CN219008131U

CN219008131U - Airplane transport vehicle

Info

Publication number: CN219008131U
Application number: CN202320170873.1U
Authority: CN
Inventors: 杨健; 刘达; 王子琦; 王荣华; 张伟建
Original assignee: LIAONING GENERAL AVIATION ACADEMY
Current assignee: LIAONING GENERAL AVIATION ACADEMY
Priority date: 2023-02-10
Filing date: 2023-02-10
Publication date: 2023-05-12
Anticipated expiration: 2033-02-10

Abstract

The utility model discloses an aircraft carrier vehicle, comprising: automobile body, tractor, jack, leading wheel, hand capstan winch, shaft, landing leg, deflector, fender and aircraft tire fixation clamp, the both sides at automobile body rear portion correspond and are provided with the guide channel, tractor, leading wheel, shaft, landing leg, deflector all are connected with the automobile body and set gradually from front to back, and the leading wheel can realize going up and down through the jack, and hand capstan winch is fixed in the front portion of automobile body top, and the fender is two, corresponds to set up in the top of wheel, and aircraft tire fixation clamp is two, and the one-to-one is installed in the rear of fender. The aircraft carrier vehicle is reasonable in structure and convenient to use, and can realize convenient loading, unloading, fixing and transferring of a small aircraft.

Description

Airplane transport vehicle

Technical Field

The utility model provides an aircraft carrier vehicle, and belongs to a transfer device equipped in an aircraft ground off-site transfer process.

Background

With the tremendous development of the aviation industry in China, the position of aircraft in the industry is gradually increased. The consumption level of people in the aviation industry is also significantly increased. All areas have begun to build general airports, which are convenient for organizing airplane entertainment flight, teaching flight, and developing station activities, etc. The current country is gradually opened aiming at aviation policies, the production capacity of light sport aircrafts is obviously increased, and the pilot training quantity is favorable for promoting personal entertainment flight. However, the current domestic low-altitude airspace is not completely released, and when enterprises or individuals want to fly at different airports, the small airplanes are more in transition due to the fact that the application of the airlines is difficult and are influenced by external factors, and the small airplanes are more in transition by means of ground vehicles.

At present, the aircraft is transported through a large transport vehicle, and the transport process of the transport vehicle involves numerous work, is high in transport cost, is high in overall height, and can not even be in the same row at a height-limiting position. In addition, when the large-scale freight transportation vehicle is used, the loading, fixing, unbinding and unloading processes of the airplane are complex and time-consuming due to the fact that the height of the vehicle body is high, and the whole process is time-consuming and labor-consuming due to the fact that a crane, a forklift and the like are needed to be matched.

Therefore, the provision of a novel ground transfer vehicle for an aircraft is a problem to be solved.

Disclosure of Invention

In view of the above, the present utility model aims to provide an aircraft carrier vehicle, so as to solve the problems of time and effort consumption in loading, unloading, fixing and transferring an aircraft of the existing transfer vehicle.

The technical scheme provided by the utility model is as follows: an aircraft carrier comprising: the automobile body includes automobile body frame and cooperation are fixed in the automobile body floor of automobile body frame top, the both sides at automobile body rear portion correspond and are provided with the guide channel, the tractor be fixed in the front end of automobile body, the jack vertically set up in the rear end of tractor, the lateral part of jack with automobile body fixed connection, the bottom with the leading wheel is connected, hand winch is fixed in the front portion of automobile body top, the shaft is fixed in the below at automobile body middle part, including bear axle and symmetrical connection in bear the wheel of axle both sides, the landing leg be two, symmetrical install in the below at automobile body rear portion and angularly adjustable, the deflector be two, rotate connect in the rear end of automobile body and with the guide channel one-to-one sets up, the fender be two, correspond set up in the top of wheel, the wheel is fixed for two, the corresponding fender of installation behind the aircraft.

Preferably, the landing leg comprises a landing leg body and a welding rotating plate, wherein the welding rotating plate is fixedly connected with the bottom of the vehicle body, a middle mounting hole and a plurality of circumferential mounting holes which are arranged at intervals around the middle mounting hole are formed in the welding rotating plate, two mounting holes are formed in the upper portion of the landing leg body at intervals and correspond to the middle mounting hole and the circumferential mounting hole respectively, and the landing leg body is fixedly connected with the welding rotating plate through two pin shafts at different angles.

Further preferably, a clamp is further provided at the rear of the vehicle body for fixing the folded guide plate to the bottom of the vehicle body.

Further preferably, the aircraft tire fixing clamp is arc-shaped, and both ends of the aircraft tire fixing clamp are detachably connected with the vehicle body.

Further preferably, one end of the aircraft tire fixing clip is connected with the rear side of the fender through a buckle, the other end of the aircraft tire fixing clip is provided with an insert, the end of the insert is provided with a through hole, and the end passes through the vehicle body floor and is connected with a connecting piece arranged below the vehicle body frame through a pin.

Further preferably, the buckle is a buckle with adjustable length.

Further preferably, auxiliary handles are provided at intervals on the outer side of the vehicle body frame.

The airplane transport vehicle provided by the utility model has the advantages that the structure is reasonable, the use is convenient, the convenient loading, unloading, fixing and transferring of a small airplane can be realized, the problem of road surface trafficability can be solved, and the convenient transferring can be realized when the airplane transport vehicle is mounted on a household automobile.

Drawings

The utility model will be described in further detail with reference to the accompanying drawings and embodiments:

FIG. 1 is a perspective view of an aircraft carrier provided by the present utility model;

FIG. 2 is a side view of an aircraft carrier provided by the present utility model;

FIG. 3 is a schematic view of the installation of a tire mounting clip.

Detailed Description

The utility model will be further explained below in connection with specific embodiments, but is not limited to the utility model.

As shown in fig. 1 to 3, the present utility model provides an aircraft carrier comprising: automobile body 1, tractor 2, jack 3, leading wheel 4, hand winch 5, shaft, landing leg 7, deflector 8, fender 9 and aircraft tire fixation clamp 10, automobile body 1 includes automobile body frame 11 and cooperation are fixed in automobile body floor 12 of automobile body frame 11 top, the both sides correspondence at automobile body 1 rear portion is provided with guide channel 13 for leading the direction of motion of aircraft, tractor 2 is fixed in the front end of automobile body 1 for with tractor quick connect, jack 3 vertical set up in the rear end of tractor 2, the lateral part of jack 3 with automobile body 1 fixed connection, the bottom with deflector 4 is connected, can realize the regulation to the height that the leading wheel is located, hand winch 5 is fixed in the front portion of automobile body 1 top for make the aircraft along this aircraft carrier vehicle in the guide channel through the hand winch be connected with aircraft bearing structure, the shaft is fixed in the below at automobile body 1 middle part, including bearing axle and symmetry be connected in automobile body 6, preferably set up in two pairs of wheels 9, the side of wheels are installed in the side of being symmetrical, the aircraft wheel is fixed to the deflector 1, the side of being installed in two, the side of being 9, the aircraft tire is fixed in the side of being installed to the aircraft tire is fixed to the side of the wheel is fixed to the wheel 1.

The aircraft carrier is simple in structure, convenient to move, low in overall height and high in road height limiting position trafficability, the guide plates are opened by adjusting the height of the jack and the inclination of the supporting legs, the guide wheels, the supporting legs and the free ends of the guide plates are all grounded, the aircraft body is in an inclined state, at the moment, the aircraft tires are aligned to the guide plates, a steel cable of the hand winch is connected with a bearing structure (such as a main landing gear plate spring) of the aircraft, preferably, the Y-shaped connection is realized, the aircraft can be loaded onto the aircraft body by winding the steel cable of the hand winch, the height of the jack is adjusted after the aircraft gets on the aircraft, the supporting legs are put down, the aircraft body is flatly placed, the aircraft is fixed by the tire fixing clips of the aircraft, the aircraft can be fixed in the reverse order operation in the unloading process, the whole process can be transported by connecting the tractor with the tractor, and the folding guide wheels, the fork truck and the guide plates, and the whole process can be transported without a crane, labor force and a lot.

The landing leg structure in the prior art can be adopted, the angle of the landing leg can be adjusted, the landing leg 7 comprises a landing leg body and a welding rotating plate, the welding rotating plate is fixedly connected with the bottom of the vehicle body 1, a middle mounting hole and a plurality of circumferential mounting holes which are arranged around the middle mounting hole at intervals are formed in the welding rotating plate, two mounting holes are formed in the upper portion of the landing leg body at intervals, the two mounting holes correspond to the middle mounting hole and the circumferential mounting hole respectively, and the landing leg body is fixedly connected with the welding rotating plate through two pin shafts to achieve different angles.

As an improvement of the solution, the rear part of the vehicle body 1 is further provided with a clamp (not shown in the figure) for fixing the folded guide plate 8 to the bottom of the vehicle body 1.

As an improvement of the technical scheme, the aircraft tire fixing clamp 10 is arc-shaped, and both ends of the aircraft tire fixing clamp are detachably connected with the vehicle body 1.

As shown in fig. 3, one end of the aircraft tire fixing clip 10 is connected to the rear side of the fender 9 by a buckle 101, the other end is provided with an insert 102, the end of the insert 102 is provided with a through hole, and the end is connected to a connector mounted below the vehicle body frame 11 by a pin 103 after passing through the vehicle body floor 12.

As an improvement of the technical solution, the buckle 101 is a buckle with adjustable length, and may be a buckle in the prior art, for example: the length is adjustable by a threaded connecting rod.

As an improvement of the technical scheme, the outer side of the car body frame 11 is provided with auxiliary handles 111 at intervals, which are used for increasing stress points when people move the car, and can also be used for increasing fixed hanging points of ropes and the like when other objects are transported.

The embodiments of the utility model have been written in an incremental manner with emphasis on the differences between the various embodiments being placed upon which similar parts may be seen.

The embodiments of the present utility model have been described in detail with reference to the drawings, but the present utility model is not limited to the above embodiments, and various changes can be made within the knowledge of those skilled in the art without departing from the spirit of the present utility model.

Claims

1. An aircraft carrier vehicle, comprising: the automobile body (1), tractor (2), jack (3), leading wheel (4), hand winch (5), shaft, landing leg (7), deflector (8), fender (9) and aircraft tire fixation clamp (10), automobile body (1) include automobile body frame (11) and cooperate be fixed in automobile body floor (12) above automobile body frame (11), the both sides at automobile body (1) rear portion correspond and are provided with guide channel (13), tractor (2) are fixed in the front end of automobile body (1), jack (3) vertical set up in the rear end of tractor (2), the lateral part of jack (3) with automobile body (1) fixed connection, the bottom with deflector (4) are connected, winch (5) are fixed in the front portion of automobile body (1) top, be fixed in the below at automobile body (1) middle part, including bearing shaft and symmetrical connection in wheel (6) of bearing shaft both sides, landing leg (7) are in two symmetrical installation in automobile body (1) are in two the rear end of being adjusted and being connected with deflector (9) one by one respectively the guide channel, the two aircraft tire fixing clips (10) are correspondingly arranged above the wheels (6), and are correspondingly arranged behind the mud guard (9) one by one.

2. An aircraft carrier according to claim 1, wherein: the landing leg (7) comprises a landing leg body and a welding rotating plate, wherein the welding rotating plate is fixedly connected with the bottom of the vehicle body (1), a middle mounting hole and a plurality of circumferential mounting holes which surround the middle mounting hole are formed in the welding rotating plate at intervals, two mounting holes are formed in the upper portion of the landing leg body at intervals and correspond to the middle mounting hole and the circumferential mounting hole respectively, and the landing leg body is fixedly connected with the welding rotating plate at different angles through two pin shafts.

3. An aircraft carrier according to claim 1, wherein: the rear part of the vehicle body (1) is also provided with a clamp for fixing the folded guide plate (8) at the bottom of the vehicle body (1).

4. An aircraft carrier according to claim 1, wherein: the aircraft tire fixing clamp (10) is arc-shaped, and two ends of the aircraft tire fixing clamp are detachably connected with the vehicle body (1).

5. The aircraft carrier according to claim 4, wherein: one end of the aircraft tire fixing clamp (10) is connected with the rear side of the mudguard (9) through a buckle (101), the other end of the aircraft tire fixing clamp is provided with an insert (102), the end part of the insert (102) is provided with a through hole, and the end part passes through the vehicle body floor (12) and is connected with a connecting piece arranged below the vehicle body frame (11) through a pin (103).

6. The aircraft carrier as recited in claim 5 wherein: the hasp (101) is a hasp with adjustable length.

7. An aircraft carrier according to claim 1, wherein: auxiliary handles (111) are arranged at intervals on the outer side of the vehicle body frame (11).