CN220612960U - Automatic assembly device of aero-turbine rotor - Google Patents
Automatic assembly device of aero-turbine rotor Download PDFInfo
- Publication number
- CN220612960U CN220612960U CN202322294154.3U CN202322294154U CN220612960U CN 220612960 U CN220612960 U CN 220612960U CN 202322294154 U CN202322294154 U CN 202322294154U CN 220612960 U CN220612960 U CN 220612960U
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- assembly
- workbench
- turbine rotor
- linear guide
- assembly device
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- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 claims description 9
- 239000000741 silica gel Substances 0.000 claims description 9
- 229910002027 silica gel Inorganic materials 0.000 claims description 9
- 230000003028 elevating effect Effects 0.000 claims description 4
- 238000005259 measurement Methods 0.000 abstract description 14
- 210000001503 joint Anatomy 0.000 abstract description 4
- 238000000034 method Methods 0.000 description 9
- 230000009286 beneficial effect Effects 0.000 description 8
- 238000010586 diagram Methods 0.000 description 3
- 238000012986 modification Methods 0.000 description 3
- 230000004048 modification Effects 0.000 description 3
- 238000012360 testing method Methods 0.000 description 3
- 238000004519 manufacturing process Methods 0.000 description 2
- 230000006978 adaptation Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 230000001737 promoting effect Effects 0.000 description 1
- 238000012546 transfer Methods 0.000 description 1
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- Jib Cranes (AREA)
Abstract
The utility model belongs to the technical field of aerial hair assembly, and particularly relates to an automatic assembly device of an aerial hair turbine rotor, which comprises a base, wherein a workbench is arranged on the base, two sides of the workbench are provided with a switching assembly, a screw gun head storage box, a liftable cantilever box measurement and control panel and a small screw gun assembly, the inner side of the workbench is provided with a linear guide lifting platform, the linear guide lifting platform is in threaded connection with a lifting piece, the front side of the lifting piece is provided with a locking turntable assembly, the rear side of the workbench is provided with a power assisting mechanical arm, the front end of the power assisting mechanical arm is connected with a heavy screw gun, and the top end of the workbench is provided with a balance hanging assembly. The assembly with high quality, high reliability and quick response efficiency is guaranteed to be realized through an automatic butt joint assembly technology, and the technical difficulty of engine assembly is effectively reduced.
Description
Technical Field
The utility model belongs to the technical field of aerial turbine assembly, and particularly relates to an automatic assembly device of an aerial turbine rotor.
Background
An aero-engine (aero-engine) is a highly complex and precise thermodynamic machine, and as a heart of an airplane, not only is the power of the airplane in flight, but also is an important driving force for promoting the development of aviation industry, and each important revolution in the human aviation history is indistinguishable from the technical progress of the aero-engine.
In the prior art, the butt joint assembly of the low-vortex rotor of the aeroengine is conventionally assembled by means of manual or special fixtures, bearing collision damage and low-vortex rotor shaft neck damage accidents occur in a manual assembly mode, and the low-vortex rotor is required to be repeatedly assembled and disassembled because of the need of matching a low-vortex rotor adjusting pad, so that the probability of occurrence of quality accident risk of the low-vortex rotor is increased. When the nut is screwed down, the blind assembly operation is performed, and the assembly quality accidents frequently occur because tooth grooves cannot be visually observed. Thus, the manual assembly mode has low production efficiency and is easy to make mistakes.
Disclosure of Invention
In view of the above problems, an object of the present utility model is to: the automatic assembly device for the aero-turbine rotor solves the problems of low production efficiency and easy error in the traditional manual or special fixture assembly of the aero-engine low-vortex rotor.
In order to achieve the above purpose, the utility model adopts the technical scheme that: the utility model provides an automatic assembly device of turbine rotor takes turns by plane, includes the base, be provided with the workstation on the base, the both sides of workstation are provided with switching subassembly, screw rifle head storage and receive box, liftable cantilever box measurement and control panel and small-size screw rifle subassembly, the inboard of workstation is provided with linear guide elevating platform, linear guide elevating platform threaded connection has the lifter, locking revolving stage subassembly is installed to the front side of lifter, helping hand arm is installed to the rear side of workstation, helping hand arm's front end is connected with heavy screw rifle, balanced hanging subassembly is installed on the top of workstation.
The beneficial effects of the utility model are as follows: the assembly with high quality, high reliability and quick response efficiency is guaranteed to be realized through an automatic butt joint assembly technology, and the technical difficulty of engine assembly is effectively reduced.
In order to prevent oil bodies, nuts and the like from falling on the surface of a metal structure of the device;
as a further improvement of the above technical scheme: the base comprises a base body and an oil-resistant anti-slip silica gel pad, and the vertical projection of the locking rotary table assembly is positioned on the oil-resistant anti-slip silica gel pad.
The beneficial effects of this improvement are: the oil-resistant and anti-skid silica gel pad plays a role in protecting the base body.
In order to enable the lifting piece to drive the locking turntable assembly to stably move;
as a further improvement of the above technical scheme: the linear guide lifting platform comprises a screw rod, a driving part and linear guide rails, wherein the driving part is arranged at the top of the workbench and is connected with the screw rod in a driving mode, guide rails in the linear guide rails are arranged on the left inner wall and the right inner wall of the workbench, and sliding tables in the linear guide rails are arranged on two sides of the lifting part.
The beneficial effects of this improvement are: the lifting piece can drive the locking turntable component to stably move under the driving of the linear guide rail lifting table.
In order to achieve concentricity and runout testing of the workpiece;
as a further improvement of the above technical scheme: an adjustable universal meter frame is arranged on the front side of the lifting piece.
The beneficial effects of this improvement are: the rotating workpiece can be subjected to concentricity and run-out testing by an adjustable universal meter rack-mounted measuring instrument such as a micrometer.
In order to realize accurate assembly and processing of the workpiece;
as a further improvement of the above technical scheme: the locking turntable assembly comprises an outer support, a locking turntable and an indicator lamp, wherein the locking turntable is arranged on the outer support, and the indicator lamp is arranged on the outer support on the periphery of the locking turntable.
The beneficial effects of this improvement are: the corresponding program can be selected for assembly guidance according to the set program, and when the assembly is rotated to the assembly position, the indicator lamp is correspondingly installed Kong Liang.
In order to realize intelligent recording of the assembly process;
as a further improvement of the above technical scheme: the measurement and control panel of the liftable cantilever box comprises a mechanical cantilever and a measurement and control panel, one end of the mechanical cantilever is arranged at the rear side of the workbench, and the measurement and control panel is arranged at the other end of the mechanical cantilever.
The beneficial effects of this improvement are: the measurement and control panel of the liftable cantilever box can automatically record the screwing process of each bolt and measure the screwing torque in real time, and can also realize monitoring accidents and intelligent assembly guidance.
For convenience and safety, the workpiece is moved;
as a further improvement of the above technical scheme: the balance hanging assembly comprises a tripod and a balance hanging, the tripod is arranged on the workbench, and the balance hanging is arranged on the tripod.
The beneficial effects of this improvement are: the balance hanging component can easily and safely hang and pick up the movable workpiece.
To meet various assembly requirements for the workpiece;
as a further improvement of the above technical scheme: the switching assembly comprises a first frame body, a switching tool and a switching screw gun are placed on the first frame body, the small screw gun assembly comprises a second frame body, and the small screw gun is placed on the second frame body.
The beneficial effects of this improvement are: the use of the adapter assembly and the small screw gun assembly can meet various assembly requirements of the device on the workpiece.
None of the parts of the device are the same as or can be implemented using prior art.
Drawings
FIG. 1 is a schematic diagram of a first embodiment of the present utility model;
FIG. 2 is a schematic diagram of a second embodiment of the present utility model;
FIG. 3 is a schematic diagram III of the structure of the present utility model;
in the figure: 1. a base; 101. a base; 102. oil-resistant and anti-skid silica gel pad; 2. a work table; 3. a switching component; 31. a first frame body; 32. a switching tool; 33. a switching screw gun; 4. a screw gun head storage box; 5. a measurement and control panel of the liftable cantilever box; 51. a mechanical cantilever; 52. a measurement and control panel; 6. a small screw gun assembly; 61. a second frame body; 62. a small screw gun; 7. a linear guide rail lifting table; 71. a screw rod; 72. a driving part; 73. a linear guide rail; 8. a lifting member; 9. locking the turntable assembly; 91. an outer bracket; 92. locking the turntable; 93. an indicator light; 10. an adjustable universal meter mount; 11. a power-assisted mechanical arm; 12. heavy screw guns; 13. a balance crane assembly; 131. a tripod; 132. and (5) balancing the crane.
Detailed Description
In order that those skilled in the art may better understand the technical solutions of the present utility model, the following detailed description of the present utility model with reference to the accompanying drawings is provided for exemplary and explanatory purposes only and should not be construed as limiting the scope of the present utility model.
Example 1:
as shown in fig. 1-3: an automatic assembling device of a ship turbine rotor comprises a base 1, wherein a workbench 2 is arranged on the base 1, a switching component 3, a screw gun head storage box 4, a liftable cantilever box measurement and control panel 5 and a small screw gun component 6 are arranged on two sides of the workbench 2, a linear guide lifting table 7 is arranged on the inner side of the workbench 2, a lifting piece 8 is connected with the linear guide lifting table 7 in a threaded manner, a locking rotary table component 9 is arranged on the front side of the lifting piece 8, a power-assisted mechanical arm 11 is arranged on the rear side of the workbench 2, a heavy screw gun 12 is connected with the front end of the power-assisted mechanical arm 11, a balance hanging component 13 is arranged on the top end of the workbench 2, the assembling with high quality, high reliability and quick reaction efficiency is ensured through an automatic butt joint assembling technology, the difficulty of an engine assembling technology is effectively reduced, the base 1 comprises a base body 101 and an anti-skid silica gel pad 102, the vertical projection of the locking turntable assembly 9 is positioned on an oil-resistant and anti-slip silica gel pad 102, the oil-resistant and anti-slip silica gel pad 102 plays a role of protecting a base 101, the linear guide lifting table 7 comprises a screw 71, a driving part 72 and a linear guide rail 73, the driving part 72 is arranged at the top of the workbench 2 and drives the connecting screw 71, the guide rails in the linear guide rail 73 are arranged on the left and right inner walls of the workbench 2, a sliding table in the linear guide rail 73 is arranged on two sides of a lifting piece 8, the lifting piece 8 can drive the locking turntable assembly 9 to stably move under the driving of the linear guide lifting table 7, an adjustable universal meter frame 10 is arranged on the front side of the lifting piece 8, a measuring instrument such as a micrometer is arranged on the adjustable universal meter frame 10 to perform concentricity and jump test on a rotating workpiece, and the locking turntable assembly 9 comprises an outer bracket 91, the locking rotary table 92 and the pilot lamp 93, locking rotary table 92 installs on the outer support 91, pilot lamp 93 installs on the outer support 91 of locking rotary table 92 week side, can select corresponding procedure to assemble according to setting for guiding, during assembly part rotation to the assembly position, pilot lamp 93 plays at corresponding installation Kong Liang, liftable cantilever box measurement and control panel 5 includes mechanical cantilever 51 and measurement and control panel 52, the one end of mechanical cantilever 51 is installed in the rear side of workstation 2, measurement and control panel 52 installs the other end at mechanical cantilever 51, liftable cantilever box measurement and control panel 5 can the automatic recording every bolt tightening process and the real-time measurement tightening torque, can also realize control accident and intelligent assembly guiding, balanced hanging subassembly 13 includes tripod 131 and balanced hanging 132, tripod 131 installs on workstation 2, balanced hanging 132 installs on tripod 131, and balanced hanging subassembly 13 can light safe hang and get the removal work piece, switching subassembly 3 includes support body one 31, switching frock 32 and switching frock 33 have been placed on support body one 31, and two small-size gun assembly type 6 screw type 6 on the support body one kind of assembly type 6, and two small-size screw type assembly type 6 are satisfied.
The working principle of the technical scheme is as follows: the assembly is moved and lifted by the balance hanging assembly 13, the assembly to be assembled is moved to the locking turntable 92 to be positioned, then the driving part 72 drives the screw rod 71 to rotate, so that the lifting piece 8 stably moves under the support of the linear guide rail 73, and the locking turntable assembly 9 and the assembly to be assembled on the locking turntable assembly 9 are driven to move to a proper operation height; when blind hole assembly is carried out, an operator assembles and connects the transfer screw gun 33 with the heavy screw gun 12, so that the locking turntable assembly 9 drives the workpiece to move below the heavy screw gun 12, and the power-assisted mechanical arm 11 drives the heavy screw gun 12 to move for working so as to carry out blind hole assembly; after the locking turntable assembly 9 drives the to-be-assembled part to move above the heavy screw gun 12, an operator can assemble the switching tool 32 with the heavy screw gun 12 and then assemble the to-be-assembled part; when the locking rotary table assembly 9 drives the to-be-assembled part to move downwards to the sitting position, an operator can hold the small screw gun 62 inserted on the second frame body 61, and the assembly work is carried out on the to-be-assembled part in cooperation with the rotation function of the locking rotary table 92.
It should be noted that, in this document, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.
The principles and embodiments of the present utility model have been described herein with reference to specific examples, the description of which is intended only to facilitate an understanding of the method of the present utility model and its core ideas. The foregoing is merely illustrative of the preferred embodiments of the utility model, and it is noted that there is virtually no limit to the specific structure which may be imposed by those skilled in the art without departing from the spirit of the utility model, and that modifications, adaptations, or variations of the foregoing features may be combined in a suitable manner; such modifications, variations and combinations, or the direct application of the inventive concepts and aspects to other applications without modification, are contemplated as falling within the scope of the present utility model.
Claims (8)
1. Automatic assembly device of ship turbine rotor, its characterized in that: including base (1), be provided with workstation (2) on base (1), the both sides of workstation (2) are provided with adapter subassembly (3), screw rifle head storage box (4), liftable cantilever box observe and control panel (5) and small-size screw rifle subassembly (6), the inboard of workstation (2) is provided with linear guide elevating platform (7), linear guide elevating platform (7) threaded connection has lifting part (8), locking revolving stage subassembly (9) are installed to the front side of lifting part (8), helping hand arm (11) are installed to the rear side of workstation (2), the front end of helping hand arm (11) is connected with heavy screw rifle (12), balanced hanging subassembly (13) are installed on the top of workstation (2).
2. The automatic assembly device for a ship turbine rotor according to claim 1, wherein: the base (1) comprises a base body (101) and an oil-resistant anti-slip silica gel pad (102), and the vertical projection of the locking rotary table assembly (9) is positioned on the oil-resistant anti-slip silica gel pad (102).
3. The automatic assembly device for a ship turbine rotor according to claim 1, wherein: the linear guide lifting table (7) comprises a screw (71), a driving component (72) and linear guide (73), the driving component (72) is installed at the top of the workbench (2) and is connected with the screw (71) in a driving mode, guide rails in the linear guide (73) are installed on the left inner wall and the right inner wall of the workbench (2), and sliding tables in the linear guide (73) are installed on two sides of the lifting piece (8).
4. The automatic assembly device for a ship turbine rotor according to claim 1, wherein: an adjustable universal meter frame (10) is arranged on the front side of the lifting piece (8).
5. The automatic assembly device for a ship turbine rotor according to claim 1, wherein: the locking turntable assembly (9) comprises an outer support (91), a locking turntable (92) and an indicator lamp (93), wherein the locking turntable (92) is installed on the outer support (91), and the indicator lamp (93) is installed on the outer support (91) on the periphery of the locking turntable (92).
6. The automatic assembly device for a ship turbine rotor according to claim 1, wherein: the measuring and controlling panel (5) of the liftable cantilever box comprises a mechanical cantilever (51) and a measuring and controlling panel (52), one end of the mechanical cantilever (51) is arranged at the rear side of the workbench (2), and the measuring and controlling panel (52) is arranged at the other end of the mechanical cantilever (51).
7. The automatic assembly device for a ship turbine rotor according to claim 1, wherein: the balance hanging assembly (13) comprises a tripod (131) and a balance hanging (132), the tripod (131) is installed on the workbench (2), and the balance hanging (132) is installed on the tripod (131).
8. The automatic assembly device for a ship turbine rotor according to claim 1, wherein: the switching assembly (3) comprises a first frame body (31), a switching tool (32) and a switching screw gun (33) are arranged on the first frame body (31), the small screw gun assembly (6) comprises a second frame body (61), and a small screw gun (62) is arranged on the second frame body (61).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322294154.3U CN220612960U (en) | 2023-08-25 | 2023-08-25 | Automatic assembly device of aero-turbine rotor |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322294154.3U CN220612960U (en) | 2023-08-25 | 2023-08-25 | Automatic assembly device of aero-turbine rotor |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220612960U true CN220612960U (en) | 2024-03-19 |
Family
ID=90229373
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202322294154.3U Active CN220612960U (en) | 2023-08-25 | 2023-08-25 | Automatic assembly device of aero-turbine rotor |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220612960U (en) |
-
2023
- 2023-08-25 CN CN202322294154.3U patent/CN220612960U/en active Active
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