CN215942831U - Aircraft front connector foundry goods processing location frock - Google Patents
Aircraft front connector foundry goods processing location frock Download PDFInfo
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- CN215942831U CN215942831U CN202122102734.9U CN202122102734U CN215942831U CN 215942831 U CN215942831 U CN 215942831U CN 202122102734 U CN202122102734 U CN 202122102734U CN 215942831 U CN215942831 U CN 215942831U
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- 238000003754 machining Methods 0.000 claims abstract description 34
- 238000005266 casting Methods 0.000 claims abstract description 32
- 230000005540 biological transmission Effects 0.000 claims description 26
- 230000000694 effects Effects 0.000 abstract description 4
- 230000009286 beneficial effect Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000009434 installation Methods 0.000 description 1
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Abstract
The utility model relates to the technical field of machining of airplane front joint castings, in particular to a machining and positioning tool for airplane front joint castings, which can be adaptively adjusted according to the size of a workpiece, improve the positioning effect, improve the compatibility and reduce the use limitation; including first link, the second link, first mount pad, the axle bed, the screwed pipe, first screw rod, first link, first anchor clamps, the second mount pad, the second connecting seat, the second screw rod, the second anchor clamps, lock nut and handle, the bottom left side and the bottom right side of first link all are provided with the second link, the top left side at first link is installed to first mount pad, the top of first mount pad is provided with the axle bed, the screwed pipe is installed in the axle bed, first screw rod spiral shell dress is in the screwed pipe, the right-hand member of first screw rod is provided with first link, the right-hand member of first link is provided with first anchor clamps, the top right side at first link is installed to the second mount pad.
Description
Technical Field
The utility model relates to the technical field of machining of airplane front joint castings, in particular to a machining and positioning tool for airplane front joint castings.
Background
The machining and positioning tool for the airplane front joint casting is a positioning auxiliary device for machining the airplane front joint casting, and is widely used in the field of machining of the airplane front joint casting; the existing machining and positioning tool for the front connector casting of the airplane is mainly fixedly installed and connected, effective corresponding adjustment cannot be carried out according to the size of an actual workpiece, the workpiece with a single size can only be positioned, and the use limitation is high.
SUMMERY OF THE UTILITY MODEL
In order to solve the technical problems, the utility model provides the machining and positioning tool for the airplane front joint casting, which can be adaptively adjusted according to the size of a workpiece, improve the positioning effect, improve the compatibility and reduce the use limitation.
The utility model relates to a machining and positioning tool for an airplane front joint casting, which comprises a first connecting frame, a second connecting frame, a first mounting seat, a shaft seat, a threaded pipe, a first screw rod, a first connecting seat, a first clamp, a second mounting seat, a second connecting seat, a second screw rod, a second clamp, a locking nut and a handle, wherein the second connecting frame is arranged on the left side of the bottom end and the right side of the bottom end of the first connecting frame, the first mounting seat is arranged on the left side of the top end of the first connecting frame, the shaft seat is arranged on the top end of the first mounting seat, the threaded pipe is arranged in the shaft seat, the first screw rod is screwed in the threaded pipe, the first connecting seat is arranged on the right end of the first screw rod, the first clamp is arranged on the right end of the first connecting seat, the second mounting seat is arranged on the right side of the top end of the first connecting frame, the second connecting seat is arranged on the top end of the second mounting seat, the second screw rod transversely penetrates through the second connecting seat, the second clamp is arranged on the left end of the second screw rod, the locking nut is sleeved on the second screw rod in a threaded mode, the right end of the second screw rod is provided with a handle, the middle of the top end of the first connecting frame is provided with an operating platform, the threaded pipe is driven through a power mechanism, and the bottom end of the first connecting seat is provided with a limiting mechanism.
The utility model discloses a machining and positioning tool for an airplane front connector casting.
The power mechanism comprises a first transmission wheel, a power motor, a second transmission wheel and a transmission belt, the first transmission wheel is installed at the left part of the threaded pipe, the power motor is installed at the left side of the bottom end of the first connecting frame, the second transmission wheel is arranged at the output end of the left part of the power motor, and the transmission belt is installed on the first transmission wheel and the second transmission wheel.
According to the machining and positioning tool for the airplane front joint casting, the third connecting frames are arranged on the left side of the top end and the right side of the top end of the first connecting frame, the left end and the right end of the fourth connecting frame are respectively connected with the upper portions of the two groups of third connecting frames, and the bottom end of the fourth connecting frame is provided with a plurality of groups of illuminating lamps.
According to the machining and positioning tool for the airplane front joint casting, the supports are arranged at the bottom ends of the two groups of second connecting frames.
According to the machining and positioning tool for the airplane front joint casting, the support frames are arranged on the lower portions of the two groups of third connecting frames, and the bottom ends of the two groups of support frames are connected with the top end of the first connecting frame.
The machining and positioning tool for the airplane front joint casting further comprises brackets, and the brackets are mounted at the lower parts of the two groups of second connecting frames.
Compared with the prior art, the utility model has the beneficial effects that: arrange the work piece in on the operation panel, then promote the handle, make the second anchor clamps paste tightly with the right-hand member of work piece, then rotate lock nut, make lock nut paste tightly with the left end of second connecting seat, it is spacing to carry out the second screw rod, later start motor power, motor power drives the rotation of second drive wheel, pivoted second drive wheel passes through the drive belt and drives first drive wheel and screwed pipe rotation, the pivoted screwed pipe drives first screw rod and stretches out, make the left end of first anchor clamps and work piece paste tightly, the completion to the fixed of work piece can, thereby can carry out adaptability adjustment according to the size of work piece, improve the location effect, improve compatibility, reduce the use limitation.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a partially enlarged view of the portion A in FIG. 1;
FIG. 3 is a partially enlarged view of the portion B in FIG. 1;
FIG. 4 is a partially enlarged view of the portion C of FIG. 1;
in the drawings, the reference numbers: 1. a first connecting frame; 2. a second link frame; 3. a first mounting seat; 4. a shaft seat; 5. a threaded pipe; 6. a first screw; 7. a first connecting seat; 8. a first clamp; 9. a second mounting seat; 10. a second connecting seat; 11. a second screw; 12. a second clamp; 13. locking the nut; 14. a handle; 15. an operation table; 16. a slide rail; 17. a slide base; 18. a connecting rod; 19. a first drive pulley; 20. a power motor; 21. a second transmission wheel; 22. a transmission belt; 23. a third connecting frame; 24. a fourth link frame; 25. an illuminating lamp; 26. a support; 27. a support frame; 28. a bracket.
Detailed Description
The following detailed description of embodiments of the present invention is provided in connection with the accompanying drawings and examples. The following examples are intended to illustrate the utility model but are not intended to limit the scope of the utility model.
As shown in fig. 1 to 4, the machining and positioning tool for the airplane front joint casting comprises a first connecting frame 1, a second connecting frame 2, a first mounting seat 3, a shaft seat 4, a threaded pipe 5, a first screw 6, a first connecting seat 7, a first clamp 8, a second mounting seat 9, a second connecting seat 10, a second screw 11, a second clamp 12, a locking nut 13 and a handle 14, wherein the second connecting frame 2 is arranged on the left side of the bottom end and the right side of the bottom end of the first connecting frame 1, the first mounting seat 3 is arranged on the left side of the top end of the first connecting frame 1, the shaft seat 4 is arranged on the top end of the first mounting seat 3, the threaded pipe 5 is arranged in the shaft seat 4, the first screw 6 is screwed in the threaded pipe 5, the first connecting seat 7 is arranged on the right end of the first screw 6, the first clamp 8 is arranged on the right end of the first connecting seat 7, the second mounting seat 9 is arranged on the right side of the top end of the first connecting frame 1, a second connecting seat 10 is arranged at the top end of the second mounting seat 9, a second screw rod 11 transversely penetrates through the second connecting seat 10, a second clamp 12 is arranged at the left end of the second screw rod 11, a locking nut 13 is sleeved on the second screw rod 11 in a threaded manner, a handle 14 is arranged at the right end of the second screw rod 11, an operating platform 15 is arranged in the middle of the top end of the first connecting frame 1, the threaded pipe 5 is driven by a power mechanism, and a limiting mechanism is arranged at the bottom end of the first connecting seat 7; arrange the work piece in on the operation panel 15, then promote handle 14, make second anchor clamps 12 paste tightly with the right-hand member of work piece, then rotate lock nut 13, make lock nut 13 paste tightly with the left end of second connecting seat 10, it is spacing to carry out second screw rod 11, later start power unit, power unit drives screwed pipe 5 and rotates, pivoted screwed pipe 5 drives first screw rod 6 and stretches out, make first anchor clamps 8 paste tightly with the left end of work piece, accomplish fixed to the work piece can, thereby can carry out adaptability adjustment according to the size of work piece, improve positioning effect, improve compatibility, reduce and use the limitation.
The utility model relates to a machining and positioning tool for an airplane front joint casting, wherein a limiting mechanism comprises a sliding rail 16, a sliding seat 17 and a connecting rod 18, the sliding rail 16 is installed at the top end of a first connecting frame 1, the sliding seat 17 is arranged on the sliding rail 16 in a sliding manner, the connecting rod 18 is arranged at the top end of the sliding seat 17, and the top end of the connecting rod 18 is connected with a first connecting seat 7; through setting up slide rail 16, slide 17 and connecting rod 18, can effectively spacing to first screw rod 6, guarantee first screw rod 6 stretch out stability, improve the practicality.
The utility model relates to a machining and positioning tool for an airplane front joint casting, wherein a power mechanism comprises a first transmission wheel 19, a power motor 20, a second transmission wheel 21 and a transmission belt 22, the first transmission wheel 19 is arranged at the left part of a threaded pipe 5, the power motor 20 is arranged at the left side of the bottom end of a first connecting frame 1, the second transmission wheel 21 is arranged at the output end of the left part of the power motor 20, and the transmission belt 22 is arranged on the first transmission wheel 19 and the second transmission wheel 21; the power motor 20 is started, the power motor 20 drives the second driving wheel 21 to rotate, the rotating second driving wheel 21 drives the first driving wheel 19 and the threaded pipe 5 to rotate through the driving belt 22, so that the first screw rod 6 is driven to stretch out, the workpiece is clamped and fixed through the first clamp 8, the positioning efficiency is effectively improved, and the practicability is improved.
According to the machining and positioning tool for the airplane front joint casting, the third connecting frames 23 are arranged on the left side of the top end and the right side of the top end of the first connecting frame 1, the left end and the right end of the fourth connecting frame 24 are respectively connected with the upper parts of the two groups of third connecting frames 23, and a plurality of groups of illuminating lamps 25 are arranged at the bottom end of the fourth connecting frame 24; through setting up multiunit light 25, can effectively throw light on to the processing region of below, improve the practicality.
According to the machining and positioning tool for the airplane front joint casting, the bottom ends of the two groups of second connecting frames 2 are provided with the supports 26; through setting up two sets of supports 26, the area of contact of two sets of second link 2 of effective increase and ground improves holistic stability.
According to the machining and positioning tool for the airplane front joint casting, the supporting frames 27 are arranged at the lower parts of the two groups of third connecting frames 23, and the bottom ends of the two groups of supporting frames 27 are connected with the top end of the first connecting frame 1; through setting up two sets of support frames 27, can effectively strengthen the fixed and support to two sets of third link 23, improve the stability of two sets of third link 23.
The machining and positioning tool for the airplane front joint casting further comprises brackets 28, wherein the brackets 28 are arranged at the lower parts of the two groups of second connecting frames 2; by providing the bracket 28, the workpiece to be processed can be housed, and the convenience of use can be improved.
The machining and positioning tool for the airplane front joint casting has the advantages that a workpiece is placed on the operating table 15, the handle 14 is pushed to enable the second clamp 12 to be attached to the right end of the workpiece, the locking nut 13 is rotated to enable the locking nut 13 to be attached to the left end of the second connecting seat 10, the second screw rod 11 is limited, then the power mechanism is started, the power mechanism drives the threaded pipe 5 to rotate, the rotating threaded pipe 5 drives the first screw rod 6 to extend out, the first clamp 8 is attached to the left end of the workpiece, and the workpiece is fixed.
According to the machining and positioning tool for the airplane front joint casting, the installation mode, the connection mode or the arrangement mode are common mechanical modes, and the machining and positioning tool can be implemented as long as the beneficial effects of the machining and positioning tool are achieved; the power motor and the illuminating lamp of the machining and positioning tool for the airplane front joint casting are purchased from the market, and technicians in the industry only need to install and operate the tool according to the accompanying instructions.
The above description is only a preferred embodiment of the present invention, and it should be noted that, for those skilled in the art, several modifications and variations can be made without departing from the technical principle of the present invention, and these modifications and variations should also be regarded as the protection scope of the present invention.
Claims (7)
1. A machining and positioning tool for an airplane front connector casting is characterized by comprising a first connecting frame (1), a second connecting frame (2), a first mounting seat (3), a shaft seat (4), a threaded pipe (5), a first screw (6), a first connecting seat (7), a first clamp (8), a second mounting seat (9), a second connecting seat (10), a second screw (11), a second clamp (12), a locking nut (13) and a handle (14), wherein the left side of the bottom end and the right side of the bottom end of the first connecting frame (1) are respectively provided with the second connecting frame (2), the first mounting seat (3) is arranged on the left side of the top end of the first connecting frame (1), the top end of the first mounting seat (3) is provided with the shaft seat (4), the threaded pipe (5) is arranged in the shaft seat (4), the first screw (6) is screwed in the threaded pipe (5), the right end of the first screw (6) is provided with the first connecting seat (7), the right-hand member of first connecting seat (7) is provided with first anchor clamps (8), the top right side at first link (1) is installed in second mount pad (9), the top of second mount pad (9) is provided with second connecting seat (10), second screw rod (11) transversely pass second connecting seat (10), the left end of second screw rod (11) is provided with second anchor clamps (12), lock nut (13) spiral shell cover is established on second screw rod (11), the right-hand member of second screw rod (11) is provided with handle (14), the top middle part of first link (1) is provided with operation panel (15), screwed pipe (5) drive through power unit, the bottom of first connecting seat (7) is provided with stop gear.
2. The machining and positioning tool for the airplane front joint casting according to claim 1, wherein the limiting mechanism comprises a sliding rail (16), a sliding seat (17) and a connecting rod (18), the sliding rail (16) is mounted at the top end of the first connecting frame (1), the sliding seat (17) is slidably arranged on the sliding rail (16), the connecting rod (18) is arranged at the top end of the sliding seat (17), and the top end of the connecting rod (18) is connected with the first connecting seat (7).
3. The machining and positioning tool for the airplane front joint casting according to claim 2, wherein the power mechanism comprises a first transmission wheel (19), a power motor (20), a second transmission wheel (21) and a transmission belt (22), the first transmission wheel (19) is installed at the left part of the threaded pipe (5), the power motor (20) is installed at the left side of the bottom end of the first connecting frame (1), the second transmission wheel (21) is arranged at the output end of the left part of the power motor (20), and the transmission belt (22) is installed on the first transmission wheel (19) and the second transmission wheel (21).
4. The machining and positioning tool for the airplane front joint casting according to claim 3, characterized in that third connecting frames (23) are arranged on the left side and the right side of the top end of the first connecting frame (1), the left end and the right end of the fourth connecting frame (24) are respectively connected with the upper portions of the two groups of third connecting frames (23), and a plurality of groups of illuminating lamps (25) are arranged at the bottom end of the fourth connecting frame (24).
5. The machining and positioning tool for the airplane front joint casting according to claim 4, characterized in that the bottom ends of the two groups of second connecting frames (2) are provided with supports (26).
6. The machining and positioning tool for the airplane front joint casting according to claim 5, wherein support frames (27) are arranged at the lower portions of the two groups of third connecting frames (23), and the bottom ends of the two groups of support frames (27) are connected with the top end of the first connecting frame (1).
7. The machining and positioning tool for the airplane front joint casting according to claim 6, further comprising brackets (28), wherein the brackets (28) are mounted at the lower parts of the two groups of second connecting frames (2).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122102734.9U CN215942831U (en) | 2021-09-01 | 2021-09-01 | Aircraft front connector foundry goods processing location frock |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122102734.9U CN215942831U (en) | 2021-09-01 | 2021-09-01 | Aircraft front connector foundry goods processing location frock |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN215942831U true CN215942831U (en) | 2022-03-04 |
Family
ID=80431223
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202122102734.9U Active CN215942831U (en) | 2021-09-01 | 2021-09-01 | Aircraft front connector foundry goods processing location frock |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN215942831U (en) |
-
2021
- 2021-09-01 CN CN202122102734.9U patent/CN215942831U/en active Active
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|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: A machining and positioning fixture for aircraft front joint castings Granted publication date: 20220304 Pledgee: Xi'an Caijin Financing Guarantee Co.,Ltd. Pledgor: Shaanxi Huachen Aviation Technology Co.,Ltd. Registration number: Y2024980006966 |