CN106363331A - Interior and exterior clamping device applied to welding of plane box section - Google Patents
Interior and exterior clamping device applied to welding of plane box section Download PDFInfo
- Publication number
- CN106363331A CN106363331A CN201611079929.3A CN201611079929A CN106363331A CN 106363331 A CN106363331 A CN 106363331A CN 201611079929 A CN201611079929 A CN 201611079929A CN 106363331 A CN106363331 A CN 106363331A
- Authority
- CN
- China
- Prior art keywords
- welding
- box section
- clamping device
- interior
- exterior
- 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.)
- Pending
Links
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
- B23K37/0426—Fixtures for other work
- B23K37/0435—Clamps
- B23K37/0443—Jigs
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- Physics & Mathematics (AREA)
- Optics & Photonics (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Jigs For Machine Tools (AREA)
Abstract
The invention relates to an interior and exterior clamping device applied to welding of a plane box section and particularly relates to an extension type interior and exterior clamping device applied to design of a plane box section welding tool. The extension type interior and exterior clamping device is mainly used for clamping the interior and the exterior during welding of the plane box section. The extension type interior and exterior clamping device comprises a positioning bolt, a positioning clamping plate, a check block, a shaft pin, a sleeve and a supporting seat, wherein the positioning clamping plate is sleeved in the sleeve; the shaft pin is inserted into the inner chamber of the positioning clamping plate; the check block is mounted at the tail end of the shaft pin; the overall device is mounted on the supporting seat. The invention provides an extension type interior and exterior clamping device which is applied to the design of the plane box section welding tool, and the extension type interior and exterior clamping device has the advantages of lowering the production cost of the tool, realizing the aim of take-down without dismounting, also shortening the welding time of a single product and being simple and rapid to operate.
Description
Technical field
The present invention relates to a kind of device of inside and outside clamping when welding for aircraft box section, more particularly, to aircraft box section Welder
The scalable inside and outside clamping device of one kind that installing timing uses, it is mainly used for inside and outside clamping during the welding of aircraft box section.
Background technology
The device generally playing inside and outside clamping action in design aircraft box section welding tooling must dismantle clamping element one by one
To realize product undercarriage, to lead to the product single single-unit time long, inconvenient operation.Therefore, design a kind of scalable curb pins
Tight device, realizes being not required to dismantle just can reach undercarriage purpose, saves single product weld interval, simple and quick, tool simultaneously
There is realistic meaning.
Content of the invention
The present invention in order to overcome drawbacks described above, its objective is to provide a kind of dress of inside and outside clamping when welding for aircraft box section
Put, thus while reducing welding tooling cost, ensure that and can be saved single product weld interval using the present invention, and because
Clamping device is simple and reliable for structure, easy to operate, can effectively ensure that product quality and required precision.
The present invention to achieve these goals, adopts the following technical scheme that one kind for curb pins during the welding of aircraft box section
Tight device, it includes: fastening screw, locating clamp plate, block, pivot pin, sleeve, bearing；
Described locating clamp plate is enclosed within sleeve, and pivot pin assigns in the inner chamber of locating clamp plate, and block is arranged on pivot pin tail end；Entirely
Device is arranged on bearing.
Further, fastening screw passes through the side of sleeve to be fastened on locating clamp plate.
Further, described locating clamp plate, pivot pin act on simultaneously and can hold out against product shape face.
Further, described block, sleeve act on simultaneously and can compress product design face.
Beneficial effects of the present invention:
The invention provides the scalable inside and outside clamping apparatus structure of one kind using during the design of aircraft box section welding tooling, reducing
While tooling production cost, realize being not required to dismantle just can reach undercarriage purpose, save single product weld interval, operation simultaneously
Simple and fast.
Brief description
Fig. 1 is the structural representation of the present invention.
Specific embodiment
1 describe the present invention below in conjunction with the accompanying drawings:
A kind of device of inside and outside clamping when welding for aircraft box section, it includes: fastening screw 1, locating clamp plate 2, block 3, axle
Pin 4, sleeve 5, bearing 6；
Described locating clamp plate 2 is enclosed within sleeve 5, and pivot pin 4 assigns in the inner chamber of locating clamp plate 2, and block 3 is arranged on pivot pin 4 tail
End；Whole device is arranged on 6 on bearing.
Fastening screw 1 passes through the side of sleeve 5 to be fastened on locating clamp plate 2.
Described locating clamp plate 2, pivot pin 4 act on simultaneously and can hold out against product shape face 7.
Described block 3, sleeve 5 act on simultaneously and can compress product design face 8.
Described fastening screw 1 has stopping function.As long as extracting positioning to insert, locating clamp plate 2 will shrink in the lateral direction,
Realization is not required to dismantle keeper, and product gets final product undercarriage, easy to operate simple.Described locating clamp plate pivot pin acts on simultaneously and can hold out against product
Product outer mold surface, block sleeve acts on simultaneously and can compress product design face.Thus playing positioning action.Described block 3 can be to left-handed
Tightly, block 3 can screw out to the right, and when block 3 screws out to the right, pivot pin 5 is dismountable, and locating clamp plate 2 and sleeve 5 can individual play folder
Tight effect.
Claims (4)
1. a kind of device of inside and outside clamping when welding for aircraft box section is it is characterised in that it includes: fastening screw (1), positioning
Clamp (2), block (3), pivot pin (4), sleeve (5), bearing (6)；
Described locating clamp plate (2) is enclosed within sleeve (5), and pivot pin (4) assigns in the inner chamber of locating clamp plate (2), and block (3) is installed
In pivot pin (4) tail end；Whole device is arranged on bearing (6).
2. inside and outside clamping when welding for aircraft box section according to claim 1 device it is characterised in that: fastening screw
(1) side of sleeve (5) is passed through to be fastened on locating clamp plate (2).
3. inside and outside clamping when welding for aircraft box section according to claim 1 device it is characterised in that: described positioning
Clamp (2), pivot pin (4) act on simultaneously and can hold out against product shape face (7).
4. inside and outside clamping when welding for aircraft box section according to claim 1 device it is characterised in that: described block
(3), sleeve (5) acts on simultaneously and can compress product design face (8).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611079929.3A CN106363331A (en) | 2016-11-30 | 2016-11-30 | Interior and exterior clamping device applied to welding of plane box section |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611079929.3A CN106363331A (en) | 2016-11-30 | 2016-11-30 | Interior and exterior clamping device applied to welding of plane box section |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106363331A true CN106363331A (en) | 2017-02-01 |
Family
ID=57892381
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201611079929.3A Pending CN106363331A (en) | 2016-11-30 | 2016-11-30 | Interior and exterior clamping device applied to welding of plane box section |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106363331A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108544162A (en) * | 2018-04-17 | 2018-09-18 | 广州松兴电气股份有限公司 | A kind of inside clamping and positioning device for box body |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4405075A (en) * | 1981-05-11 | 1983-09-20 | Combustion Engineering, Inc. | Structure for aligning and butt-welding tube ends |
| CN2680681Y (en) * | 2003-12-12 | 2005-02-23 | 上海汽车股份有限公司 | Quick mounting and dismounting clamp special for stress shot-peening |
| CN203245761U (en) * | 2013-04-24 | 2013-10-23 | 哈尔滨飞机工业集团有限责任公司 | Push-pull-type positioning device |
| CN205032881U (en) * | 2015-09-14 | 2016-02-17 | 江西洪都航空工业集团有限责任公司 | Positioning device suitable for welding of aircraft box section |
| CN205521067U (en) * | 2016-01-20 | 2016-08-31 | 哈尔滨飞机工业集团有限责任公司 | Take extending structure's locator |
-
2016
- 2016-11-30 CN CN201611079929.3A patent/CN106363331A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4405075A (en) * | 1981-05-11 | 1983-09-20 | Combustion Engineering, Inc. | Structure for aligning and butt-welding tube ends |
| CN2680681Y (en) * | 2003-12-12 | 2005-02-23 | 上海汽车股份有限公司 | Quick mounting and dismounting clamp special for stress shot-peening |
| CN203245761U (en) * | 2013-04-24 | 2013-10-23 | 哈尔滨飞机工业集团有限责任公司 | Push-pull-type positioning device |
| CN205032881U (en) * | 2015-09-14 | 2016-02-17 | 江西洪都航空工业集团有限责任公司 | Positioning device suitable for welding of aircraft box section |
| CN205521067U (en) * | 2016-01-20 | 2016-08-31 | 哈尔滨飞机工业集团有限责任公司 | Take extending structure's locator |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108544162A (en) * | 2018-04-17 | 2018-09-18 | 广州松兴电气股份有限公司 | A kind of inside clamping and positioning device for box body |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20170201 |