy；The positive and negative use of traditional drill jig is changed into rotation to use, drilling efficiency is improved.
Description
Technical field
The invention belongs to aircraft assembling manufacturing technical field, it is related to a kind of novel supporting plate nut drill jig.
Background technology
With flourishing for China Aviation industry, aircraft assembling manufacturing industry, especially civil aircraft and general-purpose aircraft are filled
Direction with manufacture just progressively towards higher precision, higher efficiency strides forward, and this requires the work used in assembling manufacturing field
Tool, more should be easy to operate on the premise of machining accuracy is met, and improves throughput rate.
Plate nut drill jig is aircraft assembling manufacturing field frequency of usage self-control specific purpose tool higher, traditional supporting plate spiral shell
Female drill jig is influenceed (bushing plate is square, handle and bushing plate into 180 degree) by self structure form, it is impossible to complete some narrow and small
The plate nut rivet hole in space is drilled.And drill jig needs positive and negative use to drill two rivet holes, and it is not convenient to use, brill
Hole efficiency is affected.
The content of the invention
For the problem that prior art is present, the present invention provides a kind of new plate nut drill jig.
The technical scheme is that：
A kind of novel supporting plate nut drill jig, including bushing plate 1, bolt hole alignment pin 2, jump ring 3, rivet hole alignment pin 4, bullet
Spring 5, handle 6.
Described bushing plate 1 is cylinder, and the profile of cylinder is used to reduce area occupied, realizes boring in small space
Hole；Two drill jig holes are set on bushing plate 1, are used to drill two rivet holes respectively in order.Described bushing plate 1 is for material
The steel after quenching and surface oxidation treatment is carried out, thickness is 5mm, and the following table surface roughness of bushing plate 1 is 1.6, it is to avoid with aircraft
Cut is produced during contact.
Described bolt hole alignment pin 2 is located on bushing plate 1, the positioning for realizing bolt hole, bolt hole alignment pin 2
Size determines that the two should be small―gap suture cooperation according to the bolt hole of plate nut.Described bolt hole alignment pin 2 and bushing plate 1
Between be gap coordinate, the two is connected by jump ring 3, it is ensured that bolt hole alignment pin can be rotated.
Described rivet hole alignment pin 4 is located on bushing plate 1, and for realizing first positioning of rivet hole, rivet hole is fixed
The size of position pin 4 determines that the two should be small―gap suture cooperation according to the rivet hole of plate nut；Rivet hole alignment pin 4 and bushing plate
Between be gap coordinate, need to ensure that rivet hole alignment pin can be rotated freely, connected by the flattening and bushing plate 1 at non-working surface end
Connect.
Described spring 5 is arranged between rivet hole alignment pin 4 and bushing plate 1, the receipts for realizing rivet hole alignment pin 4
Contracting.
Described handle 6 is used to realize the holding function of drill jig, is connected using welding or in the form of being spirally connected with bushing plate 1,
Handle 6 determines according to working space with the angle of bushing plate 1, usually 35 degree, is changed into angle handle, energy from traditional staight shank
Enough increase the applicability of instrument；Can increase on handle and rise as high as the banks or annular knurl is to increase holding dynamics.
Beneficial effects of the present invention are：It is simple structure of the present invention, with low cost, disclosure satisfy that the supporting plate spiral shell in small space
Female rivet hole is drilled, it is ensured that borehole accuracy；And the positive and negative use of traditional drill jig is changed into rotation to use, drilling effect is improved
Rate.Easy to operate using the present invention in actual test, instrument applicability, borehole accuracy have all strengthened, and drilling efficiency is improved
30%.
Brief description of the drawings
Fig. 1 is novel supporting plate nut drill jig three-dimensional structure diagram；
Fig. 2 is novel supporting plate nut drill jig front view；
Fig. 3 is novel supporting plate nut drill jig side view；
Fig. 4 is novel supporting plate nut drill jig top view；
In figure：1 bushing plate；2 bolt hole alignment pins；3 jump rings；4 rivet hole alignment pins；5 springs；6 handles；7 drill jig hole A；8
Drill jig hole B.
Specific embodiment
Below in conjunction with specific embodiment, the invention will be further described.
A kind of novel supporting plate nut drill jig, including the bushing plate 1 of cylinder, bolt hole alignment pin 2, jump ring 3, rivet hole are fixed
Position pin 4, spring 5, handle 6.Two drill jig hole A7 and drill jig hole B8 are set on bushing plate 1, two rivets are drilled in order respectively
Hole, drill jig hole A7 drills first rivet hole, and drill jig hole B8 drills second rivet hole.Bushing plate 1 is material to be quenched
With the steel after surface oxidation treatment, thickness is 5mm, and the following table surface roughness of bushing plate 1 is 1.6.Bolt hole alignment pin 2 is used for real
The positioning of existing bolt hole, the size of bolt hole alignment pin 2 determines that the two coordinates for small―gap suture according to the bolt hole of plate nut,
For gap coordinates between bolt hole alignment pin 2 and bushing plate 1, the two is connected by jump ring 3, and bolt hole alignment pin can be rotated.
Rivet hole alignment pin 4 is used to realize first positioning of rivet hole, the rivet of the size of rivet hole alignment pin 4 according to plate nut
Hole determines that the two should be small―gap suture cooperation；For gap coordinates between rivet hole alignment pin 4 and bushing plate, need to ensure that rivet hole is determined
Position pin can be rotated freely, be connected with bushing plate 1 by the flattening at non-working surface end.Spring 5 is arranged on the He of rivet hole alignment pin 4
Between bushing plate 1, the contraction for realizing rivet hole alignment pin 4.Handle 6 is connected with bushing plate 1 using welding method, handle 6
It is 35 degree with the angle between bushing plate 1, increase holding dynamics of rising as high as the banks is increased on handle.
During using present invention drilling, bolt hole alignment pin 2 is inserted at aircraft bolt hole first, it is ensured that bushing plate 1 and brill
Hole surface is developed.Now rivet hole alignment pin 4 is pressed into bushing plate 1 by aircraft, is not worked.Using drill jig on bushing plate 1
Hole A7 drills first rivet hole, using handle 6, by plate nut drill jig around bolt hole alignment pin 2, close to boring surface rotation
Turn, make on first rivet hole that rivet hole alignment pin drills before being stretched into the presence of spring 5, finally using on bushing plate
Drill jig hole B8 drills second rivet hole.
Claims (3)
1. a kind of novel supporting plate nut drill jig, it is characterised in that the novel supporting plate nut drill jig includes bushing plate (1), bolt hole
Alignment pin (2), jump ring (3), rivet hole alignment pin (4), spring (5), handle (6)；
Described bushing plate (1) is cylinder, can reduce area occupied, realizes drilling in small space；Bushing plate sets on (1)
Two drill jig holes are put, is used to drill two rivet holes respectively in order；Described bushing plate (1) is to be quenched and table for material
Steel after the oxidation processes of face, thickness is (5) mm, and the following table surface roughness of bushing plate (1) is 1.6, it is to avoid produced when being contacted with aircraft
Raw cut；
Described bolt hole alignment pin (2) on bushing plate (1), the positioning for realizing bolt hole, bolt hole alignment pin (2)
Size according to the bolt hole of plate nut determine, the two be small―gap suture coordinate；Described bolt hole alignment pin (2) and bushing plate
(1) for gap coordinates between, the two is connected by jump ring (3), it is ensured that bolt hole alignment pin can be rotated；
On bushing plate (1), for realizing first positioning of rivet hole, rivet hole is fixed for described rivet hole alignment pin (4)
The size of position pin (4) determines that the two coordinates for small―gap suture according to the rivet hole of plate nut；Rivet hole alignment pin (4) and drill jig
For gap coordinates between plate, it is ensured that rivet hole alignment pin can be rotated freely, by flattening and the bushing plate (1) at non-working surface end
Connection；
Described spring (5) between rivet hole alignment pin (4) and bushing plate (1), for realizing rivet hole alignment pin (4)
Contraction；Described handle (6) is connected with bushing plate (1) for realizing the holding function of drill jig using welding or in the form of being spirally connected
Connect, handle (6) determines with the angle of bushing plate (1) according to working space, band angle handle, by increasing capacitance it is possible to increase the applicability of instrument.
2. a kind of novel supporting plate nut drill jig according to claim 1, it is characterised in that described handle (6) and drill jig
The angle of plate (1) is 35 degree.
3. a kind of novel supporting plate nut drill jig according to claim 1 and 2, it is characterised in that handle can also increase on (6)
Plus rise as high as the banks or annular knurl, for increasing holding dynamics.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710285559.7A CN106925816B (en) | 2017-04-27 | 2017-04-27 | A kind of plate nut drill jig |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710285559.7A CN106925816B (en) | 2017-04-27 | 2017-04-27 | A kind of plate nut drill jig |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106925816A true CN106925816A (en) | 2017-07-07 |
| CN106925816B CN106925816B (en) | 2019-09-20 |
Family
ID=59438492
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710285559.7A Expired - Fee Related CN106925816B (en) | 2017-04-27 | 2017-04-27 | A kind of plate nut drill jig |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106925816B (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108994349A (en) * | 2018-09-12 | 2018-12-14 | 中航成飞民用飞机有限责任公司 | Plate nut rivet hole drill jig |
| CN109967686A (en) * | 2017-12-28 | 2019-07-05 | 上海众大汽车配件有限公司 | A kind of riveting die auxiliary device and riveting die |
| CN111841942A (en) * | 2020-06-24 | 2020-10-30 | 贵州新安航空机械有限责任公司 | Paint spraying tool for rivet hole |
| CN112404516A (en) * | 2020-12-07 | 2021-02-26 | 北京星航机电装备有限公司 | Mounting tool for supporting plate nut |
Citations (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6220796B1 (en) * | 1999-07-11 | 2001-04-24 | Vance Chiang | Multipurpose drilling jig |
| CN201493513U (en) * | 2009-09-14 | 2010-06-02 | 哈尔滨飞机工业集团有限责任公司 | Plate nut rivet hole drilling tool |
| CN201519784U (en) * | 2009-06-30 | 2010-07-07 | 成都飞机工业（集团）有限责任公司 | High-efficient handle drilling machine |
| JP4731549B2 (en) * | 2004-03-11 | 2011-07-27 | シンセス ゲーエムベーハー | Reset tool |
| CN202317161U (en) * | 2011-11-18 | 2012-07-11 | 哈尔滨飞机工业集团有限责任公司 | Adjustable nut rivet drilling guide tool |
| CN202984743U (en) * | 2012-11-29 | 2013-06-12 | 哈尔滨飞机工业集团有限责任公司 | Perforating tool for helicopter front movable fairing supporting plate nut |
| CN203245418U (en) * | 2013-05-27 | 2013-10-23 | 宁波市镇海金雳机械制造有限公司 | Connecting rod tap drill jig tool |
| CN103386600A (en) * | 2013-07-22 | 2013-11-13 | 山东太古飞机工程有限公司 | Boeing aircraft airtight support plate nut installation process device and process |
| CN204657539U (en) * | 2015-03-26 | 2015-09-23 | 沈阳飞机工业（集团）有限公司 | Plate nut hole guiding device |
| CN205437255U (en) * | 2015-12-22 | 2016-08-10 | 中国航空工业集团公司济南特种结构研究所 | Carriage nut jig |
| CN206882853U (en) * | 2017-04-27 | 2018-01-16 | 沈阳飞机工业（集团）有限公司 | A kind of novel supporting plate nut drill jig |
-
2017
- 2017-04-27 CN CN201710285559.7A patent/CN106925816B/en not_active Expired - Fee Related
Patent Citations (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6220796B1 (en) * | 1999-07-11 | 2001-04-24 | Vance Chiang | Multipurpose drilling jig |
| JP4731549B2 (en) * | 2004-03-11 | 2011-07-27 | シンセス ゲーエムベーハー | Reset tool |
| CN201519784U (en) * | 2009-06-30 | 2010-07-07 | 成都飞机工业（集团）有限责任公司 | High-efficient handle drilling machine |
| CN201493513U (en) * | 2009-09-14 | 2010-06-02 | 哈尔滨飞机工业集团有限责任公司 | Plate nut rivet hole drilling tool |
| CN202317161U (en) * | 2011-11-18 | 2012-07-11 | 哈尔滨飞机工业集团有限责任公司 | Adjustable nut rivet drilling guide tool |
| CN202984743U (en) * | 2012-11-29 | 2013-06-12 | 哈尔滨飞机工业集团有限责任公司 | Perforating tool for helicopter front movable fairing supporting plate nut |
| CN203245418U (en) * | 2013-05-27 | 2013-10-23 | 宁波市镇海金雳机械制造有限公司 | Connecting rod tap drill jig tool |
| CN103386600A (en) * | 2013-07-22 | 2013-11-13 | 山东太古飞机工程有限公司 | Boeing aircraft airtight support plate nut installation process device and process |
| CN204657539U (en) * | 2015-03-26 | 2015-09-23 | 沈阳飞机工业（集团）有限公司 | Plate nut hole guiding device |
| CN205437255U (en) * | 2015-12-22 | 2016-08-10 | 中国航空工业集团公司济南特种结构研究所 | Carriage nut jig |
| CN206882853U (en) * | 2017-04-27 | 2018-01-16 | 沈阳飞机工业（集团）有限公司 | A kind of novel supporting plate nut drill jig |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109967686A (en) * | 2017-12-28 | 2019-07-05 | 上海众大汽车配件有限公司 | A kind of riveting die auxiliary device and riveting die |
| CN108994349A (en) * | 2018-09-12 | 2018-12-14 | 中航成飞民用飞机有限责任公司 | Plate nut rivet hole drill jig |
| CN108994349B (en) * | 2018-09-12 | 2020-06-19 | 中航成飞民用飞机有限责任公司 | Drilling jig for rivet hole of supporting plate nut |
| CN111841942A (en) * | 2020-06-24 | 2020-10-30 | 贵州新安航空机械有限责任公司 | Paint spraying tool for rivet hole |
| CN112404516A (en) * | 2020-12-07 | 2021-02-26 | 北京星航机电装备有限公司 | Mounting tool for supporting plate nut |
Also Published As
| Publication number | Publication date |
|---|---|
| CN106925816B (en) | 2019-09-20 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN106925816A (en) | A kind of novel supporting plate nut drill jig | |
| CN206882853U (en) | A kind of novel supporting plate nut drill jig | |
| CN201586773U (en) | Drilling cover die | |
| CN205587709U (en) | Drilling machine of hydraulic prop column cap | |
| CN202571412U (en) | Double-end self-centering tungsten steel drill | |
| CN101850436B (en) | Vertical hole-enlarging positioning guided tooling | |
| CN202963553U (en) | Tool for guaranteeing location degree of trolley frame hole | |
| CN203696170U (en) | Built-up jig for machining main body and sleeve of lathe wrench | |
| CN204867551U (en) | Take drill bushing of chip breaking function | |
| CN202539638U (en) | Deep hole drill bit guide sleeve | |
| CN208879765U (en) | Vehicle window aluminium frame inside casing punching tooling | |
| CN201711571U (en) | Vertical expanding positioning guide tool | |
| CN205393622U (en) | Drilling nozzle drilling frock | |
| CN204182983U (en) | The accurate positioning drill jig in rectangular cylinder workpiece five hole | |
| CN203621965U (en) | Tool of drilling machine for machining holes in worm sector | |
| CN202954743U (en) | Down-the-hole drill bit | |
| CN215879994U (en) | Drilling assistor for oil well pin shaft | |
| CN201108944Y (en) | Double-dovetail groove ram head | |
| CN204159943U (en) | For the composite drill of cage guide processing | |
| CN201603902U (en) | Pipeline socket counterbore processing cutter | |
| CN205110506U (en) | Riveting hole drift | |
| CN204565228U (en) | A kind of hard alloy steel tapering drill bit | |
| CN114290026B (en) | Combined part riveting tool and use method thereof | |
| CN202606941U (en) | Alloy blade for drill bit | |
| CN203610737U (en) | Multistage drill bit |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20190920 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |