CN203345206U - Locator used for plane butt joint positions - Google Patents
Locator used for plane butt joint positions Download PDFInfo
- Publication number
- CN203345206U CN203345206U CN2013202238956U CN201320223895U CN203345206U CN 203345206 U CN203345206 U CN 203345206U CN 2013202238956 U CN2013202238956 U CN 2013202238956U CN 201320223895 U CN201320223895 U CN 201320223895U CN 203345206 U CN203345206 U CN 203345206U
- Authority
- CN
- China
- Prior art keywords
- handle
- latch
- lock
- semi
- butt joint
- 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
Links
Images
Abstract
The utility model relates to a locator used for plane butt joint positions in the field of plane assembling. The locator comprises a plug pin (1), a lock seat (2), a cushion block (3) and a handle nut (4). A semi-circular-shaped hollow cavity is further formed in the middle of the lock seat (2). Two lugs screwed tightly with a tool framework extend out of the lower portion of the lock seat (2). The plug pin (1) comprises a handle. A semi-circular-shaped boss matched with the semi-circular-shaped hollow cavity of the lock seat (2) is further arranged under a handheld part of the handle. A threaded head is arranged at the front end of the plug pin (1) and is matched with the handle nut (4). The locator used for the plant butt joint positions improves the performance of technique equipment, improves the quality of products, and improves assembling efficiency.
Description
Technical field
The utility model relates to aircraft docking site registration device in a kind of aircraft assembling field.
Background technology
Aircraft components docking assembling must just can be carried out by frock aircraft docking assembling auxiliary device.Aircraft components docking assembling auxiliary device is to be used for a kind of production tooling of location and clamping part in the aircraft fitting process.Whether accurate assembly quality and the efficiency of assembling that directly has influence on aircraft of design of aircraft components docking assembling auxiliary device.
Generally being used at present the steady arm of parts docking in industry, is mainly that special screw thread docking latch inserts in butt hole, and the handle nut is tightened and completes location from opposite side, difficulty below this form exists when manufacturing and use:
1, screw thread docking pin be substantially all special, special-purpose docking pin, and its modularization, interchangeability are poor, manufacture more time-consuming, require great effort; If lose, need again manufacture.
2, infinite place device is in use sold in screw thread docking, makes that handle bolt and parts can't be confirmed whether to hook, latch is easily along the course play.
3, screw thread docking pin, generally without handle, makes unloading process numerous and diverse.
Therefore, in product trial assembly process, may produce a large amount of reclamation works, fitting work efficiency is low, and assembly quality is not high.
The utility model content
Technical problem to be solved in the utility model is: provide a kind of steady arm for the aircraft docking site, easy to process, modularization and can effectively confirm whether the aircraft docking site connects and put in place.
For solving the problems of the technologies described above, the technical solution of the utility model is: a kind of steady arm for the aircraft docking site, steady arm comprises latch 1, lock 2, cushion block 3, handle nut 4, lock 2 increases semicircular cavities at middle part, 2 ears tightening with the frock skeleton are stretched out in bottom, latch 1 comprises handle, increases the semi-circular boss coordinated with lock 2 semicircular cavities under its Handheld Division, and the threaded head of latch 1 front end coordinates with handle nut 4.
The utility model has the advantages of: after screw thread is docked to pin assembly and changes automatic locking positioning device into, compress more reliably, make the registration device auto lock, solved steady arm in use easily along the problem of course direction play; After latch band handle, solved the inconvenient problem of dismantling.Can adopt normalisation, modularization during fabrication, this registration device can be widely used in the various hole positioning forms of aircraft.In sum, the utility model has improved the performance of production tooling, has also improved the quality of product simultaneously, has improved efficiency of assembling.
The accompanying drawing explanation
The front elevation that Fig. 1 is the utility model registration device;
The cutaway view that Fig. 2 is the utility model registration device;
Fig. 3 is that latch is connected, locks schematic diagram with lock.
Wherein, 1-latch, 2-lock, 3-cushion block, 4-handle nut
The specific embodiment
Below in conjunction with accompanying drawing, the utility model is described in further detail:
As shown in Figure 1 lock 2 is arranged on clamp body, during use, latch 1 is put between knock hole 5 and parts 6, tighten handle nut 4, free handle latch 1 is screwed, make the surface laminating of latch 1 end face and parts 6, thereby complete location.
Be illustrated in figure 3 as latch 1 lock 2 connects, the locking schematic diagram, latch 1 be loaded in the hole of lock 2, inwardly advance the semi-circular portions of latch 1 to stretch into the internal cavity of lock 2, and semi-circular portions and lock 2 internal cavities of rotation latch 1 are locked.
Operating process is as follows:
A manufactures all parts in the utility model
B installs the utility model device on the type frame;
C is arranged on lock 2 on clamp body, during use, latch 1 is put between knock hole 5 and parts 6, tightens handle nut 4, and latch 1 is screwed, and makes the surface laminating of latch 1 end face and parts 6, thereby completes location.
The invention discloses the innovation of the aircraft components docking assembling auxiliary device in a kind of aircraft assembling field.Solve the larger problem of aircraft components butting error, dismantled inconvenient problem.The problem that this auxiliary device is mainly used in aircraft various ways hole location and compresses.
Claims (1)
1. the steady arm for the aircraft docking site, it is characterized in that, this steady arm comprises latch (1), lock (2), cushion block (3), handle nut (4), lock (2) increases semicircular cavities at middle part, 2 ears tightening with the frock skeleton are stretched out in bottom, latch (1) comprises handle, increases the semi-circular boss coordinated with lock (2) semicircular cavities under its Handheld Division, and the threaded head of latch (1) front end coordinates with handle nut (4).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2013202238956U CN203345206U (en) | 2013-04-27 | 2013-04-27 | Locator used for plane butt joint positions |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2013202238956U CN203345206U (en) | 2013-04-27 | 2013-04-27 | Locator used for plane butt joint positions |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203345206U true CN203345206U (en) | 2013-12-18 |
Family
ID=49745132
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2013202238956U Expired - Lifetime CN203345206U (en) | 2013-04-27 | 2013-04-27 | Locator used for plane butt joint positions |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203345206U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107253531A (en) * | 2017-04-21 | 2017-10-17 | 陕西飞机工业（集团）有限公司 | A kind of coordination installation method for hanging intersection point locator |
| CN110143291A (en) * | 2019-05-29 | 2019-08-20 | 陕西飞机工业（集团）有限公司 | A kind of device and method that concentricity is detected, corrected |
-
2013
- 2013-04-27 CN CN2013202238956U patent/CN203345206U/en not_active Expired - Lifetime
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107253531A (en) * | 2017-04-21 | 2017-10-17 | 陕西飞机工业（集团）有限公司 | A kind of coordination installation method for hanging intersection point locator |
| CN110143291A (en) * | 2019-05-29 | 2019-08-20 | 陕西飞机工业（集团）有限公司 | A kind of device and method that concentricity is detected, corrected |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN101685943A (en) | Cabinet body frame tee joint | |
| CN203679353U (en) | Valve body drilling jig for marine stop valve | |
| CN203345206U (en) | Locator used for plane butt joint positions | |
| CN203343948U (en) | Countersunk bolt and nut detaching tool | |
| CN202192462U (en) | Combined clamp | |
| CN201815894U (en) | Structure of integrated adjusting pressure plate | |
| CN204036050U (en) | Part bore hole location special fixture | |
| CN207447934U (en) | The clutch case machining frock that a kind of vertical machining centre uses | |
| CN203401395U (en) | External grinding tool used for sleeve type part | |
| CN205519804U (en) | Motor flange jig | |
| CN202804721U (en) | Novel part machining jig | |
| CN207810215U (en) | Multidirectional V-type clamping structure on platform supporting rack | |
| CN210388065U (en) | Special-shaped part lever clamping device | |
| CN204603828U (en) | The cutter head just milling tool of handle of a knife | |
| CN104400473A (en) | Special fixture for processing cross groove | |
| CN204209343U (en) | Steel bow bridge welding unit positioner | |
| CN204366479U (en) | A kind of motor aluminum component long shell bores milling positioner | |
| CN201274627Y (en) | Three-way connection piece for cabinet frame | |
| CN210790738U (en) | Inner hexagonal powerful sleeve | |
| CN207656290U (en) | A kind of fixture processed simultaneously for gonnecting rod body lid | |
| CN203541758U (en) | Hydraulic type pressing clamp | |
| CN206216117U (en) | A kind of welding tooling of special bolt product | |
| CN203390590U (en) | Clamp for machining milling fall face of engine connecting rod cap | |
| CN107088759A (en) | A kind of turning attachment | |
| CN206855044U (en) | Hood is accurately positioned stationary fixture |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CX01 | Expiry of patent term | ||
| CX01 | Expiry of patent term |
Granted publication date: 20131218 |