CN115871948B - Motor aircraft runway - Google Patents
Motor aircraft runway Download PDFInfo
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- CN115871948B CN115871948B CN202310126051.8A CN202310126051A CN115871948B CN 115871948 B CN115871948 B CN 115871948B CN 202310126051 A CN202310126051 A CN 202310126051A CN 115871948 B CN115871948 B CN 115871948B
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Abstract
The invention relates to the technical field of airports, and provides a motor runway, which comprises an airplane runway, wherein the airplane runway comprises a plurality of motor runway units, and a plurality of motor runway unit arrays are arranged; the reverse wind field manufacturing vehicles are arranged at one end of the runway and used for providing wind fields required by taking off and landing of the aircraft to assist the taking off and landing of the aircraft; the motor runway unit comprises: the top of the vehicle body is a plane; a plurality of wheels rotatably arranged at the bottom of the vehicle body; and the power device is arranged at the bottom of the vehicle body and used for driving the wheels to rotate. Through above-mentioned technical scheme, solved the fixed airport mobility in the prior art poor and the long problem of aircraft take off and land distance.
Description
Technical Field
The invention relates to the technical field of airports, in particular to an aircraft runway.
Background
The airport is used as a fixed building, although the airport is heavily protected in war, the airport is used as a primary target to be attacked, the risk of being destroyed or destroyed cannot be avoided, and if the airport is destroyed, a method for ensuring the normal landing of a fighter aircraft is still available, so that the fighter is very important; the development of temporary airport reserves is therefore particularly critical in the field of spares.
The runway has long length, high bearing capacity and levelness, the conventional ground can not meet the requirements, and the common 1A-level runway is 800 meters long; if the arresting cable and the catapult are arranged on the aircraft carrier runway for auxiliary take-off and landing, the runway length can be shortened, but the structure of the carrier-borne aircraft of the aircraft carrier is reinforced through special design, and can bear strong impact load during catapult take-off and landing, the arresting cable or the catapult is applied to the land-based aircraft, and the aircraft body is damaged or even broken by strong impact force on the premise of not reinforcing the aircraft structure.
Disclosure of Invention
The invention provides a motor aircraft runway, which solves the problems of poor mobility of a fixed airport and long take-off and landing distance of an aircraft in the related technology.
The technical scheme of the invention is as follows:
a motor aircraft runway comprising:
an aircraft runway comprising a plurality of motor runway elements, a plurality of motor runway element arrays arranged;
the reverse wind field manufacturing vehicles are provided with a plurality of wind fields which are arranged at one end of the runway, and are used for providing the requirements of taking off and landing of the aircraft;
the motor runway unit comprises:
the top of the vehicle body is a plane;
the wheels are provided with a plurality of wheels which are rotatably arranged at the bottom of the vehicle body;
the power device is arranged at the bottom of the vehicle body and is used for driving the wheels to rotate.
As a further technical solution, the vehicle body has a butt-joint cylinder, and further includes:
the tractor is provided with a pulling disc, the butt joint cylinder is clamped with the pulling disc, and the tractor is used for driving the car body to move.
As a further technical solution, the vehicle body includes:
the butt-joint cylinder is arranged at one end of the first vehicle plate, and the power device is arranged at the bottom of the first vehicle plate;
the second sweep rotates and sets up first sweep is kept away from the one end of butt joint cylinder, the wheel sets up the second sweep with first sweep bottom, the second sweep rotate the back with first sweep butt, perhaps on the second sweep wheel and ground butt.
As a further technical solution, the wheel includes:
the steering device is arranged at the bottoms of the first sweep and the second sweep;
the wheel is arranged on the steering device, and the steering device is used for adjusting the angle of the wheel.
As a further technical solution, the steering device includes:
the rotating piece is arranged at the bottoms of the first sweep and the second sweep;
the telescopic piece is arranged at the bottom of the rotating piece, the wheels are arranged on the telescopic piece, and the power device is used for driving the rotating piece and the telescopic piece to act.
As a further technical solution, the vehicle body further includes:
the landing leg is provided with a plurality of landing legs and is arranged at the bottoms of the first sweep and the second sweep, and the landing leg is used for bearing the impact force of an airplane during taking off and landing.
As a further technical scheme, the method further comprises:
the flow guiding device is rotatably arranged on the motor runway unit at one end far away from the reverse wind field manufacturing vehicle, and the flow guiding device is used for guiding tail airflow when the aircraft takes off and lands after rotating.
As a further technical solution, the reverse wind farm manufacturing vehicle includes:
the transport vehicle is arranged at one end of the runway;
the openable warehouse is arranged on the transport vehicle;
the wind field manufacturing device is arranged in the openable warehouse.
As a further aspect, the wind field manufacturing apparatus includes:
the rotary table is rotatably arranged in the openable warehouse;
the lifting frame is hinged on the rotary table;
the pitching adjusting device is rotatably arranged on the lifting frame;
the turbofan engine is arranged on the pitching adjusting device.
The working principle and the beneficial effects of the invention are as follows:
in the invention, the motor runway units and the reverse wind field manufacturing vehicles are gathered on a temporary site, a plurality of motor runway units are spliced together under the drive of the power device to form the aircraft runway, the reverse wind field manufacturing vehicles determine working positions, the wind power and the wind direction of each reverse wind field manufacturing vehicle are adjusted, then the aircraft can take off and land on the aircraft runway under the assistance of the reverse wind field manufacturing vehicles, and the ground speed of the aircraft is reduced to the minimum when the aircraft takes off and land by the reverse wind field manufacturing vehicles, so that the take-off and landing distance of the aircraft is greatly reduced. Before taking off, an airplane can be transported to a temporary place by a certain motor runway unit to be in butt joint with the airplane runway for taking off, the fallen airplane moves to the certain motor runway unit, the connection between the motor runway unit and the whole airplane runway is released, the airplane is taken off the runway by the motor runway unit, the subsequent taking off and landing are carried out for the place to be opened, and the problems of poor mobility of a fixed airport and long taking off and landing distance of the airplane in the related art are solved.
Drawings
The invention will be described in further detail with reference to the drawings and the detailed description.
FIG. 1 is a schematic diagram of the structure of the present invention;
FIG. 2 is a schematic view of the motor runway unit structure of the present invention;
FIG. 3 is a schematic view of the motor track unit of the present invention when towed by a tractor;
FIG. 4 is an enlarged view of portion A of FIG. 3 in accordance with the present invention;
FIG. 5 is a schematic view of a reverse wind farm manufacturing vehicle according to the present invention;
FIG. 6 is a schematic view of the structure of the tractor and trailer in accordance with the present invention;
in the figure: 1. runway, 2, motor runway units, 3, reverse wind field manufacturing vehicles, 4, vehicle bodies, 5, wheels, 6, power devices, 7, tractors, 8, towing discs, 9, docking cylinders, 10, first vehicle plates, 11, second vehicle plates, 12, steering devices, 13, wheels, 14, rotating parts, 15, telescopic parts, 16, supporting legs, 17, transport vehicles, 18, openable warehouses, 19, wind field manufacturing devices, 20, a rotary table, 21, lifting frames, 22, pitching adjusting devices, 23, turbofan engines, 24 and flow guiding devices.
Detailed Description
The technical solutions of the embodiments of the present invention will be clearly and completely described below in conjunction with the embodiments of the present invention, and it is apparent that the described embodiments are only some embodiments of the present invention, not all embodiments. All other embodiments, which can be made by one of ordinary skill in the art based on the embodiments of the invention without making any inventive effort, are intended to be within the scope of the invention.
As shown in fig. 1 to 6, an aircraft runway includes:
an aircraft runway 1 comprising a plurality of motor runway elements 2, a plurality of said motor runway elements 2 being arranged in an array;
the reverse wind field manufacturing vehicles 3 are arranged at one end of the runway 1, and the reverse wind field manufacturing vehicles 3 are used for providing wind fields required by taking off and landing of the aircraft;
the motor runway unit 2 comprises:
the vehicle body 4, the top of the vehicle body 4 is a plane;
the power device 6 is arranged at the bottom of the vehicle body 4, and the power device 6 is used for driving the wheels 5 to rotate.
In this embodiment, when the fixed airport is destroyed or the aircraft needs to be lifted on the temporary site, the motor runway units 2 and the reverse wind field manufacturing vehicles 3 are gathered on the temporary site, and the motor runway units 2 are mutually butted to form the aircraft runway 1, so that the rapid assembly and transfer of the aircraft runway 1 are realized, the problem of poor maneuverability of the fixed airport in the related art is solved, the reverse wind field manufacturing vehicles 3 determine the working positions, adjust the wind direction and the wind force of the reverse wind field generated by each reverse wind field manufacturing vehicle 3, assist the aircraft to land on the aircraft runway 1, take off by the pressure difference generated by the difference of the air flow rates at the upper side and the lower side of the wing of the aircraft, further provide lift force, so that the counter wind take off is easier, the reverse wind field can also provide resistance when the aircraft lands, so that the counter wind landing is easier, the reverse wind field manufacturing vehicle 3 generates a reverse wind field to assist the taking-off and landing of the aircraft, solves the problem of long taking-off and landing distance of the aircraft in the related art, the falling aircraft moves to a certain motor runway unit 2, the motor runway unit 2 brings the aircraft off the runway at the moment, the aircraft takes off and lands for the subsequent taking-off and landing, the aircraft ready to take off is transported to the rear of the aircraft runway 1 by the certain motor runway unit 2 when taking off, the aircraft is in butt joint with the aircraft runway 1, the reverse wind field manufacturing vehicle 3 is started at the same time, after the wind speed reaches the taking-off speed, the aircraft can take off after falling and before taking off, the aircraft can be carried by the motor runway unit 2 for movement, the problems of the aircraft sliding, dragging and the like do not need to be considered, the taxiway to assist the aircraft to be in place, and the maintenance, oiling, deicing and the like of the aircraft can be completed on the motor runway unit 2 without the aircraft moving to a station by oneself.
Further, the vehicle body 4 has a docking cylinder 9, and further includes:
the tractor 7 is arranged at the front end of the car body 4, the tractor 7 is provided with a pulling tray 8, the butt-joint cylinder 9 is clamped with the pulling tray 8, and the tractor 7 is used for driving the car body 4 to move.
In this embodiment, after the hanging disc 8 on the tractor 7 is abutted against the abutting cylinder 9 on the vehicle body 4, the tractor 7 drives the vehicle body 4 to transport, the tractor 7 can drive the motor track units 2 to transport at high speed on a highway, after reaching a temporary place, the hanging disc 8 is separated from the abutting cylinder 9, the tractor 7 stands by after leaving the place, a plurality of motor track units 2 are driven by the power device 6 to automatically abut against to form the runway 1, after taking off and landing are finished, the motor track units 2 are separated from each other, the tractor 7 enters the ground again, and after the hanging disc 8 and the abutting cylinder 9 are abutted, the tractor 7 can drive the motor track units 2 again to transport on the highway.
Further, the vehicle body 4 includes:
the first vehicle plate 10, the said butt joint cylinder 9 is set up in one end of said first vehicle plate 10, the said power plant 6 is set up in the bottom of said first vehicle plate 10;
the second plate 11 is rotatably arranged at one end of the first plate 10 away from the butt-joint cylinder 9, the wheels 5 are arranged at the bottoms of the second plate 11 and the first plate 10, and the second plate 11 is abutted with the first plate 10 after being rotated, or the wheels on the second plate 11 are abutted with the ground.
In this embodiment, after the take-off and landing of the aircraft are completed, the second vehicle plate 11 is turned over to the upper side of the first vehicle plate 10, so that the length of the motor track unit 2 is reduced by nearly half, and the motor track unit is more beneficial to road transportation, at this time, the hanging plate 8 on the tractor 7 is in butt joint with the butt joint cylinder 9 on the first vehicle plate 10, so that the motor track unit 2 can be driven by the tractor 7 to carry out road transportation, after the motor track unit 2 arrives at a temporary place through road transportation, the hanging plate 8 on the tractor 7 is separated from the butt joint cylinder 9 on the first vehicle plate 10, the tractor 7 is ready to drive away from the place, and the second vehicle plate 11 above the first vehicle plate 10 is turned and unfolded, so that the length of the motor track unit 2 is increased by nearly half, and the take-off and landing of the aircraft are easier.
Further, the wheel 5 includes:
steering means 12 provided at the bottoms of the first and second deck 10 and 11;
a wheel 13 arranged on the steering device 12, the steering device 12 being used for adjusting the angle of the wheel 5.
In this embodiment, after the motor track unit 2 arrives at the temporary location and the tractor 7 leaves the temporary location and stands by, the second vehicle plate 11 turns over and spreads, and the turning device 12 below the first vehicle plate 10 and the second vehicle plate 11 can adjust the direction of the wheels 13 as required, so as to realize the actions of traversing, tilting, in-situ turning, etc. of the whole motor track unit 2, thereby improving the flexibility of the whole motor track unit 2 and facilitating the precise docking of each motor track unit 2.
Further, the steering device 12 includes:
a rotating member 14 provided at the bottoms of the first and second deck plates 10 and 11;
the telescopic piece 15 is arranged at the bottom of the rotating piece 14, the wheels 13 are arranged on the telescopic piece 15, and the power device 6 is used for driving the rotating piece 14 and the telescopic piece 15 to act.
In this embodiment, after the whole runway 1 is completed by butt-jointing a plurality of whole runway units 2, the whole runway is detected by optical ruler feedback, information is fed back, and the power device 6 drives each telescopic piece 15 under the rotary piece 14 to be independently extended or shortened to realize self-adaptive leveling, so that the flatness of the whole runway 1 is improved.
Further, the vehicle body 4 further includes:
the number of the supporting legs 16 is several, and the supporting legs 16 are arranged under the first sweep 10 and the second sweep 11, and the supporting legs 16 are used for bearing the impact force when the aircraft takes off and lands.
In this embodiment, the aircraft can generate a huge impact force on the runway 1 both during take-off and landing, and the first and second plates 10 and 11 have a plurality of legs 16 below them to bear the impact force during take-off and landing of the aircraft, so as to stabilize the structure of the runway 1.
Further, the method further comprises the following steps:
and the flow guiding device 24 is rotatably arranged on the motor runway unit 2 at the end far away from the reverse wind field manufacturing vehicle 3, and the flow guiding device 24 is used for guiding tail airflow when the aircraft takes off and lands after rotating.
In this embodiment, the deflector 24 on the motor runway unit 2 in the tail direction of the aircraft rotates during the taking-off and landing process, and the optimal angle is adjusted to guide the airflow at the tail of the aircraft, so as to further achieve the purpose of assisting the taking-off and landing of the aircraft, and further shorten the length of the runway 1.
Further, the reverse wind farm manufacturing vehicle 3 includes:
a transport vehicle 17 disposed at one end of the runway 1;
an openable bin 18 provided on the transport vehicle 17;
a wind field manufacturing device 19 is arranged in the openable warehouse 18.
In this embodiment, after the take-off and landing of the aircraft are completed, the warehouse 18 can be opened to close the shielding wind field manufacturing device 19, so that confidentiality is good when the transport vehicle 17 carries out road transport, and when the reverse wind field manufacturing vehicle 3 needs to work, the warehouse 18 can be opened, and the internal wind field manufacturing device 19 can work normally to assist the aircraft to take-off.
Further, the wind field manufacturing apparatus 19 includes:
a turret 20 rotatably disposed within the openable bin 18;
a lifting frame 21 hinged on the rotary table 20;
a pitch-up and pitch-down adjusting device 22 rotatably provided on the lifting frame 21;
a turbofan engine 23 is provided on the pitch adjustment device 22.
In this embodiment, after the reverse wind field manufacturing vehicle 3 reaches the designated position, the openable warehouse 18 is opened, the lifting frame 21 rotates to be perpendicular to the openable warehouse 18, then the direction of the turbofan engine 23 is adjusted through the rotary table 20 according to the requirement, the height of the turbofan engine 23 is adjusted through the lifting of the lifting frame 21, the turbofan engine 23 is unfolded through the rotation of the pitching adjusting device 22, the pitching angle of the turbofan engine 23 is adjusted, the turbofan engine 23 is started after the turbofan engine 23 is adjusted to the proper direction, the height and the pitching angle, after the wind power is proper, the take-off and landing of the aircraft are started, after the take-off and landing of the aircraft are completed, the rotation of the pitching adjusting device 22 returns to the turbofan engine 23, the lifting frame 21 is lowered to the lowest, the rotary table 20 rotates to return to the initial position, the lifting frame 21 rotates to be parallel to the openable warehouse 18, then the openable warehouse 18 is closed, and the volume of the whole reverse wind field manufacturing vehicle 3 is greatly reduced, and the highway transportation is more beneficial.
The foregoing description of the preferred embodiments of the invention is not intended to be limiting, but rather is intended to cover all modifications, equivalents, alternatives, and improvements that fall within the spirit and scope of the invention.
Claims (4)
1. A motor aircraft runway, comprising:
an aircraft runway (1) comprising a plurality of motor runway units (2), a plurality of motor runway units (2) being arranged in an array;
the reverse wind field manufacturing vehicles (3) are arranged at one end of the runway (1), and the reverse wind field manufacturing vehicles (3) are used for providing wind fields required by taking off and landing of the aircraft;
the motor runway unit (2) comprises:
the vehicle body (4), the top of the vehicle body (4) is a plane, and the vehicle body (4) is provided with a butt joint cylinder (9);
the wheels (5) are provided with a plurality of wheels and are rotatably arranged at the bottom of the vehicle body (4);
the power device (6) is arranged at the bottom of the vehicle body (4), and the power device (6) is used for driving the wheels (5) to rotate;
the tractor (7) is provided with a pulling disc (8), the butt-joint cylinder (9) is clamped with the pulling disc (8), and the tractor (7) is used for driving the vehicle body (4) to move;
the vehicle body (4) includes:
the butt-joint cylinder (9) is arranged at one end of the first sweep (10), and the power device (6) is arranged at the bottom of the first sweep (10);
the second vehicle plate (11) is rotatably arranged at one end, far away from the butt joint cylinder (9), of the first vehicle plate (10), the wheels (5) are arranged at the bottoms of the second vehicle plate (11) and the first vehicle plate (10), and the second vehicle plate (11) is abutted with the first vehicle plate (10) after being rotated, or the wheels (5) on the second vehicle plate (11) are abutted with the ground;
the support legs (16) are arranged at the bottoms of the first vehicle plate (10) and the second vehicle plate (11), and the support legs (16) are used for bearing the impact force of an aircraft during taking off and landing;
the wheel (5) comprises:
steering means (12) provided at the bottoms of the first and second vehicle panels (10, 11);
-wheels (13) arranged on said steering means (12), said steering means (12) being adapted to adjust the angle of said wheels (5);
the steering device (12) comprises:
a rotating member (14) provided at the bottoms of the first vehicle plate (10) and the second vehicle plate (11);
the telescopic piece (15) is arranged at the bottom of the rotating piece (14), the wheels (13) are arranged on the telescopic piece (15), and the power device (6) is used for driving the rotating piece (14) and the telescopic piece (15) to act.
2. A motor aircraft runway according to claim 1 further comprising:
and the flow guiding device (24) is rotatably arranged on the motor runway unit (2) at one end far away from the reverse wind field manufacturing vehicle (3), and the flow guiding device (24) is used for guiding tail airflow when the aircraft takes off and lands after rotating.
3. A motor aircraft runway according to claim 2, characterized in that the reverse wind farm manufacturing vehicle (3) comprises:
the transport vehicle (17) is arranged at one end of the runway (1);
an openable bin (18) arranged on the transport vehicle (17);
a wind field manufacturing device (19) arranged in the openable warehouse (18).
4. A motor aircraft runway according to claim 3, characterized in that the wind park manufacturing device (19) comprises:
the rotary table (20) is rotatably arranged in the openable warehouse (18);
the lifting frame (21) is hinged on the rotary table (20);
a pitching adjusting device (22) rotatably arranged on the lifting frame (21);
-a turbofan engine (23) arranged on said pitch-and-yaw adjustment device (22).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202310126051.8A CN115871948B (en) | 2023-02-17 | 2023-02-17 | Motor aircraft runway |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202310126051.8A CN115871948B (en) | 2023-02-17 | 2023-02-17 | Motor aircraft runway |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN115871948A CN115871948A (en) | 2023-03-31 |
| CN115871948B true CN115871948B (en) | 2023-06-06 |
Family
ID=85761254
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202310126051.8A Active CN115871948B (en) | 2023-02-17 | 2023-02-17 | Motor aircraft runway |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN115871948B (en) |
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| US4462560A (en) * | 1982-01-26 | 1984-07-31 | The United States Of America As Represented By The Secretary Of The Air Force | Airplane take-off system |
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Also Published As
| Publication number | Publication date |
|---|---|
| CN115871948A (en) | 2023-03-31 |
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