CN219792272U - Aircraft rudder lifting appliance - Google Patents

Aircraft rudder lifting appliance Download PDF

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Publication number
CN219792272U
CN219792272U CN202320827359.0U CN202320827359U CN219792272U CN 219792272 U CN219792272 U CN 219792272U CN 202320827359 U CN202320827359 U CN 202320827359U CN 219792272 U CN219792272 U CN 219792272U
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China
Prior art keywords
fixedly connected
motor
lifting
joint
base
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CN202320827359.0U
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Chinese (zh)
Inventor
刘跃旺
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Tianjin Hangyuan Technology Co ltd
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Tianjin Hangyuan Technology Co ltd
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Priority to CN202320827359.0U priority Critical patent/CN219792272U/en
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Abstract

The utility model discloses an aircraft rudder lifting appliance, which belongs to the technical field of lifting appliances and comprises a base, wherein the top of the base is fixedly connected with a supporting frame, the top of the supporting frame is provided with a sliding groove, a fixing frame is fixedly connected in the sliding groove through a lifting assembly, the top of the fixing frame is clamped with a lifting rod, and one end of the lifting rod is fixedly connected with a first storage box. The rudder lifting device has the beneficial effects that through the arrangement of the supporting plate, the telescopic frame, the clamping buckle and the tightening buckle, the clamping is conveniently placed on rudders of different sizes, the second motor, the rotating shaft, the collecting roller and the stretching belt are arranged, the rudder to be clamped is conveniently pulled and lifted, the lifting operation is conveniently carried out, the second storage box and the bearing block are arranged, the rudder lifting is conveniently and more stable, and the height to be lifted is conveniently adjusted by arranging the first motor, the threaded rod, the threaded cylinder and the sliding plate.

Description

Aircraft rudder lifting appliance
Technical Field
The utility model relates to the technical field of lifting appliances, in particular to an aircraft rudder lifting appliance.
Background
Rudders, which refer to the movable airfoil sections on a vertical tail for the purpose of achieving directional maneuvering of an aircraft. Typically with a hinge at the rear of the vertical stabilizer. The pilot can control the course of the airplane by operating the left and right deflection of the pilot through the pedals. The rudder turns left, the airflow acts on the rudder to generate a moment for enabling the tail to right, the nose is enabled to be left, and the heading of the airplane is changed. When the rudder turns right, the machine head turns right, and when the rudder is overhauled and installed, a lifting appliance is needed to be used for assisting;
the existing lifting appliance solves the problem of use, but also has the problems that the lifting height of the lifting appliance cannot be adjusted according to requirements and the lifting appliance cannot be flushed and cleaned according to the used clamping buckle.
Disclosure of Invention
(1) Technical problem to be solved
Aiming at the defects of the prior art, the utility model aims to provide an aircraft rudder lifting appliance, which has the characteristics of adjusting the lifting height of the lifting appliance according to requirements and flushing and cleaning the used clamping buckle.
(2) Technical proposal
In order to achieve the above purpose, the utility model provides the aircraft rudder lifting appliance, which comprises a base, wherein the top of the base is fixedly connected with a supporting frame, the top of the supporting frame is provided with a sliding groove, a fixing frame is fixedly connected in the sliding groove through a lifting assembly, the top of the fixing frame is clamped with a hanging rod, one end of the hanging rod is fixedly connected with a first storage box, one side of the first storage box is fixedly connected with a second motor, the output end of the second motor is fixedly connected with a rotating shaft, the rotating shaft penetrates through the first storage box and is positioned in the first storage box, the outer surface of the rotating shaft is fixedly connected with a collecting roller, the outer surface of the collecting roller is sleeved with a stretching belt, and the stretching belt penetrates through the first storage box and is fixedly connected with a supporting plate.
When the aircraft rudder lifting tool adopting the technical scheme is used, the second motor, the rotating shaft, the collecting roller and the stretching belt are used for conveniently pulling and lifting the rudder in clamping.
Further, the rising subassembly includes first motor, first motor fixed connection is in the bottom of spout, the output shaft fixedly connected with threaded rod of first motor, the surface threaded connection of threaded rod has a screw thread section of thick bamboo, the surface fixedly connected with sliding plate of screw thread section of thick bamboo, the top fixedly connected with catch bar of sliding plate, the top fixedly connected with of catch bar is in the bottom of mount.
Further, two expansion brackets are movably connected to the bottom of the supporting plate, clamping buckles are fixedly connected to the bottoms of the two expansion brackets, tightening buckles are fixedly connected to the clamping buckles, a second storage box is fixedly connected to one end of the hanging rod, and a bearing block is placed in the second storage box.
Further, one side fixedly connected with water tank of support frame and place the case, the inner wall bottom fixedly connected with water pump of water tank, the output fixedly connected with communicating pipe of water pump, pass water tank and joint in one side of water tank communicating pipe, the other end fixedly connected with shower nozzle of communicating pipe, two drawers have been placed to place the incasement.
Further, one side fixedly connected with connecting rod of support frame, the other end fixedly connected with light of connecting rod, the toolbox has been placed at the top of base, place the clearance pole in the toolbox, one side fixedly connected with spacing of base, the joint has the dead lever on the spacing.
Further, the storage groove is formed in the support frame, the storage battery is fixedly connected to the bottom of the storage groove, the controller is fixedly connected to the front face of the support frame, the storage battery is electrically connected with the controller through a wire, and the controller is electrically connected with the water pump, the first motor, the second motor and the illuminating lamp through wires respectively.
(3) Advantageous effects
In summary, the utility model has the following beneficial effects:
1. through setting up backup pad, expansion bracket, joint knot and restraint and detain, conveniently place the joint to the rudder of equidimension not, through setting up second motor, pivot, collection roller and stretching strap, conveniently carry out pulling to the rudder of joint and promote, conveniently carry out the lifting operation, through setting up second containing box and bearing block, it is more stable when conveniently lifting to the rudder, through setting up first motor, threaded rod, screw thread section of thick bamboo and sliding plate, conveniently adjust to the height that the rudder lifted;
2. through setting up connecting rod and light, conveniently throw light on when the rudder lifts by crane and use, through setting up spacing and dead lever, conveniently install the use to different positions, through setting up water tank, water pump, communicating pipe and shower nozzle, conveniently wash the clearance to the joint knot after using, conveniently use next time;
3. through setting up placement box and drawer, conveniently place lifting device and take, through setting up toolbox and clearance pole, convenient debris that produces when lifting is accomodate, make things convenient for the staff to carry out unified processing.
Drawings
In order to more clearly illustrate the embodiments of the present utility model or the technical solutions in the prior art, the drawings required for the description of the embodiments or the prior art will be briefly described, and it is apparent that the drawings in the following description are only one embodiment of the present utility model, and other drawings can be obtained according to the drawings without inventive effort for a person skilled in the art.
FIG. 1 is a schematic view of the present utility model in elevation and cross section;
FIG. 2 is a schematic diagram of the front view of the present utility model;
FIG. 3 is a schematic view of the structure of the lift assembly of FIG. 1 according to the present utility model.
The marks in the drawings are:
1. a base; 2. a support frame; 3. a storage groove; 4. a storage battery; 5. a limiting frame; 6. a fixed rod; 7. a water tank; 8. a water pump; 9. a communicating pipe; 10. a spray head; 11. placing a box; 12. a drawer; 13. a chute; 14. a lifting assembly; 141. a first motor; 142. a threaded rod; 143. a thread cylinder; 144. a sliding plate; 145. a push rod; 15. a fixing frame; 16. a boom; 17. a first storage box; 18. a second motor; 19. a rotating shaft; 20. a take-up roller; 21. stretching the belt; 22. a support plate; 23. a telescopic frame; 24. a clamping buckle; 25. fastening the bundles; 26. a second storage box; 27. a bearing block; 28. a connecting rod; 29. a lighting lamp; 30. a tool box; 31. cleaning a rod; 32. and a controller.
Detailed Description
In order to make the technical means, the creation characteristics, the achievement of the purpose and the effect of the present utility model easy to understand, the technical solutions in the embodiments of the present utility model are clearly and completely described below to further illustrate the present utility model, and it is obvious that the described embodiments are only some embodiments of the present utility model, not all versions.
Examples:
the utility model is described in further detail below with reference to fig. 1-3.
Referring to fig. 1-3, the present utility model provides a technical solution: the utility model provides an aircraft rudder hoist, including base 1, the top fixedly connected with support frame 2 of base 1, spout 13 has been seted up at the top of support frame 2, through rising subassembly 14 fixedly connected with mount 15 in the spout 13, the top joint of mount 15 has jib 16, the first containing box 17 of one end fixedly connected with of jib 16, one side fixedly connected with second motor 18 of first containing box 17, the output fixedly connected with pivot 19 of second motor 18, pivot 19 passes first containing box 17 and is located first containing box 17, the surface fixedly connected with of pivot 19 collects roller 20, collect roller 20's surface has cup jointed tensile area 21, through setting up second motor 18, pivot 19, collect roller 20 and tensile area 21, conveniently carry out pulling to the rudder of joint and promote, conveniently carry out the lifting operation, tensile area 21 passes first containing box 17 and fixedly connected with backup pad 22.
Specifically, the lifting assembly 14 includes a first motor 141, the first motor 141 is fixedly connected to the bottom of the chute 13, an output shaft of the first motor 141 is fixedly connected with a threaded rod 142, an outer surface of the threaded rod 142 is in threaded connection with a threaded cylinder 143, an outer surface of the threaded cylinder 143 is fixedly connected with a sliding plate 144, a pushing rod 145 is fixedly connected to the top of the sliding plate 144, and the top end of the pushing rod 145 is fixedly connected to the bottom of the fixing frame 15.
Through adopting above-mentioned technical scheme, through first motor 141, threaded rod 142, screw thread section of thick bamboo 143 and sliding plate 144, the height that conveniently lifts up to the rudder is adjusted.
Specifically, two expansion brackets 23 are movably connected to the bottom of the supporting plate 22, clamping buckles 24 are fixedly connected to the bottoms of the two expansion brackets 23, tightening buckles 25 are fixedly connected to the two clamping buckles 24, a second storage box 26 is fixedly connected to one end of the suspender 16, and a bearing block 27 is placed in the second storage box 26.
Through adopting above-mentioned technical scheme, through expansion bracket 23, joint knot 24 and tightening knot 25, the convenience carries out the joint to the rudder of equidimension not, through second containing box 26 and bearing block 27, the convenience is more stable when lifting to the rudder.
Specifically, one side fixedly connected with water tank 7 of support frame 2 and place case 11, the inner wall bottom fixedly connected with water pump 8 of water tank 7, the output fixedly connected with communicating pipe 9 of water pump 8, communicating pipe 9 pass water tank 7 and joint in one side of water tank 7, the other end fixedly connected with shower nozzle 10 of communicating pipe 9, place two drawers 12 in the case 11.
Through adopting above-mentioned technical scheme, through water tank 7, water pump 8, communicating pipe 9 and shower nozzle 10, conveniently wash the clearance to joint knot 24 after the use, through placing case 11 and drawer 12, the instrument of using when conveniently placing the hoist and mount, conveniently take.
Specifically, one side fixedly connected with connecting rod 28 of support frame 2, the other end fixedly connected with light 29 of connecting rod 28, toolbox 30 has been placed at the top of base 1, has placed clearance pole 31 in the toolbox 30, and one side fixedly connected with spacing 5 of base 1, joint has dead lever 6 on the spacing 5.
Through adopting above-mentioned technical scheme, through connecting rod 28 and light 29, conveniently throw light on when hoist and mount, through toolbox 30 and clearance pole 31, conveniently accomodate to debris that produce when hoist and mount, through spacing 5 and dead lever 6, conveniently fix to the position of difference.
Specifically, the storage groove 3 is formed in the support frame 2, the storage battery 4 is fixedly connected to the bottom of the storage groove 3, the controller 32 is fixedly connected to the front face of the support frame 2, the storage battery 4 is electrically connected to the controller 32 through wires, and the controller 32 is electrically connected to the water pump 8, the first motor 141, the second motor 18 and the lighting lamp 29 through wires.
By adopting the technical scheme, the storage battery 4 and the controller 32 facilitate the operation and the use of staff.
The working principle of the utility model is as follows: when the device is used, a worker places the device at a required position, the base 1 is clamped and fixed through the fixing rod 6, the device is convenient to use at different positions, the worker places rudders to be hoisted on the two clamping buckles 24, clamping and fixing are carried out through the clamping buckles 25, clamping and connection are conveniently carried out on the rudders in different directions, the storage battery 4 supplies power to the controller 32, the controller 32 controls the second motor 18 to work, the rotating shaft 19 is driven to rotate, the collecting roller 20 is driven to rotate, the stretching belt 21 is driven to shrink, the supporting plate 22 is driven to lift, the hoisting is convenient for the hoisting of the rudders to be hoisted, the controller 32 controls the first motor 141 to work, the threaded rod 142 is driven to rotate, the threaded cylinder 143 is driven to lift or lower on the threaded rod 142, the sliding plate 144 is driven to lift or lower in the sliding groove 13, the pushing rod 145 is driven to push the fixing frame 15, and the hoisting height is convenient to adjust;
the controller 32 control light 29, conveniently throw light on when using, through the bearing block 27, it is more stable when conveniently lifting to the rudder, through drawer 12, the instrument of using when conveniently placing, conveniently take, through toolbox 30, the debris of conveniently placing the clearance and using, after the use, controller 32 control water pump 8 draws water in water tank 7, through communicating pipe 9 blowout at shower nozzle 10, the convenience is washed the clearance to the joint knot 24 after the use, the convenience is used next time.
The present embodiment is only for explanation of the present utility model and is not to be construed as limiting the present utility model, and modifications to the present embodiment, which may not creatively contribute to the present utility model as required by those skilled in the art after reading the present specification, are all protected by patent laws within the scope of claims of the present utility model.

Claims (6)

1. Aircraft rudder lifting appliance, comprising a base (1), characterized in that: the utility model discloses a base, including base (1), support frame (1), spout (13) have been seted up at the top of base (1), through rising subassembly (14) fixedly connected with mount (15) in spout (13), the top joint of mount (15) has jib (16), the one end fixedly connected with first containing box (17) of jib (16), one side fixedly connected with second motor (18) of first containing box (17), the output fixedly connected with pivot (19) of second motor (18), pivot (19) pass first containing box (17) and are located first containing box (17), the surface fixedly connected with of pivot (19) is collected roller (20), the surface of collecting roller (20) has cup jointed stretching strap (21), stretching strap (21) pass first containing box (17) and fixedly connected with backup pad (22).
2. An aircraft rudder lifting appliance according to claim 1, wherein: the lifting assembly (14) comprises a first motor (141), the first motor (141) is fixedly connected to the bottom of the sliding groove (13), an output shaft of the first motor (141) is fixedly connected with a threaded rod (142), the outer surface of the threaded rod (142) is in threaded connection with a threaded cylinder (143), the outer surface of the threaded cylinder (143) is fixedly connected with a sliding plate (144), the top of the sliding plate (144) is fixedly connected with a pushing rod (145), and the top of the pushing rod (145) is fixedly connected to the bottom of the fixing frame (15).
3. An aircraft rudder lifting appliance according to claim 1, wherein: the bottom swing joint of backup pad (22) has two expansion brackets (23), two the equal fixedly connected with joint knot (24) in bottom of expansion bracket (23), two equal joint has binding buckle (25) on joint knot (24), the one end fixedly connected with second containing box (26) of jib (16), placed bearing block (27) in second containing box (26).
4. An aircraft rudder lifting appliance according to claim 1, wherein: one side fixedly connected with water tank (7) of support frame (2) and place case (11), the inner wall bottom fixedly connected with water pump (8) of water tank (7), the output fixedly connected with communicating pipe (9) of water pump (8), communicating pipe (9) pass water tank (7) and joint in one side of water tank (7), the other end fixedly connected with shower nozzle (10) of communicating pipe (9), place two drawers (12) in case (11).
5. An aircraft rudder lifting appliance according to claim 1, wherein: one side fixedly connected with connecting rod (28) of support frame (2), other end fixedly connected with light (29) of connecting rod (28), toolbox (30) have been placed at the top of base (1), cleaning rod (31) have been placed in toolbox (30), one side fixedly connected with spacing (5) of base (1), joint has dead lever (6) on spacing (5).
6. An aircraft rudder lifting appliance according to claim 1, wherein: the storage tank (3) has been seted up on support frame (2), the bottom fixedly connected with battery (4) of storage tank (3), the positive fixedly connected with controller (32) of support frame (2), battery (4) and controller (32) pass through wire electric connection, controller (32) respectively with water pump (8), first motor (141), second motor (18) and light (29) pass through wire electric connection.
CN202320827359.0U 2023-04-14 2023-04-14 Aircraft rudder lifting appliance Active CN219792272U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202320827359.0U CN219792272U (en) 2023-04-14 2023-04-14 Aircraft rudder lifting appliance

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202320827359.0U CN219792272U (en) 2023-04-14 2023-04-14 Aircraft rudder lifting appliance

Publications (1)

Publication Number Publication Date
CN219792272U true CN219792272U (en) 2023-10-03

Family

ID=88157303

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202320827359.0U Active CN219792272U (en) 2023-04-14 2023-04-14 Aircraft rudder lifting appliance

Country Status (1)

Country Link
CN (1) CN219792272U (en)

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