Airplane wheel cooling device

Abstract

The utility model discloses an airplane wheel cooling device, which not only can reduce the damage to an airplane tire and a hub, but also is wide in applicability, simple to operate and convenient and flexible to use, and comprises a chassis, an adjusting bracket, trundles, a slide rail, a tray, a foot margin, a fixed plate, a shell, a controller, a motor, fan blades, a protective net and a cable, trundles are mounted on the chassis; a sliding rail is mounted on the chassis; a tray is mounted on the sliding rail; ground feet are mounted on the tray; a cable is placed on the tray; a fixing plate is mounted on the adjusting bracket; a shell is mounted on the fixing plate; a controller is mounted on the shell; a motor is mounted on the shell; fan blades are mounted on the motor; and a protective net is mounted at the rear end of the motor on the shell.

Description

Technical field:

[0001] The utility model relates to the technical field of aircraft support equipment, in particular to a cooling device, in particular to an aircraft wheel cooling device, which can not only reduce the damage to aircraft tires and wheel hubs, but also has wide applicability, simple operation, and convenient and flexible use. Background technology:

[0002] In a traditional aircraft wheel cooling device, the hub and the cooling device are fixed by fastening devices such as elastic support arms. This fixing method is likely to cause damage to the aircraft wheel hub. In addition, the traditional aircraft wheel cooling device has a single scope of use and can meet the cooling needs of a certain aircraft model. Therefore, there is a need for an aircraft wheel cooling device that is widely applicable, simple to operate, and convenient and flexible to use. Summary of the invention:

[0003] The technical problem to be solved by the utility model is to overcome the shortcomings of the background technology and provide an aircraft wheel cooling device, in particular an aircraft wheel cooling device which has wide applicability, is simple to operate, and is convenient and flexible to use.

[0004] In order to solve the above problems, the following technical scheme is adopted to realize an aircraft wheel cooling device, comprising a chassis, an adjusting bracket, casters, slide rails, a tray, feet, a fixing plate, a shell, a controller, a motor, a fan blade, a protective net, and a cable, wherein the chassis is provided with an adjusting bracket; the chassis is provided with casters; the chassis is provided with slide rails; the chassis is provided with a tray; the slide rails are provided with a tray; the tray is provided with feet; the tray is provided with a cable; the adjusting bracket is provided with a fixing plate; the shell is provided with a shell; the fixing plate is provided with a controller; the shell is provided with a motor; the shell is provided with a fan blade; and the shell is provided with a protective net at the rear end of the motor.

[0005] The beneficial effects produced by the utility model are as follows: the adjustment bracket of the aircraft wheel cooling device can adjust the height of the cooling device, can meet the cooling requirements of various aircraft models, has a wide range of applications, adopts a non-fixed method to replace the fixed form of the traditional fastening device, does not damage the aircraft tires and wheels, the cables and other equipment of the cooling device can be placed on the tray, is simple to operate, and is easy to use. Description of the drawings:

[0006] Figure 1 It is a main structural schematic diagram of the utility model.

[0007] Figure 2 It is a right-side structural schematic diagram of the utility model.

[0008] Figure 3 It is a schematic diagram of the structure of the utility model when viewed from above.

[0009] Figure 4 It is a schematic diagram of the structure of the utility model from top view.

[0010] Figure 5 It is a left-side structural schematic diagram of the utility model.

[0011] Figure 6 It is a three-dimensional structural schematic diagram of the utility model. Specific implementation method:

[0012] The utility model is further described with reference to the accompanying drawings: it should be understood that these embodiments are only used to illustrate the utility model and are not used to limit the scope of the utility model. In addition, it should be understood that after reading the content taught by the utility model, those skilled in the art can make various changes or modifications to the utility model, and these equivalent forms also fall within the scope defined by the claims attached to this application.

[0013] A cooling device for aircraft wheels comprises a chassis 1, an adjusting bracket 2, a caster 3, a slide rail 4, a tray 5, a foot 6, a fixing plate 7, a shell 8, a controller 9, a motor 10, a fan blade 11, a protective net 12, and a cable 13, wherein the adjusting bracket 2 is installed on the chassis 1; the caster 3 is installed on the chassis 1; the slide rail 4 is installed on the chassis 1; the tray 5 is installed on the slide rail 4; the foot 6 is installed on the tray 5; the cable 13 is placed on the tray 5; the fixing plate 7 is installed on the adjusting bracket 2; the shell 8 is installed on the fixing plate 7; the controller 9 is installed on the shell 8; the motor 10 is installed on the shell 8; the fan blade 11 is installed on the motor 10; and the protective net 12 is installed on the shell 8 at the rear end of the motor 10.

[0014] The adjusting bracket 2 is used to adjust the height of the cooling device, which can meet the cooling requirements of tires and wheels of different aircraft models and has wide applicability.

[0015] The caster 3 has a braking function.

[0016] The tray 5 has a storage function and can store equipment such as cables placed on the cooling device.

[0017] The number of the feet 6 is several.

[0018] The function of the foot 6 is to stabilize the device on the ground to prevent the device from moving when working.

[0019] The fan blades 11 are provided in a certain number.

[0020] Usage: Quickly transport the aircraft wheel cooling device to the side of the aircraft that has just landed, adjust the adjustment bracket 2 so that the shell 8 contacts the aircraft wheel hub, brake the caster 3, adjust the foot 6 to the ground and lock the lock on the foot 6, which reduces the damage to the aircraft wheel hub caused by the traditional fastening device. Connect the power cord, press the start button on the controller 9, and the motor 10 drives the fan blades 11 to send air through the shell 8 into the aircraft tire for heat dissipation. When the heat dissipation is completed, disconnect the power supply, place the power cord on the tray 5, remove the shell 8 from the aircraft tire, and put the device in the designated installation box for next use.

Claims

1. An aircraft wheel cooling device, comprising a chassis (1), an adjustment bracket (2), a caster (3), a slide rail (4), a tray (5), a foot (6), a fixing plate (7), a housing (8), a controller (9), a motor (10), a fan blade (11), a protective net (12), and a cable (13), characterized in that: The chassis (1) is provided with an adjustment bracket (2); the chassis (1) is provided with a caster (3); the chassis (1) is provided with a slide rail (4); the slide rail (4) is provided with a tray (5); the tray (5) is provided with a foot (6); a cable (13) is placed on the tray (5); the adjustment bracket (2) is provided with a fixing plate (7); the fixing plate (7) is provided with a housing (8); the housing (8) is provided with a controller (9); the housing (8) is provided with a motor (10); the motor (10) is provided with a fan blade (11); and a protective net (12) is provided at the rear end of the motor (10) on the housing (8).

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