CN106736139A - One kind is applied to aircraft airspeed pipe apparatus for welding and positioning - Google Patents
One kind is applied to aircraft airspeed pipe apparatus for welding and positioning Download PDFInfo
- Publication number
- CN106736139A CN106736139A CN201611080697.3A CN201611080697A CN106736139A CN 106736139 A CN106736139 A CN 106736139A CN 201611080697 A CN201611080697 A CN 201611080697A CN 106736139 A CN106736139 A CN 106736139A
- Authority
- CN
- China
- Prior art keywords
- bearing
- straight fork
- iii
- shaped bearing
- welding
- 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
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K37/00—Auxiliary devices or processes, not specially adapted to a procedure covered by only one of the preceding main groups
- B23K37/04—Auxiliary devices or processes, not specially adapted to a procedure covered by only one of the preceding main groups for holding or positioning work
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K37/00—Auxiliary devices or processes, not specially adapted to a procedure covered by only one of the preceding main groups
- B23K37/04—Auxiliary devices or processes, not specially adapted to a procedure covered by only one of the preceding main groups for holding or positioning work
- B23K37/053—Auxiliary devices or processes, not specially adapted to a procedure covered by only one of the preceding main groups for holding or positioning work aligning cylindrical work; Clamping devices therefor
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K2101/00—Articles made by soldering, welding or cutting
- B23K2101/04—Tubular or hollow articles
- B23K2101/06—Tubes
Landscapes
- Physics & Mathematics (AREA)
- Optics & Photonics (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Butt Welding And Welding Of Specific Article (AREA)
Abstract
It is applied to aircraft airspeed pipe apparatus for welding and positioning the present invention relates to one kind, it is mainly used for aircraft airspeed pipe apparatus for welding and positioning.Clamping locator I, circle bearing, straight fork-shaped bearing I, bearing I, bearing long, bearing II, bearing III, straight fork-shaped bearing II, straight fork-shaped bearing III, straight fork-shaped bearing IV, clamping locator II are arranged on base；Big right clamp, big left clamp, small left clamp, small right clamp are separately mounted on straight fork-shaped bearing I, straight fork-shaped bearing II, straight fork-shaped bearing III, straight fork-shaped bearing IV；Big plug is lain on device with small plug by steel wire, ensures to be used when pitot inner cavity surface and axiality during for welding；Circle clamping plate I, circle clamping plate II, circle clamping plate III are screwed onto on bearing I, the bearing III of bearing II respectively.The present invention shortens the manufacturing cycle, reduces manufacturing cost, using the light manufacturing cycle for shortening product, draws the usual accurate advantage of tool locating.
Description
Technical field
It is applied to aircraft airspeed pipe apparatus for welding and positioning the present invention relates to one kind, it is mainly used for the welding of aircraft airspeed pipe
Positioner.
Background technology
When air speed tubing pincers mounted welder is manufactured and designed, it is impossible to ensure its appearance and size, prevent its welding deformation.It is common
Tool structure complex partses are heavy, and the manufacturing cycle is long to be more expensive to manufacture, in-convenience in use, every time using will be by crane etc.
Instrument increased production time.
The content of the invention
The present invention welds positioning dress to overcome drawbacks described above its object is to provide a kind of aircraft airspeed pipe that is applied to
Put, shorten the manufacturing cycle, reduce manufacturing cost, using the light manufacturing cycle for shortening product, draw usual tool locating accurate
True advantage, the dimensional accuracy that improve frock parts is manufactured so as to improve using three-dimensional software design, Computerized Numerical Control processing technology
The positioning precision of product.
The present invention to achieve these goals, is adopted the following technical scheme that：
One kind is applied to aircraft airspeed pipe apparatus for welding and positioning, clamping locator I, circle bearing, straight fork-shaped bearing I, bearing I, length
Bearing, bearing II, bearing III, straight fork-shaped bearing II, straight fork-shaped bearing III, straight fork-shaped bearing IV, clamping locator II are arranged on
On base；
Big right clamp, big left clamp, small left clamp, small right clamp are separately mounted to straight fork-shaped bearing I, straight fork-shaped bearing II, straight
On fork-shaped bearing III, straight fork-shaped bearing IV；
Big plug is lain on device with small plug by steel wire, ensures to make when pitot inner cavity surface and axiality during for welding
With；
Circle clamping plate I, circle clamping plate II, circle clamping plate III are screwed onto on bearing I, the bearing III of bearing II respectively；
Positioning head is arranged on side plate locator, and side plate locator is with being bolted on bearing long, block is welded on round bearing.
Further, side plate locator is used to adjust positioning head position.
Further, the block, big plug, small plug and positioning head are consistent with aircraft airspeed tube cavity face；The circle
Clamping plate I, circle clamping plate II, the working face of circle clamping plate III are consistent in aircraft airspeed pipe profile.
Beneficial effects of the present invention：
The present invention shortens the manufacturing cycle, reduces manufacturing cost, using the light manufacturing cycle for shortening product, draws usual frock
Accurate positioning advantage, designed using three-dimensional software, Computerized Numerical Control processing technology manufacture improve the dimensional accuracy of frock parts so as to
Improve the positioning precision of product.Improve welding efficiency.Can be very good to ensure aircraft inside panel its appearance and size, prevent it
Deform during welding.Therefore practicality is preferable, it is easy to popularization and application, has larger development and application values in professional domain.
Brief description of the drawings
Fig. 1 is structural representation of the invention.
In figure：1- bases, 2- clamping locators I, 3- circle bearings, the straight fork-shaped bearings I of 4-, the big right clamps of 5-, the big left cards of 6-
Plate, 7- blocks, the small left clamps of 8-, the small right clamps of 9-, the big plugs of 10-, the small plugs of 11-, 12- circle clamping plates I, 13- circle clamping plates II,
14- circle clamping plates III, 15- bearings I, 16- positioning heads, 17- side plate locators, 18- bearings long, 19- bearings II, 20- bearings III,
The straight fork-shaped bearings II of 21-, the straight fork-shaped bearings III of 22-, the straight fork-shaped bearings IV of 23-, 24- clamping locators II.
Specific embodiment
1 the present invention will be described in detail below in conjunction with the accompanying drawings：
One kind is applied to aircraft airspeed pipe apparatus for welding and positioning, clamping locator I 2, circle bearing 3, straight fork-shaped bearing I 4, bearing I
15th, bearing long 18, bearing II 19, bearing III 20, straight fork-shaped bearing II 21, straight fork-shaped bearing III 22, straight fork-shaped bearing IV 23, folder
Tight locator II 24 is arranged on base 1；
Big right clamp 5, big left clamp 6, small left clamp 8, small right clamp 9 are separately mounted to straight fork-shaped bearing I 4, straight fork-shaped bearing
II 21, on straight fork-shaped bearing III 22, straight fork-shaped bearing IV 23；
Big plug 10 is lain on device with small plug 11 by steel wire, when ensureing pitot inner cavity surface and axiality during for welding
Use；
Circle clamping plate I 12, circle clamping plate II 13, circle clamping plate III 14 are screwed onto on the bearing III 20 of I 15 bearing of bearing II 19 respectively；
Positioning head 16 is arranged on side plate locator 17, and side plate locator 17 is with being bolted on bearing long 18, block 7 is welded in circle
On bearing 3.
Side plate locator 17 is used to adjust the position of positioning head 16, and position is fixed during work, and pitot can be facilitated when not working
Depart from this positioner.
The block 7, big plug 10, small plug 11 and positioning head 16 are consistent with aircraft airspeed tube cavity face；The circle folder
Plate I 12, circle clamping plate II 13, the working face of circle clamping plate III 14 are consistent in aircraft airspeed pipe profile.
Claims (3)
- It is 1. a kind of to be applied to aircraft airspeed pipe apparatus for welding and positioning, it is characterised in that：Clamping locator I（2）, circle bearing（3）, it is straight Fork-shaped bearing I（4）, bearing I（15）, bearing long（18）, bearing II（19）, bearing III（20）, straight fork-shaped bearing II（21）, straight fork Shape bearing III（22）, straight fork-shaped bearing IV（23）, clamping locator II（24）Installed in base（1）On；Big right clamp（5）, big left clamp（6）, small left clamp（8）, small right clamp（9）It is separately mounted to straight fork-shaped bearing I（4）、 Straight fork-shaped bearing II（21）, straight fork-shaped bearing III（22）, straight fork-shaped bearing IV（23）On；Big plug（10）With small plug（11）Being lain on device by steel wire, pitot inner cavity surface and coaxial is ensured during for welding Used when spending；Circle clamping plate I（12）, circle clamping plate II（13）, circle clamping plate III（14）Bearing I is screwed onto respectively（15）Bearing II（19）Bearing III （20）On；Positioning head（16）Installed in side plate locator（17）On, side plate locator（17）With being bolted in bearing long（18）Upper, block （7）It is welded in round bearing（3）On.
- 2. according to claim 1 suitable for aircraft airspeed pipe apparatus for welding and positioning, it is characterised in that：Side plate locator （17）For adjusting positioning head（16）Position.
- 3. according to claim 1 suitable for aircraft airspeed pipe apparatus for welding and positioning, it is characterised in that：The block（7）、 Big plug（10）, small plug（11）And positioning head（16）It is consistent with aircraft airspeed tube cavity face；The round clamping plate I（12）, circle folder Plate II（13）, circle clamping plate III（14）Working face be consistent in aircraft airspeed pipe profile.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611080697.3A CN106736139B (en) | 2016-11-30 | 2016-11-30 | One kind being suitable for aircraft airspeed pipe apparatus for welding and positioning |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611080697.3A CN106736139B (en) | 2016-11-30 | 2016-11-30 | One kind being suitable for aircraft airspeed pipe apparatus for welding and positioning |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106736139A true CN106736139A (en) | 2017-05-31 |
| CN106736139B CN106736139B (en) | 2019-05-31 |
Family
ID=58901282
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201611080697.3A Active CN106736139B (en) | 2016-11-30 | 2016-11-30 | One kind being suitable for aircraft airspeed pipe apparatus for welding and positioning |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106736139B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107234391A (en) * | 2017-06-30 | 2017-10-10 | 江苏悦达专用车有限公司 | A kind of high-pressure nozzle assembly welding tooling |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN204353713U (en) * | 2014-12-08 | 2015-05-27 | 江西洪都航空工业集团有限责任公司 | A kind of fixture for aircraft metal tube welding boring |
| CN204504601U (en) * | 2015-03-05 | 2015-07-29 | 江西洪都航空工业集团有限责任公司 | A kind of positioner for airplane tail spray inside panel |
| CN104999208A (en) * | 2015-06-02 | 2015-10-28 | 中航飞机股份有限公司西安飞机分公司 | Welding jig for conducting vacuum electron beam welding on airplane flap sliding rail structural part |
| KR101612084B1 (en) * | 2014-10-07 | 2016-04-12 | 최봉열 | Fixing equipment of bellows tube for welding |
| CN105598629A (en) * | 2014-11-14 | 2016-05-25 | 陕西飞机工业（集团）有限公司 | A flexible locating device for a thin wall pipe |
-
2016
- 2016-11-30 CN CN201611080697.3A patent/CN106736139B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR101612084B1 (en) * | 2014-10-07 | 2016-04-12 | 최봉열 | Fixing equipment of bellows tube for welding |
| CN105598629A (en) * | 2014-11-14 | 2016-05-25 | 陕西飞机工业（集团）有限公司 | A flexible locating device for a thin wall pipe |
| CN204353713U (en) * | 2014-12-08 | 2015-05-27 | 江西洪都航空工业集团有限责任公司 | A kind of fixture for aircraft metal tube welding boring |
| CN204504601U (en) * | 2015-03-05 | 2015-07-29 | 江西洪都航空工业集团有限责任公司 | A kind of positioner for airplane tail spray inside panel |
| CN104999208A (en) * | 2015-06-02 | 2015-10-28 | 中航飞机股份有限公司西安飞机分公司 | Welding jig for conducting vacuum electron beam welding on airplane flap sliding rail structural part |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107234391A (en) * | 2017-06-30 | 2017-10-10 | 江苏悦达专用车有限公司 | A kind of high-pressure nozzle assembly welding tooling |
Also Published As
| Publication number | Publication date |
|---|---|
| CN106736139B (en) | 2019-05-31 |
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