CN218489928U

CN218489928U - Ground traction starting comprehensive distribution vehicle for airplane helicopter

Info

Publication number: CN218489928U
Application number: CN202222831512.5U
Authority: CN
Inventors: 薛祥越; 王东风; 郝海涛
Original assignee: Individual
Current assignee: Individual
Priority date: 2022-10-26
Filing date: 2022-10-26
Publication date: 2023-02-17
Anticipated expiration: 2032-10-26

Abstract

The utility model relates to the technical field of accessory traction, in particular to a ground traction starting comprehensive distribution vehicle for an airplane helicopter, which comprises a vehicle body, wherein a storage battery is arranged inside the vehicle body, a panel is arranged inside the vehicle body, and an alternating current socket, a direct current socket and a binding post are respectively arranged on the upper surface of the panel; an inverter is arranged inside the handle; wherein the battery is parallelly connected with DC socket, terminal, dc-to-ac converter, the dc-to-ac converter is parallelly connected with AC socket, terminal and cable electric connection, and the cable passes the automobile body and extends to the outside for aircraft start provides ground power, also can provide required power for aircraft ground circular telegram inspection simultaneously, this application is through increasing at its inside start-up and directly, AC power supply system, make the automobile body use as ground power, when aircraft start-up needs ground power, the cable is direct to the feeder ear of aircraft, for the aircraft power supply, the distribution guarantee car can regard as the power supply use of peripheral equipment, greatly increased its application scope.

Description

Ground traction starting comprehensive distribution vehicle for airplane helicopter

Technical Field

The utility model relates to an accessory pulls technical field, especially relates to aircraft helicopter ground pulls starts to synthesize distribution car.

Background

Luggage/cargo tractors, motor vehicles for towing aircraft containerized/bulk cargo trailers and various types of ground equipment.

Through retrieval, as in the chinese utility model patent, the application number: "CN202121845698.9" discloses a "step-drive type electric tractor", which includes: the device comprises a vehicle body, wherein a support is arranged on one side of the vehicle body, a cambered iron core polyurethane wheel is rotatably connected to the support, and a super polyurethane wheel is rotatably connected to the other side of the vehicle body; the high-elasticity wear-resistant solid rubber wheels are rotationally connected to the two sides of the vehicle body; the connecting rod is arranged on one side of the vehicle body, and one end of the connecting rod is provided with a pulling handle; the first traction assembly and the second traction assembly are installed on the vehicle body. This formula electric traction car is driven to step pulls the subassembly through setting up different first subassembly and the second of pulling, makes the accessory of multiple difference all can connect and install on this tractor, and the adaptation scope is wide, can install multiple traction accessory, is fit for multiple occasion, and various traction accessories can both be installed on the tractor, realize that the diversification pulls, practice thrift manufacturing cost greatly.

But the step that proposes in the aforesaid drives formula electric traction car has only realized how to install various traction accessories on the tractor, realizes diversified the traction, but above-mentioned step drives formula electric traction car and has only basic function, uses as the tractor of airport freight promptly, and application scope is less, consequently, this application has proposed one kind and can regard as aircraft ground start power, and formula tractor is driven to the great step of application scope simultaneously.

SUMMERY OF THE UTILITY MODEL

The embodiment of the application starts the comprehensive distribution car through providing aircraft helicopter ground traction, has solved among the prior art that the walking frame tractor can only use as airport freight's tractor, the less problem of application scope.

The embodiment of the application provides a ground traction starting comprehensive distribution vehicle for an airplane helicopter, which comprises a vehicle body, wherein driving wheels are arranged on the front side and the rear side of the vehicle body respectively and are driven by a driving motor, front wheels and rear wheels are arranged at the middle positions of the left side and the right side of the vehicle body respectively, the vehicle body is positioned on the same side surface of the rear wheels and is fixedly connected with a handle, traction assemblies are arranged at the top and the left end of the vehicle body respectively,

a storage battery is arranged in the vehicle body, a panel is arranged in the vehicle body, and an alternating current socket, a direct current socket and a binding post are respectively arranged on the upper surface of the panel;

an inverter is arranged inside the handle;

the storage battery is connected with the direct current socket, the binding post and the inverter in parallel, the inverter is connected with the alternating current socket in parallel, the binding post is electrically connected with the cable, the cable penetrates through the vehicle body to extend to the outside and is used for providing a ground power supply for starting the airplane and providing a required power supply for ground electrification inspection of the airplane.

Preferably, the cable is wound around an outer surface of the vehicle body.

Preferably, the equal fixed mounting in both ends has an electromagnetism push rod around the automobile body is close to the side of handle, the top of electromagnetism push rod can be dismantled respectively and be connected with camera and light, electric connection can be dismantled through interface and battery to camera and light.

Preferably, two cavities are formed in the upper surface of the handle, a first cover plate is hinged to the outer portion of each cavity, one cavity is used for placing the inverter, and the other cavity is used for placing the camera, the illuminating lamp and the image storage device.

Preferably, the upper surface of the vehicle body is hinged with a second cover plate at the position of the panel.

Preferably, the left end fixedly connected with connecting block of automobile body, the automobile body passes through the connecting block and is connected with the snowboard rotation.

Preferably, still install sucking disc formula loudspeaker on the preceding terminal surface of automobile body, loudspeaker pass through the sucking disc and can dismantle with the automobile body and be connected.

One or more technical solutions provided in the embodiments of the present application have at least the following technical effects or advantages:

1. the utility model discloses in, compare with current step type tractor, this application makes the automobile body use as ground power supply through increasing at its inside and starting and directly, AC power supply system, when the aircraft starts needs ground power supply, cable direct connection to the feeder ear of aircraft, for the aircraft power supply, the distribution guarantee car can regard as the power supply source use of external equipment, greatly increased its application scope.

2. The utility model discloses in, through the camera and the light that set up, be convenient for to the real-time recording external condition, the illumination can be realized to the camera simultaneously for daily emergency lighting.

3. The utility model discloses in, through the snow pushing plate who sets up for snow removing on the runway.

4. The utility model discloses in, through the loudspeaker that sets up, under the big or comparatively noisy environment of noise when aircraft engine is taking a trial run, can shout when taking place unusually and remind.

Drawings

Fig. 1 is a schematic structural view of a ground traction starting comprehensive distribution train of an airplane helicopter in the application;

FIG. 2 is a schematic top view of the ground traction starting comprehensive distribution vehicle of the helicopter in the present application;

fig. 3 is a schematic view of the interior of the vehicle body of the airplane helicopter ground traction starting comprehensive distribution vehicle in the application.

In the figure: the snow sweeper comprises a vehicle body 1, a horn 2, a camera 3, a handle 4, an electromagnetic push rod 5, a rear wheel 6, a driving wheel 8, a front wheel 9, a snow removing plate 10, a connecting block 11, a cable 12, a traction assembly 13, an inverter 14, a storage battery 15, a panel 16, an alternating current socket 17, a direct current socket 18, a wiring terminal 20, a cover plate I22, a cover plate I23, a lighting lamp 24 and a cover plate II 24.

Detailed Description

In order to facilitate understanding of the present invention, the present invention will be described more fully hereinafter with reference to the accompanying drawings. The preferred embodiments of the present invention are shown in the drawings. The invention may, however, be embodied in many different forms and should not be construed as limited to the embodiments set forth herein. Rather, these embodiments are provided so that this disclosure will be thorough and complete.

It will be understood that when an element is referred to as being "secured to" another element, it can be directly on the other element or intervening elements may also be present. When an element is referred to as being "connected" to another element, it can be directly connected to the other element or intervening elements may also be present. The terms "vertical," "horizontal," "left," "right," and the like as used herein are for illustrative purposes only and do not represent the only embodiments.

Unless defined otherwise, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this invention belongs. The terminology used herein in the description of the invention is for the purpose of describing particular embodiments only and is not intended to be limiting of the invention. As used herein, the term "and/or" includes any and all combinations of one or more of the associated listed items.

Referring to fig. 1-3, the present invention provides a technical solution:

the ground traction starting comprehensive distribution vehicle for the airplane helicopter comprises a vehicle body 1, wherein driving wheels 8 are arranged on the front side and the rear side of the vehicle body 1, the driving wheels 8 are driven by a driving motor and used for guaranteeing the running of the vehicle, front wheels 9 and rear wheels 6 are arranged in the middle positions of the left side and the right side of the vehicle body 1 respectively and play a role in supporting, the vehicle body 1 is positioned on the same side surface of the rear wheels 6 and fixedly connected with a handle 4, and traction assemblies 13 are arranged on the top and the left end of the vehicle body 1 and used for traction of goods shelves in an airport;

a storage battery 15 is arranged in the vehicle body 1, a panel 16 is arranged in the vehicle body 1, and an alternating current socket 17, a direct current socket 18 and a binding post 20 are respectively arranged on the upper surface of the panel 16;

an inverter 14 is arranged in the handle 4;

the storage battery 15 is connected in parallel with the direct current socket 18, the binding post 20 and the inverter 14, the inverter 14 is connected in parallel with the alternating current socket 17, the binding post 20 is electrically connected with the cable 12, and the cable 12 penetrates through the vehicle body 1 to extend to the outside and is used for providing a ground power supply for starting the aircraft and providing a required power supply for ground electrification inspection of the aircraft.

In this scenario, as shown in fig. 1: the cable 12 is wound around the outer surface of the vehicle body 1.

In this solution, as shown in fig. 1 and 2: equal fixed mounting in both ends has electromagnetism push rod 5 around automobile body 1 is close to the side of handle 4, and the top of electromagnetism push rod 5 can be dismantled respectively and be connected with camera 3 and light 23, and electric connection can be dismantled through interface and battery 15 to camera 3 and light 23.

So set up, through camera 3 and the light 23 that sets up, be convenient for to the real-time recording external conditions, camera 3 can realize the illumination simultaneously for daily emergency lighting.

In this solution, as shown in fig. 1 and 2: two cavities are formed in the upper surface of the handle 4, a first cover plate 22 is hinged to the outer portion of each cavity, one cavity is used for placing the inverter 14, and the other cavity is used for placing the camera 3, the illuminating lamp 23 and the image storage device.

So set up, when camera 3 and light 23 do not use, can put into the cavity, avoid losing, through the apron 22 that sets up, be convenient for to inverter 22's maintenance simultaneously.

In this solution, as shown in fig. 1 and 2: the upper surface of the vehicle body 1 is hinged with a second cover plate 24 at the position of the panel 16.

Due to the arrangement, the panel 16 is protected, when external equipment needs to supply power, only the second cover plate 24 needs to be opened, and the alternating current plug 17 or the direct current plug 18 is selected to be used, so that the power supply capacity of the traction cart is enriched.

In this solution, as shown in fig. 1 and 2: the left end fixedly connected with connecting block 11 of automobile body 1, automobile body 1 rotates through connecting block 1 and snowboard 10 to be connected for the snow removing.

In this scenario, as shown in fig. 1: still install sucking disc formula loudspeaker 2 on the preceding terminal surface of automobile body 1, loudspeaker 2 can dismantle with automobile body 1 through the sucking disc and be connected for under the big or comparatively noisy environment of noise when the engine is tried on, can shout when taking place to remind.

In summary, the following steps: the application mainly provides an aircraft helicopter ground pulls starts to synthesize distribution car, it is in the use, utilize battery 15 in the automobile body 1 as the main power supply, the realization is to automobile body 1 power supply, and through the cable 12 that sets up, make automobile body 1 use as ground power supply, when the aircraft starts needs ground power supply, cable 12 directly links to the feeder ear of aircraft, for the aircraft power supply, and utilize inverter 14 to become 220V with the voltage contravariant of battery 15 after be connected with AC socket 17, and through DC socket 18, realize the power supply to external equipment, at this moment, the distribution guarantee car can regard as external equipment's power supply to use, greatly increased its application scope.

Meanwhile, the camera 3 and the illuminating lamp 23 are arranged, so that the external conditions can be recorded in real time conveniently, and meanwhile, the camera 3 can realize illumination and is used for daily emergency illumination; through the snow board 10 that pushes away that sets up for snow removing on the runway, and through loudspeaker 2 that sets up, under the big or comparatively noisy environment of noise when aircraft engine is taking a trial run, can shout when taking place to remind.

It can be said that: since most of the power supply of the existing airplane is 28V, the most preferable power supply in the present application is that the storage battery 15 is a lithium ion battery using lithium iron phosphate as a positive electrode material and carbon as a negative electrode material, and the voltage is 28 ± 1.5V, and similarly, the inverter 14 is made by inverting 28V to 220V aerospace special inverter.

The above description is only a preferred embodiment of the present invention and is not intended to limit the present invention, and those skilled in the art can make various modifications and variations. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.

Claims

1. Aircraft helicopter ground traction starts synthesizes distribution car, including automobile body (1), both sides all are provided with drive wheel (8) around automobile body (1), drive wheel (8) are through driving motor drive, the left and right sides intermediate position department of automobile body (1) is provided with front wheel (9) and rear wheel (6) respectively, automobile body (1) be located rear wheel (6) with on the side with handle (4) fixed connection, the top and the left end of automobile body (1) all are provided with and pull subassembly (13), its characterized in that:

a storage battery (15) is arranged in the vehicle body (1), a panel (16) is arranged in the vehicle body (1), and an alternating current socket (17), a direct current socket (18) and a binding post (20) are respectively arranged on the upper surface of the panel (16);

an inverter (14) is arranged in the handle (4);

the storage battery (15) is connected with the direct-current socket (18), the binding post (20) and the inverter (14) in parallel, the inverter (14) is connected with the alternating-current socket (17) in parallel, the binding post (20) is electrically connected with the cable (12), and the cable (12) penetrates through the automobile body (1) to extend to the outside and be used for providing a ground power supply for starting an airplane and providing a required power supply for ground power-on inspection of the airplane.

2. An aircraft helicopter ground traction start-up integrated distribution train as defined in claim 1, wherein: the cable (12) is wound on the outer surface of the vehicle body (1).

3. An aircraft helicopter ground traction start-up integrated distribution train as defined in claim 1, wherein: the automobile body (1) is close to the equal fixed mounting in both ends around the side of handle (4) has electromagnetism push rod (5), the top of electromagnetism push rod (5) can be dismantled respectively and be connected with camera (3) and light (23), electric connection can be dismantled through interface and battery (15) in camera (3) and light (23).

4. An aircraft helicopter ground traction start-up integrated distribution train as defined in claim 1, wherein: two cavities are formed in the upper surface of the handle (4), a first cover plate (22) is hinged to the outer portion of each cavity, one cavity is used for placing the inverter (14), and the other cavity is used for placing the camera (3), the illuminating lamp (23) and the image storage.

5. An aircraft helicopter ground traction start-up integrated distribution train as defined in claim 1, wherein: the upper surface of the car body (1) is hinged with a second cover plate (24) at the position of the panel (16).

6. An aircraft helicopter ground traction start-up integrated distribution train as defined in claim 1, wherein: the left end fixedly connected with connecting block (11) of automobile body (1), automobile body (1) is connected with snowboard (10) rotation through connecting block (11).

7. An aircraft helicopter ground traction start-up integrated distribution train as defined in claim 1, wherein: still install sucking disc formula loudspeaker (2) on the preceding terminal surface of automobile body (1), loudspeaker (2) can be dismantled with automobile body (1) through the sucking disc and be connected.