CN214001727U

CN214001727U - Airplane wheel chock conveying device

Info

Publication number: CN214001727U
Application number: CN202022839601.5U
Authority: CN
Inventors: 郭宇; 朱杰威; 杨梦娜; 吉起旺; 魏文博; 付鑫; 韩源
Original assignee: Nanjing Vocational University of Industry Technology NUIT
Current assignee: Nanjing Vocational University of Industry Technology NUIT
Priority date: 2020-12-02
Filing date: 2020-12-02
Publication date: 2021-08-20
Anticipated expiration: 2030-12-02

Abstract

The utility model discloses an aircraft wheel fender conveyer relates to air transportation technical field, including handrail frame, mobile device and mounting panel, handrail frame and mounting panel pass through the mobile device and connect, be equipped with in the mounting panel and deposit the subassembly and be used for saving and release aircraft wheel fender, this utility model can assist airport crew member to store, carry aircraft wheel fender, reduce crew member's work load, promote crew member and place and retrieve the efficiency that aircraft wheel kept off to can protect crew member's personal safety.

Description

Airplane wheel chock conveying device

Technical Field

The utility model relates to an air transportation technical field specifically is an aircraft fender conveyer.

Background

At present, after an airplane stops at a parking position, crew members are required to place wheel blocks of the airplane at the front position and the rear position of wheels of the airplane so as to prevent the airplane from sliding; before the airplane takes off, the crew members are required to recover the wheel barriers, however, the wheel barriers placed by the cargo airplane of the airliner are too heavy, the placing quantity of the wheel barriers has certain requirements, a plurality of crew members are required to go to and fro the wheel barrier placing positions and the airplane wheel positions to place each wheel barrier in place, and the parking apron of the airport is too hot in summer due to the limitation of functions and materials; in winter, rain and snow are cold and easy to slip, and great troubles are caused for the crew to place the wheel gear.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide an aircraft fender conveyer to solve the problem that proposes among the above-mentioned background art.

In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides an aircraft wheel fender conveyer, includes handrail frame, mobile device and mounting panel, handrail frame and mounting panel pass through the mobile device and connect, be equipped with in the mounting panel and deposit the subassembly and be used for saving and release aircraft wheel fender.

Preferably, the handrail frame comprises a hexagonal frame, a solar cell panel and a handrail, the solar cell panel is a monocrystalline silicon solar cell and is installed in the hexagonal frame, the handrail is in threaded connection with the hexagonal frame, and the solar cell panel and the handrail are arranged at intervals.

Preferably, the moving device comprises support rods and universal wheels, the support rods are uniformly distributed on six corners of the hexagonal frame, and the universal wheels are connected below each support rod through bolts.

Preferably, the upper surface of the mounting plate is recessed inwards, a drain hole is formed in the center of the mounting plate, six storage holes are uniformly formed in the mounting plate, a storage battery is arranged between every two storage holes, and the storage battery is electrically connected with the solar panel.

Preferably, deposit the subassembly and include flexible railing and electric push rod, flexible railing is installed on the output shaft of electric push rod, flexible railing and electric push rod are installed in the recess that the storage hole bottom corresponds, the electric push rod passes through control switch and battery electric connection.

Compared with the prior art, the utility model discloses a beneficial effect is:

the utility model discloses a can assist airport crew to store, carry the aircraft fender, reduce crew's work load, promote crew and place and pull down the efficiency that the aircraft fender was taken turns to can protect crew's personal safety.

Drawings

FIG. 1 is a schematic structural view of the present invention;

FIG. 2 is a schematic front view of the present invention;

FIG. 3 is a schematic diagram of the circuit structure of the present invention;

FIG. 4 is a cross-sectional view taken along line A-A of FIG. 2;

fig. 5 is a schematic bottom view of the utility model.

In the figure: 1-armrest frame; 11-a hexagonal frame; 12-a solar panel; 13-a handrail;

2-a mobile device; 21-a support bar; 22-universal wheels;

3, mounting a plate; 31-a drain hole; 32-a storage well; 33-a storage battery;

4-a storage assembly; 41-telescopic railings; 42-electric push rod.

Detailed Description

The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some of the embodiments, not all of the embodiments. All other embodiments obtained by a person skilled in the art without any inventive work based on the embodiments of the present invention belong to the scope of the present invention.

Referring to fig. 1 to 5, the present invention provides a technical solution: the utility model provides an aircraft wheel fender conveyer, includes handrail frame 1, mobile device 2 and mounting panel 3, handrail frame 1 and mounting panel 3 pass through mobile device 2 and connect, be equipped with storage assembly 4 in the mounting panel 3 and be used for saving and release aircraft wheel fender.

In this embodiment, handrail frame 1 includes hexagon frame 11, solar cell panel 12 and handrail 13, solar cell panel 12 is single crystalline silicon solar cell and installs in hexagon frame 11, handrail 13 threaded connection is on hexagon frame 11, solar cell panel 12 sets up with handrail 13 interval, and this handrail frame 1 is used for doing the utility model discloses the electricity generation and as the handrail when removing.

In the present embodiment, the moving device 2 includes support rods 21 and universal wheels 22, the support rods 21 are uniformly distributed on six corners of the hexagonal frame 11, and the universal wheels 22 are bolted below each support rod 21.

In this embodiment, 3 upper surfaces of mounting panel are inwards sunken and central point puts and is equipped with wash port 31, evenly be equipped with six storage holes 32 on the mounting panel 3, per two be equipped with battery 33 between the storage hole 32, battery 33 and solar cell panel 12 electric connection, 3 upper surfaces of mounting panel are inwards sunken the wash port 31 drainage of being convenient for, and battery 33 of setting can store electric power, avoids solar cell panel 12 because of weather or the unable electric energy that produces of trouble.

In this embodiment, deposit subassembly 4 including flexible railing 41 and electric putter 42, flexible railing 41 is installed on electric putter 42's output shaft, flexible railing 41 and electric putter 42 are installed in the recess that storage hole 32 bottom corresponds, electric putter 42 passes through control switch 43 and battery 33 electric connection, and flexible railing 41 erects the support when stretching out the aircraft wheel fender, can emit in storage hole 32 with the aircraft wheel fender when the withdrawal.

The working principle is as follows: when the airplane stops at a parking position, a crew puts wheel blocks in the six storage holes 32 of the mounting plate 3 and is supported by the closed storage assembly 4, then pushes the handrails 13 to transport the wheel blocks to the positions where the wheel blocks need to be placed through the universal wheels 22, presses the control switch 43 to start the electric push rods 42 to draw back the telescopic railings 41, automatically puts the wheel blocks down from the storage holes 32, and places the wheel blocks at the front and rear positions of the airplane wheels to fix the airplane; before the aircraft is ready to take off, the crew puts the wheel fender back into the storage hole 32 again, and then puts the utility model together with the wheel fender carrying back into the equipment room.

The drain hole 31 is used for draining water; the upper surface of the mounting plate 3 is concave inwards, so that rainwater can flow out of the water drainage hole 31 conveniently, and the solar cell panel 12 and the storage battery 33 are used for providing power for the electric push rod 42.

Based on the above, this utility model discloses can assist airport crew to store, carry the aircraft wheel fender, reduce crew's work load, promote crew and place and pull down the efficiency that the aircraft wheel kept off to can protect crew's personal safety.

It will be appreciated by those skilled in the art that the present invention may be practiced in other embodiments that depart from its spirit or essential characteristics. The embodiments disclosed above are therefore to be considered in all respects as illustrative and not restrictive. All changes that come within the meaning and range of equivalency of the claims are to be embraced within their scope.

Claims

1. The utility model provides an aircraft wheel fender conveyer which characterized in that: including handrail frame (1), mobile device (2) and mounting panel (3), handrail frame (1) and mounting panel (3) are connected through mobile device (2), be equipped with storage assembly (4) in mounting panel (3) and be used for saving and release aircraft fender.

2. An aircraft wheel chock transportation device according to claim 1, in which: the handrail frame (1) comprises a hexagonal frame (11), a solar cell panel (12) and a handrail (13), wherein the solar cell panel (12) is a monocrystalline silicon solar cell and is installed in the hexagonal frame (11), the handrail (13) is in threaded connection with the hexagonal frame (11), and the solar cell panel (12) and the handrail (13) are arranged at intervals.

3. An aircraft wheel chock transportation device according to claim 2, in which: the moving device (2) comprises supporting rods (21) and universal wheels (22), wherein the supporting rods (21) are uniformly distributed on six corners of the hexagonal frame (11), and the universal wheels (22) are connected below each supporting rod (21) through bolts.

4. An aircraft wheel chock transportation device according to claim 2, in which: mounting panel (3) upper surface is inwards sunken and central point puts and is equipped with wash port (31), evenly be equipped with six storage holes (32) on mounting panel (3), per two be equipped with battery (33) between storage hole (32), battery (33) and solar cell panel (12) electric connection.

5. An aircraft wheel chock transportation device according to claim 4, in which: deposit subassembly (4) including flexible railing (41) and electric putter (42), install on the output shaft of electric putter (42) flexible railing (41), install in the recess that storage hole (32) bottom corresponds flexible railing (41) and electric putter (42), electric putter (42) are through control switch (43) and battery (33) electric connection.