CN108751038A - A kind of repair lifting device and its application method for airplane wheel - Google Patents
A kind of repair lifting device and its application method for airplane wheel Download PDFInfo
- Publication number
- CN108751038A CN108751038A CN201810524161.9A CN201810524161A CN108751038A CN 108751038 A CN108751038 A CN 108751038A CN 201810524161 A CN201810524161 A CN 201810524161A CN 108751038 A CN108751038 A CN 108751038A
- Authority
- CN
- China
- Prior art keywords
- wheel
- bottom plate
- import
- plate
- export
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Withdrawn
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/40—Maintaining or repairing aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B66—HOISTING; LIFTING; HAULING
- B66F—HOISTING, LIFTING, HAULING OR PUSHING, NOT OTHERWISE PROVIDED FOR, e.g. DEVICES WHICH APPLY A LIFTING OR PUSHING FORCE DIRECTLY TO THE SURFACE OF A LOAD
- B66F7/00—Lifting frames, e.g. for lifting vehicles; Platform lifts
- B66F7/10—Lifting frames, e.g. for lifting vehicles; Platform lifts with platforms supported directly by jacks
- B66F7/16—Lifting frames, e.g. for lifting vehicles; Platform lifts with platforms supported directly by jacks by one or more hydraulic or pneumatic jacks
- B66F7/20—Lifting frames, e.g. for lifting vehicles; Platform lifts with platforms supported directly by jacks by one or more hydraulic or pneumatic jacks by several jacks with means for maintaining the platforms horizontal during movement
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B66—HOISTING; LIFTING; HAULING
- B66F—HOISTING, LIFTING, HAULING OR PUSHING, NOT OTHERWISE PROVIDED FOR, e.g. DEVICES WHICH APPLY A LIFTING OR PUSHING FORCE DIRECTLY TO THE SURFACE OF A LOAD
- B66F7/00—Lifting frames, e.g. for lifting vehicles; Platform lifts
- B66F7/28—Constructional details, e.g. end stops, pivoting supporting members, sliding runners adjustable to load dimensions
Landscapes
- Engineering & Computer Science (AREA)
- Life Sciences & Earth Sciences (AREA)
- Geology (AREA)
- Mechanical Engineering (AREA)
- Structural Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Transportation (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transmission Devices (AREA)
Abstract
The invention discloses a kind of repair lifting devices and its application method for airplane wheel, are related to aircraft maintenance facility field.The present invention includes bottom plate, and the bottom surface of bottom plate is uniformly installed there are four universal wheel, and the one side middle part of bottom plate is provided with a first import and export, and the upper surface of bottom plate is symmetrically provided with two cambered ways, and the upper surface middle part of bottom plate is rotatably connected to a Rotational Cylindrical；The middle part week side of plate during the top of Rotational Cylindrical is rotatably connected to one, Rotational Cylindrical is fixed with a turbine, and turbine and the worm screw engaged transmission being fixed on motor output shaft, motor are fixedly mounted on the upper surface of bottom plate；Middle plate one side is provided with second import and export corresponding with first import and export.The present invention, come the lifting of controlroof, to realize the lifting of airplane wheel, and is coordinated the engagement driving of turbine and worm to realize that the certain angle of airplane wheel turns to, improves the maintenance efficiency of airplane wheel and the lifting stability of airplane wheel by synchronous fuel tank.
Description
Technical field
The invention belongs to aircraft maintenance facility field, more particularly to a kind of repair lifting device for airplane wheel and
Its application method.
Background technology
With the fast development of China's transport service and tourist industry, people or article mostly use greatly this mode of aircraft and go out
It goes or transports, to pursue the maximized saving time, but frequent use of aircraft also brings certain repair to maintenance personal
Pressure.
Currently, existing aircraft maintenance ancillary equipment only has simple lifting function, and the stability lifted is poor, cannot
Enough airplane wheel is driven to carry out certain steering, this repairs airplane wheel to maintenance personal and brings inconvenience.
Invention content
The purpose of the present invention is to provide a kind of repair lifting devices and its application method for airplane wheel, by same
Step oil cylinder carrys out the lifting of controlroof, to realize the lifting of airplane wheel, and the engagement of turbine and worm is coordinated to drive to realize
The certain angle of airplane wheel turns to, and solves existing aircraft maintenance ancillary equipment lifting stability difference and can not drive aircraft
Wheel carries out the problem of certain angle rotation.
In order to solve the above technical problems, the present invention is achieved by the following technical solutions：
The present invention is a kind of repair lifting device for airplane wheel, including bottom plate, the bottom surface of the bottom plate uniformly pacify
There are four universal wheel, the one side middle parts of the bottom plate to be provided with a first import and export for dress, and the upper surface of the bottom plate is symmetrically provided with
The upper surface middle part of two cambered ways, the bottom plate is rotatably connected to a Rotational Cylindrical；
The middle part week side of plate during the top of the Rotational Cylindrical is rotatably connected to one, the Rotational Cylindrical is fixed with a turbine,
The turbine and the worm screw engaged transmission being fixed on motor output shaft, the motor are fixedly mounted on the upper surface of bottom plate；
The middle plate one side is provided with second import and export corresponding with first import and export, and the lower surface of the middle plate is symmetrical
It is fixed with first support bar compatible with cambered way, the upper surface of the middle plate is symmetrically installed with one group and synchronizes oil
Cylinder, the piston rod end of the synchronous fuel tank are fixedly connected with the lower surface of top plate；
The side of the top plate is provided with a third inlet and outlet corresponding with second import and export, the upper surface edge of the top plate
Sliding slot is symmetrically provided on length direction, the upper surface of the top plate is provided with the several groups card slot being connected with sliding slot, the top plate
Upper surface slide be connected with two card wheel blocks；
Wheel chamber compatible with airplane wheel profile is symmetrically provided on the close face of the two card wheel blocks, the card wheel block
Bottom surface is uniformly fixed with several sliding blocks compatible with sliding slot, and one side of the card wheel block far from wheel chamber is hinged with one second
The bottom end of strut, the second support bar is fixed with a kelly compatible with card slot.
Further, the bottom end of the first support bar is fixedly connected with a bearing, all sides of the bearing and arc
Slideway is adapted.
Further, one side of the bottom plate far from first import and export is fixed with a push bracket.
A kind of application method of repair lifting device for airplane wheel, includes the following steps：
Step 1 pushes push bracket, and airplane wheel is made to be located at first import and export, second import and export and third inlet and outlet
It is interior；
Step 2 pushes two card wheel blocks simultaneously two card wheel blocks to be made to block airplane wheel, then by kelly and card slot
Mutually it is clamped；
Step 3 controls synchronous fuel tank, the piston rod of synchronous fuel tank is made to jack up top plate, and top plate is driven by card wheel block to fly
Wheel carries out elevating movement；
Step 4 starts motor, makes worm screw engaged transmission and turbine engaged transmission, and middle plate is driven by card wheel block to fly
Wheel carries out divertical motion.
The invention has the advantages that：
1, the present invention lifts top plate based on middle plate by synchronous fuel tank, so that two card wheel blocks drive
Airplane wheel is lifted, and is repaired to airplane wheel convenient for people, improves the maintenance efficiency of airplane wheel and for flying
The practicability of the repair lifting device of wheel.
2, the present invention drives the engaged transmission of worm screw and turbine by motor, and plate carries out certain angle in so that Rotational Cylindrical is driven
Rotation so that card wheel block drive airplane wheel rotate come personnel easy to repair repair, mitigation maintenance personal
Labour pressure.
3, the present invention is blocked airplane wheel by two card wheel blocks, and avoids aircraft by the clamping of kelly and card slot
Wheel rolls, and improves the stability that repair lifting device lifts airplane wheel.
Certainly, it implements any of the products of the present invention and does not necessarily require achieving all the advantages described above at the same time.
Description of the drawings
In order to illustrate the technical solution of the embodiments of the present invention more clearly, will be described below to embodiment required
Attached drawing is briefly described, it should be apparent that, drawings in the following description are only some embodiments of the invention, for ability
For the those of ordinary skill of domain, without creative efforts, it can also be obtained according to these attached drawings other attached
Figure.
Fig. 1 is a kind of structural schematic diagram of repair lifting device for airplane wheel of the present invention；
Fig. 2 is the front view of Fig. 1；
Fig. 3 is scheme of installation of the middle plate of the present invention on bottom plate；
Fig. 4 is the structural schematic diagram of the bottom plate of the present invention；
Fig. 5 is the structural schematic diagram of the top plate of the present invention；
Fig. 6 is the structural schematic diagram of the card wheel block of the present invention；
In attached drawing, parts list represented by the reference numerals are as follows：
1- bottom plates, plate in 2-, 3- motors, 4- top plates, 5- card wheel blocks, 101- first import and exports, 102- cambered ways, 103-
Rotational Cylindrical, 104- push bracket, 201- second import and exports, 202- first support bars, 203- synchronous fuel tanks, 401- thirds inlet and outlet,
402- sliding slots, 403- card slots, 501- take turns chamber, 502- sliding blocks, 503- second support bars, 1031- turbines, 5031- kellies.
Specific implementation mode
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation describes, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, those of ordinary skill in the art are obtained all other without creative efforts
Embodiment shall fall within the protection scope of the present invention.
In the description of the present invention, it is to be understood that, term " setting ", "ON", " upper surface ", " lower surface ", " side
Indicating positions or the position relationship such as face ", " all sides ", are merely for convenience of description of the present invention and simplification of the description, rather than indicate
Or imply that signified component or element must have a particular orientation, with specific azimuth configuration and operation, therefore cannot understand
For limitation of the present invention.
As shown in Figs 1-4, the present invention is a kind of repair lifting device for airplane wheel, including bottom plate 1, bottom plate 1
Bottom surface is uniformly installed there are four universal wheel, and the one side middle part of bottom plate 1 is provided with a first import and export 101, the upper surface pair of bottom plate 1
Title is provided with two cambered ways 102, and the upper surface middle part of bottom plate 1 is rotatably connected to a Rotational Cylindrical 103；
The middle part week side of plate 2 during the top of Rotational Cylindrical 103 is rotatably connected to one, Rotational Cylindrical 103 is fixed with a turbine
1031, turbine 1031 and the worm screw engaged transmission being fixed on 3 output shaft of motor, motor 3 are fixedly mounted on the upper surface of bottom plate 1
On；Motor 3 drives the engaged transmission of worm screw and turbine 1031, so that plate 2 is rotated during Rotational Cylindrical 103 drives, realizes
Two card wheel blocks 5 drive the rotation of airplane wheel certain angles, can effectively improve the maintenance efficiency of maintenance personal.
As shown in figure 3,2 one side of middle plate is provided with second import and export 201 corresponding with first import and export 101, middle plate 2
Lower surface is symmetrically fixed with first support bar 202 compatible with cambered way 102, and first support bar 202 can be that middle plate 2 rotates
During support force is provided, the upper surface of the balance of plate 2 in guarantee, middle plate 2 is symmetrically installed with one group of synchronous fuel tank
203, the quantity of one group of synchronous fuel tank 203 is two, and the piston rod end of synchronous fuel tank 203 is fixed with the lower surface of top plate 4 to be connected
It connects；
As shown in Figure 1 and Figure 5, the side of top plate 4 is provided with a third inlet and outlet 401 corresponding with second import and export 201,
The upper surface of top plate 4 is symmetrically provided with sliding slot 402 on along its length, if the upper surface of top plate 4 is provided with and is connected with sliding slot 402
Dry group card slot 403, the upper surface slide of top plate 4 are connected with two card wheel blocks 5；
As shown in fig. 6, being symmetrically provided with wheel chamber 501 compatible with airplane wheel profile on the close face of two card wheel blocks 5, block
The bottom surface of wheel block 5 is uniformly fixed with three sliding blocks 502 compatible with sliding slot 402, one side of the card wheel block 5 far from wheel chamber 501
It is hinged with a second support bar 503, the bottom end of second support bar 503 is fixed with a kelly 5031 compatible with card slot 403, card
Slot 403 is clamped achievable two card wheel blocks 5 with kelly 5031 and is blocked to airplane wheel, ensures the lifting stability of airplane wheel.
Wherein, the bottom end of first support bar 202 is fixedly connected with a bearing, all sides and 102 phase of cambered way of bearing
Adaptation, can reduce the frictional force of first support bar 202 and cambered way 102.
Wherein, one side of the bottom plate 1 far from first import and export 101 is fixed with a push bracket 104, and push bracket 104 is moved convenient for people
Dynamic bottom plate 1.
A kind of application method of repair lifting device for airplane wheel, includes the following steps：
Step 1 pushes push bracket 104, and airplane wheel is made to be located at first import and export 101, second import and export 201 and the
In three inlet and outlet 401；
Step 2 pushes two card wheel blocks 5 simultaneously two card wheel blocks 5 to be made to block airplane wheel, then by kelly 5031
It is clamped with 403 phase of card slot；
Step 3 controls synchronous fuel tank 203, so that the piston rod of synchronous fuel tank 203 is jacked up top plate 4, top plate 4 passes through card wheel
Block 5 drives airplane wheel to carry out elevating movement；
Step 4 starts motor 3, and worm screw engaged transmission and 1031 engaged transmission of turbine, middle plate 2 is made to pass through card wheel block
5 drive airplane wheel to carry out divertical motion, consequently facilitating maintenance personal repairs airplane wheel.
In the description of this specification, the description of reference term " one embodiment ", " example ", " specific example " etc. means
Particular features, structures, materials, or characteristics described in conjunction with this embodiment or example are contained at least one implementation of the present invention
In example or example.In the present specification, schematic expression of the above terms may not refer to the same embodiment or example.
Moreover, particular features, structures, materials, or characteristics described can be in any one or more of the embodiments or examples to close
Suitable mode combines.
Present invention disclosed above preferred embodiment is only intended to help to illustrate the present invention.There is no detailed for preferred embodiment
All details are described, are not limited the invention to the specific embodiments described.Obviously, according to the content of this specification,
It can make many modifications and variations.These embodiments are chosen and specifically described to this specification, is in order to preferably explain the present invention
Principle and practical application, to enable skilled artisan to be best understood by and utilize the present invention.The present invention is only
It is limited by claims and its full scope and equivalent.
Claims (4)
1. the bottom surface of a kind of repair lifting device for airplane wheel, including bottom plate (1), the bottom plate (1) is uniformly equipped with
Four universal wheels, it is characterised in that：
It is provided with a first import and export (101) in the middle part of the one side of the bottom plate (1), the upper surface of the bottom plate (1) is symmetrically provided with
The upper surface middle part of two cambered ways (102), the bottom plate (1) is rotatably connected to a Rotational Cylindrical (103)；
The middle part week side of plate (2) during the top of the Rotational Cylindrical (103) is rotatably connected to one, the Rotational Cylindrical (103) is fixed
There are a turbine (1031), the turbine (1031) and the worm screw engaged transmission being fixed on motor (3) output shaft, the motor
(3) it is fixedly mounted on the upper surface of bottom plate (1)；
Middle plate (2) one side is provided with second import and export (201) corresponding with first import and export (101), the middle plate (2)
Lower surface be symmetrically fixed with the compatible first support bar (202) of cambered way (102), the upper surface of the middle plate (2)
Symmetrically it is installed with one group of synchronous fuel tank (203), the following table of the piston rod end and top plate (4) of the synchronous fuel tank (203)
Face is fixedly connected；
The side of the top plate (4) is provided with a third inlet and outlet (401) corresponding with second import and export (201), the top plate
(4) upper surface is symmetrically provided with sliding slot (402) on along its length, the upper surface of the top plate (4) is provided with and sliding slot (402) phase
The upper surface slide of the several groups card slot (403) of connection, the top plate (4) is connected with two card wheel blocks (5)；
It is symmetrically provided with wheel chamber (501) compatible with airplane wheel profile, the card wheel on the close face of the two card wheel blocks (5)
The bottom surface of block (5) is uniformly fixed with and the compatible several sliding blocks (502) of sliding slot (402), the separate wheel chamber of the card wheel block (5)
(501) one side is hinged with a second support bar (503), and the bottom end of the second support bar (503) is fixed with one and card slot
(403) compatible kelly (5031).
2. a kind of repair lifting device for airplane wheel according to claim 1, which is characterized in that first described
The bottom end of strut (202) is fixedly connected with a bearing, and all sides of the bearing are adapted with cambered way (102).
3. a kind of repair lifting device for airplane wheel according to claim 1, which is characterized in that the bottom plate
(1) one side far from first import and export (101) is fixed with a push bracket (104).
4. a kind of application method of repair lifting device for airplane wheel as described in any one of claims 1-3, special
Sign is, includes the following steps：
Step 1, push push bracket (104), make airplane wheel be located at first import and export (101), second import and export (201) and
Third is imported and exported in (401)；
Step 2 pushes two card wheel blocks (5) simultaneously two card wheel blocks (5) to be made to block airplane wheel, then by kelly
(5031) it is mutually clamped with card slot (403)；
Step 3, control synchronous fuel tank (203) make the piston rod of synchronous fuel tank (203) jack up top plate (4), and top plate (4) passes through
Card wheel block (5) drives airplane wheel to carry out elevating movement；
Step 4 starts motor (3), and worm screw engaged transmission and turbine (1031) engaged transmission, middle plate (2) is made to pass through card wheel
Block (5) drives airplane wheel to carry out divertical motion.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810524161.9A CN108751038A (en) | 2018-05-28 | 2018-05-28 | A kind of repair lifting device and its application method for airplane wheel |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810524161.9A CN108751038A (en) | 2018-05-28 | 2018-05-28 | A kind of repair lifting device and its application method for airplane wheel |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108751038A true CN108751038A (en) | 2018-11-06 |
Family
ID=64003129
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810524161.9A Withdrawn CN108751038A (en) | 2018-05-28 | 2018-05-28 | A kind of repair lifting device and its application method for airplane wheel |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108751038A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111268163A (en) * | 2020-03-25 | 2020-06-12 | 安徽三联学院 | Airplane tire clamping device and working method thereof |
| CN113247300A (en) * | 2021-05-12 | 2021-08-13 | 成都航空职业技术学院 | Protective equipment for maintenance of unmanned helicopter |
-
2018
- 2018-05-28 CN CN201810524161.9A patent/CN108751038A/en not_active Withdrawn
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111268163A (en) * | 2020-03-25 | 2020-06-12 | 安徽三联学院 | Airplane tire clamping device and working method thereof |
| CN113247300A (en) * | 2021-05-12 | 2021-08-13 | 成都航空职业技术学院 | Protective equipment for maintenance of unmanned helicopter |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN208441100U (en) | A kind of hydraulic engineering pile body pile pulling device | |
| CN108751038A (en) | A kind of repair lifting device and its application method for airplane wheel | |
| CN211072466U (en) | Lifting device for automobile manufacturing | |
| CN108981497A (en) | A kind of space rocket rocket body rolling device | |
| CN204872792U (en) | Horizontal rotation device based on light sense control rotation angle | |
| CN201330082Y (en) | Electric skid stacking/unstacking machine and its stacking/unstacking support device | |
| CN205582725U (en) | Transformer core production platform | |
| CN208306048U (en) | A kind of glue stations | |
| CN106073620B (en) | A kind of accurate adjustable intelligent window cleaning equipment of wiping angle | |
| CN108110662A (en) | It is a kind of to carry the power distribution cabinet transporter for facilitating installation | |
| CN209336279U (en) | A kind of laminating machine scrap (bridge) support device | |
| CN203615011U (en) | Supporting mechanism | |
| CN208536701U (en) | A kind of space rocket rocket body rolling device | |
| CN208846050U (en) | A kind of long distance wireless multi-angle monitoring device based on cloud service | |
| CN209240651U (en) | A kind of swift elevating mechanism of printing machine | |
| CN209428069U (en) | A kind of movable lifting of strength support | |
| CN108788088B (en) | Bracket for involution | |
| CN209239437U (en) | A kind of disassembling fixture | |
| CN207903836U (en) | A kind of drilling rod lifting rotating device | |
| CN206493226U (en) | A kind of mechanical correcting device of emery wheel | |
| CN110261548A (en) | One kind being used for factory garden air environmental pollution intellectual monitoring instrument | |
| CN220053068U (en) | Laminating machine for carton processing | |
| CN221703969U (en) | Digital metering pump | |
| CN205223902U (en) | Two -way turning device of traffic awl | |
| CN221546365U (en) | Building engineering template fixing device |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WW01 | Invention patent application withdrawn after publication | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20181106 |