CN221987961U - A turboprop aircraft engine installation vehicle - Google Patents
A turboprop aircraft engine installation vehicle Download PDFInfo
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- CN221987961U CN221987961U CN202323629198.3U CN202323629198U CN221987961U CN 221987961 U CN221987961 U CN 221987961U CN 202323629198 U CN202323629198 U CN 202323629198U CN 221987961 U CN221987961 U CN 221987961U
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- 238000009434 installation Methods 0.000 title claims abstract description 21
- 239000000725 suspension Substances 0.000 claims description 6
- 230000005611 electricity Effects 0.000 abstract description 4
- 230000000694 effects Effects 0.000 description 2
- 238000011900 installation process Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 239000002002 slurry Substances 0.000 description 1
- 230000009466 transformation Effects 0.000 description 1
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Abstract
The utility model discloses a turboprop aircraft engine mounting vehicle, which relates to the technical field of mounting devices and comprises: the lifting platform is arranged on the vehicle body, lifting driving parts for driving the lifting platform to move up and down are arranged on the vehicle body, a telescopic auxiliary workbench is arranged on the lifting platform, and a plurality of auxiliary parts are arranged around the vehicle body; according to the utility model, the plurality of moving wheels move to corresponding positions, the plurality of auxiliary parts assist in fixing the whole trolley, the vortex-paddle engine is hoisted to the lifting platform through the hoisting assembly, an operator stands on the lifting platform, and the lifting driving part can drive the lifting platform to move up and down, so that the vortex-paddle engine is conveniently installed to the corresponding positions; the telescopic auxiliary workbench can be telescopic, so that the service area of the lifting platform is increased; when the whole machine fails and cannot be driven by electricity, the traction wheels are put down to get rid of poverty, and then other vehicles are used for traction to convey the installation vehicle to a designated place, so that the disassembly and the installation of the turboprop engine are facilitated.
Description
Technical Field
The utility model relates to the technical field of mounting devices, in particular to a vortex slurry aircraft engine mounting vehicle.
Background
Aircraft engines are used as the core power components of aircraft and require frequent handling and inspection and maintenance. But the aeroengine has the mounting difficulties of large volume, heavy weight, complex structure, small mounting clearance and the like, so that the precise attitude adjustment and positioning are difficult to realize when the aeroengine is assembled and disassembled, and the assembling and disassembling quality can have important influence on the power performance of the aeroplane. At present, manual operation mechanical equipment is generally adopted in China to carry out aeroengine installation operation, so that not only is the installation efficiency low, but also the installation accuracy is difficult to guarantee. The installation process is also accompanied by various risks of damaging the engine; thus, the method comprises the steps of; industry needs to change the current situation. The problem of difficulty in disassembly and assembly of the aircraft engine is solved through automatic transformation, and the aircraft engine is required. To this end we provide a turboprop aircraft engine mounting vehicle.
Disclosure of utility model
The technical problems solved by the utility model are as follows: at present, manual operation mechanical equipment is generally adopted in China to carry out aeroengine installation operation, so that not only is the installation efficiency low, but also the installation accuracy is difficult to guarantee. The installation process is also accompanied by various problems with risk of damaging the engine.
The utility model can be realized by the following technical scheme: a turboprop aircraft engine mounting vehicle comprising: the lifting device comprises a vehicle body, wherein a lifting platform is arranged on the vehicle body, a lifting driving piece for driving the lifting platform to move up and down is arranged on the vehicle body, a telescopic auxiliary workbench is arranged on the lifting platform, a plurality of auxiliary pieces are arranged around the vehicle body, a hoisting assembly is arranged on the vehicle body, the hoisting assembly is located above the lifting platform, and a plurality of moving wheels are arranged at the bottom of the vehicle body.
The utility model further technically improves that: the lift driving member includes: the folding telescopic frame is vertically arranged on the vehicle body, the top telescopic end of the folding telescopic frame is connected with the bottom of the lifting platform, and a driving cylinder for driving the folding telescopic frame to stretch is arranged on the vehicle body.
The utility model further technically improves that: the telescopic auxiliary workbench comprises: the bottom plate and two folding frames, bottom plate horizontal sliding mounting is on lift platform to two folding frames set up in the both sides of bottom plate relatively, and the one end and the lift platform of folding frame are connected.
The utility model further technically improves that: each auxiliary piece comprises a rotating foot which is rotatably arranged at the bottom of the vehicle body, and one end, far away from the vehicle body, of the rotating foot is provided with a supporting foot in a threaded manner.
The utility model further technically improves that: the hoisting assembly comprises a suspension rod, a cantilever is horizontally arranged on the suspension rod, a sliding table is horizontally and slidably arranged on the cantilever, and a telescopic lifting hook is arranged on the sliding table.
The utility model further technically improves that: the bottom of the car body is provided with a plurality of escape traction wheels.
Compared with the prior art, the utility model has the following beneficial effects:
According to the device, the rotating feet are rotated to the periphery of the trolley, the supporting feet are rotated to adjust the supporting height of the trolley, so that the whole trolley is supported and fixed, the telescopic lifting hooks are used for driving the vortex-paddle engine to lift, the telescopic lifting hooks and the vortex-paddle engine are driven to horizontally move through sliding, the telescopic lifting hooks are used for driving the vortex-paddle engine to move to the lifting platform, an operator stands on the lifting platform, and the telescopic lifting frames are driven to extend and retract through the stretching of the driving air cylinders, so that the lifting platform is driven to move up and down, and the vortex-paddle engine is conveniently installed at the corresponding position; the bottom plate horizontally slides and drives the two folding frames to stretch, so that the use area of the telescopic auxiliary workbench is adjusted, the installation and the use of operators are facilitated, and the use area of the lifting platform is increased; when the whole machine fails and cannot be driven by electricity, the traction wheels are put down to get rid of poverty, and then other vehicles are used for traction to convey the installation vehicle to a designated place, so that the disassembly and the installation of the turboprop engine are facilitated.
Drawings
The present utility model is further described below with reference to the accompanying drawings for the convenience of understanding by those skilled in the art.
FIG. 1 is a schematic perspective view of the present utility model;
Fig. 2 is a schematic top view of the present utility model.
In the figure: 1. a vehicle body; 2. a lifting platform; 3. a retractable auxiliary workbench; 301. a bottom plate; 302. a folding frame; 4. folding the telescopic frame; 5. a driving cylinder; 6. a rotating foot; 7. supporting feet; 8. suspending the rod; 9. a cantilever; 10. a sliding table; 11. a telescopic lifting hook; 12. the traction wheel is released.
Detailed Description
In order to further describe the technical means and effects adopted by the utility model for achieving the preset aim, the following detailed description is given below of the specific implementation, structure, characteristics and effects according to the utility model with reference to the attached drawings and the preferred embodiment.
Referring to fig. 1-2, the present utility model provides a turboprop aircraft engine mounting vehicle; comprising the following steps: the lifting device comprises a vehicle body 1, wherein a lifting platform 2 is arranged on the vehicle body 1, a lifting driving piece for driving the lifting platform 2 to move up and down is arranged on the vehicle body 1, a telescopic auxiliary workbench 3 is arranged on the lifting platform 2, a plurality of auxiliary pieces are arranged around the vehicle body 1, a hoisting assembly is arranged on the vehicle body 1 and is positioned above the lifting platform 2, and a plurality of moving wheels are arranged at the bottom of the vehicle body 1; the whole trolley moves to the corresponding position through a plurality of moving wheels, a plurality of auxiliary parts assist in fixing the whole trolley, the vortex-propeller engine is hoisted to the lifting platform 2 through the hoisting assembly, an operator stands on the lifting platform 2, and the lifting driving part can drive the lifting platform 2 to move up and down, so that the vortex-propeller engine is conveniently installed to the corresponding position; the telescopic auxiliary workbench 3 can be telescopic, so that the use area of the lifting platform 2 is increased.
The lift driving member includes: the folding telescopic frame 4 is vertically arranged on the vehicle body 1, the top telescopic end of the folding telescopic frame 4 is connected with the bottom of the lifting platform 2, and the vehicle body 1 is provided with a driving cylinder 5 for driving the folding telescopic frame 4 to extend; the folding expansion bracket 4 is driven to extend and retract by driving the expansion of the air cylinder 5, so as to drive the lifting platform 2 to move up and down.
The telescopic auxiliary table 3 includes: a base 301 and two folding frames 302, the base 301 is horizontally and slidably mounted on the lifting platform 2, and the two folding frames 302 are oppositely arranged at two sides of the base 301, and one end of the folding frame 302 is connected with the lifting platform 2; the base plate 301 is horizontally slid, and meanwhile, the two folding frames 302 are driven to stretch, so that the using area of the telescopic auxiliary workbench 3 is adjusted, and the installation and the use of operators are facilitated.
Each auxiliary piece comprises a rotating foot 6, the rotating foot 6 is rotatably arranged at the bottom of the vehicle body 1, one end of the rotating foot 6 far away from the vehicle body 1 is provided with a supporting foot 7 in a threaded manner, and the supporting foot 7 is provided with a supporting foot; when the whole trolley moves to the corresponding position, the rotating feet 6 are rotated to the periphery of the trolley, and the supporting feet 7 are rotated to adjust the supporting height of the trolley, so that the whole trolley is supported and fixed.
The hoisting assembly comprises a suspension rod 8, a cantilever 9 is horizontally arranged on the suspension rod 8, a sliding table 10 is horizontally arranged on the cantilever 9 in a sliding manner, and a telescopic lifting hook 11 is arranged on the sliding table 10; the vortex-paddle engine is driven to hoist through the telescopic lifting hook 11, the telescopic lifting hook 11 and the vortex-paddle engine are driven to horizontally move through sliding, and the vortex-paddle engine is driven to move to the lifting platform 2 through the telescopic lifting hook 11.
The bottom of the vehicle body 1 is provided with a plurality of escape traction wheels 12; when the complete machine fails and cannot be driven by electricity, the traction wheel 12 is put down, and then the other vehicles are used for traction to transport the installation vehicle to a designated place.
When the trolley is used, the whole trolley moves to the corresponding position through a plurality of moving wheels, the rotating feet 6 are rotated to the periphery of the trolley, the supporting feet 7 are rotated to adjust the supporting height of the trolley, so that the whole trolley is supported and fixed, the telescopic lifting hooks 11 are used for driving the vortex-propeller engine to hoist, the telescopic lifting hooks 11 and the vortex-propeller engine are driven to horizontally move through sliding, the vortex-propeller engine is driven to move to the lifting platform 2 through the telescopic lifting hooks 11, an operator stands on the lifting platform 2, and the folding telescopic frames 4 are driven to stretch and shrink through the expansion of the driving air cylinders 5, so that the lifting platform 2 is driven to move up and down, and the vortex-propeller engine is convenient to install at the corresponding position; the base plate 301 is used for horizontally sliding, and simultaneously, the two folding frames 302 are driven to stretch, so that the use area of the telescopic auxiliary workbench 3 is adjusted, the installation and the use of operators are facilitated, and the use area of the lifting platform 2 is improved; when the complete machine fails and cannot be driven by electricity, the traction wheel 12 is put down, and then the other vehicles are used for traction to transport the installation vehicle to a designated place.
The present utility model is not limited in any way by the above-described preferred embodiments, but is not limited to the above-described preferred embodiments, and any person skilled in the art will appreciate that the present utility model can be embodied in the form of a program for carrying out the method of the present utility model, while the above disclosure is directed to various equivalent embodiments, which are capable of being modified or altered in some ways, any simple modification, equivalent variations and alterations made to the above embodiments according to the technical principles of the present utility model will still fall within the scope of the technical aspects of the present utility model.
Claims (5)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202323629198.3U CN221987961U (en) | 2023-12-28 | 2023-12-28 | A turboprop aircraft engine installation vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202323629198.3U CN221987961U (en) | 2023-12-28 | 2023-12-28 | A turboprop aircraft engine installation vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN221987961U true CN221987961U (en) | 2024-11-12 |
Family
ID=93374700
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202323629198.3U Active CN221987961U (en) | 2023-12-28 | 2023-12-28 | A turboprop aircraft engine installation vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN221987961U (en) |
-
2023
- 2023-12-28 CN CN202323629198.3U patent/CN221987961U/en active Active
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