CN212528424U - Aviation complex surface part gluing tool demoulding device - Google Patents
Aviation complex surface part gluing tool demoulding device Download PDFInfo
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- CN212528424U CN212528424U CN202021153133.XU CN202021153133U CN212528424U CN 212528424 U CN212528424 U CN 212528424U CN 202021153133 U CN202021153133 U CN 202021153133U CN 212528424 U CN212528424 U CN 212528424U
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- 238000000034 method Methods 0.000 abstract description 16
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- 230000001174 ascending effect Effects 0.000 description 2
- 239000002699 waste material Substances 0.000 description 2
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
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Abstract
The utility model discloses a complicated profile of aviation spare splices frock shedder, including backup pad and mounting panel, the left side at backup pad top and the bottom fixed connection of mounting panel, the equal fixedly connected with telescopic link in both sides of backup pad bottom, the bottom fixedly connected with base of two telescopic links, the right side fixedly connected with reference column of mounting panel, the left end of reference column runs through the mounting panel and extends to the left side of mounting panel, and the left side of reference column is rotated and is connected with the screw rod, the right-hand member fixedly connected with elastic connection spare of screw rod, and elastic connection spare's right-hand member is rotated and is connected with the couple, the utility. This complicated profile spare of aviation splices frock shedder passes through the motion drive couple motion of telescopic link and screw rod, gets a in-process, makes the work piece receive a relatively less power and just can realize the drawing of patterns, has avoided the work piece to take place deformation because of the atress is too big in the drawing of patterns in-process, influences the problem of product quality, has improved work efficiency.
Description
Technical Field
The utility model relates to a shedder technical field specifically is a complicated profile of aviation spare splices frock shedder.
Background
A conventional composite material tooling product is molded on a template in a frame, and after a workpiece is molded, the workpiece needs to be manually taken, but for a deep U-shaped workpiece, when the molded surface of the workpiece is a special-shaped surface, the workpiece is easily taken by hand, the workpiece is easily damaged in the workpiece taking process, the quality of the workpiece is reduced, and the workpiece is more seriously directly scrapped.
According to patent number CN209504890U a frock shedder is spliced to complicated surface spare, including being used for the support frame with frame connection, the reference column, the carousel, the screw rod, connecting piece and fixed knot, reference column fixed mounting is on the support frame, the carousel meets and can rotate on the reference column with the reference column, the screw rod passes the reference column after cooperating with the carousel, this complicated surface spare splices frock shedder, the utility model discloses cooperate the use with current frame, can make the smooth drawing of patterns of work piece at the in-process that uses to guarantee the quality of work piece, but this complicated surface spare splices frock shedder can only give the ascending power of work piece horizontal direction carrying out the in-process, and the resistance that the work piece received when getting is great, pulls the in-process work piece and damages easily, thereby influences the work piece quality, and uses the worker to get the piece, wastes time and energy, and the use limitation.
SUMMERY OF THE UTILITY MODEL
Not enough to prior art, the utility model provides a complicated profile of aviation spare splices frock shedder has solved and can only give the ascending power of work piece horizontal direction carrying out the in-process, and the resistance that the work piece received when getting is great, pulls the in-process work piece and damages easily to influence the work piece quality, and use the manual work to get the piece, waste time and energy, use the great problem of limitation.
In order to achieve the above purpose, the utility model discloses a following technical scheme realizes: a demoulding device of an aviation complex surface part gluing tool comprises a supporting plate and a mounting plate, wherein the left side of the top of the supporting plate is fixedly connected with the bottom of the mounting plate, the two sides of the bottom of the supporting plate are fixedly connected with telescopic rods, the bottom ends of the two telescopic rods are fixedly connected with a base, the right side of the mounting plate is fixedly connected with a positioning column, the left end of the positioning column penetrates through the mounting plate and extends to the left side of the mounting plate, the left side of the positioning column is rotatably connected with a screw rod, the right end of the screw rod penetrates through the positioning column and extends to the right end of the positioning column, the right end of the surface of the screw rod and positioned on the positioning column is in threaded connection with a turntable, the right end of the positioning column is in rotary connection with the turntable, the surface of the rotary table is fixedly connected with an outer gear ring, the right end of the screw is fixedly connected with an elastic connecting piece, and the right end of the elastic connecting piece is rotatably connected with a hook.
Preferably, the top fixedly connected with motor of mounting panel, the one end fixedly connected with dwang of motor output shaft, the fixed surface of dwang is connected with and outer ring gear engaged with gear.
Preferably, the elastic connecting piece includes fixed frame, the top and the equal fixedly connected with slide rail in bottom of fixed frame inner wall, two sliding connection has the movable block between the relative one side of slide rail, the right side fixedly connected with connecting rod of movable block, the right-hand member of connecting rod runs through fixed frame and extends to the outside of fixed frame.
Preferably, the right-hand member fixedly connected with connecting block of connecting rod, the right side and the couple of connecting block rotate to be connected, between the right side of movable block and the right side of fixed frame inner wall and be located the fixed surface of connecting rod and be connected with the spring.
Preferably, the left end of the screw is fixedly connected with a baffle.
Preferably, the right side fixedly connected with gusset plate at backup pad top, the one end rotation connection of motor is kept away from with the dwang in the left top of gusset plate.
Advantageous effects
The utility model provides a complicated profile of aviation spare splices frock shedder. Compared with the prior art, the method has the following beneficial effects:
(1) the aviation complex-profile part gluing tool demoulding device is fixedly connected with the bottom of a mounting plate through the left side of the top of the supporting plate, telescopic rods are fixedly connected with the two sides of the bottom of the supporting plate, bases are fixedly connected with the bottom ends of the two telescopic rods, a positioning column is fixedly connected with the right side of the mounting plate, the left end of the positioning column penetrates through the mounting plate and extends to the left side of the mounting plate, a screw rod is rotatably connected with the left side of the positioning column, the right end of the screw rod penetrates through the positioning column and extends to the right end of the positioning column, the mounting plate and the screw rod are driven to move through the telescopic rods, a hook is driven to move through the screw rod, during a part taking process, a workpiece is subjected to a force vertical to a mould, and is subjected to a force parallel to the mould, so that the demoulding can be realized, the screw rod is connected with the hook through the elastic connecting piece, so that the force applied to the workpiece in the demoulding process is gradually increased from small to large, and the workpiece is prevented from being damaged by overlarge instantaneous tension applied to the workpiece when demoulding is started.
(2) This complicated profile part of aviation splices frock shedder, the right-hand member that just is located the reference column through the surface of screw rod is connected with the carousel, and the right-hand member and the carousel of reference column rotate to be connected, and through the cooperation of motor, gear, screw rod, reference column and carousel, with the motor drive screw rod motion, reduced operating personnel's the amount of labour and artificial misoperation, improved product quality and work efficiency.
Drawings
FIG. 1 is a perspective view of the structure of the present invention;
FIG. 2 is a cross-sectional view of the structure of the present invention;
fig. 3 is a sectional view of the elastic connector of the present invention.
In the figure: the device comprises a supporting plate 1, a mounting plate 2, an expansion rod 3, a base 4, a positioning column 5, a screw 6, a rotary table 7, an outer gear ring 8, an elastic connecting piece 9, a fixed frame 91, a slide rail 92, a movable block 93, a connecting rod 94, a connecting block 95, a spring 96, a motor 10, a rotating rod 11, a gear 12, a hook 13, a baffle 14 and a reinforcing plate 15.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Referring to fig. 1-3, the present invention provides a technical solution: a demoulding device of an aviation complex surface part gluing tool comprises a supporting plate 1 and a mounting plate 2, wherein a reinforcing plate 15 is fixedly connected to the right side of the top of the supporting plate 1, the top of the left side of the reinforcing plate 15 is rotatably connected with one end, away from a motor, of a rotating rod 11, a motor 10 is fixedly connected to the top of the mounting plate 2, the motor 10 is connected with a control system and an external power supply through a lead, one end of an output shaft of the motor 10 is fixedly connected with the rotating rod 11, the surface of the rotating rod 11 is fixedly connected with a gear 12 meshed with an outer gear ring 8, the left side of the top of the supporting plate 1 is fixedly connected with the bottom of the mounting plate 2, two sides of the bottom of the supporting plate 1 are both fixedly connected with telescopic rods 3, each telescopic rod 3 is an electric telescopic rod and is connected with the, the left end of the positioning column 5 penetrates through the mounting plate 2 and extends to the left side of the mounting plate 2, the left side of the positioning column 5 is rotatably connected with a screw 6, a guide block is arranged on the positioning column 5, a guide groove corresponding to the screw 6 is formed in the surface of the screw 6, the screw 6 is guaranteed not to rotate in the moving process, the left end of the screw 6 is fixedly connected with a baffle 14, the screw 6 is prevented from being separated from the positioning column 5 when moving, the right end of the screw 6 penetrates through the positioning column 5 and extends to the right end of the positioning column 5, the surface of the screw 6 and the right end of the positioning column 5 are in threaded connection with a rotary table 7, the right end of the positioning column 5 is rotatably connected with the rotary table 7, the surface of the rotary table 7 is fixedly connected with an outer gear ring 8, the right end of the screw 6 is fixedly connected with an elastic connecting piece 9, the right side fixedly connected with connecting rod 94 of movable block 93, the right-hand member fixedly connected with connecting block 95 of connecting rod 94, connecting block 95's right side and couple 13 rotate to be connected, between the right side of movable block 93 and the right side of fixed frame 91 inner wall and be located connecting rod 94's fixed surface is connected with spring 96, connecting rod 94's right-hand member runs through fixed frame 91 and extends to fixed frame 91's outside elastic connector 9's right-hand member and rotates and be connected with couple 13, connecting piece 9 passes through bolted connection with couple 13, can change the couple 13 of different shapes as required.
During the use, with base 4 fixed connection on the mould, earlier with the pre-buried corner allowance at the work piece of couple 13, when treating the work piece shaping back needs the drawing of patterns, flexible backup pad 1 and the motion of mounting panel 2 of drive through telescopic link 3, and then drive screw rod 6 and couple 13 motion, make the work piece break away from the mould, drive dwang 11 and gear 12 through control motor 10 after that and rotate and then drive outer ring gear 8 and sleeve 7 and rotate, make screw rod 6 drive elastic connection spare 9 and couple 13 along axial displacement, take out the work piece from the mould, can be according to particular case during the use, the order and the range of control screw rod 6 and 3 actions of telescopic link.
It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (6)
1. The utility model provides a frock shedder is glued to complicated profile of aviation spare, includes backup pad (1) and mounting panel (2), the left side at backup pad (1) top and the bottom fixed connection of mounting panel (2), its characterized in that: the support plate is characterized in that telescopic rods (3) are fixedly connected to the two sides of the bottom of the support plate (1), two bottom ends of the telescopic rods (3) are fixedly connected with a base (4), a positioning column (5) is fixedly connected to the right side of the mounting plate (2), the left end of the positioning column (5) penetrates through the mounting plate (2) and extends to the left side of the mounting plate (2), a screw rod (6) is rotatably connected to the left side of the positioning column (5), the right end of the screw rod (6) penetrates through the positioning column (5) and extends to the right end of the positioning column (5), a turntable (7) is in threaded connection with the right end of the positioning column (5), the right end of the positioning column (5) is rotatably connected with the turntable (7), an outer gear ring (8) is fixedly connected to the surface of the turntable (7), and an elastic connecting piece (9, the right end of the elastic connecting piece (9) is rotatably connected with a hook (13).
2. The aviation complex surface part gluing tool demolding device as claimed in claim 1, wherein the aviation complex surface part gluing tool demolding device is characterized in that: the top fixedly connected with motor (10) of mounting panel (2), the one end fixedly connected with dwang (11) of motor (10) output shaft, the fixed surface of dwang (11) is connected with gear (12) with outer ring gear (8) engaged with mutually.
3. The aviation complex surface part gluing tool demolding device as claimed in claim 1, wherein the aviation complex surface part gluing tool demolding device is characterized in that: elastic connector (9) are including fixed frame (91), the top and the equal fixedly connected with slide rail (92) in bottom of fixed frame (91) inner wall, two sliding connection has movable block (93) between the relative one side of slide rail (92), the right side fixedly connected with connecting rod (94) of movable block (93), the right-hand member of connecting rod (94) runs through fixed frame (91) and extends to the outside of fixed frame (91).
4. The aviation complex surface part gluing tool demolding device as claimed in claim 3, wherein the aviation complex surface part gluing tool demolding device is characterized in that: the right-hand member fixedly connected with connecting block (95) of connecting rod (94), the right side and the couple (13) of connecting block (95) rotate to be connected, just be located fixed surface of connecting rod (94) and be connected with spring (96) between the right side of movable block (93) and the right side of fixed frame (91) inner wall.
5. The aviation complex surface part gluing tool demolding device as claimed in claim 1, wherein the aviation complex surface part gluing tool demolding device is characterized in that: and the left end of the screw rod (6) is fixedly connected with a baffle (14).
6. The aviation complex surface part gluing tool demolding device as claimed in claim 2, wherein the aviation complex surface part gluing tool demolding device is characterized in that: the right side fixedly connected with gusset plate (15) at backup pad (1) top, the one end rotation connection of motor is kept away from with dwang (11) at the left top of gusset plate (15).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021153133.XU CN212528424U (en) | 2020-06-20 | 2020-06-20 | Aviation complex surface part gluing tool demoulding device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021153133.XU CN212528424U (en) | 2020-06-20 | 2020-06-20 | Aviation complex surface part gluing tool demoulding device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212528424U true CN212528424U (en) | 2021-02-12 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202021153133.XU Expired - Fee Related CN212528424U (en) | 2020-06-20 | 2020-06-20 | Aviation complex surface part gluing tool demoulding device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN212528424U (en) |
-
2020
- 2020-06-20 CN CN202021153133.XU patent/CN212528424U/en not_active Expired - Fee Related
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| Date | Code | Title | Description |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20210212 |