CN209335007U - A kind of welding positioning mold for aviation compressor structural framing welding processing - Google Patents
A kind of welding positioning mold for aviation compressor structural framing welding processing Download PDFInfo
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- CN209335007U CN209335007U CN201822041468.1U CN201822041468U CN209335007U CN 209335007 U CN209335007 U CN 209335007U CN 201822041468 U CN201822041468 U CN 201822041468U CN 209335007 U CN209335007 U CN 209335007U
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Abstract
The utility model discloses a kind of welding positioning molds for aviation compressor structural framing welding processing, including the first right angle arm rest group, the second right angle arm rest group, third right angle arm rest group, the 4th right angle arm rest group, the 5th right angle arm rest group and the 6th right angle arm rest group, the first right angle arm rest group, the second right angle arm rest group, third right angle arm rest group, the 4th right angle arm rest group surround a cuboid framework；There is the first welding post hole at the top of first right angle arm rest group, there is the second welding post hole at the top of second right angle arm rest group, there is third welding post hole at the top of third right angle arm rest group, there is the 4th welding post hole at the top of 4th right angle arm rest group, there is the 5th welding post hole at the top of 5th right angle arm rest group, there is the 6th welding post hole at the top of the 6th right angle arm rest group.The utility model controls the molding welding deformation of aviation compressor structural framing by welding positioning mold, improves welding efficiency, welding deformation amount is smaller, quality is higher.
Description
Technical field
The utility model relates to a kind of cup more particularly to a kind of welderings for aviation compressor structural framing welding processing
Connect positioning mold.
Background technique
Aviation compressor structural framing is to apply in military, Aerospace manufacturing field, because the particularity of use environment is very strong, very
Multi-processing mode, such as riveting, can not all replace welding at overall processing.As shown in Figure 1, aviation compressor structural framing includes
The vertical aluminum corner brace 34 of four boxes 30, the first vertical aluminum corner brace 32, the second vertical aluminum corner brace 33, third, the 4th vertical aluminum corner brace 35, first connect
Aluminum corner brace 36, second connects aluminum corner brace 37, third connection aluminum corner brace 38, the 5th vertical aluminum corner brace 39, the 6th vertical aluminum corner brace 310, first laterally
The lateral aluminum corner brace 312 of aluminum corner brace 311, second, third transverse direction aluminum corner brace 313 and the 4th connection aluminum corner brace 314, the first vertical aluminum corner brace 32 are pushed up
Four boxes 30 are individually fixed at the top of portion, the second vertical aluminum corner brace 33, at the top of the vertical aluminum corner brace 34 of third, at the top of the 4th vertical aluminum corner brace 35
Four angles bottom, first connection aluminum corner brace 36 is connected and fixed between the first vertical aluminum corner brace 32 and the vertical aluminum corner brace 34 of third, second
Connection aluminum corner brace 37 is connected and fixed between the vertical aluminum corner brace 34 of third and the 4th vertical aluminum corner brace 35, and third connection aluminum corner brace 38 is connected and fixed
Between the 4th vertical 35 top of aluminum corner brace and the second vertical 33 top of aluminum corner brace, it is perpendicular that the 4th connection aluminum corner brace 314 is connected and fixed on the 4th
To between 35 middle and lower part of aluminum corner brace and the second vertical 33 middle and lower part of aluminum corner brace, first 311 one end of lateral aluminum corner brace, the second lateral aluminum corner brace 312
One end is individually fixed in third connection 38 both ends of aluminum corner brace, and it is another that the first lateral aluminum corner brace 311 is fixed at the top of the 6th vertical aluminum corner brace 310
One end bottom, the second 312 other end bottom of lateral aluminum corner brace is fixed at the top of the 5th vertical aluminum corner brace 39, and third transverse direction aluminum corner brace 313 connects
It connects and is fixed between first lateral 311 other end of aluminum corner brace and second 312 other end of lateral aluminum corner brace.
Aviation compressor structural framing because material be profile, thin-wall part, weld it is easy to appear deformation, finally present at
Product will be unable to controlled.Aviation compressor structural framing is aviation compressor structural member, in addition to very harsh to weight demands, aviation pressure
Contracting machine structural framing has also shape and has very high requirement, and work has vibration again when use, therefore welds aviation compressor knot
Structure frame is always a technological difficulties.Prior welding mode is not provided with welding auxiliary equipment, and welding deformation is big, size not by
Control increases the risk that weld cracks repeatedly after the shape of school, single component splicing butt welding efficiency is very low, and size is unable to satisfy
It is required that.
Utility model content
Place in view of the shortcomings of the prior art, the purpose of this utility model is to provide one kind to be used for aviation compressor
The welding positioning mold of structural framing welding processing positions aviation compressor structural framing loose mail by welding positioning mold, so
Weld job is carried out to each welding post hole afterwards, it is molding to control aviation compressor structural framing by welding positioning mold
Deformation is welded, the deflection after aviation compressor structural framing can be allowed to weld is smaller, welding quality is higher, may be implemented primary
All welding operations of aviation compressor structural framing can be completed in clamping, and welding efficiency is increased substantially.
The purpose of this utility model is achieved through the following technical solutions:
A kind of welding positioning mold for aviation compressor structural framing welding processing, including the first right angle arm rest group,
Second right angle arm rest group, third right angle arm rest group, the 4th right angle arm rest group, the 5th right angle arm rest group and the 6th right angle arm rest group,
First right angle arm rest group, the second right angle arm rest group, third right angle arm rest group, the 4th right angle arm rest group surround a cuboid frame
Frame；The first right angle arm rest group is mutually perpendicular to be fixedly welded by two the first right angle arm rests, two the first right angle arm rests
Top all has the first welding notch, and the first welding notch of two the first right angle arm rests, which is matched, is combined into the first welding post hole,
The first positioning plate is fixed at the top of the first right angle arm rest group；The second right angle arm rest group is by two the second right angle arm rest phases
It is mutually vertically fixedly welded, all has the second welding notch at the top of two the second right angle arm rests, two the second right angle arm rests
Second welding notch is fixed with the second positioning plate at the top of the second right angle arm rest group with the second welding post hole is combined into；Institute
It states third right angle arm rest group to be mutually perpendicular to be fixedly welded by two third right angle arm rests, at the top of two third right angle arm rests
Notch is welded with third, the third welding notches of two third right angle arm rests is with being combined into third welding post hole, and described the
Third positioning plate is fixed at the top of three right angle arm rest groups；4th right angle arm rest group is mutually perpendicular to by two the 4th right angle arm rests
It is fixedly welded, the 4th welding notch, the 4th weldering of two the 4th right angle arm rests is all had at the top of two the 4th right angle arm rests
Notch is connect with the 4th welding post hole is combined into, is fixed with the 4th positioning plate at the top of the 4th right angle arm rest group；Described 5th
Right angle arm rest group is mutually perpendicular to be fixedly welded by two the 5th right angle arm rests, and the 5th right angle arm rest is by the first transverse arm A
It is vertically formed by connecting with the first vertical arm A, the first transverse arm A and the first vertical arm A of the 5th right angle arm rest have at link position to be turned
Corner A, the corner portion A of two the 5th right angle arm rests all have the 5th welding notch, the 5th welding of two the 5th right angle arm rests
Notch, which is matched, is combined into the 5th welding post hole；6th right angle arm rest group is mutually perpendicular to fixed weldering by two the 6th right angle arm rests
It connecing, the 6th right angle arm rest is vertically formed by connecting by the first transverse arm B and the first vertical arm B, and the first of the 6th right angle arm rest
There is transverse arm B and the first vertical arm B corner portion B, the corner portion B of two the 6th right angle arm rests to all have the 6th weldering at link position
Notch is connect, the 6th welding notch of two the 6th right angle arm rests, which is matched, is combined into the 6th welding post hole.
In order to which the utility model is better achieved, the 5th right angle arm rest group transverse direction is far from the 5th welding post hole
One end and the second right angle arm rest group screw thread detachable connection, the 6th right angle arm rest group transverse direction far from the 6th welding
The one end in station hole and third right angle arm rest group screw thread detachable connection.
Preferably, being placed with cubic posting at the top of the cuboid framework, the four directions posting, which has, successively to be had
There are first jiao, second jiao, the third angle and fourth angle, first jiao of cooperation of the four directions posting is placed in the first right angle arm rest group
Top and correspondence are located at the first positioning plate bottom, and second jiao of cooperation of the four directions posting is placed in the second right angle arm rest group top
Portion and it is corresponding be located at the second positioning plate bottom, the third angle cooperation of the four directions posting is placed at the top of third right angle arm rest group
And it is corresponding be located at third positioning plate bottom, the fourth angle cooperation of the four directions posting be placed at the top of the 4th right angle arm rest group and
It is corresponding to be located at the 4th positioning plate bottom.
Preferably, the first right angle arm rest of the first right angle arm rest group is provided with several positioning along its length direction
The second right angle arm rest of screw hole A, the second right angle arm rest group are provided with several positioning screw holes B along its length direction, described
The third right angle arm rest of third right angle arm rest group is provided with several positioning screw holes C along its length direction, and the 4th right angle leans on
4th right angle arm rest of arm group is provided with several positioning screw holes D along its length direction, and the first of the 5th right angle arm rest group
Transverse arm A and the first vertical arm A is provided with several positioning screw holes E respectively along its length direction, and the of the 6th right angle arm rest group
One transverse arm B and the first vertical arm B is provided with several positioning screw holes F respectively along its length direction.
Preferably, the 5th right angle arm rest group bottom outside and the 6th right angle arm rest group bottom outside are fixed with first
Position riser.
Preferably, the first positioning bottom of the riser is fixed with the first positioning bearing soleplate.
The utility model compared with the prior art, have the following advantages that and the utility model has the advantages that
(1) the utility model positions aviation compressor structural framing loose mail by welding positioning mold, then to each weldering
It connects station hole and carries out weld job, control the molding welding deformation of aviation compressor structural framing by welding positioning mold,
After aviation compressor structural framing can be allowed to weld deflection is smaller, welding quality is higher.
(2) clamped one time, which may be implemented, in the utility model can be completed all welding operations of aviation compressor structural framing,
Welding efficiency is increased substantially.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of aviation compressor structural framing；
Fig. 2 is the structural schematic diagram that the utility model welds positioning mold.
Wherein, title corresponding to the appended drawing reference in attached drawing are as follows:
Tetra- box of 30-, the vertical aluminum corner brace of 32- first, the vertical aluminum corner brace of 33- second, the vertical aluminum corner brace of 34- third, 35-the
Four vertical aluminum corner braces, the connection aluminum corner brace of 36- first, the connection aluminum corner brace of 37- second, 38- third connect aluminum corner brace, 39-the five vertical angles
Aluminium, the vertical aluminum corner brace of 310- the 6th, the lateral aluminum corner brace of 311- first, the lateral aluminum corner brace of 312- second, 313- third transverse direction aluminum corner brace,
The connection aluminum corner brace of 314- the 4th, the first right angle 1- arm rest group, the first welding post of 11- hole, the second right angle 2- arm rest group, 21-
Second welding post hole, 3- third right angle arm rest group, 31-third welding post holes, the 4th right angle arm rest group of 4-, 41-
Four welding post holes, the 5th right angle arm rest group of 5-, the 5th welding post hole 51-, the 6th right angle arm rest group of 6-, 61- the 6th
Welding post hole, the positioning riser of 7- first, the positioning bearing soleplate of 8- first, the four directions 9- posting, the first positioning plate of 10-,
The second positioning plate of 12-, 13- third positioning plate, the 4th positioning plate of 14-.
Specific embodiment
The utility model is described in further detail below with reference to embodiment:
Embodiment
As shown in Fig. 2, a kind of welding positioning mold for aviation compressor structural framing welding processing, including first straight
Angle arm rest group 1, the second right angle arm rest group 2, third right angle arm rest group 3, the 4th right angle arm rest group 4,5 and of the 5th right angle arm rest group
6th right angle arm rest group 6, the first right angle arm rest group 1, the second right angle arm rest group 2, third right angle arm rest group 3, the 4th right angle arm rest
Group 4 surrounds a cuboid framework.First right angle arm rest group 1 is mutually perpendicular to be fixedly welded by two the first right angle arm rests,
The first welding notch is all had at the top of two the first right angle arm rests, the first welding notch of two the first right angle arm rests, which is matched, to be combined into
First welding post hole 11 is fixed with the first positioning plate 10 at the top of first right angle arm rest group 1.Second right angle arm rest group 2 is by two
Second right angle arm rest is mutually perpendicular to be fixedly welded, and all has the second welding notch at the top of two the second right angle arm rests, and two
Second welding notch of the second right angle arm rest is fixed at the top of the second right angle arm rest group 2 with the second welding post hole 21 is combined into
Second positioning plate 12.Third right angle arm rest group 3 is mutually perpendicular to be fixedly welded by two third right angle arm rests, and two thirds are straight
Third welding notch is all had at the top of the arm rest of angle, the third welding notch of two third right angle arm rests, which is matched, is combined into third Welder
Position hole 31, is fixed with third positioning plate 13 at the top of third right angle arm rest group 3.4th right angle arm rest group 4 is leaned on by two the 4th right angles
Arm is mutually perpendicular to be fixedly welded, and the 4th welding notch is all had at the top of two the 4th right angle arm rests, two the 4th right angles lean on
4th welding notch of arm is fixed with the 4th positioning plate at the top of the 4th right angle arm rest group 4 with the 4th welding post hole 41 is combined into
14.5th right angle arm rest group 5 is mutually perpendicular to be fixedly welded by two the 5th right angle arm rests, and the 5th right angle arm rest is by the first cross
Arm A and the first vertical arm A are vertically formed by connecting, and the first transverse arm A and the first vertical arm A of the 5th right angle arm rest have at link position
Corner portion A, the corner portion A of two the 5th right angle arm rests all have the 5th welding notch, the 5th weldering of two the 5th right angle arm rests
Notch is connect with being combined into the 5th welding post hole 51.6th right angle arm rest group 6 is mutually perpendicular to fix by two the 6th right angle arm rests
It is welded, the 6th right angle arm rest is vertically formed by connecting by the first transverse arm B and the first vertical arm B, and the first of the 6th right angle arm rest is horizontal
There is arm B and the first vertical arm B corner portion B, the corner portion B of two the 6th right angle arm rests to all have the 6th weldering at link position
Notch is connect, the 6th welding notch of two the 6th right angle arm rests, which is matched, is combined into the 6th welding post hole 61.
As shown in Fig. 2, the one end of 5 transverse direction of the 5th right angle arm rest group far from the 5th welding post hole 51 and the second right angle
2 screw thread detachable connection of arm rest group, the one end of 6 transverse direction of the 6th right angle arm rest group far from the 6th welding post hole 61 and the
Three right angle arm rest groups, 3 screw thread detachable connection.
As shown in Fig. 2, being placed with cubic posting 9 at the top of cuboid framework, cubic posting 9 is with successively with first
Angle, second jiao, the third angle and fourth angle, it is at the top of the first right angle arm rest group 1 and right that first jiao of cooperation of cubic posting 9 is placed in
10 bottom of the first positioning plate should be located at, second jiao of cooperation of cubic posting 9 is placed in 2 top of the second right angle arm rest group and corresponds to
Positioned at 12 bottom of the second positioning plate, the third angle cooperation of cubic posting 9 is placed in 3 top of third right angle arm rest group and corresponds to
Positioned at 13 bottom of third positioning plate, the fourth angle cooperation of cubic posting 9 is placed in 4 top of the 4th right angle arm rest group and corresponding position
In 14 bottom of the 4th positioning plate.
As shown in Fig. 2, the first right angle arm rest of the first right angle arm rest group 1 is provided with several positioning spiral shells along its length direction
The second right angle arm rest of hole A, the second right angle arm rest group 2 are provided with several positioning screw holes B along its length direction, and third right angle leans on
The third right angle arm rest of arm group 3 is provided with several positioning screw holes C along its length direction, and the 4th of the 4th right angle arm rest group 4 is straight
Angle arm rest is provided with several positioning screw holes D, the first transverse arm A and the first vertical arm A of the 5th right angle arm rest group 5 along its length direction
It is provided with several positioning screw holes E respectively along its length direction, the first transverse arm B and the first vertical arm B of the 6th right angle arm rest group 6 divide
Several positioning screw holes F is not provided with along its length direction.
As shown in Fig. 2, 5 bottom outside of the 5th right angle arm rest group and 6 bottom outside of the 6th right angle arm rest group are fixed with first
Position riser 7；First positioning 7 bottom of riser is fixed with the first positioning bearing soleplate 8.
In use, as shown in Fig. 2, four boxes 30 being placed in cubic 9 bottom of posting and are positioned by screw, by third
Vertical aluminum corner brace 34 is placed in 1 inside of the first right angle arm rest group and is positioned by screw, and the 4th vertical aluminum corner brace 35 is placed in second
Arm rest group 2 inside in right angle is simultaneously positioned by screw, and the second vertical aluminum corner brace 33 is placed in 3 inside of third right angle arm rest group and is led to
Screw positioning is crossed, the first vertical aluminum corner brace 32 is placed in 4 inside of the 4th right angle arm rest group and is positioned by screw, laterally by first
Aluminum corner brace 311 is placed in the whole inside two the first transverse arm A of the 5th right angle arm rest group 5 and is positioned by screw, laterally by second
Aluminum corner brace 312 is placed in the whole inside two the first transverse arm B of the 6th right angle arm rest group 6 and is positioned by screw, vertical by the 6th
Aluminum corner brace 310 is placed in the whole inside two the first vertical arm A of the 5th right angle arm rest group 5 and is positioned by screw, vertical by the 5th
Aluminum corner brace 39 is placed in the whole inside two the first vertical arm B of the 6th right angle arm rest group 6 and is positioned by screw.Then by U-shaped
Folder is successively by four boxes 30, the first vertical aluminum corner brace 32, the second vertical aluminum corner brace 33, the vertical aluminum corner brace 34 of third, the 4th vertical aluminum corner brace
35, the first connection aluminum corner brace 36, second connects aluminum corner brace 37, third connects aluminum corner brace 38, the 5th vertical aluminum corner brace 39, the 6th vertical aluminum corner brace
310, the first lateral aluminum corner brace 312 of lateral aluminum corner brace 311, second, third transverse direction aluminum corner brace the 313, the 4th connect aluminum corner brace 314 and weld and position
Mold cramping is fixed, and the utility model can use independent screw by four boxes 30, the first vertical aluminum corner brace 32, the second vertical aluminum corner brace
33, the vertical aluminum corner brace 34 of third, the 4th vertical aluminum corner brace 35, first connect aluminum corner brace 36, second and connect aluminum corner brace 37, third connection aluminum corner brace
38, the 5th vertical aluminum corner brace 39, the 6th vertical the 310, first lateral aluminum corner brace 311, second of aluminum corner brace lateral aluminum corner brace 312, third lateral angle
Aluminium the 313, the 4th connects aluminum corner brace 314 and welding positioning mold positioning is fixed, can also be by the way of independent U-shaped folder by four boxes
30, the vertical aluminum corner brace 34 of the first vertical aluminum corner brace 32, the second vertical aluminum corner brace 33, third, the 4th vertical aluminum corner brace 35, first connect aluminum corner brace
36, the second connection aluminum corner brace 37, third connection aluminum corner brace 38, the 5th vertical aluminum corner brace 39, the 6th lateral aluminum corner brace of vertical aluminum corner brace 310, first
311, the second lateral aluminum corner brace 312, third transverse direction aluminum corner brace the 313, the 4th connect aluminum corner brace 314 and welding positioning mold positioning is fixed, when
Realization can also be so combined with U-shaped folder two ways using screw by four boxes 30, the first vertical aluminum corner brace 32, the second vertical angle
The vertical aluminum corner brace 34 of aluminium 33, third, the 4th vertical aluminum corner brace 35, first connect aluminum corner brace 36, second and connect aluminum corner brace 37, third connection aluminum corner brace
38, the 5th vertical aluminum corner brace 39, the 6th vertical the 310, first lateral aluminum corner brace 311, second of aluminum corner brace lateral aluminum corner brace 312, third lateral angle
Aluminium the 313, the 4th connects aluminum corner brace 314 and welding positioning mold positioning is fixed.
Finally, first by welding equipment in the first welding post hole 11, the second welding post hole 21, third welding post
Hole 31, the 4th welding post hole 41, the 5th welding post hole 51, each position in the 6th welding post hole 61 are successively to aviation pressure
Contracting machine structural framing loose mail combines each position and is subjected to, then reverse welding positioning mold and aviation compressor again
The combination of structural framing loose mail is attached lines welding, so far can conveniently realize the welding behaviour of aviation compressor structural framing
Make, the aviation compressor structural framing final product quality after welding is higher.
The above is only the preferred embodiment of the utility model only, is not intended to limit the utility model, all at this
Made any modifications, equivalent replacements, and improvements etc., should be included in the utility model within the spirit and principle of utility model
Protection scope within.
Claims (6)
1. a kind of welding positioning mold for aviation compressor structural framing welding processing, it is characterised in that: straight including first
Angle arm rest group (1), the second right angle arm rest group (2), third right angle arm rest group (3), the 4th right angle arm rest group (4), the 5th right angle lean on
Arm group (5) and the 6th right angle arm rest group (6), the first right angle arm rest group (1), the second right angle arm rest group (2), third right angle arm rest group
(3), the 4th right angle arm rest group (4) surrounds a cuboid framework；The first right angle arm rest group (1) is leaned on by two the first right angles
Arm is mutually perpendicular to be fixedly welded, and all has the first welding notch at the top of two the first right angle arm rests, two the first right angles lean on
First welding notch of arm is fixed with the with the first welding post hole (11) is combined at the top of the first right angle arm rest group (1)
One positioning plate (10)；The second right angle arm rest group (2) is mutually perpendicular to be fixedly welded by two the second right angle arm rests, and two
The second welding notch is all had at the top of second right angle arm rest, the second welding notch of two the second right angle arm rests, which is matched, is combined into second
Welding post hole (21), the second right angle arm rest group (2) top are fixed with the second positioning plate (12)；Third right angle arm rest
Group (3) is mutually perpendicular to be fixedly welded by two third right angle arm rests, and third weldering is all had at the top of two third right angle arm rests
Notch is connect, the third welding notch of two third right angle arm rests, which is matched, is combined into third welding post hole (31), the third right angle
Third positioning plate (13) are fixed at the top of arm rest group (3)；The 4th right angle arm rest group (4) is mutual by two the 4th right angle arm rests
It is vertically fixedly welded, all has the 4th welding notch at the top of two the 4th right angle arm rests, the of two the 4th right angle arm rests
Four welding notches are fixed with the 4th positioning with the 4th welding post hole (41) is combined at the top of the 4th right angle arm rest group (4)
Plate (14)；The 5th right angle arm rest group (5) is mutually perpendicular to be fixedly welded by two the 5th right angle arm rests, and the described 5th is straight
Angle arm rest is vertically formed by connecting by the first transverse arm A and the first vertical arm A, and the first transverse arm A and the first vertical arm A of the 5th right angle arm rest exist
There is corner portion A, the corner portion A of two the 5th right angle arm rests to all have the 5th welding notch, two the 5th straight at link position
5th welding notch of angle arm rest, which is matched, is combined into the 5th welding post hole (51)；The 6th right angle arm rest group (6) is by two
Six right angle arm rests are mutually perpendicular to be fixedly welded, and the 6th right angle arm rest is vertically connected by the first transverse arm B and the first vertical arm B
It forms, the first transverse arm B and the first vertical arm B of the 6th right angle arm rest have corner portion B at link position, and two the 6th right angles lean on
The corner portion B of arm all has the 6th welding notch, and the 6th welding notch of two the 6th right angle arm rests is welded with being combined into the 6th
Station hole (61).
2. a kind of welding positioning mold for aviation compressor structural framing welding processing described in accordance with the claim 1,
It is characterized in that: the one end of the 5th right angle arm rest group (5) transverse direction far from the 5th welding post hole (51) and the second right angle
Arm rest group (2) screw thread detachable connection, the 6th right angle arm rest group (6) transverse direction is far from the 6th welding post hole (61)
One end and third right angle arm rest group (3) screw thread detachable connection.
3. a kind of welding positioning mold for aviation compressor structural framing welding processing according to claim 1 or 2,
It is characterized by: being placed with cubic posting (9) at the top of the cuboid framework, the four directions posting (9), which has, successively to be had
There are first jiao, second jiao, the third angle and fourth angle, first jiao of cooperation of the four directions posting (9) is placed in the first right angle and leans on
At the top of arm group (1) and it is corresponding be located at the first positioning plate (10) bottom, second jiao of cooperation of the four directions posting (9) is placed in the
It is at the top of two right angle arm rest groups (2) and corresponding positioned at the second positioning plate (12) bottom, the third angle cooperation of the four directions posting (9)
Be placed at the top of third right angle arm rest group (3) and it is corresponding be located at third positioning plate (13) bottom, the of the four directions posting (9)
Quadrangular fit, which is placed at the top of the 4th right angle arm rest group (4) and corresponds to, is located at the 4th positioning plate (14) bottom.
4. a kind of welding positioning mold for aviation compressor structural framing welding processing according to claim 1 or 2,
It is characterized by: the first right angle arm rest of the first right angle arm rest group (1) is provided with several positioning spiral shells along its length direction
The second right angle arm rest of hole A, the second right angle arm rest group (2) are provided with several positioning screw holes B along its length direction, described
The third right angle arm rest of third right angle arm rest group (3) is provided with several positioning screw holes C, the 4th right angle along its length direction
4th right angle arm rest of arm rest group (4) is provided with several positioning screw holes D, the 5th right angle arm rest group along its length direction
(5) the first transverse arm A and the first vertical arm A is provided with several positioning screw holes E respectively along its length direction, and the 6th right angle leans on
The the first transverse arm B and the first vertical arm B of arm group (6) are provided with several positioning screw holes F respectively along its length direction.
5. a kind of welding positioning mold for aviation compressor structural framing welding processing described in accordance with the claim 1,
Be characterized in that: the 5th right angle arm rest group (5) bottom outside and the 6th right angle arm rest group (6) bottom outside are fixed with first and determine
Position riser (7).
6. a kind of welding positioning mold for aviation compressor structural framing welding processing according to claim 5,
Be characterized in that: first positioning riser (7) bottom is fixed with the first positioning bearing soleplate (8).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822041468.1U CN209335007U (en) | 2018-12-06 | 2018-12-06 | A kind of welding positioning mold for aviation compressor structural framing welding processing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822041468.1U CN209335007U (en) | 2018-12-06 | 2018-12-06 | A kind of welding positioning mold for aviation compressor structural framing welding processing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209335007U true CN209335007U (en) | 2019-09-03 |
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ID=67756270
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201822041468.1U Active CN209335007U (en) | 2018-12-06 | 2018-12-06 | A kind of welding positioning mold for aviation compressor structural framing welding processing |
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| Country | Link |
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| CN (1) | CN209335007U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114161033A (en) * | 2021-11-12 | 2022-03-11 | 鑫磊压缩机股份有限公司 | Welding equipment and welding method for underframe of screw machine |
-
2018
- 2018-12-06 CN CN201822041468.1U patent/CN209335007U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114161033A (en) * | 2021-11-12 | 2022-03-11 | 鑫磊压缩机股份有限公司 | Welding equipment and welding method for underframe of screw machine |
| CN114161033B (en) * | 2021-11-12 | 2024-06-04 | 鑫磊压缩机股份有限公司 | Welding equipment and welding method for screw machine underframe |
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