CN209174614U - A kind of aerospace parts Special reforming equipment - Google Patents

A kind of aerospace parts Special reforming equipment Download PDF

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Publication number
CN209174614U
CN209174614U CN201821660328.6U CN201821660328U CN209174614U CN 209174614 U CN209174614 U CN 209174614U CN 201821660328 U CN201821660328 U CN 201821660328U CN 209174614 U CN209174614 U CN 209174614U
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CN
China
Prior art keywords
fixedly connected
slot
slide
aerospace parts
sliding slot
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Active
Application number
CN201821660328.6U
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Chinese (zh)
Inventor
赵世山
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Tianjin Yijie Haite General Aviation Service Co Ltd
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Tianjin Yijie Haite General Aviation Service Co Ltd
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Priority to CN201821660328.6U priority Critical patent/CN209174614U/en
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Abstract

The utility model discloses a kind of aerospace parts Special reforming equipments, including bottom plate, the upper surface of bottom plate offers workpiece slot, bottom plate is symmetrically fixedly connected with support column close to the upper surface of end positions, two support columns are fixedly connected with support plate between the side wall on top, slide opening corresponding with workpiece groove location is offered in support plate, it is interspersed in slide opening and the matched nose bar of slide opening, and nose bar is slidably connected with slide opening, symmetrical sliding slot there are two being opened up on the inner wall of slide opening, the lateral wall of nose bar corresponds to be fixedly connected with and the matched sliding block of sliding slot at the position of sliding slot, and sliding block is slidably connected with corresponding sliding slot, sliding slot is fixedly connected with the first spring close to the side of bottom plate.The utility model improves the shaping efficiency of aerospace parts, and conveniently aerospace parts are fixed, and prevents from shifting in reforming process, and then improves shaping quality.

Description

A kind of aerospace parts Special reforming equipment
Technical field
The utility model relates to aviation part shaping technique field more particularly to a kind of aerospace parts Special reforming equipments.
Background technique
Aerospace parts are typically designed that complicated, functional requirement is stringent, it is necessary to meet rigidity, intensity, fatigue, airtight, reliability Deng requirement.As the continuous growth for using the time, or impact in operation are excessive, numerous parts are under huge pressure Generate deformation, part deformation then can the production work to single unit system can all impact, sometimes small deviation even meeting Cause huge loss;But the cost of aerospace parts is all more expensive, it is excessively unrestrained if directly abandoned for deformation part Take, generally can all carry out corresponding shaping corrective operations, to realize recycling.
In the prior art, aerospace parts need manually to be operated in reforming process, shadow to influencing working efficiency, and And aerospace parts inconvenience in reforming process it is fixed positioning, is easy to shift in reforming process, influence whole Form quality amount.
Utility model content
Purpose of the utility model is to solve aerospace parts shaping inefficiency in the prior art, and it is inconvenient into The problem of row stationary positioned, and a kind of aerospace parts Special reforming equipment proposed.
To achieve the goals above, the utility model adopts the technical scheme that
A kind of aerospace parts Special reforming equipment, including bottom plate, the upper surface of the bottom plate offer workpiece slot, the bottom Plate is symmetrically fixedly connected with support column close to the upper surface of end positions, and two support columns are solid between the side wall on top Surely be connected with support plate, slide opening corresponding with workpiece groove location offered in the support plate, be interspersed in the slide opening with The matched nose bar of slide opening, and nose bar is slidably connected with slide opening, opens up that there are two symmetrical sliding slot, institutes on the inner wall of the slide opening The lateral wall for stating nose bar correspond to be fixedly connected at the position of sliding slot with the matched sliding block of sliding slot, and sliding block and corresponding sliding slot are sliding Dynamic connection, the sliding slot are fixedly connected with the first spring close to the side of bottom plate, and the other end of first spring is slided with corresponding The side wall of block is fixedly connected, and the upper surface of the support plate is fixedly connected with driving motor, and the output axis connection of driving motor There is cam, the nose bar is equipped with close to one end of cam to be consolidated with the matched idler wheel of cam, the nose bar far from one end of cam Surely it is connected with pressure block.
Preferably, slide cartridge is fixedly connected in the one side wall of the workpiece slot, the cylinder bottom inside the slide cartridge is fixedly connected Have a second spring, the other end of the second spring be fixedly connected with the matched slide bar of slide cartridge, and slide bar and slide cartridge sliding connect It connects, the slide bar is fixedly connected with and the matched L-type baffle of workpiece slot, and L-type baffle and workpiece far from one end of second spring Slot is slidably connected, and the L-type baffle slidably connects fixture block far from the side of slide bar, and the upper surface of the fixture block is rotatably connected to Threaded rod, the other end of the threaded rod runs through the horizontal plane of L-type baffle and upwardly extends, and the water of threaded rod and L-type baffle Flat thread connection.
Preferably, the sliding block offers ball grooves close to the side of sliding slot slot bottom, rolls and is connected in the ball grooves Ball, the ball passes through the notch of ball grooves far from one end of ball grooves slot bottom and extends outwardly, and rolls and be connected to sliding slot Slot bottom.
Preferably, the L-type baffle is far from being fixedly connected with L-type pull rod on the side wall of fixture block.
Preferably, the threaded rod is fixedly connected with handle far from one end of fixture block.
Preferably, the lower surface of the fixture block is connected with non-slip mat.
Compared with prior art, the utility model provides a kind of aerospace parts Special reforming equipment, has following beneficial Effect:
1, the aerospace parts Special reforming equipment passes through setting workpiece slot, nose bar, sliding slot, sliding block, the first spring, driving Aerospace parts to shaping are placed in workpiece slot by motor, cam and pressure block, and starting driving motor band moving cam rotates, convex Wheel drives nose bar to slide along slide opening, meanwhile, sliding block is slided along sliding slot, by the first spring reset in sliding slot, and then is made It obtains nose bar to pump, drives pressure block to carry out shaping operation to aerospace parts, avoid manual operation, greatly improve The efficiency of shaping operation.
2, the aerospace parts Special reforming equipment passes through setting workpiece slot, slide cartridge, second spring, slide bar, L-type baffle, folder Block and threaded rod pull L-type baffle to slide along workpiece slot, meanwhile, the cylinder bottom direction of slide bar towards slide cartridge is slided and compresses the Aerospace parts to shaping are placed in workpiece slot by two springs, unclamp L-type baffle, second spring resets, to make L-type baffle Limit is clamped to the aerospace parts in workpiece slot, rotating threaded rod makes fixture block slide downward, aerospace parts is compressed solid It is fixed, to effectively prevent shifting in reforming process and influencing shaping quality.
It is not directed to part in the device to be the same as those in the prior art or can be realized by using the prior art, the utility model The shaping efficiency of aerospace parts is improved, and conveniently aerospace parts are fixed, prevents from shifting in reforming process, into And improve shaping quality.
Detailed description of the invention
Fig. 1 be the utility model proposes a kind of aerospace parts Special reforming equipment structural schematic diagram;
Fig. 2 is the enlarged drawing of part A in Fig. 1;
Fig. 3 is the enlarged drawing of part B in Fig. 1.
In figure: 1 bottom plate, 2 workpiece slots, 3 support columns, 4 support plates, 5 nose bars, 6 sliding slots, 7 sliding blocks, 8 first springs, 9 drivings Motor, 10 cams, 11 pressure blocks, 12 slide cartridges, 13 second springs, 14 slide bars, 15L type baffle, 16 fixture blocks, 17 threaded rods, 18 rollings Pearl, 19 L-type pull rods, 20 handles.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole Embodiment.
In the description of the present invention, it should be understood that term " on ", "lower", "front", "rear", "left", "right", The orientation or positional relationship of the instructions such as "top", "bottom", "inner", "outside" is to be based on the orientation or positional relationship shown in the drawings, and is only For ease of description the utility model and simplify description, rather than the device or element of indication or suggestion meaning must have it is specific Orientation, be constructed and operated in a specific orientation, therefore should not be understood as limiting the present invention.
Referring to Fig.1-3, a kind of aerospace parts Special reforming equipment, including bottom plate 1, the upper surface of bottom plate 1 offer workpiece Slot 2, bottom plate 1 are symmetrically fixedly connected with support column 3, side wall of two support columns 3 close to top close to the upper surface of end positions Between be fixedly connected with support plate 4, slide opening corresponding with 2 position of workpiece slot is offered in support plate 4, be interspersed in slide opening with The matched nose bar 5 of slide opening, and nose bar 5 is slidably connected with slide opening, opens up that there are two symmetrical sliding slots 6 on the inner wall of slide opening, convex The lateral wall of bar 5 corresponds to be fixedly connected with and the matched sliding block 7 of sliding slot 6, and sliding block 7 and corresponding sliding slot 6 at the position of sliding slot 6 It is slidably connected, sliding slot 6 is fixedly connected with the first spring 8 close to the side of bottom plate 1, the other end of the first spring 8 and corresponding sliding block 7 Side wall be fixedly connected, the upper surface of support plate 4 is fixedly connected with driving motor 9, and the output shaft of driving motor 9 be connected with it is convex Wheel 10, nose bar 5 is equipped with close to one end of cam 10 and fixes with the matched idler wheel of cam 10, nose bar 5 far from one end of cam 10 It is connected with pressure block 11, the aerospace parts to shaping are placed in workpiece slot 2, starting driving motor 9 is rotated with moving cam 10, convex 10 drive nose bar 5 of wheel is slided along slide opening, meanwhile, sliding block 7 is slided along sliding slot 6, it is resetted by the first spring 8 in sliding slot 6, So that nose bar 5 pumps, drives pressure block 11 to carry out shaping operation to aerospace parts, avoid artificial behaviour Make, substantially increases the efficiency of shaping operation.
Slide cartridge 12 is fixedly connected in the one side wall of workpiece slot 2, the cylinder bottom inside slide cartridge 12 is fixedly connected with second spring 13, the other end of second spring 13 be fixedly connected with the matched slide bar 14 of slide cartridge 12, and slide bar 14 is slidably connected with slide cartridge 12, Slide bar 14 is fixedly connected with and the matched L-type baffle 15 of workpiece slot 2, and L-type baffle 15 and work far from one end of second spring 13 Part slot 2 is slidably connected, and L-type baffle 15 slidably connects fixture block 16 far from the side of slide bar 14, and the upper surface of fixture block 16, which rotates, to be connected It is connected to threaded rod 17, the other end of threaded rod 17 runs through the horizontal plane of L-type baffle 15 and upwardly extends, and threaded rod 17 and L-type The horizontal plane of baffle 15 is threadedly coupled, and L-type baffle 15 is pulled to slide along workpiece slot 2, meanwhile, cylinder of the slide bar 14 towards slide cartridge 12 Second spring 13 is slided and is compressed in bottom direction, and the aerospace parts to shaping are placed in workpiece slot 2, release L-type baffle 15, and second Spring 13 resets, so that L-type baffle 15 be made to be clamped limit to the aerospace parts in workpiece slot 2, rotating threaded rod 17 makes to press from both sides 16 slide downward of block, aerospace parts are fixed, to effectively prevent shifting in reforming process and influencing shaping quality.
Sliding block 7 offers ball grooves close to the side of 6 slot bottom of sliding slot, rolls in ball grooves and is connected with ball 18, ball 18 One end far from ball grooves slot bottom passes through the notch of ball grooves and extends outwardly, and rolls the slot bottom for being connected to sliding slot 6, reduces and slides Frictional force between block 7 and sliding slot 6.
L-type baffle 15 is fixedly connected with L-type pull rod 19 on the side wall far from fixture block 16, facilitates and pulls L-type baffle along work Part slot 2 slides.
Threaded rod 17 is fixedly connected with handle 20 far from one end of fixture block 16, convenient for controlling the rotation of threaded rod 17.
The lower surface of fixture block 16 is connected with non-slip mat, improves the stability that fixture block 16 clamps.
In the utility model, the aerospace parts to shaping are placed in workpiece slot 2, start driving motor 9 with moving cam 10 Rotation, cam 10 drive nose bar 5 to slide along slide opening, meanwhile, sliding block 7 is slided along sliding slot 6, passes through the first bullet in sliding slot 6 Spring 8 resets, so that nose bar 5 pumps, drives pressure block 11 to carry out shaping operation to aerospace parts, avoids Manual operation substantially increases the efficiency of shaping operation;L-type baffle 15 is pulled to slide along workpiece slot 2, meanwhile, 14 court of slide bar The cylinder bottom direction of slide cartridge 12 slide and compress second spring 13, the aerospace parts to shaping are placed in workpiece slot 2, L is unclamped Type baffle 15, second spring 13 resets, so that L-type baffle 15 be made to be clamped limit to the aerospace parts in workpiece slot 2, rotates Threaded rod 17 makes 16 slide downward of fixture block, aerospace parts is fixed, thus effectively prevent shifting in reforming process and Influence shaping quality.
The preferable specific embodiment of the above, only the utility model, but the protection scope of the utility model is not It is confined to this, anyone skilled in the art is within the technical scope disclosed by the utility model, practical according to this Novel technical solution and its utility model design are subject to equivalent substitution or change, should all cover the protection model in the utility model Within enclosing.

Claims (6)

1. a kind of aerospace parts Special reforming equipment, including bottom plate (1), which is characterized in that the upper surface of the bottom plate (1) opens up Have workpiece slot (2), the bottom plate (1) is symmetrically fixedly connected with support column (3) close to the upper surface of end positions, two branch Dagger (3) is fixedly connected with support plate (4) between the side wall on top, is offered on the support plate (4) and workpiece slot (2) The corresponding slide opening in position, be interspersed in the slide opening with the matched nose bar of slide opening (5), and nose bar (5) is slidably connected with slide opening, It is opened up on the inner wall of the slide opening there are two symmetrical sliding slot (6), the lateral wall of the nose bar (5) corresponds to the position of sliding slot (6) The place of setting is fixedly connected with and sliding slot (6) matched sliding block (7), and sliding block (7) is slidably connected with corresponding sliding slot (6), the cunning Slot (6) is fixedly connected with the first spring (8) close to the side of bottom plate (1), the other end of first spring (8) and corresponding sliding block (7) side wall is fixedly connected, and the upper surface of the support plate (4) is fixedly connected with driving motor (9), and driving motor (9) Output shaft is connected with cam (10), and the nose bar (5) is equipped with close to the one end of cam (10) and cam (10) matched idler wheel, The nose bar (5) is fixedly connected with pressure block (11) far from the one end of cam (10).
2. a kind of aerospace parts Special reforming equipment according to claim 1, which is characterized in that the workpiece slot (2) It is fixedly connected in one side wall slide cartridge (12), the internal cylinder bottom of the slide cartridge (12) is fixedly connected with second spring (13), described The other end of second spring (13) is fixedly connected with and slide cartridge (12) matched slide bar (14), and slide bar (14) and slide cartridge (12) are sliding Dynamic connection, the slide bar (14) are fixedly connected with and workpiece slot (2) matched L-type baffle far from the one end of second spring (13) (15), and L-type baffle (15) is slidably connected with workpiece slot (2), and the L-type baffle (15) connects far from a Slideslip of slide bar (14) It is connected to fixture block (16), the upper surface of the fixture block (16) is rotatably connected to threaded rod (17), the other end of the threaded rod (17) Through L-type baffle (15) horizontal plane and upwardly extend, and threaded rod (17) is threadedly coupled with the horizontal plane of L-type baffle (15).
3. a kind of aerospace parts Special reforming equipment according to claim 1, which is characterized in that the sliding block (7) is close The side of sliding slot (6) slot bottom offers ball grooves, rolls and is connected with ball (18) in the ball grooves, the ball (18) is separate One end of ball grooves slot bottom passes through the notch of ball grooves and extends outwardly, and rolls the slot bottom for being connected to sliding slot (6).
4. a kind of aerospace parts Special reforming equipment according to claim 2, which is characterized in that the L-type baffle (15) L-type pull rod (19) are fixedly connected on side wall far from fixture block (16).
5. a kind of aerospace parts Special reforming equipment according to claim 2, which is characterized in that the threaded rod (17) is remote One end from fixture block (16) is fixedly connected with handle (20).
6. a kind of aerospace parts Special reforming equipment according to claim 2, which is characterized in that under the fixture block (16) Surface is connected with non-slip mat.
CN201821660328.6U 2018-10-14 2018-10-14 A kind of aerospace parts Special reforming equipment Active CN209174614U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201821660328.6U CN209174614U (en) 2018-10-14 2018-10-14 A kind of aerospace parts Special reforming equipment

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201821660328.6U CN209174614U (en) 2018-10-14 2018-10-14 A kind of aerospace parts Special reforming equipment

Publications (1)

Publication Number Publication Date
CN209174614U true CN209174614U (en) 2019-07-30

Family

ID=67361126

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201821660328.6U Active CN209174614U (en) 2018-10-14 2018-10-14 A kind of aerospace parts Special reforming equipment

Country Status (1)

Country Link
CN (1) CN209174614U (en)

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