CN103111782A - Welding tool used for cabin in multilayer abnormal shape structure - Google Patents
Welding tool used for cabin in multilayer abnormal shape structure Download PDFInfo
- Publication number
- CN103111782A CN103111782A CN2012104141156A CN201210414115A CN103111782A CN 103111782 A CN103111782 A CN 103111782A CN 2012104141156 A CN2012104141156 A CN 2012104141156A CN 201210414115 A CN201210414115 A CN 201210414115A CN 103111782 A CN103111782 A CN 103111782A
- Authority
- CN
- China
- Prior art keywords
- hole
- brace summer
- compression beam
- flange
- multilayer
- 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
Links
Images
Abstract
The invention discloses a welding tool used for a cabin in a multilayer abnormal shape structure. The welding tool comprises a front flange, snap rings, compressing devices, clamping plate positioning pins, a support beam, a pull rod, positioning blocks, a clamping plate, a fast dismantling plug, a rear flange, a base, a shape following compressing beam, an internally supporting tire, hook-shaped bolts, an upper compressing beam, a lower compressing beam and clamping shafts. The clamping shafts are respectively and fixedly connected with the front flange and the rear flange. The pull rod, the support beam and the shape following compressing beam are arranged between the front flange and the rear flange and are fixedly connected. The internally supporting tire is fixed with the front flange through bolts. The positioning blocks are fixed with the support beam through the clamping plate positioning pins. The snap rings are respectively and fixedly connected with the support beam and the shape following compressing beam through bolts. The clamping plate, the upper compressing beam and the lower compressing beam are respectively and fixedly connected with the support beam through bolts. The compressing devices are respectively arranged on the snap rings, the rear flange, the shape following compressing beam, the upper compressing beam and the lower compressing beam. The welding tool can meet requirements for welding of multilayer irregular shaped products, is accurate in positioning, and convenient to operate, and ensures quality of the products.
Description
Technical field
The present invention relates to welding tooling, be specifically related to a kind of welding tooling for multilayer abnormally-structured cabin body.
Background technology
Along with the product aerodynamic configuration becomes increasingly complex, progressively changed to irregular profile by regular profile, by single layer structure progressively to the progressively transformation of sandwich construction, connect mode according to traditional manual argon arc welding, welding tooling is too complicated, welding efficiency is low, when Product jointing, there is the welding location difficulty, there is no clear and definite reference for assembling, is out of shape the defectives such as wayward, more can't guarantee the welding quality of product.
If adopt vacuum electron beam welder to carry out the welding of product, and the power source of vacuum electron beam welder is the manipulator on workbench, and welding gun is fixed, realize the welding of product, need to be with soldered parts fixation on the manipulator of vacuum electron beam welder workbench, therefore complete the welding of product by manipulator with respect to the motion of welding gun, can't directly complete the welding to product, need a cover to be applicable to the welding tooling of the multilayer abnormally-structured cabin body of vacuum electron beam welder.
Summary of the invention
The objective of the invention is for the abnormally-structured section structure spare of multilayer, a kind of welding tooling that can utilize vacuum electron beam welder that multilayer abnormally-structured cabin body is welded is provided.Solve welding product and located fast, looked for fast the problem of benchmark, guaranteed simultaneously the quality of welding product.
Technical scheme of the present invention, a kind of welding tooling for multilayer abnormally-structured cabin body comprises forward flange, snap ring, compactor, clamp alignment pin, brace summer, pull bar, locating piece, clamp, Quick-release latch, rear flange, pedestal, conformal compression beam, interior support, hook bolt, upper compression beam, lower compression beam and clamping axle.
Described forward flange is disc, the center is provided with through hole, be evenly arranged 4 90 ° of scallop holes around central through hole, vertically the diameter both sides are evenly equipped with through hole around scallop hole, are used for the assembling pull bar, in level diameter both sides, through hole is arranged, be respectively used to assemble brace summer and conformal compression beam, at vertical diameter two ends, a lifting eye arranged respectively, below the level diameter, arc-shaped edges along 2 scallop holes is evenly distributed with through hole, is used for support in assembling;
described rear flange is the disk that a side has the raised annular frame, the disc centre position is provided with through hole, around central through hole, the inboard of ring frame has been evenly arranged 4 90 ° of scallop holes, slot is arranged on ring frame, fluted on the frame of slot one side, tapped through hole is arranged in groove, compactor is placed in one and is threaded, be evenly equipped with through hole on the disk in the ring frame outside and with around the forward flange scallop hole, vertically the uniform through hole in diameter both sides is corresponding coaxial, be used for the assembling pull bar, in level diameter bilateral symmetry, a pair of through hole and a pair of slotted hole are arranged, through hole is used for the assembling brace summer, slotted hole is used for assembling conformal compression beam, at vertical diameter two ends, a lifting eye is arranged respectively,
Described clamping axle is section " ten " oblique crank Z, on middle ledge, through hole is arranged, and the clamping axle is placed in respectively the through hole of forward flange and rear flange center, and is bolted;
Described pull bar is straight-bar, one end has screw thread, and fix with the forward flange screw thread, on other end side lever, pin-and-hole is arranged, pedestal is multidiameter shape, has counterbore, sidewall that symmetrical pin-and-hole is arranged on taper end, the taper end of pedestal is placed in the other end of pull bar by rear flange respectively the counterbore of the taper end of pedestal, the pin-and-hole that Quick-release latch is connected with pedestal by the pin-and-hole on the root pull bar connection that is fixed;
Described locating piece is that the trapezoidal single piece of some projections is arranged on cuboid, in recessed part, pin-and-hole is arranged, and is used for clamp alignment pin and brace summer and fixes;
described brace summer is section " work " font rectangular body spare, on crossbeam, lower plane has some through holes, be used for the installation of locating piece and hook bolt, there are some tapped through holes the brace summer left and right side, be used for the installation of compactor, the column part of brace summer two ends is screw rod, the up and down projection has through hole, brace summer is placed between forward flange and rear flange, and the screw rod at brace summer two ends is packed in forward flange and the corresponding through hole of rear flange, with the clamp alignment pin, brace summer two ends projection and forward flange and rear flange are positioned, then with nut, the screw rod of brace summer two ends and forward flange and rear flange are fixed,
Described conformal compression beam is straight-bar for half, half is the single piece of bent stick, there is screw thread at two ends, the straight-bar end is fixedly connected with by the slotted hole screw nut of rear flange level diameter below, crooked rod end is fixedly connected with by the circular hole screw nut of the below of the level diameter on forward flange, and some tapped through holes are arranged on bent stick, is used for installing compressor, one right angle boss is arranged in the middle of bent stick, be used for installing snap ring; The camber of bent stick is 5 °～20 ° of peak and horizontal sextant angles;
Described snap ring is the semicircle annular, and there is through hole at two ends, and are fixedly connected with conformal compression beam bolt, are evenly distributed with some tapped through holes on it, is used for installing compressor;
Described clamp is the circular arc plate, and there is through hole at two ends, and is fixedly connected with the brace summer bolt;
Described hook bolt is " L " shape, and an end has screw thread, is fixedly connected with brace summer with forward flange respectively, is mainly used in the applying of product and frock;
Described upper compression beam and lower compression beam are " several " font, and there is through hole at the angle, two ends, and are fixedly connected with the brace summer bolt respectively, and some tapped through holes are arranged on intermediate transverse girder, are used for installing compressor, wherein descend the crossbeam of compression beam longer than the crossbeam of upper compression beam;
Described interior support is section " L " shape, and there is through hole the side, and spill weldering bakie is arranged at the bottom, and interior support is fixedly connected with circular hole bolt, the nut on forward flange scallop hole limit by its through hole.
The invention has the beneficial effects as follows: realize the fixed frame of soldered product by using forward flange, rear flange, conformal compression beam, pull bar and brace summer, by the location that interior support, upper compression beam, lower compression beam, snap ring and clamp are realized soldered product, compactor is realized the fastening of soldered product.This frock can satisfy the welding of multilayer, irregular profile product, and accurate positioning is easy to operate, has guaranteed the quality of product.
Description of drawings
Fig. 1 is a kind of welding tooling structural representation for multilayer abnormally-structured cabin body;
Fig. 2 is a kind of welding tooling endothecium structure Welding Structure schematic diagram for multilayer abnormally-structured cabin body;
Fig. 3 is a kind of welding tooling layer structure Welding Structure schematic diagram for multilayer abnormally-structured cabin body;
Fig. 4 is a kind of welding tooling forward flange structural representation for multilayer abnormally-structured cabin body;
Fig. 5 is a kind of welding tooling rear flange front view for multilayer abnormally-structured cabin body;
Fig. 6 is a kind of welding tooling rear flange structural representation for multilayer abnormally-structured cabin body;
Fig. 7 is a kind of welding tooling clamp locating pin structure schematic diagram for multilayer abnormally-structured cabin body;
Fig. 8 is a kind of welding tooling clamping axle construction schematic diagram for multilayer abnormally-structured cabin body;
Fig. 9 is a kind of welding tooling pull bar and pedestal connection diagram for multilayer abnormally-structured cabin body;
Figure 10 is a kind of welding tooling positioning block structure schematic diagram for multilayer abnormally-structured cabin body;
Figure 11 is a kind of welding tooling support beam structure schematic diagram for multilayer abnormally-structured cabin body;
Figure 12 is a kind of welding tooling conformal compression beam structural representation for multilayer abnormally-structured cabin body;
Figure 13 is a kind of welding tooling Snap ring structure schematic diagram for multilayer abnormally-structured cabin body;
Figure 14 is a kind of welding tooling clamp structure schematic diagram for multilayer abnormally-structured cabin body;
Figure 15 is a kind of welding tooling hook bolt structural representation for multilayer abnormally-structured cabin body;
Figure 16 is a kind of for compression beam structural representation on the welding tooling of multilayer abnormally-structured cabin body;
Figure 17 is a kind of for compressing the girder construction schematic diagram under the welding tooling of multilayer abnormally-structured cabin body;
Figure 18 is a kind of for support structural representation in the welding tooling of multilayer abnormally-structured cabin body.
In figure: 1. 16. times compression beam of compression beam, 17. clamping axles on forward flange 2. snap ring 3. compactor 4. clamp alignment pin 5. brace summer 6. pull bar 7. locating piece 8. clamp 9. Quick-release latch 10. rear flange 11. pedestal 12. interior support 14. hook bolts 15. of conformal compression beam 13.
The specific embodiment
The present invention will be further described below in conjunction with drawings and Examples.
As Fig. 1, Fig. 2, shown in Figure 3, a kind of welding tooling for abnormally-structured cabin body comprises forward flange 1, snap ring 2, compactor 3, clamp alignment pin 4, brace summer 5, pull bar 6, locating piece 7, clamp 8, Quick-release latch 9, rear flange 10, pedestal 11, conformal compression beam 12, interior support 13, hook bolt 14, upper compression beam 15, lower compression beam 16 and clamping axle 17.
As shown in Figure 4, forward flange 1 is disc, the center is provided with through hole, be used for assembling clamping axle 17,4 90 ° of scallop holes have been evenly arranged around central through hole, vertically the diameter both sides are evenly equipped with 4 through holes around scallop hole, be used for assembling pull bar 6, in level diameter both sides, 2 pairs of through holes are arranged, be respectively used to assemble brace summer 5 and conformal compression beam 12, at vertical diameter two ends, a lifting eye arranged respectively, below the level diameter, arc-shaped edges along 2 scallop holes is evenly distributed with 5 pairs of through holes, support 13 in being used for installing;
as Fig. 5, shown in Figure 6, rear flange 10 is the disk that a side has the raised annular frame, the disc centre position is provided with through hole, be used for assembling clamping axle 17, around central through hole, the inboard of ring frame has been evenly arranged 4 90 ° of scallop holes, 4 slots are evenly arranged on ring frame, fluted on the frame of slot one side, tapped through hole is arranged in groove, compactor 3 is placed in one, be evenly equipped with 4 through holes on the disk in the ring frame outside, be used for assembling pull bar 6, in level diameter bilateral symmetry, a pair of through hole and a pair of slotted hole are arranged, circular hole is used for assembling brace summer 5, slotted hole is used for assembling conformal compression beam 12, at vertical diameter two ends, a lifting eye is arranged respectively,
As shown in Figure 7, clamp alignment pin 4 is " L " shape;
As shown in Figure 8, clamping axle 17 is section " ten " oblique crank Z, on middle ledge, through hole is arranged, and 2 clamping axles 17 are placed in respectively the through hole of forward flange 1 and rear flange 10 centers, are bolted;
As shown in Figure 9, four pull bars 6 are straight-bar, one end has screw thread, and fix with forward flange 1 screw thread, on other end side lever, pin-and-hole being arranged, pedestal 11 is multidiameter shape, counterbore is arranged on taper end, sidewall has symmetrical pin-and-hole, and the taper end of pedestal 11 is placed in the other end of pull bar 6 by rear flange 10 respectively the counterbore of the taper end of pedestal 11, and Quick-release latch 9 is by the connection that is fixed of the pin-and-hole on root pull bar 6 and pin-and-hole on pedestal is connected;
As shown in figure 10, locating piece 7 has the trapezoidal single piece of some projections on cuboid, in recessed part, pin-and-hole is arranged, and is used for clamp alignment pin 4 fixing with brace summer 5;
as shown in figure 11, two brace summers 5 are section " work " font rectangular body spare, on crossbeam, lower plane has some through holes, be used for the installation of locating piece 7 and hook bolt 14, there are some tapped through holes the crossbeam left and right side, be used for the installation of compactor 3, the column part of brace summer 5 two ends is screw rod, the up and down projection has through hole, brace summer 5 is placed between forward flange 1 and rear flange 10, and the screw rod at brace summer 5 two ends is packed in forward flange 1 and the corresponding through hole of rear flange 10, with clamp alignment pin 4, brace summer 5 two ends projections and forward flange 1 and rear flange 10 are positioned, then with nut, the screw rod of brace summer 5 two ends and forward flange 1 and rear flange 10 are fixed,
As shown in figure 12,2 conformal compression beam 12 are straight-bar for half, half is the single piece of bent stick, there is screw thread at two ends, and the straight-bar end is fixedly connected with by the slotted hole screw nut below rear flange 10 level diameters, and crooked rod end is fixedly connected with by the circular hole screw nut of the below of the level diameter on forward flange 1, some tapped through holes are arranged on bent stick, be used for installing compressor 3, a right angle boss is arranged in the middle of bent stick, be used for installing snap ring 2; The camber of bent stick is 5 °～20 ° of peak and horizontal sextant angles;
As shown in figure 13, snap ring 2 is the semicircle annular, and there is through hole at two ends, and are fixedly connected with conformal compression beam 12 bolts respectively, are evenly distributed with some tapped through holes on ring, are used for installing compressor 3;
As shown in figure 14, clamp 8 is the circular arc plate, and there is through hole at two ends, and is fixedly connected with brace summer 5 bolts respectively;
As shown in figure 15, hook bolt 14 is " L " shape, and an end has screw thread, is fixedly connected with brace summer 5 with forward flange 1 respectively, is mainly used in the applying of product and frock;
As shown in figure 16, a upper compression beam 15 is " several " font, and there is through hole at the angle, two ends, and is fixedly connected with brace summer 5 bolts respectively, and some through holes are arranged on intermediate transverse girder, is used for installing compressor 3;
Shown in Figure 17, a lower compression beam 16 is " several " font, and there is through hole at the angle, two ends, and is fixedly connected with brace summer 5 bolts respectively, and some through holes are arranged on intermediate transverse girder, is used for installing compressor 3, wherein descends the crossbeam of compression beam 16 longer than the crossbeam of upper compression beam 15;
As shown in figure 18,5 interior supports 13 are section " L " shape, and there is through hole the side, and spill weldering bakie is arranged at the bottom, and interior support 13 is fixedly connected with by 5 pairs of circular hole bolts on its through hole and forward flange 1 scallop hole limit.
The course of work:
At first carry out the welding of product endothecium structure, as shown in Figure 2, clamping axle 17 first is installed on forward flange 1 and rear flange 10 respectively, and is fixed with bolt; Two symmetrical brace summers 5 are connected with rear flange with forward flange 1 respectively with nut with clamp alignment pin 4 and are connected, with clamp alignment pin 4 and bolt, two locating pieces 7 are arranged on respectively on brace summer 5, when soldered product is planar profile, can uneasyly fill locating piece 7, when soldered product is the inclined-plane profile, locating piece 7 just is installed, and is utilized the trapezoidal inclined plane location on locating piece 7; Soldered product is placed on locating piece 7, is positioned on forward flange 1 with clamp alignment pin 4 and hook bolt 14 front end with welding product; Position with rear end and the rear flange 10 of clamp alignment pin 4 with welding product, and axially hold out against with the compactor 3 on rear flange 10; Four pull bars 6 are arranged between forward flange 1 and rear flange 10, and the front end of railing 6 is fixing with nut and forward flange 1, and the rear end of pull bar 6 is fixed with rear flange 10 with Quick-release latch 9 and pedestal 11; Conformal compression beam 12 is arranged between forward flange 1 and rear flange 10, all adopts nut to fix; Snap ring 2 is installed on conformal compression beam 12, and with being arranged on compactor 3 on snap ring 2 with the bottom compression of welding product; With the hook bolt 14 that is arranged on left and right brace summer 5, the both sides of welding product are fixed, install compression beam 15 and lower compression beam 16 on brace summer 5, and the compactor 3 of using on compression beam 15 and lower compression beam 16 compresses the upper and lower profile of soldered product.So just complete the front installation of welding of soldered product endothecium structure, can carry out the welding of product.
After soldered product endothecium structure welding is completed, carry out again the welding of soldered product layer structure, on basis shown in Figure 2, first four pull bars 6 are pulled down between forward flange 1 and rear flange 10, be arranged on conformal compression beam 12 snap ring 2 and on compactor 3 pull down together; Upper compression beam 15 and lower compression beam 16 and corresponding compactor 3 are pulled down from brace summer 5, then begin the installation of soldered product layer structure, as shown in Figure 3, interior support 13 is arranged on forward flange 1, after the outer superstructure of product is in place, snap ring 2 is installed to the top of brace summer 5, connect with bolt, compress with 3 pairs of products of the compactor on snap ring 2, the top that clamp 8 is installed to brace summer 5 connects with bolt, and compresses product upper outer layer structure; With nut, are connected with rear flange with forward flange 1 respectively in the two ends of conformal compression beam 12 and are connected, with bolt, snap ring 2 is arranged on conformal compression beam 12, and with the compactor 3 on snap ring 2, product bottom layer structure is compressed, with the compactor 3 on conformal compression beam 12, product bottom layer structure is compressed, with bolt, clamp 8 is arranged on the below of brace summer 5, tightened bolt presses product bottom layer structure; With nut, Quick-release latch 9 and pedestal 11, four pull bars 6 are arranged between forward flange 1 and rear flange 10, install and all complete, can begin the welding of product layer structure.
After Product jointing is completed, by pulling out clamp alignment pin 4 and bolt, nut, pull down successively pull bar 6, snap ring 2, clamp 8, conformal compression beam 12 and compactor 3, the brace summer 5 of then dismantling is disassembled frock fully, takes out product, namely completes the welding fully of product.In the process of frock turnover or whole turnover electron-beam welder, adopt and carry out the running of frock with the lifting eye on forward flange and rear flange.
Claims (10)
1. a welding tooling that is used for multilayer abnormally-structured cabin body, is characterized in that, comprises forward flange (1), snap ring (2), compactor (3), clamp alignment pin (4), brace summer (5), pull bar (6), locating piece (7), clamp (8), Quick-release latch (9), rear flange (10), pedestal (11), conformal compression beam (12), interior support (13), hook bolt (14), upper compression beam (15), lower compression beam (16) and clamping axle (17), clamping axle (17) is fixedly connected with rear flange (10) with forward flange (1) by bolt respectively, brace summer (5) and conformal compression beam (12) are placed in respectively between forward flange (1) and rear flange (10), and be connected and fixed by screw nut, pull bar (6) is placed between forward flange (1) and rear flange (10), one end and forward flange (1) screw nut is connected and fixed, the other end is fixing by Quick-release latch (9) and pedestal (11), pedestal (11) is arranged in installing hole on rear flange (10), interior support (13) is fixed with forward flange (1) bolt, hook bolt (14) is arranged on forward flange (1) and brace summer (5), be connected and fixed by screw thread and nut, locating piece (7) is fixing by clamp alignment pin (4) with brace summer (5), snap ring (2) is fixedly connected with conformal compression beam (12) bolt with brace summer (5) respectively, clamp (8), upper compression beam (15) is fixedly connected with brace summer (5) bolt respectively with lower compression beam (16), and compactor (3) is installed on respectively snap ring (2), brace summer (5), rear flange (10), conformal compression beam (12), on upper compression beam (15) and lower compression beam (16).
2. a kind of welding tooling for multilayer abnormally-structured cabin body according to claim 1, it is characterized in that: described forward flange (1) is disc, the center is provided with through hole, be used for assembling clamping axle (17), 4 90 ° of scallop holes have been evenly arranged around central through hole, vertically the diameter both sides are evenly equipped with 4 through holes around scallop hole, be used for assembling pull bar (6), in horizontal diameter both sides, through hole is arranged, be respectively used to assemble brace summer (5) and conformal compression beam (12), at vertical diameter two ends, a lifting eye is arranged respectively, below horizontal diameter, arc-shaped edges along 2 scallop holes is evenly distributed with through hole, support (13) in being used for installing.
3. a kind of welding tooling for multilayer abnormally-structured cabin body according to claim 1, it is characterized in that: described rear flange (10) is the disk that a side has the raised annular frame, the disc centre position is provided with through hole, be used for assembling clamping axle (17), around central through hole, the inboard of ring frame has been evenly arranged 4 90 ° of scallop holes, slot is evenly arranged on ring frame, fluted on the frame of slot one side, tapped through hole is arranged in groove, compactor (3) is placed in one and is threaded, be evenly equipped with through hole on the disk in the ring frame outside, be used for assembling pull bar (6), in the horizontal diameter bilateral symmetry, a pair of through hole and a pair of slotted hole are arranged, circular hole is used for assembling brace summer (5), slotted hole is used for assembling conformal compression beam (12), at vertical diameter two ends, a lifting eye is arranged respectively.
4. a kind of welding tooling for multilayer abnormally-structured cabin body according to claim 1, it is characterized in that: described clamping axle (17) is section " ten " oblique crank Z, on middle ledge, through hole is arranged, clamping axle (17) is placed in respectively the through hole of forward flange (1) and rear flange (10) center, and is bolted.
5. a kind of welding tooling for multilayer abnormally-structured cabin body according to claim 1, it is characterized in that: described pull bar (6) is straight-bar, one end has screw thread, and fix with forward flange (1) screw thread, on other end side lever, pin-and-hole is arranged, pedestal (11) is multidiameter shape, counterbore is arranged on taper end, sidewall has symmetrical pin-and-hole, the taper end of pedestal (11) is placed in the other end of pull bar (6) by rear flange (10) respectively the counterbore of the taper end of pedestal (11), Quick-release latch (9) is fixedly connected with pull bar (6) with pin-and-hole on pedestal (11) by the pin-and-hole on root pull bar (6).
6. a kind of welding tooling for multilayer abnormally-structured cabin body according to claim 1, it is characterized in that: described brace summer (5) is section " work " font rectangular body spare, on crossbeam, lower plane has some through holes, be used for the installation of locating piece (7) and hook bolt (14), there are some tapped through holes the crossbeam left and right side, be used for the installation of compactor (3), the column part of brace summer (5) two ends is screw rod, the up and down projection has through hole, brace summer (5) is placed between forward flange (1) and rear flange (10), and the screw rod at brace summer (5) two ends is packed in forward flange (1) and the corresponding through hole of rear flange (10), with clamp alignment pin (4), brace summer (5) two ends projection and forward flange (1) and rear flange (10) are positioned, then with nut, the screw rod of brace summer (5) two ends and forward flange (1) and rear flange (10) are fixed.
7. a kind of welding tooling for multilayer abnormally-structured cabin body according to claim 1, it is characterized in that: described conformal compression beam (12) is straight-bar for half, half is the single piece of bent stick, there is screw thread at two ends, the straight-bar end is fixedly connected with by the slotted hole screw nut of rear flange (10) level diameter below, crooked rod end is fixedly connected with by the circular hole screw nut of the below of the horizontal diameter on forward flange (1), some tapped through holes are arranged on bent stick, and compactor (3) is placed in tapped through hole and is threaded, one right angle boss is arranged in the middle of bent stick, be used for installing snap ring (2).
8. a kind of welding tooling for multilayer abnormally-structured cabin body according to claim 1 is characterized in that: the camber of described conformal compression beam (12) bent stick is 5 °～20 ° of peak and horizontal sextant angles.
9. a kind of welding tooling for multilayer abnormally-structured cabin body according to claim 1, it is characterized in that: upper compression beam (15) and lower compression beam (16) are " several " font, there is through hole at the angle, two ends, and be fixedly connected with brace summer (5) bolt respectively, some tapped through holes are arranged on intermediate transverse girder, and compactor (3) is placed in tapped through hole and is threaded, and the crossbeam of lower compression beam (16) is grown up long in the crossbeam of upper compression beam (15).
10. a kind of welding tooling for multilayer abnormally-structured cabin body according to claim 1, it is characterized in that: locating piece (7) has the trapezoidal single piece of some projections on cuboid, in recessed part, pin-and-hole is arranged, be used for clamp alignment pin (4) fixing with brace summer (5).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210414115.6A CN103111782B (en) | 2012-10-26 | 2012-10-26 | Welding tool used for cabin in multilayer abnormal shape structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210414115.6A CN103111782B (en) | 2012-10-26 | 2012-10-26 | Welding tool used for cabin in multilayer abnormal shape structure |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN103111782A true CN103111782A (en) | 2013-05-22 |
| CN103111782B CN103111782B (en) | 2015-03-11 |
Family
ID=48410196
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201210414115.6A Active CN103111782B (en) | 2012-10-26 | 2012-10-26 | Welding tool used for cabin in multilayer abnormal shape structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103111782B (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107649815A (en) * | 2017-11-01 | 2018-02-02 | 辽宁忠旺特种车辆制造有限公司 | Doorframe welding frock and its peace tune method before a kind of right side |
| CN107900573A (en) * | 2017-12-28 | 2018-04-13 | 绵竹市鑫达机械加工有限责任公司 | A kind of vapour hair engine base welding tooling and the welding method using the frock |
| CN109093270A (en) * | 2018-11-05 | 2018-12-28 | 北京星航机电装备有限公司 | A kind of large size metal plate weldering cabin lid form fabrication device and method |
| CN110625242A (en) * | 2019-09-02 | 2019-12-31 | 北京星航机电装备有限公司 | Device and method for controlling welding deformation of ultra-long longitudinal weld by using electron beam |
| CN114310387A (en) * | 2021-12-21 | 2022-04-12 | 北京星航机电装备有限公司 | Horizontal machining tool and method for non-circular-section special-shaped cabin section |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110587231B (en) * | 2019-09-06 | 2021-03-05 | 北京星航机电装备有限公司 | Method for processing composite cabin body made of thermal protection material and metal material |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2253403A (en) * | 1939-02-04 | 1941-08-19 | Westinghouse Electric & Mfg Co | Welding apparatus |
| JP2002239778A (en) * | 2001-02-09 | 2002-08-28 | Mitsubishi Heavy Ind Ltd | Welding apparatus |
| US7241973B1 (en) * | 2001-07-17 | 2007-07-10 | Lincoln Global, Inc. | Welding accessory arrangement |
| CN101468430A (en) * | 2007-12-28 | 2009-07-01 | 中国科学院沈阳自动化研究所 | Novel laser welding and assembling clamp for GIS controlling cabinet |
| CN101628369A (en) * | 2009-08-06 | 2010-01-20 | 江苏辉能电气有限公司 | Rotating shaft welding fixture of drawer seat drive mechanism of low-voltage switch board |
| CN201664831U (en) * | 2010-03-11 | 2010-12-08 | 北京星航机电设备厂 | Curved surface heterotype cabin body welding tool |
| CN203109488U (en) * | 2012-10-26 | 2013-08-07 | 北京星航机电装备有限公司 | Welding fixture used for multilayer irregular structured cabin |
-
2012
- 2012-10-26 CN CN201210414115.6A patent/CN103111782B/en active Active
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2253403A (en) * | 1939-02-04 | 1941-08-19 | Westinghouse Electric & Mfg Co | Welding apparatus |
| JP2002239778A (en) * | 2001-02-09 | 2002-08-28 | Mitsubishi Heavy Ind Ltd | Welding apparatus |
| US7241973B1 (en) * | 2001-07-17 | 2007-07-10 | Lincoln Global, Inc. | Welding accessory arrangement |
| CN101468430A (en) * | 2007-12-28 | 2009-07-01 | 中国科学院沈阳自动化研究所 | Novel laser welding and assembling clamp for GIS controlling cabinet |
| CN101628369A (en) * | 2009-08-06 | 2010-01-20 | 江苏辉能电气有限公司 | Rotating shaft welding fixture of drawer seat drive mechanism of low-voltage switch board |
| CN201664831U (en) * | 2010-03-11 | 2010-12-08 | 北京星航机电设备厂 | Curved surface heterotype cabin body welding tool |
| CN203109488U (en) * | 2012-10-26 | 2013-08-07 | 北京星航机电装备有限公司 | Welding fixture used for multilayer irregular structured cabin |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107649815A (en) * | 2017-11-01 | 2018-02-02 | 辽宁忠旺特种车辆制造有限公司 | Doorframe welding frock and its peace tune method before a kind of right side |
| CN107900573A (en) * | 2017-12-28 | 2018-04-13 | 绵竹市鑫达机械加工有限责任公司 | A kind of vapour hair engine base welding tooling and the welding method using the frock |
| CN109093270A (en) * | 2018-11-05 | 2018-12-28 | 北京星航机电装备有限公司 | A kind of large size metal plate weldering cabin lid form fabrication device and method |
| CN110625242A (en) * | 2019-09-02 | 2019-12-31 | 北京星航机电装备有限公司 | Device and method for controlling welding deformation of ultra-long longitudinal weld by using electron beam |
| CN114310387A (en) * | 2021-12-21 | 2022-04-12 | 北京星航机电装备有限公司 | Horizontal machining tool and method for non-circular-section special-shaped cabin section |
Also Published As
| Publication number | Publication date |
|---|---|
| CN103111782B (en) | 2015-03-11 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN103111782B (en) | Welding tool used for cabin in multilayer abnormal shape structure | |
| CN103151550B (en) | Device for assembling laminated stacks | |
| CN203109488U (en) | Welding fixture used for multilayer irregular structured cabin | |
| CN201486156U (en) | Accurate adjustment device for adjusting gap between large-sized steel members | |
| CN205184145U (en) | Hook tail frame welding upset frock | |
| CN103111748B (en) | Welding tool for semicircular closed box body | |
| CN103128537B (en) | Vehicle body of railway vehicle assembling flexible technology device | |
| CN207344196U (en) | A kind of crossbeam fixture | |
| CN207873537U (en) | Cylinder group welds positioning device in a kind of fog gun | |
| CN203227961U (en) | Clamping device for welding of arm bodies | |
| CN215747492U (en) | Sieve case chassis welding frock with adjustable | |
| CN214350519U (en) | Gearbox housing shaft sleeve assembly welding frock | |
| CN205817145U (en) | One leads slow beam assembly welding fixture | |
| CN103934603A (en) | Installation trolley of flanges on large-caliber steel tube and application method of installation trolley | |
| CN208787838U (en) | Fuel tank cap puppet's mounted welder | |
| CN208894926U (en) | A kind of automobile crane horn body twist correcting device | |
| CN208409031U (en) | A kind of welding tooling of support unit | |
| CN202377769U (en) | Flexible process device for railway vehicle body assembly | |
| CN204780483U (en) | A frock that is used for on tub truss fixed interim structure | |
| CN205159814U (en) | Electrical equipment fixing device | |
| CN202461923U (en) | Bearing assembling device for vibrating screen | |
| CN204308481U (en) | Side bar overall group in telescopic excavator left and right is to mold | |
| CN204771335U (en) | Bicycle automobile body work piece welding set | |
| CN208840770U (en) | A kind of Frame Welding tooling | |
| CN220636896U (en) | Bearing dismounting device |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C53 | Correction of patent of invention or patent application | ||
| CB02 | Change of applicant information |
Address after: 100074 Fengtai District City, east of the north of Beijing, Wang Gang Road, No. 9 Applicant after: Beijing Xinghang Mechanical & Electric Equipment Co., Ltd. Address before: 100074 Fengtai District City, east of the north of Beijing, Wang Gang Road, No. 9 Applicant before: Beijing Xinghang Mechanical-Electrical Equipment Factory |
|
| COR | Change of bibliographic data |
Free format text: CORRECT: APPLICANT; FROM: BEIJING XINGHANG M+E EQUIPMENT FACTORY TO: BEIJING XINGHANG MECHANICAL + ELECTRIC EQUIPMENT CO., LTD. |
|
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CB03 | Change of inventor or designer information |
Inventor after: Dai Chai Shi Inventor after: Li Hepeng Inventor after: Li Chenbin Inventor after: Hu Xiaoyong Inventor before: Dai Chai Shi |
|
| CB03 | Change of inventor or designer information |