CN115415823A - Supporting and fixing device for airplane part machining - Google Patents
Supporting and fixing device for airplane part machining Download PDFInfo
- Publication number
- CN115415823A CN115415823A CN202211373313.2A CN202211373313A CN115415823A CN 115415823 A CN115415823 A CN 115415823A CN 202211373313 A CN202211373313 A CN 202211373313A CN 115415823 A CN115415823 A CN 115415823A
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- base
- pedestal
- fixedly connected
- motor
- supporting
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23Q—DETAILS, COMPONENTS, OR ACCESSORIES FOR MACHINE TOOLS, e.g. ARRANGEMENTS FOR COPYING OR CONTROLLING; MACHINE TOOLS IN GENERAL CHARACTERISED BY THE CONSTRUCTION OF PARTICULAR DETAILS OR COMPONENTS; COMBINATIONS OR ASSOCIATIONS OF METAL-WORKING MACHINES, NOT DIRECTED TO A PARTICULAR RESULT
- B23Q3/00—Devices holding, supporting, or positioning work or tools, of a kind normally removable from the machine
- B23Q3/02—Devices holding, supporting, or positioning work or tools, of a kind normally removable from the machine for mounting on a work-table, tool-slide, or analogous part
- B23Q3/06—Work-clamping means
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- Mechanical Engineering (AREA)
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Abstract
The invention provides a supporting and fixing device for airplane part machining, which relates to the technical field of supporting and fixing devices and comprises a base, wherein the main body of the base is of a rectangular structure, a support is fixedly connected to the bottom end of the base, the base and the support form a supporting structure together, a transverse groove is formed in the top end of the base, and a first electric push rod is arranged in the transverse groove formed in the base.
Description
Technical Field
The invention relates to the technical field of supporting and fixing devices, in particular to a supporting and fixing device for airplane part machining.
Background
In the manufacturing process of the airplane, a plurality of parts need to be machined, and various corresponding supporting and fixing clamps are needed for machining the parts more stably during machining operation.
The prior supporting and fixing device has the following defects in the practical application process:
1. in the process of supporting an airplane part, the size of the part of the airplane is large, so that an effective traction structure is lacked when the orientation of the airplane part needs to be adjusted in the machining process, and the existing supporting and fixing device is inconvenient and limited when the orientation of the airplane part needs to be adjusted;
2. the existing supporting and fixing device supports airplane parts, and due to the fact that a plurality of parts are machined in a special shape, the airplane parts are required to be adjusted in different gradients in the machining process, and the airplane parts are required to be manually measured in the adjusting process, so that limitation exists.
In view of the above, the present invention provides a supporting and fixing device for machining aircraft parts, which is improved in view of the existing structure and defects.
Disclosure of Invention
The invention provides a supporting and fixing device for airplane part machining, which solves the problem that the existing supporting and fixing device has limitation because a plurality of parts are processed in a special shape in the process of supporting airplane parts, so that the parts need to be adjusted in different inclinations in the machining process, but the parts need to be manually measured in the adjustment process.
The invention provides a purpose and an effect of a supporting and fixing device for airplane part machining, which specifically comprise the following steps: the base, the main part of base is the rectangle structure, and the bottom fixedly connected with support of base, and the bearing structure has been constituteed jointly to base and support, and the top of base has seted up the transverse groove to the transverse groove internally mounted who sets up in the base has electric putter one, the internally mounted of mount pad has hydraulic push rod, and the bottom of pedestal is the fixedly connected with mount pad also, and the one end of keeping away from the pedestal among the hydraulic push rod is connected with the pedestal, and the front end of pedestal installs the spirit level.
Furthermore, the inside of the bearing seat is rotatably connected with a supporting column, the outer side of the supporting column is fixedly connected with a second bevel gear, the second bevel gear is in meshing transmission with the first bevel gear, the top end of the supporting column is provided with a weighing device, the weighing device is used for detecting weight, and the outer side of the base is fixedly connected with a side plate.
Further, the outside winding of gyro wheel has the haulage rope, one side fixedly connected with couple of keeping away from the gyro wheel in the haulage rope, the haulage rope has constituteed connection structure jointly with the couple, and the pedestal is installed on the top of weighing the ware, be two mount pads of linear array fixedly connected with on the top face of pedestal, add man-hour when the aircraft part on the pedestal needs to be processed, if the position to the part is adjusted to needs, can carry out the position adjustment along the transverse groove that the base top was seted up through the electric putter one of start-up installation in the base, and the part that is spacing on the pedestal is being carried out horizontal position adjustment operation through the indirect drive of bearing the seat can, and synchronous starter motor one to one helical gear one carries out rotation drive, drive pillar and pedestal through the meshing transmission of helical gear one and helical gear two and rotate, and then reach quick the position of adjusting the spare part and in order to reach the purpose of convenient processing.
Furthermore, the inside sliding connection of the transverse groove that the base top was seted up bears the seat, bears the seat and is inside hollow structure, and bears the inside of seat and still install motor one to the transmission shaft is installed on the left side of motor one, installs bevel gear one on the transmission shaft that the left side of motor one was installed.
Furthermore, the top of pedestal is annular array and has seted up the recess, and the inside sliding connection of recess that the pedestal top was seted up has an electromagnetic block, keeps away from one side of pedestal in the electromagnetic block and installs electric putter two, and spacing is installed on the top of electric putter two, and the protection pad is installed to spacing bottom.
Further, install the distancer on the transmission shaft that two tops of motor were installed, the distancer is infrared range finding structure, and the outside fixedly connected with support of base, and wherein vertical adjacent support in per two places is a set of, and two sets of supports difference fixed connection are in the left and right sides face position of base.
Furthermore, the curb plate is equipped with four places altogether, and wherein every two horizontal adjacent curb plates in place are a set of, and two sets of curb plates fixed connection respectively are in the front and back both sides face position of base to motor two is installed to the bottom of curb plate, and the transmission shaft is installed on the top of motor two.
Further, every group the gyro wheel is installed to the inboard of support, and the motor three is installed to the front end of support, and the transmission shaft that the three rear sides of motor were installed is connected with the gyro wheel, and the motor three is used for driving the gyro wheel and rotates, and the top of base is two guide plates of linear array fixedly connected with.
Compared with the prior art, the invention has the following beneficial effects:
1. when the airplane parts on the pedestal need to be machined, if the positions of the parts need to be adjusted, the bearing seat can be adjusted along a transverse groove formed in the top end of the pedestal by starting an electric push rod I installed in the pedestal, the parts limited on the pedestal are indirectly driven by the bearing seat to perform transverse position adjustment operation, a synchronous starting motor drives a bevel gear I to rotate, a support column and the pedestal are driven to rotate through meshing transmission of the bevel gear I and a bevel gear II, and the purpose of quickly adjusting the positions of the parts to achieve convenient machining is achieved.
2. When the part is placed on the pedestal, can realize automatic operation of weighing through the pedestal to installing the extrusion of weighing the ware on the pillar top, and can start the two pairs of distancers of motor of installing in the curb plate bottom according to the difference of part weight after weighing the ware detection and accomplish and rotate the drive, and position adjustment through lieing in the distancer on every group curb plate realizes adjusting the scope that the distancer found the range, if when weighing the ware and detecting the quality of current part when too big, then can be synchronous with the distancer of installing on every group curb plate outside rotate in order to enlarge the discernment scope of distancer, then can carry out quick alarm operation through the alarm in the distancer when the operator is too close the base in the course of working, and then reach safer purpose.
3. When the part of placing on the pedestal carries out different inclination's processing operation as required, then the hydraulic rod that can be synchronous start-up is installed inside the mount pad and is adjusted the deflection angle of pedestal and spare part to carry out real-time monitoring to the inclination of current pedestal through the spirit level of installing at the pedestal front end, and can ensure more accurately to the adjustment of spare part through the monitoring of spirit level, make the part can be more stable when adding man-hour.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the drawings of the embodiments will be briefly described below.
The drawings in the following description relate to some embodiments of the invention only and are not intended to limit the invention.
In the drawings:
FIG. 1 is a front side view of a support fixture according to an embodiment of the present invention, partially broken away and disassembled;
FIG. 2 is a schematic structural diagram showing a support fixture according to an embodiment of the present invention in a partially broken away and disassembled state from top side;
FIG. 3 is a schematic view of an assembled structure of a support fixture according to an embodiment of the present invention;
FIG. 4 illustrates a top view of a support fixture according to an embodiment of the present invention;
FIG. 5 shows a schematic view of a base-to-hook display structure supporting a fixture according to an embodiment of the present invention;
FIG. 6 is a schematic view of a seat-to-pad display structure of a support fixture according to an embodiment of the present invention;
FIG. 7 shows an enlarged schematic view at A in FIG. 2 of a support fixture according to an embodiment of the invention;
fig. 8 is an enlarged schematic view of the supporting fixture at B in fig. 2 according to an embodiment of the present invention.
List of reference numerals
1. A base; 2. a support frame; 3. an electric push rod I; 4. a bearing seat; 5. a first motor; 6. a first bevel gear; 7. a second bevel gear; 8. a pillar; 9. a weighing device; 10. a side plate; 11. a second motor; 12. a range finder; 13. a support; 14. a roller; 15. a third motor; 16. a guide plate; 17. a hauling rope; 18. hooking; 19. a base body; 20. a mounting seat; 21. a hydraulic push rod; 22. a pedestal; 23. a level gauge; 24. an electromagnetic block; 25. a second electric push rod; 26. a limiting frame; 27. a pad.
Detailed Description
The embodiments of the present invention will be described in further detail with reference to the drawings and examples. The following examples are intended to illustrate the invention but are not intended to limit the scope of the invention.
Example (b):
as shown in figures 1 to 8:
the invention provides a supporting and fixing device for processing airplane parts, which comprises: base 1, base 1's main part is the rectangle structure, and base 1's bottom fixedly connected with support frame 2, base 1 has constituteed bearing structure jointly with support frame 2, and the transverse groove has been seted up on base 1's top, and the transverse groove internally mounted who sets up in base 1 has electric putter 3, the internally mounted of mount pad 20 has hydraulic rod 21, and also fixedly connected with mount pad 20 in pedestal 22's bottom, the one end of keeping away from pedestal 19 among hydraulic rod 21 is connected with pedestal 22, and level 23 is installed to pedestal 22's front end, pedestal 22's top is the annular array and has seted up the recess, the inside sliding connection of recess that set up on pedestal 22 top has electromagnetic block 24, keep away from one side of pedestal 22 among the electromagnetic block 24 and install electric putter two 25, spacing 26 is installed on electric putter two 25's top, protection pad 27 is installed to spacing 26's bottom.
Wherein, the inside sliding connection of the transverse groove that base 1 top was seted up has bearing seat 4, bearing seat 4 is inside hollow structure, and bearing seat 4's inside still installs motor 5, and the transmission shaft is installed in the left side of motor 5, install bevel gear 6 on the transmission shaft of motor 5 left side installation, bearing seat 4's internal rotation is connected with pillar 8, pillar 8's outside fixedly connected with bevel gear two 7, bevel gear two 7 and bevel gear one 6 meshing transmission, weigher 9 is installed on pillar 8's top, weigher 9 is used for detecting weight, and base 1's outside fixedly connected with curb plate 10, when the processing operation of different inclination is carried out to the part of placing on pedestal 22 to needs, then hydraulic push rod 21 that can synchronous start-up and install inside mount pad 20 comes to adjust pedestal 22 and the deflection angle of spare part, and carry out real-time monitoring to the inclination of current pedestal 22 through level 23 of installing at pedestal 22 front end, and can ensure that the adjustment of spare part is more accurate through the monitoring of level 23, make the part can be more stable when adding man-hour.
Wherein, the side plates 10 are provided with four positions altogether, wherein every two transversely adjacent side plates 10 are in a group, and two groups of side plates 10 are fixedly connected to the front and rear side surfaces of the base 1 respectively, and the bottom end of the side plates 10 is provided with a second motor 11, the top end of the second motor 11 is provided with a transmission shaft, a distance meter 12 is installed on the transmission shaft installed at the top end of the second motor 11, the distance meter 12 is in an infrared distance measurement structure, and the outer side of the base 1 is fixedly connected with a bracket 13, wherein every two longitudinally adjacent brackets 13 are in a group, and the two groups of brackets 13 are fixedly connected to the left and right side surfaces of the base 1 respectively, when a part is placed on the pedestal 22, the automatic weighing operation can be realized by extruding the weighing device 9 installed at the top end of the support column 8 through the seat body 19, the motor two 11 installed at the bottom end of the side plates 10 can be started to drive the distance meter 12 to rotate according to the weight of the part after the detection of the weighing device 9 is completed, and the range of the distance meter 12 can be adjusted by adjusting the position of the distance meter 12 on each group of side plates 10, and the distance meter 12, when the weighing device 9 detects that the mass of the current part is too large, the alarm can be installed on the side plates, and the side plates can be capable of performing the alarm to perform the safety alarm to the safety alarm in the process of the safety alarm if the distance meter 12, and the safety alarm can be enlarged.
Wherein, gyro wheel 14 is installed to the inboard of every group support 13, motor three 15 is installed to the front end of support 13, the transmission shaft that motor three 15 rear side was installed is connected with gyro wheel 14, and motor three 15 is used for driving gyro wheel 14 and rotates, the top of base 1 is two guide plates 16 of linear array fixedly connected with, the outside winding of gyro wheel 14 has haulage rope 17, one side fixedly connected with couple 18 of keeping away from gyro wheel 14 in the haulage rope 17, haulage rope 17 has constituteed connection structure with couple 18 jointly, and pedestal 19 is installed on the top of weighing device 9, be two mount pads 20 of linear array fixedly connected with on the top face of pedestal 19.
When in use: firstly, when the airplane parts need to be machined, the parts need to be machined can be placed at the position right above the pedestal 22, and if the parts placed on the pedestal 22 need to be clamped and limited, the electromagnetic block 24 can be placed in a groove formed in the pedestal 22 for limiting;
when the electromagnetic block 24 is installed in the pedestal 22 by power on, the electromagnetic block is magnetically adsorbed in the pedestal 22, and then the electric push rod 25 installed at the top end of the electromagnetic block 24 is started to start the limiting frame 26 and the protection pad 27 to move downwards until the limiting frame 26 and the protection pad 27 move downwards to contact and limit the parts placed on the pedestal 22, so that the purpose of quickly limiting the parts is achieved;
then when the airplane parts on the pedestal 22 need to be machined, if the positions of the parts need to be adjusted, the electric push rod I3 installed in the pedestal 1 can be started to adjust the positions of the bearing seat 4 along the transverse groove formed in the top end of the pedestal 1, the bearing seat 4 indirectly drives the parts limited on the pedestal 22 to perform transverse position adjustment operation, the synchronous starting motor I5 drives the bevel gear I6 to rotate, and the bevel gear I6 and the bevel gear II 7 are meshed for transmission to drive the support column 8 and the pedestal 22 to rotate, so that the purpose of quickly adjusting the positions of the parts to facilitate machining is achieved;
when a part is placed on the pedestal 22, the automatic weighing operation is realized by extruding the weighing device 9 arranged at the top end of the support column 8 through the seat body 19, after the detection of the weighing device 9 is finished, the motor two 11 arranged at the bottom end of the side plate 10 is started to drive the distance measuring device 12 to rotate according to the weight of the part, the distance measuring range of the distance measuring device 12 is adjusted by adjusting the position of the distance measuring device 12 positioned above each group of side plates 10, if the weighing device 9 detects that the mass of the current part is too large, the distance measuring device 12 arranged above each group of side plates 10 can be synchronously rotated outwards to enlarge the identification range of the distance measuring device 12, and if an operator is too close to the pedestal 1 in the processing process, the alarm in the distance measuring device 12 can be used for quick alarm operation, so that the purpose of higher safety is achieved;
then, when the large-scale parts need to be steered and adjusted, the hooks 18 arranged on the outer side of the traction rope 17 can be respectively connected with the far ends of the large-scale parts, the bevel gear 6 is driven to rotate by the synchronous starting motor I5, the roller 14 is driven to rotate by the synchronous starting motor III 15 arranged at the front end of the support 13, so that the traction rope 17 is wound, the parts can be steered and adjusted more stably by synchronously winding the traction rope 17, and the purpose of being more practical is achieved;
when parts placed on the pedestal 22 need to be machined at different inclination angles, the hydraulic push rod 21 mounted inside the mounting seat 20 can be synchronously started to adjust the deflection angles of the pedestal 22 and the parts, the inclination angle of the current pedestal 22 is monitored in real time through the level gauge 23 mounted at the front end of the pedestal 22, the parts can be accurately adjusted through monitoring of the level gauge 23, and the parts can be more stably machined.
The embodiments of the present invention have been presented for purposes of illustration and description, and are not intended to be exhaustive or limited to the invention in the form disclosed. Many modifications and variations will be apparent to those of ordinary skill in the art. The embodiment was chosen and described in order to best explain the principles of the invention and the practical application, and to enable others of ordinary skill in the art to understand the invention for various embodiments with various modifications as are suited to the particular use contemplated.
Claims (7)
1. The utility model provides an aircraft parts machining is with supporting fixing device which characterized in that includes: the base (1), the main body of the base (1) is of a rectangular structure, a support frame (2) is fixedly connected to the bottom end of the base (1), the base (1) and the support frame (2) jointly form a support structure, transverse grooves are formed in the top end of the base (1), electric push rod I (3) are installed inside the transverse grooves formed in the base (1), brackets (13) are fixedly connected to the outer side of the base (1), every two longitudinally adjacent brackets (13) form a group, the two groups of brackets (13) are respectively and fixedly connected to the left side surface and the right side surface of the base (1), each group of brackets (13) is provided with rollers (14) on the inner side, three motors (15) are installed at the front ends of the brackets (13), transmission shafts installed on the rear sides of the three motors (15) are connected with the rollers (14), the three motors (15) are used for driving the rollers (14) to rotate, the top end of the base (1) is provided with two guide plates (16) in a linear array manner, traction ropes (17) are wound on the outer sides of the traction ropes (14), hooks (18) far away from one side of the traction ropes (17), a hook (18) are connected with a hook (19), and a weighing seat (19) is connected with a weighing seat (19) forming a base body (9), the internally mounted of mount pad (20) has hydraulic rod (21), and the bottom of pedestal (22) is fixedly connected with mount pad (20) also, keeps away from the one end of pedestal (19) in hydraulic rod (21) and is connected with pedestal (22), and spirit level (23) are installed to the front end of pedestal (22).
2. A support fixture for use in the machining of aircraft parts, as defined in claim 1, wherein: the inside sliding connection of the transverse groove that base (1) top was seted up bears seat (4), bears seat (4) and is inside hollow structure, and bears the inside of seat (4) and still installs motor (5) to the transmission shaft is installed in the left side of motor (5), installs on the transmission shaft that motor (5) left side was installed helical gear (6).
3. A support fixture for use in the machining of aircraft parts, as defined in claim 2, wherein: the inner part of the bearing seat (4) is rotatably connected with a supporting column (8), the outer side of the supporting column (8) is fixedly connected with a second bevel gear (7), the second bevel gear (7) is in meshed transmission with the first bevel gear (6), a weighing device (9) is installed at the top end of the supporting column (8), the weighing device (9) is used for detecting weight, and the outer side of the base (1) is fixedly connected with a side plate (10).
4. A supporting and fixing device for use in the machining of aircraft parts, as claimed in claim 3, wherein: the side plates (10) are provided with four positions, wherein every two transverse adjacent side plates (10) are in one group, the two groups of side plates (10) are fixedly connected to the positions of the front side face and the rear side face of the base (1) respectively, a second motor (11) is installed at the bottom end of each side plate (10), and a transmission shaft is installed at the top end of each second motor (11).
5. A supporting and fixing device for processing aircraft parts according to claim 4, wherein: and a distance meter (12) is installed on a transmission shaft installed at the top end of the second motor (11), and the distance meter (12) is of an infrared distance measuring structure.
6. A support fixture for use in the machining of aircraft parts, as defined in claim 1, wherein: the outside winding of gyro wheel (14) has haulage rope (17), keeps away from one side fixedly connected with couple (18) of gyro wheel (14) in haulage rope (17), and haulage rope (17) and couple (18) have constituteed connection structure jointly, and the top of weighing ware (9) installs pedestal (19), is two mount pads (20) of linear array fixedly connected with on the top face of pedestal (19).
7. A support fixture for use in the machining of aircraft parts, as defined in claim 1, wherein: the top of pedestal (22) is that the annular array sets up flutedly, and the inside sliding connection of recess that pedestal (22) top was seted up has electromagnetic block (24), and one side of keeping away from pedestal (22) in electromagnetic block (24) installs electric putter two (25), and spacing (26) are installed on the top of electric putter two (25), and protection pad (27) are installed to the bottom of spacing (26).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202211373313.2A CN115415823A (en) | 2022-11-04 | 2022-11-04 | Supporting and fixing device for airplane part machining |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202211373313.2A CN115415823A (en) | 2022-11-04 | 2022-11-04 | Supporting and fixing device for airplane part machining |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN115415823A true CN115415823A (en) | 2022-12-02 |
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ID=84208393
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202211373313.2A Pending CN115415823A (en) | 2022-11-04 | 2022-11-04 | Supporting and fixing device for airplane part machining |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN115415823A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116428487A (en) * | 2023-06-09 | 2023-07-14 | 临沂天瀚电子信息科技有限责任公司 | Measuring device for communication equipment installation |
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| CN202783796U (en) * | 2012-07-18 | 2013-03-13 | 四川奥格科技有限公司 | Rotatable multifunctional airplane pavement transferring platform |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN116428487A (en) * | 2023-06-09 | 2023-07-14 | 临沂天瀚电子信息科技有限责任公司 | Measuring device for communication equipment installation |
| CN116428487B (en) * | 2023-06-09 | 2023-08-25 | 临沂天瀚电子信息科技有限责任公司 | Measuring device for communication equipment installation |
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