CN213945476U - Spot welding fixture for airplane parts - Google Patents
Spot welding fixture for airplane parts Download PDFInfo
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- CN213945476U CN213945476U CN202023092314.9U CN202023092314U CN213945476U CN 213945476 U CN213945476 U CN 213945476U CN 202023092314 U CN202023092314 U CN 202023092314U CN 213945476 U CN213945476 U CN 213945476U
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Abstract
The utility model discloses an aircraft part spot welding jig, comprising a base plate, the top left and right sides difference fixedly connected with main flange locating component and the main joint locating component of bottom plate, both sides difference fixedly connected with CP connects locating component and vice flange locating component around the top of bottom plate, a plurality of location support assembly of top fixedly connected with of bottom plate. The utility model discloses in, fix one of them aircraft part through location supporting component, main flange locating component and joint locating component, fix another aircraft part through location supporting component, vice flange locating component and main joint locating component to two aircraft part welded stability have been promoted.
Description
Technical Field
The utility model relates to an aircraft part welding subassembly technical field especially relates to an aircraft part spot welding jig.
Background
In order to guarantee the requirements of coordination of aircraft part assembly and accuracy of appearance, the precision of aircraft part welding needs to be guaranteed, the traditional aircraft part welding still needs to be manually controlled, shaking during welding can exist, the welding precision is not up to standard, and the welding convenience is poor.
SUMMERY OF THE UTILITY MODEL
The utility model aims to provide a: in order to solve the problems, the invention provides an aircraft part spot welding clamp.
In order to achieve the above purpose, the utility model adopts the following technical scheme:
the utility model provides an aircraft part spot welding jig, includes the bottom plate, the top left and right sides of bottom plate is fixedly connected with owner flange locating component and main joint locating component respectively, both sides are fixedly connected with CP respectively around the top of bottom plate and connect locating component and vice flange locating component, a plurality of location support assembly of top fixedly connected with of bottom plate.
As a further description of the above technical solution:
main flange locating component includes that first locating sleeve, first locating slide post, first fixing bolt, main tributary fagging, main nut, main screw rod, main clamp are detained and main fixing bolt constitute, first locating sleeve fixes the top at the bottom plate, first locating slide post slides even in first locating sleeve's inboard, first locating sleeve's outside sliding connection has the first fixing bolt that is used for first locating slide post to fix, the side end face fixedly connected with main tributary fagging of first locating slide post, a plurality of main fixing bolt of ring equidistance fixedly connected with are personally submitted to the side of main tributary fagging, ring equidistance sliding connection has a plurality of main screw rods to the side of main tributary fagging, the outer terminal surface fixedly connected with main clamp of main screw rod is detained, the outside of main screw rod is connected with main nut through the screw thread closure soon.
As a further description of the above technical solution:
the CP joint positioning assembly is composed of a second positioning sleeve, a second positioning sliding column, a second fixing bolt and a CP joint positioning supporting plate, the second positioning sleeve is fixed above the bottom plate, the second positioning sliding column is connected to the inner side of the second positioning sleeve in a sliding mode, the second fixing bolt used for fixing the second positioning sliding column is connected to the outer portion of the second positioning sleeve in a sliding mode, and the CP joint positioning supporting plate is fixedly connected to the side end face of the second positioning sliding column.
As a further description of the above technical solution:
the auxiliary flange positioning assembly comprises a third positioning sleeve, a third positioning sliding column, a third fixing bolt, an auxiliary support plate, an auxiliary nut, an auxiliary screw rod, an auxiliary clamping buckle and an auxiliary fixing bolt, the third positioning sleeve is fixed above the bottom plate, the third positioning sliding column is connected to the inner side of the third positioning sleeve in a sliding mode, the third fixing bolt used for fixing the third positioning sliding column is connected to the outer portion of the third positioning sleeve in a sliding mode, the auxiliary support plate is fixedly connected to the side end face of the third positioning sliding column, a plurality of auxiliary fixing bolts are fixedly connected to the side end face of the auxiliary support plate, a plurality of auxiliary screw rods are connected to the side end face of the auxiliary support plate in a sliding mode, the auxiliary clamping buckle is fixedly connected to the outer end face of each auxiliary screw rod, and the auxiliary nut is connected to the outer portion of each auxiliary screw rod in a threaded screwing mode.
As a further description of the above technical solution:
the main joint positioning assembly is composed of a fourth positioning sleeve, a fourth positioning sliding column, a fourth fixing bolt and a main joint positioning supporting plate, the fourth positioning sleeve is fixed above the bottom plate, the fourth positioning sliding column is slidably connected to the inner side of the fourth positioning sleeve, the outer portion of the fourth positioning sleeve is slidably connected with the fourth fixing bolt used for fixing the fourth positioning sliding column, and the side end face of the fourth positioning sliding column is fixedly connected with the main joint positioning supporting plate.
As a further description of the above technical solution:
the top of the positioning support component is of a concave structure.
To sum up, owing to adopted above-mentioned technical scheme, the beneficial effects of the utility model are that: one of the aircraft parts is fixed through the positioning support component, the main flange positioning component and the joint positioning component, and the other aircraft part is fixed through the positioning support component, the auxiliary flange positioning component and the main joint positioning component, so that the stability of welding the two aircraft parts is improved.
Drawings
Fig. 1 shows a schematic front view according to the invention;
fig. 2 shows a schematic top view according to the present invention;
fig. 3 shows a schematic side view according to the invention;
fig. 4 is a schematic front view of a main flange positioning assembly according to an embodiment of the present invention;
fig. 5 is a schematic front view of a main joint positioning assembly according to an embodiment of the present invention;
fig. 6 is a schematic top view of a CP joint positioning assembly according to an embodiment of the present invention;
fig. 7 is a schematic top view of a secondary flange positioning assembly provided in accordance with an embodiment of the present invention;
fig. 8 shows a schematic side view of a positioning support assembly according to an embodiment of the present invention.
Illustration of the drawings:
1. a base plate; 2. a primary flange positioning assembly; 201. a first positioning sleeve; 202. a first positioning strut; 203. a first fixed bolt; 204. a main supporting plate; 205. a main nut; 206. a main screw; 207. a main clamping buckle; 208. a main fixed bolt; 3. positioning the support assembly; 4. a CP connector positioning assembly; 401. a second positioning sleeve; 402. a second positioning strut; 403. a second fixing bolt; 404. a CP joint positioning supporting plate; 5. a secondary flange positioning assembly; 501. a third positioning sleeve; 502. a third positioning strut; 503. a third fixed bolt; 504. a sub-support plate; 505. a secondary nut; 506. an auxiliary screw; 507. the auxiliary clamping buckle; 508. a secondary fixing bolt; 6. a primary joint positioning assembly; 601. a fourth positioning sleeve; 602. a fourth positioning strut; 603. a fourth fixing bolt; 604. the main joint positions the fagging.
Detailed Description
In order to make the objects, technical solutions and advantages of the embodiments of the present invention clearer, the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are some, but not all, embodiments of the present invention. The components of embodiments of the present invention, as generally described and illustrated in the figures herein, may be arranged and designed in a wide variety of different configurations. Thus, the following detailed description of the embodiments of the present invention, presented in the accompanying drawings, is not intended to limit the scope of the invention, as claimed, but is merely representative of selected embodiments of the invention. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative efforts belong to the protection scope of the present invention.
In the description of the present invention, it should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplification of description, but do not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first," "second," and "third" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.
In the description of the present invention, it should also be noted that, unless otherwise explicitly specified or limited, the terms "disposed," "mounted," "connected," and "connected" are to be construed broadly, e.g., as meaning either a fixed connection, a removable connection, or an integral connection; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood according to specific situations by those skilled in the art.
Referring to fig. 1-8, the present invention provides a technical solution: a spot welding fixture for airplane parts comprises a bottom plate 1, wherein the left side and the right side of the top of the bottom plate 1 are respectively and fixedly connected with a main flange positioning component 2 and a main joint positioning component 6, the front side and the rear side of the top of the bottom plate 1 are respectively and fixedly connected with a CP joint positioning component 4 and an auxiliary flange positioning component 5, the top of the bottom plate 1 is fixedly connected with a plurality of positioning and supporting components 3, the positioning and supporting components 3 are used for primarily supporting and stabilizing the airplane parts, the flange plates of the two airplane parts are fixed through the main flange positioning component 2 and the auxiliary flange positioning component 5, the joint of the two airplane parts is fixed through the CP joint positioning component 4 and the main joint positioning component 6, thereby stabilize two aircraft parts and fix at the top of location supporting component 3, through stabilizing two aircraft parts and fixing, thereby promoted the welded convenience.
Specifically, as shown in fig. 4-8, the main flange positioning assembly 2 includes a first positioning sleeve 201, a first positioning sliding column 202, a first fixing pin 203, a main supporting plate 204, a main nut 205, a main screw 206, a main clamping buckle 207 and a main fixing pin 208, the first positioning sleeve 201 is fixed above the bottom plate 1, the first positioning sliding column 202 is slidably connected to the inner side of the first positioning sleeve 201, the first fixing pin 203 for fixing the first positioning sliding column 202 is slidably connected to the outside of the first positioning sleeve 201, the main supporting plate 204 is fixedly connected to the side end surface of the first positioning sliding column 202, the plurality of main fixing pins 208 are fixedly connected to the side end surface of the main supporting plate 204 at equal intervals in a ring shape, the plurality of main screws 206 are slidably connected to the side end surface of the main screw 204 at equal intervals in a ring shape, the main clamping buckle 207 is fixedly connected to the outer end surface of the main screw 206, the main nut 205 is rotatably connected to the outside of the main screw 206 by a screw thread, the CP joint positioning assembly 4 is composed of a second positioning sleeve 401, a second positioning sliding column 402, a second fixing bolt 403 and a CP joint positioning support plate 404, the second positioning sleeve 401 is fixed above the bottom plate 1, the second positioning sliding column 402 is slidably connected to the inner side of the second positioning sleeve 401, the second fixing bolt 403 for fixing the second positioning sliding column 402 is slidably connected to the outside of the second positioning sleeve 401, the CP joint positioning support plate 404 is fixedly connected to the side end surface of the second positioning sliding column 402, the sub-flange positioning assembly 5 includes a third positioning sleeve 501, a third positioning sliding column 502, a third fixing bolt 503, a sub-support plate 504, a sub-nut 505, a sub-screw 506, a sub-clamping buckle 507 and a sub-fixing bolt 508, the third positioning sleeve 501 is fixed above the bottom plate 1, the third positioning sliding column 502 is slidably connected to the inner side of the third positioning sleeve 501, and the third fixing bolt 503 for fixing the third positioning sliding column 502 is slidably connected to the outside of the third positioning sleeve 501, an auxiliary support plate 504 is fixedly connected to the side end surface of the third positioning sliding column 502, a plurality of auxiliary fixing bolts 508 are fixedly connected to the side end surface of the auxiliary support plate 504, a plurality of auxiliary screws 506 are slidably connected to the side end surface of the auxiliary support plate 504, an auxiliary clamping buckle 507 is fixedly connected to the outer end surface of the auxiliary screws 506, an auxiliary nut 505 is rotatably connected to the outer portion of the auxiliary screws 506 through threads, a main joint positioning assembly 6 is composed of a fourth positioning sleeve 601, a fourth positioning sliding column 602, a fourth fixing bolt 603 and a main joint positioning support plate 604, the fourth positioning sleeve 601 is fixed above the bottom plate 1, the fourth positioning sliding column 602 is slidably connected to the inner side of the fourth positioning sleeve 601, a fourth fixing bolt 603 used for fixing the fourth positioning sliding column 602 is slidably connected to the outer portion of the fourth positioning sleeve 601, a main joint positioning support plate 604 is fixedly connected to the side end surface of the fourth positioning sliding column 602, and the top of the positioning support assembly 3 is of an inward concave structure, when the first positioning sliding column 202 slides to the inner side of the first positioning sleeve 201, the first positioning sliding column 202 is fixed through the first fixing bolt 203, the second positioning sliding column 402, the third positioning sliding column 502 and the fourth positioning sliding column 602 are fixed in the same way as the first positioning sliding column 202, when the main flange positioning component 2 fixes the flange of the airplane part, the main fixing bolt 208 is aligned with the flange hole of the airplane part, the main clamping buckle 207 rotates to the flange by rotating the main screw 206, the main clamping buckle 207 is tightened, the main nut 205 is rotated, the main clamping buckle 207 is clamped with the flange of the airplane part, so that the flange of the airplane part is stably fixed, the auxiliary flange positioning component 5 fixes the airplane part in the same way as the main flange positioning component 2, when the CP joint positioning component 4 is fixed with the joint of the airplane part, the joint of the airplane part is placed above the positioning support component 3, through sliding second location traveller 402 for CP connects location fagging 404 to slide to the inboard that aircraft part connects, connect location fagging 404 to fix second location traveller 402 and CP through second fixing bolt 403, main joint locating component 6 fixes aircraft part's joint department, connect locating component 3 through location supporting component, main flange locating component 2 and CP and fix one of them aircraft part, connect locating component 4 through location supporting component 3, vice flange locating component 5 and main joint locating component 6 to fix another aircraft part, thereby two aircraft part welded stability have been promoted.
The above, only be the concrete implementation of the preferred embodiment of the present invention, but the protection scope of the present invention is not limited thereto, and any person skilled in the art is in the technical scope of the present invention, according to the technical solution of the present invention and the utility model, the concept of which is equivalent to replace or change, should be covered within the protection scope of the present invention.
Claims (5)
1. The utility model provides an aircraft part spot welding jig, includes bottom plate (1), its characterized in that, the top left and right sides difference fixedly connected with owner flange locating component (2) and main joint locating component (6) of bottom plate (1), both sides difference fixedly connected with CP connects locating component (4) and vice flange locating component (5) around the top of bottom plate (1), a plurality of location supporting component (3) of top fixedly connected with of bottom plate (1).
2. The aircraft part spot welding fixture according to claim 1, wherein the main flange positioning assembly (2) comprises a first positioning sleeve (201), a first positioning sliding column (202), a first fixing bolt (203), a main supporting plate (204), a main nut (205), a main screw (206), a main clamping buckle (207) and a main fixing bolt (208), the first positioning sleeve (201) is fixed above the bottom plate (1), the first positioning sliding column (202) is slidably connected to the inner side of the first positioning sleeve (201), the first fixing bolt (203) for fixing the first positioning sliding column (202) is slidably connected to the outer portion of the first positioning sleeve (201), the main supporting plate (204) is fixedly connected to the side end surface of the first positioning sliding column (202), the main supporting plate (204) is fixedly connected to the side end surface of the main supporting plate (204), and a plurality of main fixing bolts (208) are fixedly connected to the main supporting plate (204) at equal intervals in a ring shape, the side end face of the main supporting plate (204) is in annular equidistant sliding connection with a plurality of main screw rods (206), the outer end face of each main screw rod (206) is fixedly connected with a main clamping buckle (207), and the outer portion of each main screw rod (206) is connected with a main nut (205) in a screwing mode through threads.
3. An aircraft part spot welding fixture according to claim 1, wherein the CP connector positioning assembly (4) is composed of a second positioning sleeve (401), a second positioning sliding column (402), a second fixing bolt (403) and a CP connector positioning support plate (404), the second positioning sleeve (401) is fixed above the bottom plate (1), the second positioning sliding column (402) is slidably connected to the inner side of the second positioning sleeve (401), the second fixing bolt (403) for fixing the second positioning sliding column (402) is slidably connected to the outer portion of the second positioning sleeve (401), and the CP connector positioning support plate (404) is fixedly connected to the side end face of the second positioning sliding column (402).
4. The spot welding fixture for the aircraft parts according to claim 1, wherein the secondary flange positioning assembly (5) comprises a third positioning sleeve (501), a third positioning sliding column (502), a third fixing bolt (503), a secondary support plate (504), a secondary nut (505), a secondary screw (506), a secondary clamping buckle (507) and a secondary fixing bolt (508), the third positioning sleeve (501) is fixed above the base plate (1), the third positioning sliding column (502) is slidably connected to the inner side of the third positioning sleeve (501), the third fixing bolt (503) for fixing the third positioning sliding column (502) is slidably connected to the outside of the third positioning sleeve (501), the secondary support plate (504) is fixedly connected to the side end face of the third positioning sliding column (502), and a plurality of secondary fixing bolts (508) are fixedly connected to the side end face of the secondary support plate (504), the side end face of the auxiliary support plate (504) is connected with a plurality of auxiliary screws (506) in a sliding mode, the outer end face of each auxiliary screw (506) is fixedly connected with an auxiliary clamping buckle (507), and the outer portion of each auxiliary screw (506) is connected with an auxiliary nut (505) in a screwing mode through threads.
5. An aircraft part spot welding fixture as claimed in claim 1, wherein the main joint positioning assembly (6) is composed of a fourth positioning sleeve (601), a fourth positioning sliding column (602), a fourth fixing pin (603) and a main joint positioning bracing plate (604), the fourth positioning sleeve (601) is fixed above the bottom plate (1), the fourth positioning sliding column (602) is slidably connected to the inner side of the fourth positioning sleeve (601), the fourth fixing pin (603) for fixing the fourth positioning sliding column (602) is slidably connected to the outer portion of the fourth positioning sleeve (601), and the main joint positioning bracing plate (604) is fixedly connected to the side end surface of the fourth positioning sliding column (602).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202023092314.9U CN213945476U (en) | 2020-12-21 | 2020-12-21 | Spot welding fixture for airplane parts |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202023092314.9U CN213945476U (en) | 2020-12-21 | 2020-12-21 | Spot welding fixture for airplane parts |
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| Publication Number | Publication Date |
|---|---|
| CN213945476U true CN213945476U (en) | 2021-08-13 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202023092314.9U Active CN213945476U (en) | 2020-12-21 | 2020-12-21 | Spot welding fixture for airplane parts |
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| CN (1) | CN213945476U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112548462A (en) * | 2020-12-21 | 2021-03-26 | 成都市鸿侠科技有限责任公司 | Spot welding fixture for airplane parts |
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2020
- 2020-12-21 CN CN202023092314.9U patent/CN213945476U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112548462A (en) * | 2020-12-21 | 2021-03-26 | 成都市鸿侠科技有限责任公司 | Spot welding fixture for airplane parts |
| CN112548462B (en) * | 2020-12-21 | 2024-07-19 | 成都市鸿侠科技有限责任公司 | Spot welding clamp for airplane parts |
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