CN211766376U - Aircraft wheel dismouting transfer device - Google Patents

Aircraft wheel dismouting transfer device Download PDF

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Publication number
CN211766376U
CN211766376U CN202020049493.9U CN202020049493U CN211766376U CN 211766376 U CN211766376 U CN 211766376U CN 202020049493 U CN202020049493 U CN 202020049493U CN 211766376 U CN211766376 U CN 211766376U
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China
Prior art keywords
wheel
frame
airplane
rod
installation
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Active
Application number
CN202020049493.9U
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Chinese (zh)
Inventor
李慧凯
张彦荣
杨红海
董振峰
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Xinxiang Xinpu Machinery Co ltd
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Xinxiang Xinpu Machinery Co ltd
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Priority to CN202020049493.9U priority Critical patent/CN211766376U/en
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Publication of CN211766376U publication Critical patent/CN211766376U/en
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Abstract

The utility model provides an aircraft wheel dismouting transfer device, includes the frame, and the frame is equipped with the mount table, is equipped with elevating system between frame and the mount table, and both sides are equipped with the walking wheel around the frame, and the right side of frame is equipped with the leading wheel, is equipped with the direction tow bar on the leading wheel, and the top of mount table is equipped with the backing roll that is equipped with two parallel arrangement, and the axis of backing roll sets up along controlling the direction level, and the right side of mount table is equipped with the installation pole that a perpendicular thought set up. The utility model provides a pair of aircraft wheel dismouting transfer device has simple structure, small in size, easy and simple to handle, remove characteristics such as nimble, safe and reliable, accurate alignment, dismantlement and installation aircraft wheel that can be convenient, the during operation is consuming time little, work is slightly low, and does not have the injured factor of damaging aircraft shaft and dismouting personnel.

Description

Aircraft wheel dismouting transfer device
Technical Field
The utility model belongs to the technical field of the ground maintenance of aircraft wheel equipment, concretely relates to aircraft wheel dismouting transfer device.
Background
Aircraft require frequent replacement of wheels during routine maintenance. Because the wheel is inconsistent to the school, weight is heavy, traditional aircraft wheel dismantles, installs and mainly relies on the manual work to lift with the cooperation of crow bar, and the during operation is hard, intensity of labour is big, and has the factor that impairs aircraft shaft and dismouting personnel are injured.
SUMMERY OF THE UTILITY MODEL
The utility model provides a pair of aircraft wheel dismouting transfer device has simple structure, small in size, easy and simple to handle, remove characteristics such as nimble, safe and reliable, accurate alignment, dismantlement and installation aircraft wheel that can be convenient, the during operation is consuming time little, work is slightly low, and does not have the injured factor of damaging aircraft shaft and dismouting personnel.
In order to solve the technical problem, the utility model adopts the following technical scheme:
an airplane wheel dismounting and transferring device comprises a frame, wherein the frame is provided with an installation platform, a lifting mechanism is arranged between the frame and the installation platform, walking wheels are arranged on the front side and the rear side of the frame, a guide wheel is arranged on the right side of the frame, a guide towing rod is arranged on the guide wheel, two support rollers arranged in parallel are arranged on the top of the installation platform, the axes of the support rollers are horizontally arranged along the left-right direction, an installation rod arranged vertically is arranged on the right side of the installation platform, a position adjusting wheel is arranged in the middle of the installation rod, the axes of the position adjusting wheel are arranged along the up-down direction, a sliding sleeve is arranged on the top of the installation rod, a first set screw and a second set screw are arranged on the sliding sleeve, the first set screw is used for fixing the sliding sleeve, an airplane wheel fixing rod is horizontally penetrated on the sliding sleeve, the first set screw is used for fixing, the left end of the wheel fixing rod is provided with a clamping rod arranged downwards, and the right end of the wheel fixing rod is provided with a control handle arranged upwards.
The lifting mechanism is a hydraulic telescopic rod or an air pressure telescopic rod.
The walking wheel is provided with a brake.
The middle part of the mounting rod is at least provided with two position adjusting wheels.
Adopt above-mentioned technical scheme, the utility model discloses the beneficial effect who has:
when the airplane needs to be disassembled, a worker moves the frame to the position below the airplane wheel needing to be disassembled, the two support rolls which are arranged in parallel are aligned with the airplane wheel needing to be disassembled, after the airplane wheel is disassembled from the airplane, the disassembled airplane wheel is placed on the two support rolls which are arranged in parallel, the first set screw and the second set screw on the sliding sleeve on the mounting rod are unscrewed, the sliding sleeve moves to the position above the airplane wheel, the airplane wheel fixing rod of the sliding sleeve is twisted, the clamping rod at the end part of the airplane wheel fixing rod is clamped with the airplane wheel, the first set screw and the second set screw are simultaneously screwed, the airplane wheel is fastened on the frame, and the disassembling operation of the airplane wheel is completed;
when the airplane needs to be installed with the airplane wheels, the frame fastened with the airplane wheels is moved to the position below the airplane needing to be installed with the airplane wheels, the frame and the installation table are controlled through a manual hydraulic pump or a manual pneumatic pump to move, the installation table is made to lift the airplane wheels to be located at the optimal installation height, the first set screw and the second set screw on the sliding sleeve are simultaneously loosened, the airplane wheels are aligned to the airplane wheel shafts of the airplane, the airplane wheels are directly pushed to the airplane wheel shafts of the airplane, and the fastening bolts between the airplane wheels and the airplane wheel shafts are screwed to complete the installation operation of the airplane wheels.
To sum up, the utility model provides a pair of aircraft wheel dismouting transfer device has simple structure, small in size, easy and simple to handle, remove characteristics such as nimble, safe and reliable, accurate alignment, dismantlement and installation aircraft wheel that can be convenient, the during operation is consuming time little, work is slightly low, and does not have the injured factor of the aircraft shaft of damaging and dismouting personnel.
Drawings
Fig. 1 is a schematic structural view of the present invention;
fig. 2 is a top view of the sliding sleeve and wheel securing lever of fig. 1.
Frame 1, mount table 2, walking wheel 3, leading wheel 4, direction tow bar 5, backing roll 6, installation pole 7, position control wheel 8, sliding sleeve 9, wheel dead lever 10, chucking pole 11, brake valve lever 12.
Detailed Description
As shown in fig. 1 and 2, an airplane wheel dismounting and transferring device comprises a frame 1, the frame 1 is provided with an installation platform 2, a lifting mechanism is arranged between the frame 1 and the installation platform 2, walking wheels 3 are arranged on the front side and the rear side of the frame 1, a guide wheel 4 is arranged on the right side of the frame 1, a guide tow bar 5 is arranged on the guide wheel 4, two support rollers 6 which are arranged in parallel are arranged on the top of the installation platform 2, the axes of the support rollers 6 are horizontally arranged along the left-right direction, an installation rod 7 which is vertically arranged is arranged on the right side of the installation platform 2, a position adjusting wheel 8 is arranged in the middle of the installation rod 7, the airplane wheel can rotate in an auxiliary manner through the support rollers 6 and the position adjusting wheel 8, so that the airplane wheel is aligned with a wheel shaft of an airplane, the axes of the position adjusting wheel 8 are arranged along the up-down direction, a sliding sleeve 9 is arranged on the, first holding screw is used for fixed sliding sleeve 9, still wears to be equipped with an wheel dead lever 10 on the sliding sleeve 9 level, and first holding screw is used for fixed wheel dead lever 10, and wheel dead lever 10 sets up with installation pole 7 is perpendicular, and the left end portion of wheel dead lever 10 is equipped with the chucking pole 11 of downward setting, and the right-hand member portion of wheel dead lever 10 is equipped with the brake valve lever 12 of upwards setting.
The lifting mechanism is a hydraulic telescopic rod or a pneumatic telescopic rod.
The walking wheels 3 are walking wheels provided with brakes.
The middle part of the mounting rod 7 is provided with at least two position adjusting wheels 8.
When an airplane needs to be disassembled, a worker moves the frame 1 to the position below the airplane wheel needing to be disassembled, the two support rolls 6 arranged in parallel are aligned with the airplane wheel needing to be disassembled, after the airplane wheel is disassembled from the airplane, the disassembled airplane wheel is placed on the two support rolls 6 arranged in parallel, the first set screw and the second set screw on the sliding sleeve 9 on the mounting rod 7 are loosened, the sliding sleeve 9 moves to the position above the airplane wheel, the airplane wheel fixing rod 10 of the sliding sleeve 9 is twisted, the clamping rod 11 at the end part of the airplane wheel fixing rod 10 is clamped with the airplane wheel, the first set screw and the second set screw are simultaneously screwed, the airplane wheel is fastened on the frame 1, and the disassembling operation of the airplane wheel is completed;
when the airplane needs to be installed with the airplane wheels, the frame 1 fastened with the airplane wheels is moved to the position below the airplane needing to be installed with the airplane wheels, the lifting mechanism is arranged between the frame 1 and the installation table 2 to act through the manual hydraulic pump or the manual pneumatic pump, the installation table 2 is made to lift the airplane wheels to be at the optimal installation height, the first set screw and the second set screw on the sliding sleeve 9 are simultaneously unscrewed, the airplane wheels are aligned to the airplane wheel shafts of the airplane, the airplane wheels are directly pushed to the airplane wheel shafts of the airplane, and the fastening bolts between the airplane wheels and the airplane wheel shafts are screwed to complete the installation operation of the airplane wheels.
To sum up, the utility model provides a pair of aircraft wheel dismouting transfer device has simple structure, small in size, easy and simple to handle, remove characteristics such as nimble, safe and reliable, accurate alignment, dismantlement and installation aircraft wheel that can be convenient, the during operation is consuming time little, work is slightly low, and does not have the injured factor of the aircraft shaft of damaging and dismouting personnel.
The present embodiment is not intended to limit the shape, material, structure, etc. of the present invention in any form, and all of the technical matters of the present invention belong to the protection scope of the present invention to any simple modification, equivalent change and modification made by the above embodiments.

Claims (4)

1. The utility model provides an aircraft wheel dismouting transfer device which characterized in that: the airplane wheel fixing device comprises a frame, wherein the frame is provided with an installation table, a lifting mechanism is arranged between the frame and the installation table, walking wheels are arranged on the front side and the rear side of the frame, a guide wheel is arranged on the right side of the frame, a guide towing rod is arranged on the guide wheel, two support rollers arranged in parallel are arranged on the top of the installation table, the axes of the support rollers are horizontally arranged along the left and right directions, an installation rod arranged vertically is arranged on the right side of the installation table, a position adjusting wheel is arranged in the middle of the installation rod, the axes of the position adjusting wheel are arranged along the up-down direction, a sliding sleeve is arranged on the top of the installation rod, a first set screw and a second set screw are arranged on the sliding sleeve, the first set screw is used for fixing the sliding sleeve, an airplane wheel fixing rod is horizontally penetrated on the sliding sleeve, the first set screw is used for fixing the airplane wheel fixing rod, the airplane, the right end part of the wheel fixing rod is provided with a control handle which is arranged upwards.
2. An aircraft wheel disassembly and assembly transfer device as claimed in claim 1, wherein: the lifting mechanism is a hydraulic telescopic rod or an air pressure telescopic rod.
3. An aircraft wheel disassembly and assembly transfer device as claimed in claim 2, wherein: the walking wheel is provided with a brake.
4. An aircraft wheel disassembly and assembly transfer device as claimed in claim 3, wherein: the middle part of the mounting rod is at least provided with two position adjusting wheels.
CN202020049493.9U 2020-01-10 2020-01-10 Aircraft wheel dismouting transfer device Active CN211766376U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202020049493.9U CN211766376U (en) 2020-01-10 2020-01-10 Aircraft wheel dismouting transfer device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202020049493.9U CN211766376U (en) 2020-01-10 2020-01-10 Aircraft wheel dismouting transfer device

Publications (1)

Publication Number Publication Date
CN211766376U true CN211766376U (en) 2020-10-27

Family

ID=72889395

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202020049493.9U Active CN211766376U (en) 2020-01-10 2020-01-10 Aircraft wheel dismouting transfer device

Country Status (1)

Country Link
CN (1) CN211766376U (en)

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