CN219565476U - Fuselage shaping assembly fixture - Google Patents
Fuselage shaping assembly fixture Download PDFInfo
- Publication number
- CN219565476U CN219565476U CN202321322010.8U CN202321322010U CN219565476U CN 219565476 U CN219565476 U CN 219565476U CN 202321322010 U CN202321322010 U CN 202321322010U CN 219565476 U CN219565476 U CN 219565476U
- Authority
- CN
- China
- Prior art keywords
- clamping plate
- frame
- plate
- positioning
- forming
- 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.)
- Active
Links
- 238000007493 shaping process Methods 0.000 title claims description 9
- 230000006835 compression Effects 0.000 claims abstract description 44
- 238000007906 compression Methods 0.000 claims abstract description 44
- 238000000465 moulding Methods 0.000 claims abstract description 18
- 238000003825 pressing Methods 0.000 claims description 16
- 239000000463 material Substances 0.000 claims description 3
- 238000004519 manufacturing process Methods 0.000 abstract description 3
- 239000000853 adhesive Substances 0.000 description 6
- 230000001070 adhesive effect Effects 0.000 description 6
- 238000005056 compaction Methods 0.000 description 1
- 210000001503 joint Anatomy 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000000149 penetrating effect Effects 0.000 description 1
Classifications
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
Landscapes
- Moulds For Moulding Plastics Or The Like (AREA)
Abstract
The utility model discloses a machine body forming assembly tool, which belongs to the technical field of machine body forming, and particularly relates to a machine body forming assembly tool, comprising a main forming die, a forming groove arranged at the top end of the main forming die, and a forming assembly structure arranged at the top end of the main forming die; the molding assembly structure comprises: the frame body of the machine body is arranged in the forming groove, and four frames of the machine body are positioned by using a positioning angle seat, the compression clamping plate and a frame positioning plate to ensure that the frames of the machine body are perpendicular to the machine body; after the frame is positioned, the compression clamping plate and the frame positioning plate are disassembled, the upper skin is combined, the front edge part of the machine body is positioned by the front edge stop block, and then the compression clamping plate is assembled to compress the frame and the upper skin, so that the cost and the production time are effectively reduced, and compared with other assembly tools, the assembly precision and the die resetting precision of products are improved.
Description
Technical Field
The utility model relates to the technical field of machine body molding, in particular to a machine body molding assembly tool.
Background
In the shaping assembly process of small-size unmanned aerial vehicle, in order to reduce cost, improve production and assembly accuracy, most unmanned aerial vehicle fuselage is made through two sets of frock, and first shaping frock, second assembly frock. And the molded product is placed on another tool standard for operation, if the molding and the assembly of the product are separately carried out, the butt joint gap between the lower skin and the upper skin of the fuselage can not be ensured, the precision is not well ensured, the cost is huge, and the assembly efficiency is low.
Therefore, the utility model relates to a machine body forming assembly tool.
Disclosure of Invention
The present utility model has been made in view of the above and/or problems occurring in the prior art of a fuselage forming assembly fixture.
Therefore, an object of the present utility model is to provide a machine body forming assembly tool, which can solve the above-mentioned existing problems.
In order to solve the technical problems, according to one aspect of the present utility model, the following technical solutions are provided:
a fuselage shaping assembly fixture, comprising: the main forming die also comprises a forming groove arranged at the top end of the main forming die and a forming assembly structure arranged at the top end of the main forming die; the molding assembly structure comprises: the clamping plate is pressed, the clamping plate is arranged at the top end of the main forming die, the side wall of the clamping plate is provided with a frame locating plate, the bottom end of the frame locating plate extends into the forming groove, and the material is pressed and formed.
As a preferable scheme of the airframe forming assembly fixture, the utility model comprises the following steps: the front edge positioning check blocks are arranged on the rear side of the top of the main forming die, and are respectively distributed on two sides of the forming groove.
As a preferable scheme of the airframe forming assembly fixture, the utility model comprises the following steps: positioning angle seats are arranged on two sides of the middle of the top end of the main forming die, two groups of positioning angle seats are arranged on two sides of the middle of the forming groove, and bosses are fixedly arranged at the front end and the rear end of the top of each positioning angle seat.
As a preferable scheme of the airframe forming assembly fixture, the utility model comprises the following steps: the compaction clamping plate comprises:
the first pressing clamping plate is arranged at the top end of the front edge positioning stop block;
the second compression clamping plate and the third compression clamping plate are respectively arranged at the front end and the rear end of the top of the positioning angle seat, and a connecting structure is arranged between the second compression clamping plate and the boss; and
and the fourth pressing clamping plate is arranged at one end, far away from the first pressing clamping plate, of the top of the main forming die.
As a preferable scheme of the airframe forming assembly fixture, the utility model comprises the following steps: the frame positioning plate includes:
the first frame positioning plate is arranged at the rear end of the first compression clamping plate;
the second frame positioning plate is arranged at the front end of the second compression clamping plate;
the third frame positioning plate is arranged at the front end of the third compression clamping plate; and
the fourth frame positioning plate is arranged at the front end of the fourth compression clamping plate;
the bottom ends of the first frame positioning plate, the second frame positioning plate, the third frame positioning plate and the fourth frame positioning plate extend into forming grooves formed in the top end of the main forming die.
As a preferable scheme of the airframe forming assembly fixture, the utility model comprises the following steps: the connection structure includes:
and connecting holes are formed between the two sides of the pressing clamping plate II and the boss at the rear side of the top end of the locating angle seat and between the two sides of the pressing clamping plate III and the boss at the front side of the top end of the locating angle seat.
As a preferable scheme of the airframe forming assembly fixture, the utility model comprises the following steps: the connecting bolt is installed to the inner wall of connecting hole, connecting nut is threaded connection to connecting bolt's one end through the connecting hole.
As a preferable scheme of the airframe forming assembly fixture, the utility model comprises the following steps: handles are fixedly arranged on two sides of the connecting bolt and two sides of the connecting nut.
Compared with the prior art:
placing a lower skin in a forming groove of a main forming die, installing a frame body of a machine body in the forming groove, positioning four frames of the machine body by using a positioning angle seat, a compression clamping plate and a frame positioning plate, and positioning the frames on the positioning angle seat by using pins so as to ensure that the frames of the machine body are perpendicular to the machine body; after the frame is positioned, the compression clamping plate and the frame positioning plate are disassembled, the upper skin is subjected to a combination, the front edge part of the machine body is positioned by the front edge stop block, the compression clamping plate is assembled, the frame and the upper skin are compressed, the firm cementation of the frame and the upper skin is ensured, the structural adhesive is prevented from being de-bonded, and then the structural adhesive is heated and cured in a thermal oven; cost and production time are effectively reduced, and compared with other assembly tools, assembly precision and die copying precision of products are improved.
Drawings
FIG. 1 is a front view of the present utility model;
FIG. 2 is a top view of the present utility model;
FIG. 3 is a front view of a primary molding die of the present utility model;
FIG. 4 is a front view of the first, second, third and fourth compression cards of the present utility model;
fig. 5 is a front view of the connection between two sides of the second and third clamping plates and the boss at the top end of the locating angle seat.
In the figure: the main forming die 1, the forming groove 2, the first compression clamping plate 3, the second compression clamping plate 4, the third compression clamping plate 5, the fourth compression clamping plate 6, the positioning angle seat 7, the front edge positioning stop block 8, the first frame positioning plate 9, the second frame positioning plate 10, the third frame positioning plate 11, the fourth frame positioning plate 12, the connecting bolt 13, the connecting nut 14, the handle 15, the connecting hole 17, the first positioning hole 18, the second positioning hole 19, the third positioning hole 20, the fourth positioning hole 21, the fifth positioning hole 22, the sixth positioning hole 23 and the boss 24.
Detailed Description
For the purpose of making the objects, technical solutions and advantages of the present utility model more apparent, embodiments of the present utility model will be described in further detail below with reference to the accompanying drawings.
Embodiment one:
the utility model provides a machine body molding assembly fixture, which has the advantages of convenient use and improved efficiency, and referring to fig. 1-5, and comprises a main molding die 1, a molding groove 2 arranged at the top end of the main molding die 1, and a molding assembly structure arranged at the top end of the main molding die 1;
the shaping assembly structure includes: the clamping plate is pressed and installed at the top end of the main forming die 1, the side wall of the clamping plate is provided with a frame locating plate, the bottom end of the frame locating plate extends into the forming groove 2, and the material is pressed and formed.
The front edge positioning stop block 8 is installed on the top rear side of the main forming die 1, the front edge positioning stop block 8 is provided with two groups, the two groups of front edge positioning stop blocks are respectively distributed on two sides of the forming groove 2, positioning angle seats 7 are respectively installed on two sides of the middle of the top end of the main forming die 1, the two groups of positioning angle seats 7 are located on two sides of the middle of the forming groove 2, and bosses 24 are fixedly installed on the front end and the rear end of the top of the positioning angle seat 7.
When the machine is specifically used, a person skilled in the art installs the locating angle seat 7 of the main forming die 1 during assembly, places a lower skin in the forming groove 2 of the main forming die 1, installs the frame body of the machine body in the forming groove 2, locates four frames of the machine body by the locating angle seat 7, the compression clamping plate and the frame locating plate, and locates the frames on the locating angle seat 7 by using pins so as to ensure that the frames are perpendicular to the machine body;
after the frame is positioned, the pressing clamping plate and the frame positioning plate are disassembled, the upper skin is subjected to a combination, the front edge part of the machine body is positioned by the front edge stop block, then the pressing clamping plate is assembled, the frame and the upper skin are pressed, the bonding firmness of the frame and the upper skin is ensured, the structural adhesive is prevented from being de-bonded, and then the structural adhesive is heated and cured by a thermal oven.
Embodiment two:
the utility model provides a machine body forming assembly tool, referring to fig. 1-5, a compression clamping plate comprises:
the first compression clamping plate 3 is arranged at the top end of the front edge positioning stop block 8;
the second compression clamping plate 4 and the third compression clamping plate 5 are respectively arranged at the front end and the rear end of the top of the positioning angle seat 7, and a connecting structure is arranged between the second compression clamping plate 4 and the third compression clamping plate 5 and the boss 24; and
and the fourth pressing clamping plate 6 is arranged at one end, far away from the first pressing clamping plate 3, of the top of the main forming die 1.
The frame locating plate includes: the first frame positioning plate 9 is arranged at the rear end of the first compression clamping plate 3; the second frame positioning plate 10 is arranged at the front end of the second compression clamping plate 4; the third frame positioning plate 11 is arranged at the front end of the third compression clamping plate 5; the fourth frame positioning plate 12 is arranged at the front end of the fourth compression clamping plate 6; the bottom ends of the first frame positioning plate 9, the second frame positioning plate 10, the third frame positioning plate 11 and the fourth frame positioning plate 12 extend into the forming groove 2 formed in the top end of the main forming die 1.
When the machine is specifically used, a person skilled in the art installs the locating angle seat 7 of the main forming die 1 during assembly, places a lower skin in the forming groove 2 of the main forming die 1, installs the frame body of the machine body in the forming groove 2, locates four frames of the machine body by the locating angle seat 7, the compression clamping plate and the frame locating plate, and locates the frames on the locating angle seat 7 by using pins so as to ensure that the frames are perpendicular to the machine body;
after the frame is positioned, the pressing clamping plate and the frame positioning plate are disassembled, the upper skin is subjected to a combination, the front edge part of the machine body is positioned by the front edge stop block, then the pressing clamping plate is assembled, the frame and the upper skin are pressed, the bonding firmness of the frame and the upper skin is ensured, the structural adhesive is prevented from being de-bonded, and then the structural adhesive is heated and cured by a thermal oven.
Embodiment III:
the utility model provides a machine body forming assembly tool, referring to fig. 1-5, a connecting structure comprises:
the connecting holes 17 are formed between the two sides of the second pressing clamping plate 4 and the boss 24 on the rear side of the top end of the positioning angle seat 7, the two sides of the third pressing clamping plate 5 and the boss 24 on the front side of the top end of the positioning angle seat 7, the connecting bolts 13 are installed on the inner walls of the connecting holes 17, one ends of the connecting bolts 13 penetrate through the connecting holes 17 and are in threaded connection with the connecting nuts 14, and handles 15 are fixedly installed on the two sides of the connecting bolts 13 and the two sides of the connecting nuts 14.
When the clamp is specifically used, the third compression clamping plate 5 and the second compression clamping plate 4 are respectively attached to one group of bosses 24 on two sides of the top end of the positioning angle seat 7, the two groups of connecting holes 17 are corresponding to each other, the connecting bolts 13 are driven to rotate, the connecting bolts are connected with the connecting nuts 14 through the connecting holes 17, the connecting bolts are fixed, and the handles 15 fixedly installed on two sides of the connecting bolts 13 and two sides of the connecting nuts 14 are convenient to drive the connecting bolts and the connecting nuts to rotate.
Embodiment four:
the utility model provides a machine body forming assembly tool, referring to fig. 1-5, two sides of the rear end, two sides of the middle part and two sides of the front end of the top of a main forming die 1 are respectively provided with a second positioning hole 19, a fourth positioning hole 21 and a sixth positioning hole 23, a first positioning hole 18 corresponding to the second positioning hole 19 is formed on a front edge positioning stop block 8, a third positioning hole 20 corresponding to the fourth positioning hole 21 is formed on a positioning angle seat 7, a fifth positioning hole 22 corresponding to the sixth positioning hole 23 is formed on two sides of the bottom of the front end of a compression clamping plate 6, and the two positioning holes are fixedly connected through bolts penetrating through the corresponding positioning holes.
Although the utility model has been described hereinabove with reference to embodiments, various modifications thereof may be made and equivalents may be substituted for elements thereof without departing from the scope of the utility model. In particular, the features of the disclosed embodiments may be combined with each other in any manner as long as there is no structural conflict, and the exhaustive description of these combinations is not given in this specification merely for the sake of omitting the descriptions and saving resources. Therefore, it is intended that the utility model not be limited to the particular embodiment disclosed, but that the utility model will include all embodiments falling within the scope of the appended claims.
Claims (8)
1. The utility model provides a fuselage shaping assembly fixture, includes main forming die (1), its characterized in that: the molding device also comprises a molding groove (2) which is arranged at the top end of the main molding die (1), and a molding assembly structure which is arranged at the top end of the main molding die (1);
the molding assembly structure comprises: the clamping plate is pressed, the clamping plate is arranged at the top end of the main forming die (1), the side wall of the clamping plate is provided with a frame locating plate, the bottom end of the frame locating plate extends into the forming groove (2), and the material is pressed and formed.
2. The machine body forming assembly tool according to claim 1, wherein a front edge positioning stop block (8) is arranged on the rear side of the top of the main forming die (1), and the front edge positioning stop blocks (8) are provided with two groups and are respectively distributed on two sides of the forming groove (2).
3. The machine body forming assembly tool according to claim 2, wherein positioning angle seats (7) are arranged on two sides of the middle of the top end of the main forming die (1), two groups of positioning angle seats (7) are positioned on two sides of the middle of the forming groove (2), and bosses (24) are fixedly arranged at the front end and the rear end of the top of each positioning angle seat (7).
4. A fuselage forming assembly fixture as defined in claim 3 wherein the compression clamping plate comprises:
the first pressing clamping plate (3) is arranged at the top end of the front edge positioning stop block (8);
the second compression clamping plate (4) and the third compression clamping plate (5) are respectively arranged at the front end and the rear end of the top of the positioning angle seat (7), and a connecting structure is arranged between the second compression clamping plate (4) and the third compression clamping plate (5) and the boss (24); and
and the fourth pressing clamping plate (6) is arranged at the top of the main forming die (1) and far away from one end of the first pressing clamping plate (3).
5. The airframe forming assembly fixture as defined in claim 4, wherein said frame locating plate comprises:
the first frame positioning plate (9) is arranged at the rear end of the first compression clamping plate (3);
the second frame positioning plate (10) is arranged at the front end of the second compression clamping plate (4);
the third frame positioning plate (11) is arranged at the front end of the third compression clamping plate (5); and
the fourth frame positioning plate (12) is arranged at the front end of the fourth compression clamping plate (6);
the bottom ends of the first frame positioning plate (9), the second frame positioning plate (10), the third frame positioning plate (11) and the fourth frame positioning plate (12) are all extended into a forming groove (2) formed in the top end of the main forming die (1).
6. The airframe forming assembly fixture as defined in claim 4, wherein said connecting structure comprises:
and connecting holes (17) are formed between two sides of the second compression clamping plate (4) and a boss (24) at the rear side of the top end of the positioning angle seat (7) and two sides of the third compression clamping plate (5) and a boss (24) at the front side of the top end of the positioning angle seat (7).
7. The airframe shaping assembly fixture as defined in claim 6, characterized in that a connecting bolt (13) is installed on the inner wall of the connecting hole (17), and one end of the connecting bolt (13) penetrates through the connecting hole (17) to be connected with a connecting nut (14) in a threaded manner.
8. The airframe shaping assembly fixture as defined in claim 7, characterized in that handles (15) are fixedly installed on both sides of the connecting bolt (13) and both sides of the connecting nut (14).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321322010.8U CN219565476U (en) | 2023-05-29 | 2023-05-29 | Fuselage shaping assembly fixture |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321322010.8U CN219565476U (en) | 2023-05-29 | 2023-05-29 | Fuselage shaping assembly fixture |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN219565476U true CN219565476U (en) | 2023-08-22 |
Family
ID=87663533
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202321322010.8U Active CN219565476U (en) | 2023-05-29 | 2023-05-29 | Fuselage shaping assembly fixture |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN219565476U (en) |
-
2023
- 2023-05-29 CN CN202321322010.8U patent/CN219565476U/en active Active
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN206229903U (en) | Gear ring edge-cutting and hole-punching straightening die | |
| CN211590420U (en) | Punching die for sealing washer | |
| CN102601752A (en) | Aircraft wing wall panel butt joint stringer locating device | |
| CN108162478A (en) | A kind of drum-type brake pad heat pressing and molding mold and technique | |
| CN219565476U (en) | Fuselage shaping assembly fixture | |
| CN216488301U (en) | Mica protective cover for battery pack | |
| CN214188147U (en) | Fastening device for injection mold | |
| CN215152021U (en) | Composite material propeller blade forming die | |
| CN210359982U (en) | Composite window preparation is with group frame location platform | |
| CN208894992U (en) | TOX gas-liquid pressure-boosting stamping die based on a mould two pieces | |
| CN204800646U (en) | Manipulator slide device | |
| CN209110504U (en) | Starter armature harness and commutator pressing machine | |
| CN105090191A (en) | Gluing clamp for front wall panel assembly | |
| CN208452394U (en) | A kind of drum-type brake pad heat pressing and molding mold | |
| CN205715125U (en) | A kind of antenna for mobile phone foam joint tool | |
| CN211613966U (en) | Workpiece stamping device | |
| CN219053430U (en) | Can realize closely laminating be convenient for welded tool | |
| CN216138766U (en) | Leather plastic plate pressing and positioning device | |
| CN218477024U (en) | Auxiliary bottom placing tool applied to disc injection machine | |
| CN109367053A (en) | Dual-purpose mould is glued in covering paving under a kind of aircraft | |
| CN220127955U (en) | Welding positioning tool for automobile sheet metal parts | |
| CN210616352U (en) | Cambered surface equipment magnet pressure equipment workstation | |
| CN202803942U (en) | Shaping and burnishing mold for clutch mounting plate of washing machine | |
| CN220830180U (en) | Binding post forming die | |
| CN214442276U (en) | Quartering punching device |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP01 | Change in the name or title of a patent holder |
Address after: 710000, No. 12, Planning 1st Road, Phase II, National Aviation High tech Industrial Base, Xi'an City, Shaanxi Province Patentee after: Shaanxi Huanghe Xinxing New Material Technology Co.,Ltd. Address before: 710000, No. 12, Planning 1st Road, Phase II, National Aviation High tech Industrial Base, Xi'an City, Shaanxi Province Patentee before: SHAANXI HUANGHE XINXING EQUIPMENT CO.,LTD. |
|
| CP01 | Change in the name or title of a patent holder |