CN108067848A - A kind of glue riveting tubular member processing method with filler - Google Patents
A kind of glue riveting tubular member processing method with filler Download PDFInfo
- Publication number
- CN108067848A CN108067848A CN201611001101.6A CN201611001101A CN108067848A CN 108067848 A CN108067848 A CN 108067848A CN 201611001101 A CN201611001101 A CN 201611001101A CN 108067848 A CN108067848 A CN 108067848A
- Authority
- CN
- China
- Prior art keywords
- filler
- filling
- filling block
- tubular member
- glue
- 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
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P17/00—Metal-working operations, not covered by a single other subclass or another group in this subclass
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Insertion Pins And Rivets (AREA)
Abstract
The invention belongs to aviation composite part manufacturing fields, and in particular to a kind of glue riveting tubular member processing method with filler.Tubular member carries out filler by opening fabrication hole in tube wall at present, then inwardly fills filler.The construction technology difficulty is big, operation is required very high.And easily there is the defects of filler filling size does not meet drawing requirement or unreal filling, it causes part disqualification rate higher, reprocesses the problems such as Rework cycle is long.The present invention manufactures filling block forming frock, is filling block by filler precuring, in part glue riveter sequences, filling block is put into solidify afterwards by building filling block technique digital-to-analogue.Operation difficulty is small, and production efficiency is high, and can ensure packing area filling quality.
Description
Technical field
The invention belongs to aviation composite part manufacturing fields, and in particular to a kind of glue riveting tubular member with filler
Processing method.
Background technology
At present tubular member carry out filler process be：By opening fabrication hole in tube wall, filler is then inwardly filled.
The construction technology difficulty is big, operation is required very high.And easily there is filler filling size and do not meet drawing requirement or filling
The defects of unreal, causes part disqualification rate higher, reprocesses the problems such as Rework cycle is long.
The content of the invention
Filler precuring is filling block by building filling block technique digital-to-analogue, manufacture filling block forming frock by the present invention,
In part glue riveter sequences, filling block is put into solidify afterwards.
The glue riveting tubular member processing method with filler of the present invention builds filler according to the shape in filler region first
Block technique digital-to-analogue and prefabricated filling block, the size for being dimensioned slightly smaller than the filling region of the filling block；In the splicing table of down tube
Face coats filler, coats filler in the splicing face of filling block as needed, filling block is put into the filling region of down tube, and is ensured
Full of filling region；Filler is coated towards the surface of filling region in upper tube, after being closed afterwards with the down tube glue riveting knot, heating adds
It is cured.
Further, the size of the filling block is less than the filling region size 2mm.
The beneficial effects of the invention are as follows：Operation difficulty is small, and production efficiency is high, and can ensure packing area filling quality.
Description of the drawings
Fig. 1 is the structure diagram for the glue riveting tubular member that the present invention has filler.
Specific embodiment
A kind of glue riveting tubular member processing method with filler, this method are filled out first according to the shape in filler region structure
Expect block technique digital-to-analogue and prefabricated filling block 3, the size for being dimensioned slightly smaller than the filling region of the filling block 3；In the glue of down tube 1
Surface coating filler is connect, filler is coated in the splicing face of filling block 3 as needed, filling block 3 is put into the fill area of down tube 1
Domain, and ensure full of filling region；Upper tube 2 towards filling region surface coat filler, afterwards with the 1 glue riveting knot of down tube
After conjunction, temperature-pressure cures.The size of the filling block 3 is less than the filling region size 2mm.
Claims (2)
1. a kind of glue riveting tubular member processing method with filler, it is characterised in that：This method is first according to filler region
Shape builds filling block technique digital-to-analogue and prefabricated filling block (3), the ruler for being dimensioned slightly smaller than the filling region of the filling block (3)
It is very little；Filler is coated in the glue surfaces of down tube (1), filler is coated in the splicing face of filling block (3) as needed, by filling block
(3) filling region of down tube (1) is put into, and is ensured full of filling region；It is filled out in the surface coating of upper tube (2) towards filling region
Material, after being closed afterwards with the down tube (1) glue riveting knot, temperature-pressure cures.
2. glue riveting tubular member processing method according to claim 1, it is characterised in that：The size of the filling block (3)
Less than the filling region size 2mm.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611001101.6A CN108067848A (en) | 2016-11-14 | 2016-11-14 | A kind of glue riveting tubular member processing method with filler |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611001101.6A CN108067848A (en) | 2016-11-14 | 2016-11-14 | A kind of glue riveting tubular member processing method with filler |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108067848A true CN108067848A (en) | 2018-05-25 |
Family
ID=62162065
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201611001101.6A Pending CN108067848A (en) | 2016-11-14 | 2016-11-14 | A kind of glue riveting tubular member processing method with filler |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108067848A (en) |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4908930A (en) * | 1988-04-25 | 1990-03-20 | Essex Composite Systems | Method of making a torsion bar |
| EP0595607B1 (en) * | 1992-10-27 | 1997-03-05 | MITSUI TOATSU CHEMICALS, Inc. | Composite molded article and method for making same |
| CN1397691A (en) * | 2002-09-03 | 2003-02-19 | 李顶忠 | Reinforced manhole cover and its making method |
| CN101445663A (en) * | 2008-11-12 | 2009-06-03 | 中国航空工业第一集团公司北京航空制造工程研究所 | Filler and filling method for composite material structure void area |
| CN102470797A (en) * | 2009-07-01 | 2012-05-23 | 株式会社林技术研究所 | Board structure for vehicle and manufacturing method of the same |
| CN102529113A (en) * | 2011-12-27 | 2012-07-04 | 成都飞机工业（集团）有限责任公司 | Filling method of corner gaps of composite material component |
| CN103072284A (en) * | 2012-12-06 | 2013-05-01 | 中国船舶重工集团公司第七二五研究所 | Reinforcing ribs contained sandwich structure composite material and its making method |
| CN105035359A (en) * | 2015-07-28 | 2015-11-11 | 中国运载火箭技术研究院 | Composite material integrated control surface structure with progressive decrease in rigidity and processing method thereof |
| CN108067831A (en) * | 2016-11-14 | 2018-05-25 | 江西昌河航空工业有限公司 | A kind of thin-wall stamping part moulding process with splicing face |
-
2016
- 2016-11-14 CN CN201611001101.6A patent/CN108067848A/en active Pending
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4908930A (en) * | 1988-04-25 | 1990-03-20 | Essex Composite Systems | Method of making a torsion bar |
| EP0595607B1 (en) * | 1992-10-27 | 1997-03-05 | MITSUI TOATSU CHEMICALS, Inc. | Composite molded article and method for making same |
| CN1397691A (en) * | 2002-09-03 | 2003-02-19 | 李顶忠 | Reinforced manhole cover and its making method |
| CN101445663A (en) * | 2008-11-12 | 2009-06-03 | 中国航空工业第一集团公司北京航空制造工程研究所 | Filler and filling method for composite material structure void area |
| CN102470797A (en) * | 2009-07-01 | 2012-05-23 | 株式会社林技术研究所 | Board structure for vehicle and manufacturing method of the same |
| CN102529113A (en) * | 2011-12-27 | 2012-07-04 | 成都飞机工业（集团）有限责任公司 | Filling method of corner gaps of composite material component |
| CN103072284A (en) * | 2012-12-06 | 2013-05-01 | 中国船舶重工集团公司第七二五研究所 | Reinforcing ribs contained sandwich structure composite material and its making method |
| CN105035359A (en) * | 2015-07-28 | 2015-11-11 | 中国运载火箭技术研究院 | Composite material integrated control surface structure with progressive decrease in rigidity and processing method thereof |
| CN108067831A (en) * | 2016-11-14 | 2018-05-25 | 江西昌河航空工业有限公司 | A kind of thin-wall stamping part moulding process with splicing face |
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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 | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20180525 |
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| RJ01 | Rejection of invention patent application after publication |