CN112478191B - Multifunctional device for rotating wing of general aircraft - Google Patents
Multifunctional device for rotating wing of general aircraft Download PDFInfo
- Publication number
- CN112478191B CN112478191B CN202011481931.XA CN202011481931A CN112478191B CN 112478191 B CN112478191 B CN 112478191B CN 202011481931 A CN202011481931 A CN 202011481931A CN 112478191 B CN112478191 B CN 112478191B
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- Prior art keywords
- lifting
- fixed
- wing
- base
- motor
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- 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
- B64F5/10—Manufacturing or assembling aircraft, e.g. jigs therefor
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60B—VEHICLE WHEELS; CASTORS; AXLES FOR WHEELS OR CASTORS; INCREASING WHEEL ADHESION
- B60B33/00—Castors in general; Anti-clogging castors
- B60B33/02—Castors in general; Anti-clogging castors with disengageable swivel action, i.e. comprising a swivel locking mechanism
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- 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
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- 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
- B66F7/22—Lifting frames, e.g. for lifting vehicles; Platform lifts with tiltable platforms
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- 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
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Life Sciences & Earth Sciences (AREA)
- Geology (AREA)
- Structural Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Transportation (AREA)
- Aviation & Aerospace Engineering (AREA)
- Handcart (AREA)
- Automatic Assembly (AREA)
Abstract
The invention discloses a universal airplane wing rotary multifunctional device, which comprises a base, a lifting frame, a fixed table, an adjusting pressing mechanism, a pedal lifting device and a clamping turnover structure, wherein the lifting frame is arranged on the side edge of the base, compared with the traditional installation of a working airplane wing, 4 sets of special tools are not required, and a special joint for lifting the wing is not required.
Description
[ field of technology ]
The invention relates to the field of auxiliary installation of aviation aircrafts, in particular to a universal aircraft wing rotation multifunctional device.
[ background Art ]
When the general aircraft parts are transported to the final assembly site in a long distance, a special unloading lifting device, an in-situ transfer carrier vehicle, a turnover tool for adjusting the gesture of the parts and a special lifting tool for lifting the parts to the final assembly frame after the gesture is adjusted are required to be designed, 4 sets of special tools are required to be arranged for the parts of the aircraft wings, special joints for lifting are required to be arranged on the wings, the aircraft manufacturing process flow is increased, the tool manufacturing period is long, the manufacturing and maintenance costs are high, truss lifting equipment is required for unloading and lifting, operators are required to utilize a plurality of sets of tools at the same time, the operation is realized, and the working time is limited.
In view of the above drawbacks, there is a need for a multi-functional integrated device that allows for multiple functions of wing unloading from a container, component transfer, component attitude flipping, and mounting to a final assembly frame.
[ invention ]
In order to solve the problems, a universal airplane wing rotating multifunctional device is provided;
the universal aircraft wing rotating multifunctional device is characterized by comprising a base, a lifting frame, a fixed table, an adjusting and pressing mechanism, a pedal lifting device and a clamping and overturning structure, wherein the lifting frame is arranged on the side edge of the base;
the upper end of the base is provided with a fixed table, and 4 adjusting and pressing mechanisms are arranged on the fixed table;
the lifting frame is connected with a clamping turnover structure in a sliding manner through a gear set;
the clamping turnover structure is positioned right above the fixed table;
the clamping overturning structure comprises a lifting table, a fixed handle, a rotating motor and a lifting motor;
the lifting platform is a rectangular cavity;
a rotating motor is arranged in the lifting platform;
the fixed handles are respectively arranged at two sides of the lifting platform and are connected with the rotating motor;
the upper end of the lifting table is provided with a lifting motor;
the lifting motor is connected with the gear set;
the bottom of the base is provided with 4 universal wheels;
the pedal lifting device comprises pedals, a first connecting rod, a second connecting rod and a lifting barrel;
a crank block mechanism is arranged in the lifting barrel;
the pedal is sequentially connected with the first connecting rod, the second connecting rod and the crank slide block mechanism, and the crank slide block mechanism is connected with the gear set.
The adjusting and compressing mechanism comprises a fixed plate, a screw rod, a hand wheel and a top plate;
the fixed plate is fixedly arranged on the fixed table, the fixed plate is provided with a threaded hole, the screw rod penetrates through the threaded hole, the tail end of the screw rod is provided with a top plate, and the head end of the screw rod is provided with a hand wheel.
Further, locking pedals are arranged on the universal wheels.
Further, a plurality of balancing weights are further arranged on the base;
further, an electric box is further arranged on the base, a power supply is arranged in the electric box, and the power supply is connected with the rotating motor and the lifting motor.
Further, a handle is arranged on the lifting frame.
When the wing container is unloaded, the wing container is only required to be opened, the device is moved to a proper position, the fixed handles on the two sides of the device are adopted, the handles are rotated upwards, the vertically placed wings are connected, and the wings are taken out from the transport bracket through the lifting device.
During installation, the whole device is moved to a proper spacious position, the foundation is locked, the rotary handle is rotated, the overturning wing is rotated from the vertical face posture to the horizontal plane installation posture, namely, rotated by 90 degrees to the horizontal state, and the installation work on the wing is completed.
When the wing needs to be provided with the assembly type frame, the whole device is moved to a proper position, the whole wing is lifted up through pedal lifting control, then the whole device is moved to the position of the assembly type frame, the foundation is locked, the wing is lowered, and the butt joint with the assembly type frame is completed.
Compared with the traditional installation of the wing of the working machine, the invention has the advantages that 4 sets of special tools and special joints for lifting the wing are not required, the installation of the wing of the working machine can be completed through the invention, the aircraft manufacturing process flow is reduced, the tool manufacturing period is shortened, and the high manufacturing and maintenance cost is solved.
Compared with the traditional working machine, the wing unloading and lifting device does not need truss lifting equipment, the operation is simpler, and operators do not need to use a plurality of sets of tools at the same time, so that the working time is shortened;
the adjusting and pressing mechanism provided by the invention is more widely applicable, and can be adjusted according to different wing sizes during use.
The locking foot leg provided by the invention can move the whole device when being loosened, so that the wing parts can be transported in a final assembly factory, the movement is more labor-saving, and the whole device is fixed during locking, so that the installation process is smoother and safer.
[ description of the drawings ]
FIG. 1 is a front perspective view of the present invention;
FIG. 2 is a rear perspective view of the present invention;
FIG. 3 is a block diagram of an adjustment hold down mechanism of the present invention;
FIG. 4 is a block diagram of a foot lift of the present invention;
FIG. 5 is a diagram of the structure of the clamping and turning structure of the present invention;
fig. 6 is a use state diagram of the present invention.
The lifting device comprises a 1-base, a 2-lifting frame, a 3-fixed table, a 4-adjusting pressing mechanism, a 5-pedal lifting device, a 6-clamping and overturning structure, 7-universal wheels, an 8-electric box, 9-handles, 401-fixed plates, 402-screw rods, 403-hand wheels, 404-top plates, 501-pedals, 502-first connecting rods, 503-second connecting rods, 504-lifting barrels, 601-lifting tables, 602-fixed handles, 603-rotating motors and 604-lifting motors.
[ detailed description ] of the invention
The present invention will be described in further detail with reference to the drawings and examples, in order to make the objects, technical solutions and advantages of the present invention more apparent. It should be understood that the specific embodiments described herein are for purposes of illustration only and are not intended to limit the scope of the invention.
The universal aircraft wing rotating multifunctional device is characterized by comprising a base, a lifting frame, a fixed table, an adjusting and pressing mechanism, a pedal lifting device and a clamping and overturning structure, wherein the lifting frame is arranged on the side edge of the base;
the upper end of the base is provided with a fixed table, and 4 adjusting and pressing mechanisms are arranged on the fixed table;
the lifting frame is connected with a clamping turnover structure in a sliding manner through a gear set;
the clamping turnover structure is positioned right above the fixed table;
the clamping overturning structure comprises a lifting table, a fixed handle, a rotating motor and a lifting motor;
the lifting platform is a rectangular cavity;
a rotating motor is arranged in the lifting platform;
the fixed handles are respectively arranged at two sides of the lifting platform and are connected with the rotating motor;
the upper end of the lifting table is provided with a lifting motor;
the lifting motor is connected with the gear set;
the bottom of the base is provided with 4 universal wheels;
the pedal lifting device comprises pedals, a first connecting rod, a second connecting rod and a lifting barrel;
a crank block mechanism is arranged in the lifting barrel;
the pedal is sequentially connected with the first connecting rod, the second connecting rod and the crank slide block mechanism, and the crank slide block mechanism is connected with the gear set.
Further, the adjusting and compressing mechanism comprises a fixed plate, a screw rod, a hand wheel and a top plate;
the fixed plate is fixedly arranged on the fixed table, the fixed plate is provided with a threaded hole, the screw rod penetrates through the threaded hole, the tail end of the screw rod is provided with a top plate, and the head end of the screw rod is provided with a hand wheel.
Further, locking pedals are arranged on the universal wheels.
Further, a plurality of balancing weights are further arranged on the base;
further, an electric box is further arranged on the base, a power supply is arranged in the electric box, and the power supply is connected with the rotating motor and the lifting motor.
Further, a handle is arranged on the lifting frame.
When the wing container is unloaded, the wing container is only required to be opened, the device is moved to a proper position, the fixed handles on the two sides of the device are adopted, the handles are rotated upwards, the vertically placed wings are connected, and the wings are taken out from the transport bracket through the lifting device.
During installation, the whole device is moved to a proper spacious position, the foundation is locked, the rotary handle is rotated, the overturning wing is rotated from the vertical face posture to the horizontal plane installation posture, namely, rotated by 90 degrees to the horizontal state, and the installation work on the wing is completed.
When the wing needs to be provided with the assembly type frame, the whole device is moved to a proper position, the whole wing is lifted up through pedal lifting control, then the whole device is moved to the position of the assembly type frame, the foundation is locked, the wing is lowered, and the butt joint with the assembly type frame is completed.
The foregoing description of the preferred embodiments of the invention is not intended to limit the invention to the precise form disclosed, and any such modifications, equivalents, and alternatives falling within the spirit and scope of the invention are intended to be included within the scope of the invention.
Claims (5)
1. A universal aircraft wing rotary multifunctional device, characterized in that: the device comprises a base, a lifting frame, a fixed table, an adjusting and pressing mechanism, a pedal lifting device and a clamping and overturning structure, wherein the lifting frame is arranged on the side edge of the base;
the upper end of the base is provided with a fixed table, and 4 adjusting and pressing mechanisms are arranged on the fixed table;
the lifting frame is connected with a clamping turnover structure in a sliding manner through a gear set;
the clamping turnover structure is positioned right above the fixed table;
the clamping overturning structure comprises a lifting table, a fixed handle, a rotating motor and a lifting motor;
the lifting platform is a rectangular cavity;
a rotating motor is arranged in the lifting platform;
the fixed handles are respectively arranged at two sides of the lifting platform and are connected with the rotating motor;
the upper end of the lifting table is provided with a lifting motor;
the lifting motor is connected with the gear set;
the bottom of the base is provided with 4 universal wheels;
the pedal lifting device comprises pedals, a first connecting rod, a second connecting rod and a lifting barrel;
a crank block mechanism is arranged in the lifting barrel;
the pedal is sequentially connected with a first connecting rod, a second connecting rod and a crank slide block mechanism, and the crank slide block mechanism is connected with the gear set;
the adjusting and compressing mechanism comprises a fixed plate, a screw rod, a hand wheel and a top plate;
the fixing plate is fixedly arranged on the fixing table, the fixing plate is provided with a threaded hole, the screw rod penetrates through the threaded hole, the tail end of the screw rod is provided with a top plate, and the head end of the screw rod is provided with a hand wheel;
the device comprises two steps of unloading and installing;
unloading, moving the device to a proper position after the wing container is opened, adopting fixed handles on two sides of the device, rotating the fixed handles upwards through a rotating motor, connecting the vertically placed wings through connectors of the fixed handles and connecting the wings, and taking out the wings from the transportation bracket through adjusting the height of the lifting device;
the installation, remove whole device to suitable spacious position, locking lower margin, rotate fixed handle, upset wing is rotatory to the horizontal plane installation gesture from the facade gesture, and 90 to horizontality promptly, and rethread elevator motor and pedal elevating gear drive wing lift to the mounted position after, supplementary operating personnel carries out the installation operation, accomplishes the butt joint operation with the assembly type frame, accomplishes the installation work on the wing.
2. A versatile aircraft wing rotary multifunctional device according to claim 1, characterized in that: the universal wheels are provided with locking pedals.
3. A versatile aircraft wing rotary multifunctional device according to claim 1, characterized in that: the base is also provided with a plurality of balancing weights.
4. A versatile aircraft wing rotary multifunctional device according to claim 1, characterized in that: the base is also provided with an electric box, a power supply is arranged in the electric box, and the power supply is connected with the rotating motor and the lifting motor.
5. A versatile aircraft wing rotary multifunctional device according to claim 1, characterized in that: the lifting frame is provided with a handle.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011481931.XA CN112478191B (en) | 2020-12-15 | 2020-12-15 | Multifunctional device for rotating wing of general aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011481931.XA CN112478191B (en) | 2020-12-15 | 2020-12-15 | Multifunctional device for rotating wing of general aircraft |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN112478191A CN112478191A (en) | 2021-03-12 |
| CN112478191B true CN112478191B (en) | 2023-04-28 |
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ID=74917138
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202011481931.XA Active CN112478191B (en) | 2020-12-15 | 2020-12-15 | Multifunctional device for rotating wing of general aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN112478191B (en) |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP3018710U (en) * | 1995-05-29 | 1995-11-28 | 三菱電機エンジニアリング株式会社 | Trolley with lift |
| CN102249172A (en) * | 2011-07-18 | 2011-11-23 | 华中科技大学 | Multifunctional elevating and overturning device |
| US9593001B2 (en) * | 2013-08-27 | 2017-03-14 | The Boeing Company | Mechanism for translation/rotation in X-Y directions |
| CN108637724B (en) * | 2018-04-25 | 2020-06-30 | 西安飞机工业（集团）有限责任公司 | Pressing mechanism of machining tool table for airplane-type titanium alloy parts |
| CN110639741B (en) * | 2019-10-10 | 2021-08-24 | 陕西汇成天云智能科技有限公司 | Spraying device is used in production and processing of unmanned aerial vehicle wing |
| CN111137341B (en) * | 2019-12-30 | 2020-11-27 | 四川航泰航空装备有限公司 | Integrated unmanned aerial vehicle wing bracket for assembling, unloading and transporting |
-
2020
- 2020-12-15 CN CN202011481931.XA patent/CN112478191B/en active Active
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| Publication number | Publication date |
|---|---|
| CN112478191A (en) | 2021-03-12 |
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