CN107953008A - A kind of fuel manifold soldering fixture - Google Patents
A kind of fuel manifold soldering fixture Download PDFInfo
- Publication number
- CN107953008A CN107953008A CN201711146864.4A CN201711146864A CN107953008A CN 107953008 A CN107953008 A CN 107953008A CN 201711146864 A CN201711146864 A CN 201711146864A CN 107953008 A CN107953008 A CN 107953008A
- Authority
- CN
- China
- Prior art keywords
- briquetting
- ring shape
- circular ring
- stud
- fuel manifold
- 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
- B23K3/00—Tools, devices, or special appurtenances for soldering, e.g. brazing, or unsoldering, not specially adapted for particular methods
- B23K3/08—Auxiliary devices therefor
- B23K3/087—Soldering or brazing jigs, fixtures or clamping means
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Fuel-Injection Apparatus (AREA)
Abstract
The invention discloses a kind of fuel manifold soldering fixture, including circular ring shape matrix (1), observation panel (2) is equidistantly provided with circular ring shape matrix (1) excircle;Multigroup compressing unit being spacedly distributed is provided with circular ring shape matrix (1) upper surface, the compressing unit includes the briquetting (5) being threadedly coupled with stud (6), and the fulcrum bearing (3) below briquetting (5);The stud (6) is perpendicular to circular ring shape matrix (1) upper surface;Locking nut (7) is provided with above the briquetting (5) and in stud (6) end.The present invention overcomes the soldering irregular tilt problem in rear jet end face, so as to reach the design requirement of flatness≤0.3mm, subsequent correction difficulty is reduced, shortens correction man-hour, improves production efficiency.
Description
Technical field
The invention belongs to soldering tech field, and in particular to the fixture of control fuel manifold pricker post welding distortion.
Background technology
Fuel manifold is the important component of engine, and the fuel oil of engine need of work will be conveyed by manifold,
So part carries out it is particularly important that components welding technique.24 spout single-pieces need to be attached by part with oil pipe by soldering,
The technical problems such as parts warranties fuel flow, the fuel distribution uniformity and atomization quality after soldering.The component weldering of fuel manifold
Connect and share 96 weld seams;There is the control requirement of position degree and nozzle plane degree equidimension after welding, size is very in brazing process
It is difficult to guarantee.
Structural analysis is carried out for part, total pipe part is by the spout 24 with gas hood, major and minor each 24 of oil-way pipe
It is composed by vacuum brazing, technological requirement part ensures 24 relatively independent band gas hood spout ends after carrying out vacuum brazing
Fit Plane degree≤the 0.3mm in face.
Vacuum brazing is natively completed under the condition of high temperature (1050 DEG C~1065 DEG C), and material is deposited in itself at high operating temperatures
In thermal expansion, effective positioning of part can not be carried out at high temperature, so the flatness of part can not almost ensure after welding.
To sum up, the flatness for welding rear jet end face cannot meet design requirement, therefore, it is necessary to design a kind of fixture, both
Execute-in-place and size Control can be facilitated to can guarantee that size of the weldquality of part, component etc. again.
The content of the invention
The technical problem to be solved in the present invention is:It is proposed a kind of fuel manifold soldering fixture, overcome soldering rear jet end
The irregular tilt problem in face, so as to reach the design requirement of flatness≤0.3mm, reduces subsequent correction difficulty, shortens correction work
When, improve production efficiency.
Technical scheme is as follows:
A kind of fuel manifold soldering fixture, including circular ring shape matrix, are equidistantly provided with circular ring shape matrix excircle
Observation panel;
Multigroup compressing unit being spacedly distributed is provided with circular ring shape matrix upper surface, the compressing unit includes and spiral shell
The briquetting of male screw connection, and the fulcrum bearing below briquetting;
The stud is perpendicular to circular ring shape matrix upper surface;
Locking nut is provided with above the briquetting and in stud end.
The length of the briquetting is more than or equal to stud to the distance of fulcrum bearing.
The briquetting is strip, and bottom surface is a plane, and one end of briquetting is provided with connecting screw hole, the area of section of briquetting by
Screw hole end gradually increases to free end.
The fulcrum bearing is annular element, and graphite bushing is provided with inner ring.
One end of the invention by supporting seat supports spout, and briquetting compresses the other end face of spout, utilizes screw thread essence
The height of multiple briquetting seal faces is really controlled, so as to control the flatness of multiple spout welding rear end faces, vents face is solved and inclines
The problem of oblique, reduce subsequent correction difficulty, reduces correction man-hour, improves efficiency.Meanwhile briquetting uses variable cross-section form, by spiral shell
Nose end gradually increases to free end area, i.e., smaller with the briquetting section at Stud connection end, and away from stud end section area compared with
Greatly, the purpose is to increase the dead weight of that section of briquetting contacted with vents face so that even if stud bending at high temperature,
Briquetting free end (that section contacted with vents face) remains to keep pushing down vents face substantially, avoids vents face from departing from
Over-tilting (during the weld contraction being connected with oil pipe, vents face can rotate inclination) occurs for the seal face of briquetting, another
Aspect, adds graphite bushing in fulcrum bearing, avoid spout weld after due to metallic element evaporation under high vacuum and and fulcrum bearing
The situation of bonding occurs, and avoids and scraps problem caused by it cannot normally take out spout.
Brief description of the drawings
Fig. 1 is fuel manifold soldering fixture schematic perspective view;
Fig. 2 is fuel manifold soldering fixture floor map (part);
Fig. 3 is fuel manifold schematic diagram;
Fig. 4 is spout structure schematic diagram (part).
Embodiment
Technical scheme is further described below in conjunction with the accompanying drawings, but claimed scope is not limited to institute
State.
As shown in Figure 3, it is necessary to by 24 spouts 9 with gas hood and major and minor 8 soldering connection of oil-way pipe, and after ensuring soldering
Flatness≤0.3mm of 24 spouts 9.
As depicted in figs. 1 and 2, fuel manifold soldering fixture, including circular ring shape matrix 1, on 1 excircle of circular ring shape matrix
24 observation panels 2 (i.e. by after excircle decile, in Along ent location arrangements observation panel 2) are equidistantly provided with, observation panel 2 is one
Run through the notch of matrix 1 along 1 axis direction of matrix, be provided with fulcrum bearing 3 on 1 upper surface of matrix between notch, fulcrum bearing 3 is used
In one end of support spout 9, fulcrum bearing 3 on the line in 1 center of circle of matrix and on 1 upper surface of matrix with setting one perpendicular to base
The stud 6 of 1 upper surface of body, strip briquetting 5 is threaded with stud 6, the section of briquetting 5 is from nearly 6 end of stud to away from spiral shell
6 end of column becomes larger that (5 rectangular cross-section of briquetting in Fig. 1, the rectangular section area of free end are more than the square with 6 connecting pin of stud
Tee section area), 5 lower face of briquetting is a plane, for compressing end face (the top end of part as shown in Figure 4 of spout 9
Face), the top of briquetting 5 is locking nut 7, and for fixing the position of briquetting 5, the length of briquetting 5 is more than stud 6 to fulcrum bearing 3
Distance, fulcrum bearing 3 are annular element, and graphite bushing 4 is provided with its inner ring.Briquetting 5, stud 6,3 structure of locking nut 7 and fulcrum bearing
Into one group of compressing unit, 1 upper surface of circular ring shape matrix is arranged in equal spacing with 24 groups of compressing units, and every group of compressing unit both sides are
Observation panel 2 (more accurate is a little that 3 both sides of fulcrum bearing are observation panel 2).
It is one-to-one to adjust compressing unit one by one after 24 spouts 9 and major and minor oil-way pipe 8 are assembled before soldering, it will add
Add to be put into togerther in vacuum drying oven together with fixture after solder and be brazed.
Claims (4)
- A kind of 1. fuel manifold soldering fixture, it is characterised in that:Including circular ring shape matrix (1), circular ring shape matrix (1) excircle On be equidistantly provided with observation panel (2);Multigroup compressing unit being spacedly distributed is provided with circular ring shape matrix (1) upper surface, the compressing unit includes and spiral shell The briquetting (5) that column (6) is threadedly coupled, and the fulcrum bearing (3) below briquetting (5);The stud (6) is perpendicular to circular ring shape matrix (1) upper surface;Locking nut (7) is provided with above the briquetting (5) and in stud (6) end.
- A kind of 2. fuel manifold soldering fixture according to claim 1, it is characterised in that:The length of the briquetting (5) More than or equal to the distance that stud (6) arrives fulcrum bearing (3).
- A kind of 3. fuel manifold soldering fixture according to claim 1, it is characterised in that:The briquetting (5) is strip Shape, bottom surface are a plane, and one end of briquetting (5) is provided with connecting screw hole, the area of section of briquetting (5) from screw hole end to free end by It is cumulative big.
- A kind of 4. fuel manifold soldering fixture according to claim 1, it is characterised in that:The fulcrum bearing (3) is ring Shape part, is provided with graphite bushing (4) in inner ring.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201711146864.4A CN107953008B (en) | 2017-11-17 | 2017-11-17 | Clamp for brazing fuel manifold |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201711146864.4A CN107953008B (en) | 2017-11-17 | 2017-11-17 | Clamp for brazing fuel manifold |
Publications (2)
Publication Number | Publication Date |
---|---|
CN107953008A true CN107953008A (en) | 2018-04-24 |
CN107953008B CN107953008B (en) | 2020-10-13 |
Family
ID=61964660
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201711146864.4A Active CN107953008B (en) | 2017-11-17 | 2017-11-17 | Clamp for brazing fuel manifold |
Country Status (1)
Country | Link |
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CN (1) | CN107953008B (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110425043A (en) * | 2018-12-04 | 2019-11-08 | 西安成立航空制造有限公司 | A kind of fuel nozzle component and method for welding with general pipeline |
CN112091373A (en) * | 2020-09-10 | 2020-12-18 | 中国航发贵州黎阳航空动力有限公司 | Device and method for controlling welding shrinkage deformation of fuel header pipe |
CN112846617A (en) * | 2021-01-05 | 2021-05-28 | 北京动力机械研究所 | Multi-section annular pipeline welding deformation control tool |
CN116571831A (en) * | 2023-07-11 | 2023-08-11 | 成都国营锦江机器厂 | Welding tool, system and welding method for engine fuel manifold |
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CN202240231U (en) * | 2011-10-19 | 2012-05-30 | 四川蓝星机械有限公司 | Jig for circumferential seam assembly of barrel |
CN103586639A (en) * | 2013-11-11 | 2014-02-19 | 沈阳黎明航空发动机(集团)有限责任公司 | Method for machining fuel manifold with nozzles and of welding structure |
KR20140080993A (en) * | 2012-12-21 | 2014-07-01 | 한국남부발전 주식회사 | Apparatus for pipe preheating |
CN105345384A (en) * | 2015-11-13 | 2016-02-24 | 沈阳黎明航空发动机(集团)有限责任公司 | Positioning and welding clamp for header pipe and welding deformation control method |
CN205096775U (en) * | 2015-10-28 | 2016-03-23 | 东方电气集团东方汽轮机有限公司 | Combustion engine combustion chamber gas pipeline simulation assembly platform |
CN206200437U (en) * | 2016-10-21 | 2017-05-31 | 成都国光电气股份有限公司 | A kind of electronics gun housing and blast pipe weld jig |
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2017
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Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
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CN202240231U (en) * | 2011-10-19 | 2012-05-30 | 四川蓝星机械有限公司 | Jig for circumferential seam assembly of barrel |
KR20140080993A (en) * | 2012-12-21 | 2014-07-01 | 한국남부발전 주식회사 | Apparatus for pipe preheating |
CN103586639A (en) * | 2013-11-11 | 2014-02-19 | 沈阳黎明航空发动机(集团)有限责任公司 | Method for machining fuel manifold with nozzles and of welding structure |
CN205096775U (en) * | 2015-10-28 | 2016-03-23 | 东方电气集团东方汽轮机有限公司 | Combustion engine combustion chamber gas pipeline simulation assembly platform |
CN105345384A (en) * | 2015-11-13 | 2016-02-24 | 沈阳黎明航空发动机(集团)有限责任公司 | Positioning and welding clamp for header pipe and welding deformation control method |
CN206200437U (en) * | 2016-10-21 | 2017-05-31 | 成都国光电气股份有限公司 | A kind of electronics gun housing and blast pipe weld jig |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110425043A (en) * | 2018-12-04 | 2019-11-08 | 西安成立航空制造有限公司 | A kind of fuel nozzle component and method for welding with general pipeline |
CN110425043B (en) * | 2018-12-04 | 2023-11-21 | 西安成立航空制造有限公司 | Fuel nozzle assembly with main pipe and brazing method |
CN112091373A (en) * | 2020-09-10 | 2020-12-18 | 中国航发贵州黎阳航空动力有限公司 | Device and method for controlling welding shrinkage deformation of fuel header pipe |
CN112091373B (en) * | 2020-09-10 | 2021-11-16 | 中国航发贵州黎阳航空动力有限公司 | Device and method for controlling welding shrinkage deformation of fuel header pipe |
CN112846617A (en) * | 2021-01-05 | 2021-05-28 | 北京动力机械研究所 | Multi-section annular pipeline welding deformation control tool |
CN116571831A (en) * | 2023-07-11 | 2023-08-11 | 成都国营锦江机器厂 | Welding tool, system and welding method for engine fuel manifold |
CN116571831B (en) * | 2023-07-11 | 2023-11-07 | 成都国营锦江机器厂 | Welding tool, system and welding method for engine fuel manifold |
Also Published As
Publication number | Publication date |
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CN107953008B (en) | 2020-10-13 |
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