CN211968112U - Forming die for composite material of front beam of oblique beam - Google Patents
Forming die for composite material of front beam of oblique beam Download PDFInfo
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- CN211968112U CN211968112U CN202020210719.9U CN202020210719U CN211968112U CN 211968112 U CN211968112 U CN 211968112U CN 202020210719 U CN202020210719 U CN 202020210719U CN 211968112 U CN211968112 U CN 211968112U
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Abstract
The utility model relates to an oblique beam front-axle beam combined material forming die belongs to the aerospace field, including welding frame, welding frame upper surface is fixed with the template, and the template upper surface is equipped with the curb plate subassembly, and fixed surface is connected with piecemeal A, piecemeal B, locating piece A, locating piece B on the template. The utility model discloses use dummy assembly direct forming on the template curb plate subassembly, reduced curb plate subassembly's installation procedure, improved the assembly relation, improved the machining precision for the qualification rate of product rises.
Description
Technical Field
The utility model relates to an aerospace field, in particular to sloping front-beam composite forming die.
Background
The existing sloping beam front beam composite material is generally specially designed with one set of transition mold to form a composite baffle in the forming process, the composite baffle is assembled on the sloping beam front beam forming mold after being formed, and in the assembling process, installation errors are generated, so that the forming rate of the sloping beam front beam composite material is lower, meanwhile, one set of transition mold is specially designed, the number of used molds is increased, and the production cost is increased.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an oblique beam front-axle beam combined material forming die to solve the problem that proposes among the above-mentioned background art.
In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides an oblique beam front-axle beam combined material forming die, includes welding frame, welding frame upper surface fixed connection has the template, fixed surface is connected with the curb plate subassembly on the template, the peripheral laminating of curb plate subassembly has the dummy member subassembly, the template upper surface is equipped with piecemeal A, piecemeal B, locating piece A, locating piece B, piecemeal A bolted connection is on the template surface, piecemeal B bolted connection is on the template surface, locating piece A is fixed on the template upper surface by bulb round pin and socket head cap screw, locating piece B is fixed on the template upper surface by socket head cap screw, fixed surface is connected with jig board subassembly A, jig board subassembly B on the curb plate subassembly, the jig board is fixed on the template upper surface by the bulb round pin.
Furthermore, a dummy component is attached to the outer surface of the side plate component.
Further, the welding frame front surface is fixed with the frock data plate, and inside is honeycomb, and lower surface fixedly connected with a certain amount's pad foot.
Furthermore, the block A is square and is internally provided with two grooves, the positioning block A is limited by the grooves, and the positioning block A is fixed on the upper surface of the template by a ball pin and an inner hexagon screw.
Furthermore, the positioning block B is fixed on the upper surface of the template through a ball pin and an inner hexagon screw; the block B is attached to the clamping positioning block B close to the left side and attached to the clamping template close to the right side.
Furthermore, the left end of the drilling template component A is bent to be close to the surface of the template, and a drill bushing is arranged at the close end.
Furthermore, the right end of the drill jig plate component B is bent to be close to the surface of the template, and a drill bushing is arranged at the close end.
The utility model discloses a technological effect and advantage:
1. the utility model discloses a false subassembly comes shaping curb plate subassembly, saves original a set of mould, uses mould quantity to reduce, practices thrift the cost.
2. The utility model discloses a false subassembly comes shaping curb plate subassembly, and the curb plate subassembly no longer need install, has improved original assembly relation for the product percent of pass promotes.
Drawings
Fig. 1 is a schematic view of the overall structure of the present invention.
Fig. 2 is a side sectional view of the present invention.
Fig. 3 is a top view of the present invention.
Fig. 4 is an enlarged view of the position A of the present invention.
Fig. 5 is an enlarged view of the position B of the present invention.
Figure 6 is the drill plate pattern a of the present invention.
Figure 7 is the drilling template B of the present invention.
In the figure: 1. a template; 2. welding the frame; 3. a side plate assembly; 4. partitioning A; 5. positioning a block A; 6. a ball stud; 7. a socket head cap screw; 8. partitioning B; 9. positioning a block B; 10. Drilling a template assembly A; 11. drilling a template component B; 12. a tooling nameplate; 13. a dummy assembly; 14. and (4) drilling a sleeve.
Detailed Description
The technical solution in the embodiment of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiment of the present invention. It is to be understood that the embodiments described are only some embodiments of the invention, and not all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by a person of ordinary skill in the art without creative efforts belong to the protection scope of the present invention.
The utility model provides a sloping front beam combined material forming die as shown in fig. 1-7, including welding frame 2, 2 front surface fixedly connected with frock data plate 12 of welding frame, 2 upper surface fixedly connected with templates 1 of welding frame, 1 upper surface fixedly connected with locating piece B5 of template, locating piece B5 both ends embedding piecemeal A4 inboard recess, piecemeal A4 is the mouth style of calligraphy, and wherein both sides have seted up flutedly, template 1 upper surface is through bag pressure fixedly connected with curb plate assembly 3, curb plate assembly 3 is close to piecemeal A4 one side and is equipped with piecemeal B8, piecemeal B8 below is equipped with locating piece B9, locating piece B9 fixed connection is at template 1's upper surface.
More specifically, the interior of the welding frame 2 is honeycomb-shaped, a certain number of foot pads are fixedly connected to the lower surface of the welding frame, a positioning block A5 is fixed on the template 1 through a ball head pin 6 and an inner hexagon screw 7, the inner hexagon screws 7 are respectively located at the left end and the right end of the positioning block A5, the ball head pin 6 is respectively located at the left end and the right end of the positioning block A5, meanwhile, the inner hexagon screw 7 is arranged on the inner side of the template 1, a sub-block A4 is arranged on the upper surface of the template 1, the sub-block A4 is square, a groove is formed in the inner side surface of the sub-block A4, the positioning block A5 is fixedly connected to the upper surface of the template 1 and embedded in the groove of the sub-block A4 to limit the sub-block A4, a positioning block 387B 9 is fixedly connected to the upper surface of the template 1 through the inner hexagon screw 7 to limit the sub-block B, the effect of piecemeal A4 and piecemeal B8 makes the convenient drawing of patterns after the product shaping, bushing plate subassembly A10 is located the left end of curb plate subassembly 3, bushing plate subassembly B11 is located the right-hand member of curb plate subassembly 3, bushing plate subassembly both ends all have certain buckling, surround the product after the laminating shaping, the kink lower extreme is equipped with the through-hole, bushing plate subassembly relies on the bulb round pin 6 fixed connection who runs through the through-hole at template 1 upper surface, there is certain buckling in the middle of the bushing plate subassembly, the part of buckling is close to the product upper surface, drill bushing 14 has been seted up to the part of being close to, be convenient for drill it after the sloping front-sill combined material shaping, welding frame 2 is inside to be cellular, accelerate the product heat dissipation, make the product shaping faster, 9 are installed to the rubber pad to welding frame lower extreme equid.
When in use, firstly, the dummy component 13 is fixed on the upper surface of the shaping plate 1, the side component 3 is shaped, after the side plate component 3 is shaped, the dummy component 13 is removed, the side plate component 3 is fixed on the upper surface of the shaping plate 1 by bag making pressure, then the block A4 is placed, the positioning block A5 is placed in the groove at the inner side of the block A4, the block A4 is fixed on the upper surface of the shaping plate 1 by using a ball stud 6 and an inner hexagon screw, the block A4 is limited and positioned, the positioning block B9 is arranged at one side of the side plate component close to the block A4, the block B8 is similarly fixed by using the ball stud 6 and the inner hexagon screw 7, then the block B8 is placed above the positioning block B8, the side plate component 3 is attached to the left side, the positioning block 4 is attached to the right side, after the block B is installed, the product is injection-molded, after the product is shaped, the drilling component 3 is removed, then the side plate component A and the drilling plate component, after the position is determined, the ball stud 6 penetrates through a through hole in the position where the drilling template assembly is attached to the template 1, the same through hole is correspondingly formed in the template 1, the drilling template assembly A and the drilling template assembly B are fixed, then, according to the positioning of the drill bushing 14, the product is drilled, after the drilling is completed, the product is machined, then, the hexagon socket head screw 7 on the positioning block A5 is loosened, the ball stud 6 is taken down, the positioning block A5 is taken down, due to the arrangement of the block A4 and the block B8, the product is simpler to demould, the product is machined after being taken down, due to the fact that the dummy assembly 13 is arranged, the side plate assembly is directly formed on the template 1, the installation error is reduced, the assembly relation is improved, and the qualification rate of the product is greatly improved.
It will be apparent to those skilled in the art that changes and modifications may be made to the present invention without departing from the spirit and scope of the embodiments of the invention. Thus, if such modifications and variations of the embodiments of the present invention fall within the scope of the claims of the present invention and their equivalents, the present invention is also intended to include such modifications and variations.
Claims (7)
1. The utility model provides an oblique beam front-axle beam combined material forming die, includes welding frame (2), its characterized in that, welding frame (2) upper surface fixed connection has template (1), template (1) upper surface bolted connection has piecemeal A (4), template (1) upper surface is provided with locating piece A (5), template (1) surface bolted connection has piecemeal B (8), template (1) surface is provided with locating piece B (9), template (1) upper surface is provided with curb plate subassembly (3), template (1) upper surface pin joint has bushing plate subassembly A (10), bushing plate subassembly B (11).
2. The forming die for the composite material of the inclined beam and the front beam as claimed in claim 1, wherein: and a dummy component (13) is attached to the outer side of the side plate component (3).
3. The forming die for the composite material of the inclined beam and the front beam as claimed in claim 1, wherein: welding frame (2) front surface fixedly connected with frock data plate (12), welding frame (2) inside is honeycomb, and the fixed surface of lower surface is connected with a certain amount and fills up the foot.
4. The forming die for the composite material of the inclined beam and the front beam as claimed in claim 1, wherein: the block A (4) is square, and a groove is formed in the inner wall of the block A; the positioning block A (5) is clamped in the groove of the block A (4) to limit and position the block A, and the block A is fixed on the upper surface of the template (1) through a ball pin (6) and an inner hexagon screw (7).
5. The forming die for the composite material of the inclined beam and the front beam as claimed in claim 1, wherein: the positioning block B (9) is fixed on the upper surface of the template (1) through a ball head pin (6) and an inner hexagon screw (7), the positioning block B (9) is tightly clamped on the left side of the block B (8), and the template (1) is tightly attached to the right side of the block B.
6. The forming die for the composite material of the inclined beam and the front beam as claimed in claim 1, wherein: the drill plate component A (10) is arched, the left end of the drill plate component A is bent to be close to the surface of the shaping plate (1), and a drill bushing (14) is arranged at the close end.
7. The forming die for the composite material of the inclined beam and the front beam as claimed in claim 1, wherein: the drill jig plate component B (11) is arched, the right end of the drill jig plate component is bent to be close to the surface of the template (1), and a drill bushing (14) is arranged at the close end.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020210719.9U CN211968112U (en) | 2020-02-25 | 2020-02-25 | Forming die for composite material of front beam of oblique beam |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020210719.9U CN211968112U (en) | 2020-02-25 | 2020-02-25 | Forming die for composite material of front beam of oblique beam |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN211968112U true CN211968112U (en) | 2020-11-20 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202020210719.9U Active CN211968112U (en) | 2020-02-25 | 2020-02-25 | Forming die for composite material of front beam of oblique beam |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN211968112U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113843928A (en) * | 2021-09-17 | 2021-12-28 | 广联航空工业股份有限公司 | C-shaped closed angle beam forming tool and demolding method |
| CN115071005A (en) * | 2022-07-06 | 2022-09-20 | 江西昌兴航空装备股份有限公司 | Blocking die for compression molding of composite piece |
-
2020
- 2020-02-25 CN CN202020210719.9U patent/CN211968112U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113843928A (en) * | 2021-09-17 | 2021-12-28 | 广联航空工业股份有限公司 | C-shaped closed angle beam forming tool and demolding method |
| CN115071005A (en) * | 2022-07-06 | 2022-09-20 | 江西昌兴航空装备股份有限公司 | Blocking die for compression molding of composite piece |
| CN115071005B (en) * | 2022-07-06 | 2024-05-24 | 江西昌兴航空装备股份有限公司 | A blocking mould for composite material spare compression molding |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: A Composite Molding Die for Inclined Beam Front Beam Effective date of registration: 20220930 Granted publication date: 20201120 Pledgee: Jingdezhen branch of Postal Savings Bank of China Ltd. Pledgor: JIANGXI CHANGXING AVIATION EQUIPMENT CO.,LTD. Registration number: Y2022980017313 |
|
| PE01 | Entry into force of the registration of the contract for pledge of patent right |