CN216633352U - Be used for aerospace titanium alloy covering part cutting composite set that polishes - Google Patents

Be used for aerospace titanium alloy covering part cutting composite set that polishes Download PDF

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Publication number
CN216633352U
CN216633352U CN202123026418.4U CN202123026418U CN216633352U CN 216633352 U CN216633352 U CN 216633352U CN 202123026418 U CN202123026418 U CN 202123026418U CN 216633352 U CN216633352 U CN 216633352U
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China
Prior art keywords
plate
moving
seat
fixed plate
titanium alloy
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CN202123026418.4U
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Chinese (zh)
Inventor
李翠兰
吴卫
朱鹏
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Shenyang Sanbei Aviation Equipment Manufacturing Co ltd
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Shenyang Sanbei Aviation Equipment Manufacturing Co ltd
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Priority to CN202123026418.4U priority Critical patent/CN216633352U/en
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Abstract

The utility model discloses a cutting and polishing composite device for an aerospace titanium alloy skin part, and belongs to the technical field of machining; including bottom plate and support frame, still include: the device comprises a cutting mechanism, a polishing mechanism, a moving seat, a moving assembly and a clamping mechanism; wherein, it is equipped with the cavity to remove the seat inboard, fixture includes: the device comprises a fixed plate, a movable plate, a sliding sleeve, a guide rod and a first spring; can treat through being equipped with fixture and process the part and carry out the centre gripping fixed, can compress tightly the part of treating of centre gripping through the subassembly that compresses tightly among the fixture, do benefit to its stability, because the movable plate is close to the front end of fixed plate one side sets up for the slope, and then be convenient for quick will treat that the part alternates to fix between movable plate and the fixed plate.

Description

Be used for aerospace titanium alloy covering part cutting composite set that polishes
Technical Field
The utility model relates to the technical field of machining, in particular to a cutting and polishing composite device for an aerospace titanium alloy skin component.
Background
The aircraft skin is a dimensional component which is wrapped outside an aircraft framework structure and is fixed on the framework by using an adhesive or rivets to form the aerodynamic shape of the aircraft. The aircraft skin usually needs to be cut and polished in the production and processing process, the aircraft skin needs to be clamped and fixed in the existing production and processing process of the aircraft skin, and a clamping mechanism in the existing cutting and polishing device is relatively complex in the fixing operation of the aircraft skin and is not beneficial to production.
SUMMERY OF THE UTILITY MODEL
The utility model aims to provide a cutting and polishing composite device for an aerospace titanium alloy skin part, which aims to solve the problems in the background technology.
In order to achieve the purpose, the utility model provides the following technical scheme:
the utility model provides a be used for aerospace titanium alloy covering part cutting set composite of polishing, includes bottom plate and support frame, still includes:
the cutting mechanism is connected with the supporting frame;
the polishing mechanism is connected with the supporting frame;
the moving seat is arranged on the bottom plate in a sliding manner;
the moving assembly is connected with the moving seat and used for driving the moving seat to move;
the clamping mechanism is connected with the moving seat and used for fixing the part to be processed;
wherein, it is equipped with the cavity to remove the seat inboard, fixture includes:
the fixed plate is fixedly arranged on one side of the movable seat;
the moving plate is arranged on one side, containing the fixed plate, of the moving seat in a sliding mode, and the moving plate and the fixed plate are arranged in parallel and opposite to each other;
one end of the sliding sleeve is connected with one end of the moving plate, and the other end of the sliding sleeve is fixedly connected with the moving plate;
the guide rod is fixedly arranged in a cavity on the inner side of the moving seat, and the sliding sleeve is movably sleeved on the guide rod;
the spring I is sleeved on the guide rod, and two ends of the spring I are connected with the inner wall of the moving seat and the sliding sleeve respectively.
As a further scheme of the utility model: the fixed plate for one side of movable plate is equipped with the rotation groove, fixture still includes and compresses tightly the subassembly, it includes to compress tightly the subassembly:
the supporting column is arranged in the rotating groove;
the rotating rod is movably sleeved on the supporting column, and two ends of the rotating rod are respectively connected with a telescopic rod;
the second springs are respectively sleeved on the telescopic rods, and one ends of the second springs are connected with the rotating rod;
the compression block is connected with the other end of the telescopic rod and is connected with the other end of the second spring;
the torsion spring is sleeved on the support column, and two ends of the torsion spring are respectively connected with the support column and the rotating rod;
and the pull rope, one end of the pull rope is connected with the rotating rod, and the other end of the pull rope penetrates through the fixed plate and the movable seat and is connected with the sliding sleeve.
As a further scheme of the utility model: the cutting mechanism includes:
one end of the first air cylinder is connected with the support frame;
the first motor is connected with the other end of the first cylinder;
the blade is connected with the output end of the first motor.
As a further scheme of the utility model: the grinding mechanism includes:
one end of the second air cylinder is connected with the support frame;
the second motor is connected with the other end of the second cylinder;
and the polishing disc is connected with the output end of the second motor.
As a further scheme of the utility model: the moving assembly includes:
the threaded rod is supported on the bottom plate, and the movable seat is sleeved on the threaded rod in a threaded manner;
and the third motor is arranged on the bottom plate, and one end of the threaded rod is connected with the output end of the third motor.
As a further scheme of the utility model: the middle part of the bottom plate is provided with a sewage draining groove, the bottom side of the bottom plate is provided with a supporting seat, the supporting seat is provided with a collecting frame, and the front end of the movable plate, which is close to one side of the fixed plate, is obliquely arranged.
Compared with the prior art, the utility model has the beneficial effects that: the clamping mechanism is arranged on the front end of the fixed plate, the clamping mechanism is arranged on the rear end of the movable plate, the clamping mechanism is arranged on the front end of the fixed plate, and the clamping mechanism is arranged on the front end of the movable plate.
Drawings
Fig. 1 is a schematic structural diagram of a cutting and polishing composite device for an aerospace titanium alloy skin component.
Fig. 2 is a partially enlarged view of a portion a in fig. 1.
Notations for reference numerals: 1-bottom plate, 2-support frame, 3-support seat, 4-collection frame, 5-cylinder I, 6-cylinder II, 7-motor I, 8-blade, 9-motor II, 10-polishing disc, 11-threaded rod, 12-motor III, 13-moving seat, 14-spring I, 15-sliding sleeve, 16-moving plate, 17-guide rod, 18-fixing plate, 19-rotating groove, 20-support column, 21-torsion spring, 22-rotating rod, 23-spring II, 24-pressing block, 25-pull rope and 26-telescopic rod.
Detailed Description
The technical solution of the present patent will be described in further detail with reference to the following embodiments.
Referring to fig. 1, an embodiment of the present invention provides a composite cutting and polishing device for an aerospace titanium alloy skin component, including a base plate 1 and a supporting frame 2, and further including:
the cutting mechanism is connected with the support frame 2;
the polishing mechanism is connected with the support frame 2;
the moving seat 13 is arranged on the bottom plate 1 in a sliding manner;
the moving assembly is connected with the moving seat 13 and is used for driving the moving seat 13 to move;
the clamping mechanism is connected with the moving seat 13 and is used for fixing a part to be processed;
wherein, it is equipped with the cavity to remove 13 inboards of seat, fixture includes:
a fixed plate 18, wherein the fixed plate 18 is fixedly arranged on one side of the movable base 13;
the moving plate 16 is arranged on one side, containing the fixed plate 18, of the moving seat 13 in a sliding manner, and the moving plate 16 and the fixed plate 18 are arranged in parallel and opposite to each other;
one end of the sliding sleeve 15 is connected with one end of the moving plate 16;
the guide rod 17 is fixedly arranged in a cavity on the inner side of the moving seat 13, and the sliding sleeve 15 is movably sleeved on the guide rod 17;
the first spring 14 is sleeved on the guide rod 17, and two ends of the first spring 14 are respectively connected with the inner wall of the moving seat 13 and the sliding sleeve 15.
When the tool is used, a to-be-machined part is inserted between the movable plate 16 and the fixed plate 18, the movable plate 16 slides on one side of the movable seat 13, the movable plate 16 can be supported through the elastic force of the first spring 14, the to-be-machined part can be fixed between the movable plate 16 and the fixed plate 18, and the clamped to-be-machined part can be cut and polished through the cutting mechanism and the polishing mechanism.
As an embodiment of the present invention, referring to fig. 1 to 2, a rotating groove 19 is formed on one side of the fixed plate 18 opposite to the moving plate 16, and the clamping mechanism further includes a pressing assembly, which includes:
the supporting column 20 is arranged in the rotating groove 19;
the rotating rod 22 is movably sleeved on the supporting column 20, and two ends of the rotating rod 22 are respectively connected with a telescopic rod 26;
the second springs 23 are respectively sleeved on the telescopic rods 26, and one ends of the second springs 23 are connected with the rotating rod 22;
the pressing block 24 is connected with the other end of the telescopic rod 26, and the pressing block 24 is connected with the other end of the second spring 23;
the torsion spring 21 is sleeved on the support column 20, and two ends of the torsion spring 21 are respectively connected with the support column 20 and the rotating rod 22;
and one end of the pull rope 25 is connected with the rotating rod 22, and the other end of the pull rope 25 penetrates through the fixed plate 18 and the movable seat 13 and is connected with the sliding sleeve 15.
When a workpiece to be machined is inserted between the moving plate 16 and the fixed plate 18, the moving plate 16 drives the sliding sleeve 15 to move downwards, the sliding sleeve 15 further pulls the pull rope 25, the pull rope 25 pulls the rotating rod 22 to rotate around the supporting column 20, so that the pressing block 24 at the other end of the rotating rod 22 is pressed on the part to be machined, and the part to be machined can be stably clamped. After the workpiece is machined, the moving plate 16 is lifted up under the restoring force of the first spring 14 and returns to the original position, the pull rope is loosened, and the rotating rod 22 also rotates back to the original position under the restoring force of the torsion spring 21 to prepare for next machining.
Referring to fig. 1 as an embodiment of the present invention, the cutting mechanism includes:
one end of the first air cylinder 5 is connected with the support frame 2;
the motor I7, the motor I7 is connected with the other end of the cylinder I5;
and the blade 8, and the blade 8 is connected with the output end of the first motor 7.
The first air cylinder 5 can drive the first motor 7 to adjust the height, and the first motor 7 further drives the blade 8 to cut the part to be processed.
Referring to fig. 1 as an embodiment of the present invention, the polishing mechanism includes:
one end of the second cylinder 6 is connected with the support frame 2;
the second motor 9, the second motor 9 is connected with the other end of the second cylinder 6;
and the polishing disc 10 is connected with the output end of the second motor 9.
The second cylinder 6 drives the second motor 9 to move downwards, and the second motor 9 further drives the polishing disc 10 to polish the cut parts.
Referring to fig. 1 as an embodiment of the present invention, the moving assembly includes:
the threaded rod 11 is supported on the bottom plate 1, and the movable seat 13 is sleeved on the threaded rod 11 in a threaded manner;
and the motor III 12 is arranged on the bottom plate 1, and one end of the threaded rod 11 is connected with the output end of the motor III 12.
Through three 12 drives of motor the threaded rod 11 rotates, threaded rod 11 drives and removes seat 13 and is in bottom plate 1 moves, can make the part after the cutting, can be polished fast.
Referring to fig. 1 and 2, as an embodiment of the present invention, a sewage draining groove is formed in the middle of the bottom plate 1, a supporting seat 3 is arranged at the bottom side of the bottom plate 1, a collecting frame 4 is arranged on the supporting seat 3, and the front end of the moving plate 16 close to one side of the fixed plate 18 is arranged in an inclined manner; through being equipped with the blowdown groove, can make the piece that produces in cutting and the process of polishing get into in the collection frame 4, because the movable plate 16 is close to the front end of fixed plate 18 one side sets up for the slope, then be convenient for wait to process the part and alternate fast and advance between movable plate 16 and the fixed plate 18.
The working principle is as follows: when the device is used, a to-be-processed part is inserted between the moving plate 16 and the fixed plate 18, because the front end of the moving plate 16 close to one side of the fixed plate 18 is obliquely arranged, the to-be-processed part can be conveniently and rapidly inserted between the moving plate 16 and the fixed plate 18, the moving plate 16 slides on one side of the moving seat 13, the moving plate 16 can be supported by the elastic force of the first spring 14, the to-be-processed part can be fixed between the moving plate 16 and the fixed plate 18, when a to-be-processed part is inserted between the moving plate 16 and the fixed plate 18, the moving plate 16 drives the sliding sleeve 15 to move downwards, the sliding sleeve 15 further pulls the pull rope 25, the pull rope 25 pulls the rotating rod 22 to rotate around the supporting column 20, the pressing block 24 can be pressed on the to-be-processed part, when the to-be-processed part is kept stable, dwang 22 is in under torsional spring 21's the elastic drive, can drive compact heap 24 is stabilized to be pressed on waiting to process the part, can make to wait to process the part and stably by the centre gripping, can cut and polish the part of waiting to process of centre gripping through cutting mechanism and grinding machanism.

Claims (6)

1. The utility model provides a be used for aerospace titanium alloy covering part cutting set composite of polishing, includes bottom plate and support frame, its characterized in that still includes:
the cutting mechanism is connected with the supporting frame;
the polishing mechanism is connected with the supporting frame;
the moving seat is arranged on the bottom plate in a sliding manner;
the moving assembly is connected with the moving seat and used for driving the moving seat to move;
the clamping mechanism is connected with the moving seat and used for fixing the part to be processed;
wherein, it is equipped with the cavity to remove the seat inboard, fixture includes:
the fixed plate is fixedly arranged on one side of the movable seat;
the moving plate is arranged on one side, containing the fixed plate, of the moving seat in a sliding mode, and the moving plate and the fixed plate are arranged in parallel and opposite to each other;
one end of the sliding sleeve is connected with one end of the moving plate, and the other end of the sliding sleeve is fixedly connected with the moving plate;
the guide rod is fixedly arranged in a cavity on the inner side of the moving seat, and the sliding sleeve is movably sleeved on the guide rod;
the spring I is sleeved on the guide rod, and two ends of the spring I are connected with the inner wall of the moving seat and the sliding sleeve respectively.
2. The composite cutting and grinding device for the aerospace titanium alloy skin part as claimed in claim 1, wherein a side of the fixed plate opposite to the moving plate is provided with a rotating groove, the clamping mechanism further comprises a pressing assembly, and the pressing assembly comprises:
the supporting column is arranged in the rotating groove;
the rotating rod is movably sleeved on the supporting column, and two ends of the rotating rod are respectively connected with a telescopic rod;
the second springs are respectively sleeved on the telescopic rods, and one ends of the second springs are connected with the rotating rod;
the pressing block is connected with the other end of the telescopic rod and connected with the other end of the second spring;
the torsion spring is sleeved on the support column, and two ends of the torsion spring are respectively connected with the support column and the rotating rod;
and the pull rope, one end of the pull rope is connected with the rotating rod, and the other end of the pull rope penetrates through the fixed plate and the movable seat and is connected with the sliding sleeve.
3. The composite cutting and grinding device for the aerospace titanium alloy skin component as claimed in claim 1, wherein the cutting mechanism comprises:
one end of the first air cylinder is connected with the support frame;
the first motor is connected with the other end of the first cylinder;
the blade is connected with the output end of the first motor.
4. The composite cutting and grinding device for the aerospace titanium alloy skin component as claimed in claim 1, wherein the grinding mechanism comprises:
one end of the second air cylinder is connected with the support frame;
the second motor is connected with the other end of the second cylinder;
and the polishing disc is connected with the output end of the second motor.
5. The aerospace titanium alloy skin component cutting and sanding composite device of claim 1, wherein the movement assembly comprises:
the threaded rod is supported on the bottom plate, and the movable seat is sleeved on the threaded rod in a threaded manner;
and the third motor is arranged on the bottom plate, and one end of the threaded rod is connected with the output end of the third motor.
6. The composite cutting and grinding device for the aerospace titanium alloy skin part as claimed in claim 5, wherein a sewage draining groove is formed in the middle of the bottom plate, a supporting seat is arranged on the bottom side of the bottom plate, a collecting frame is arranged on the supporting seat, and the front end of one side, close to the fixed plate, of the movable plate is obliquely arranged.
CN202123026418.4U 2021-12-06 2021-12-06 Be used for aerospace titanium alloy covering part cutting composite set that polishes Active CN216633352U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202123026418.4U CN216633352U (en) 2021-12-06 2021-12-06 Be used for aerospace titanium alloy covering part cutting composite set that polishes

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202123026418.4U CN216633352U (en) 2021-12-06 2021-12-06 Be used for aerospace titanium alloy covering part cutting composite set that polishes

Publications (1)

Publication Number Publication Date
CN216633352U true CN216633352U (en) 2022-05-31

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CN202123026418.4U Active CN216633352U (en) 2021-12-06 2021-12-06 Be used for aerospace titanium alloy covering part cutting composite set that polishes

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CN (1) CN216633352U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN116475769A (en) * 2023-06-15 2023-07-25 苏州骅汉精密机械有限责任公司 Cutting equipment for cutting die casting material handle
CN116765848A (en) * 2023-08-25 2023-09-19 福建祥鑫新能源汽车配件制造有限公司 Profile cutting device for processing new energy battery tray

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN116475769A (en) * 2023-06-15 2023-07-25 苏州骅汉精密机械有限责任公司 Cutting equipment for cutting die casting material handle
CN116475769B (en) * 2023-06-15 2023-08-29 苏州骅汉精密机械有限责任公司 Cutting equipment for cutting die casting material handle
CN116765848A (en) * 2023-08-25 2023-09-19 福建祥鑫新能源汽车配件制造有限公司 Profile cutting device for processing new energy battery tray
CN116765848B (en) * 2023-08-25 2023-11-07 福建祥鑫新能源汽车配件制造有限公司 Profile cutting device for processing new energy battery tray

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