WO2010064326A1 - Automobile volante - Google Patents

Automobile volante Download PDF

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Publication number
WO2010064326A1
WO2010064326A1 PCT/JP2008/072227 JP2008072227W WO2010064326A1 WO 2010064326 A1 WO2010064326 A1 WO 2010064326A1 JP 2008072227 W JP2008072227 W JP 2008072227W WO 2010064326 A1 WO2010064326 A1 WO 2010064326A1
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WO
WIPO (PCT)
Prior art keywords
wing
flight
wings
automobile
unit
Prior art date
Application number
PCT/JP2008/072227
Other languages
English (en)
Japanese (ja)
Inventor
剛明 金森
Original Assignee
Kanamori Takaaki
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Kanamori Takaaki filed Critical Kanamori Takaaki
Priority to JP2009545747A priority Critical patent/JPWO2010064326A1/ja
Priority to PCT/JP2008/072227 priority patent/WO2010064326A1/fr
Publication of WO2010064326A1 publication Critical patent/WO2010064326A1/fr

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60F—VEHICLES FOR USE BOTH ON RAIL AND ON ROAD; AMPHIBIOUS OR LIKE VEHICLES; CONVERTIBLE VEHICLES
    • B60F5/00—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media
    • B60F5/02—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media convertible into aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C37/00—Convertible aircraft

Definitions

  • the present invention relates to a vehicle capable of traveling and flying.
  • FIG. 2 is a front view of a conventional travelable and flightable automobile 10
  • FIG. 3 is a side view of the automobile 10 of FIG.
  • the main body 50 has a left steered wheel 52a and a left drive wheel 53a, and travels using these wheels.
  • the annular wing 58 is attached to the main body 50 and generates lift necessary for flight.
  • the propulsion unit 56 is a propeller and generates thrust necessary for flight.
  • the canard 54 enhances longitudinal stability in flight.
  • the ailerons 26 and the rudder 28 are used for attitude control during flight.
  • the annular wing 58 generates lift necessary for flight even if the wing span is short, the wing can be folded to travel on the road.
  • the car 10 with the conventional flight function has a large width and height of the car, and the air routes are air routes from the hub airport to the regional airports and routes connecting the regional airports, remote islands from the regional airports, and mountains It was necessary to go through regional airports, such as air routes connecting departments. If you fly directly from road to road, you will fly long distances despite the fact that they are very close, and it will take time.
  • the present inventor has created a car that enables traveling and flying that can be taken off from the road and landed on the road by reducing the width of the car and the height of the car by using a set of arranged wings.
  • the A set of arranged wings means that the width direction of the wings is the left and right direction of the car, and the wings are arranged in the plane consisting of the vertical direction of the car and the longitudinal direction of the car, and each wing generates almost the same lift.
  • a collection of wings that control the mounting angle of each wing so that it is at an angle of attack.
  • the mounting angle of each wing is different at the longitudinal position of the car, and is controlled so that the wing behind is at an angle of attack that generates lift for the air flow behind the trailing edge of the wing, so it is behind the car
  • the mounting angle gradually increases.
  • the space between the wing in the vertical direction and the wing may be, for example, approximately the same as the chord length, and the space between the wing and the wing in the front and rear direction may be considerably smaller than the chord length.
  • the mounting angle of the wing may be made horizontal.
  • One aspect of the present invention is a car.
  • This automobile is provided with a steering wheel for determining the traveling direction and a drive wheel for transmitting driving power, and the driving steering unit for moving the steering wheel and the power required for traveling are A drive unit for transmitting to the drive wheels, a collection of arranged wings for generating lift necessary for the flight of the vehicle, a rudder for controlling the attitude of the vehicle during flight, a flight steering unit for moving the rudder And a propulsion unit that generates a propulsion force necessary for flight.
  • the rudder which controls the attitude of the vehicle is a rudder for controlling the roll, pitch and yaw of the vehicle.
  • the vehicle may further include a lateral propulsion unit so that lateral force is exerted on the vehicle at takeoff and landing.
  • the attitude of the car is inclined in the wind blowing direction from the direction in which the road advances, but the lateral propulsion unit reduces the influence of the crosswind and brings the attitude of the car closer to the road traveling Can.
  • the influence of the crosswind can be reduced and takeoff is facilitated.
  • the future air route will travel on the ground from the current position of the car, go to the road where it can take off close to the current position, take off, fly the shortest route, land on the landable road near the target point, and reach the target point Drive on the ground.
  • the inventors of the present invention have made the present invention so that they can be taken off from the road and landed on the road by reducing the width of the car and the height of the car, and the purpose is to shorten traveling time and road congestion To reduce the required parking area, reduce energy consumption, etc., and to provide environmentally friendly vehicles.
  • FIG. 1 is a side view of a car showing an embodiment of the present invention.
  • FIG. 2 is a front view of a conventional travelable and flightable vehicle.
  • FIG. 3 is a side view of the vehicle of FIG. 4 is a side view of an example of a set of deployed wings viewed from the left of the vehicle of FIG. 1;
  • FIG. 5 is a front view of the vehicle of FIG. 6 is a top view of the vehicle of FIG. 7 is a rear view of the vehicle of FIG.
  • FIG. 8 is a functional block diagram of the vehicle of FIG.
  • Reference Signs List 100 automobile according to the present invention 104 traveling steering unit, 106 operation unit, 108 power source, 110 driving unit, 112 state detecting unit, 114 front wheel driving unit, 116 power control unit, rudder controlling 120 attitude, 122 flight steering 124 elevators, 126 auxiliary wings, 127 vertical stabilizers, 128 directional rudder, 130 travel and flight switching units, 150 bodies, 152a left steering wheels, 152b right steering wheels, 153a left driving wheels, 153b right drives Wheel, 154 fore wing, 156 propelling part, 157 lateral propelling part, collection of 158 arranged wings, 160 wing mounting angle control part
  • FIG. 1 is a side view of a car 100.
  • the automobile 100 includes a set of arranged wings 158 for generating lift necessary for flight, a propeller as a propulsion unit 156, a tail wing 154 for enhancing longitudinal stability in flight, a vertical stabilizer for directional stability in flight 127, elevator 124 for pitch direction control, auxiliary wing 126 for roll direction control, rudder 128 for yaw direction control, left steering wheel 152a used during traveling, left driven wheel 153a and reduction of side wind
  • the main body 150 is provided with a left lateral propulsion portion 157a for the purpose.
  • FIG. 4 is a side view of an example of a collection of deployed wings as viewed from the left of the vehicle.
  • FIG. 4 is an example of a collection of wings of 16 leaves in total when the wings are 4 in the vertical direction and the wings are 4 in the front-back direction.
  • a total of 84 wings of the arranged wing groups is an estimated value of the effective wing area of the leaf.
  • the width of the car is 1.68 US and the chord length is 0.1 US
  • the space between the vertical wing and the wing is 0.1 US
  • the space between the wing and the longitudinal wing Since the area of one leaf is 0.168 square rice and 84 leaves, the total area is 14.112 square rice.
  • the effective efficiency of the lift of the wing decreases, and in the case of 12 leaves in the vertical direction, the effective efficiency of the lift is about 56%.
  • the effective wing area of a total of 84 leaves is about 7.7 square meters.
  • the lift of the aft wing 154 at the front of the car is 15% and the lift share of the rear 84-wing arranged wing group 158 is 85%
  • the lift of the aft wing 154 is 1.4 square rice So, the sum of 7.7 square rice and 1.4 square rice is 9.1 square rice, which can generate the lift necessary for flight.
  • the size of the wing set 158 disposed at the rear is 1.1 rice in the vertical direction, 0.76 rice in the front-rear direction, and 1.68 rice in the left-right direction.
  • the wing width is 1.2 rice
  • the chord length is 0.15 rice
  • the distance between the vertical wing and the wing is 0.15 rice
  • a collection of wings of 0.3 ⁇ 0.45 rice in the vertical direction, 0.47 rice in the front-rear direction, 1.2 rice in the left-right direction, effective efficiency of lift of multi-leaf in the vertical direction Assuming 72 to 77 percent, the effective wing area of the wing of the canard wing 154 will be approximately 1.4 square rice.
  • FIG. 5 is a front view of the vehicle 100 of FIG.
  • the same symbols as the symbols already described in the figure have the same functions as the symbols already described.
  • 6 is a top view of the vehicle 100 of FIG. 7 is a rear view of the vehicle 100 of FIG.
  • the propeller as the propulsion part 156 is equipped with four in order to improve safety.
  • FIG. 8 is a functional block diagram of the vehicle 100 of FIG. This functional block diagram uses a secondary battery, a capacitor, etc.
  • the power source 108 uses wheels incorporating a motor for the left steering wheel 152a, the right steering wheel 152b, the left driving wheel 153a, and the right driving wheel 153b.
  • the motor is used as the rotational power of the propulsion unit 156 which is a propeller.
  • the propulsion unit 156 uses a propeller and a reciprocating engine or jet engine, the secondary battery of the power source 108 is charged by a generator mechanically coupled to the engine, and the left steering wheel 152a, the right steering wheel 152b, and the left drive And the right driving wheel 153b.
  • a fuel cell, a gas turbine or the like may be used as the power source 108.
  • the operation unit 106 is a steering wheel or a control stick, and receives an operation from the driver.
  • the traveling steering unit 104 moves the left steering wheel 152 a and the right steering wheel 152 b in accordance with the operation of the operation unit 106.
  • the power source 108 transmits power to the drive unit 110, the front wheel drive unit 114, the propulsion unit 156, and the side propulsion unit 157.
  • the drive unit 110 drives the left driving wheel 153 a and the right driving wheel 153 b.
  • the front wheel drive unit 114 drives the left steering wheel 152 a and the right steering wheel 152 b.
  • the left steering wheel 152a, the right steering wheel 152b, the left driving wheel 153a, and the right driving wheel 153b are provided with a brake.
  • the switching unit 130 for traveling and flight receives an operation from the operation unit 106 and notifies the state detection unit 112 of switching between traveling and flying.
  • the state detection unit 112 detects the state of the vehicle and transmits it to the operation unit 106, the steering unit 104 for traveling, the steering unit 122 for flight, and the power control unit 116.
  • the state detection unit 112 detects, for example, the speed, the altitude, the position, and whether the vehicle is traveling on the ground or in flight.
  • the flight steering unit 122 moves the rudder 120 that controls the attitude in accordance with the operation of the operation unit 106.
  • the rudders 120 that control the attitude include elevators 124, auxiliary wings 126 and rudders 128.
  • the power control unit 116 operates the power source 108 according to the state of the vehicle 100 supplied from the operation unit 106 and the state detection unit 112.
  • the propulsion unit 156, the drive unit 110, and the front wheel drive unit 114 are operated, and a propeller, a left steering wheel 152a, a right steering wheel 152b, a left driving wheel 153a and a right driving wheel
  • the takeoff run distance can be shortened.
  • the propulsion unit 156 is not driven by the operation of the propulsion unit 156 to prevent danger, and the vehicle travels forward on the ground with wheels, and after acceleration, the propulsion unit 156 is operated.
  • the propulsion unit 156, the drive unit 110, and the front wheel drive unit 114 are operated, and a propeller, a left steering wheel 152a, a right steering wheel 152b, a left driving wheel 153a and a right driving wheel
  • a propeller By simultaneously rotating the wheels 153b to match the rotation of the wheels to the landing speed, it is possible to reduce the wear of the wheels due to the friction between the road and the wheels upon landing, and also to reduce the impact upon landing.
  • the wing attachment angle control unit 160 controls the attachment angle of the wings of the arranged wing assembly 158 according to the operation of the driver from the operation unit 106.
  • the wing attachment angle control unit 160 may use angle control to control the attachment angle of the wing for each wing when controlling the attachment angle of the wings, but the wings in the vertical direction may have the same attachment angle
  • the same parts of the wings in the vertical direction can be coupled up and down with movable mechanical elements, the mechanical elements can be moved up and down, and the wings in the vertical direction can be grouped together to use a common angle control.
  • the common angle control of the wings in the vertical direction is mechanically connected by gears or the like so as to increase the mounting angle in the back and forth direction in the back and forth direction, the mounting angles of all the wings of the collection of wings are It can also be controlled by one angle control.
  • the mounting angle can also be divided into fixed wings and variable wings.
  • the angle settings can also be continuous or stepwise.
  • Lateral propulsion unit 157 receives power from power source 108 and receives an operation of the driver from operation unit 106.
  • the lateral propulsion unit 157 cancels the lateral component of the lateral wind of the vehicle so that the vehicle does not flow in the lateral wind.
  • a propulsable mechanism composed of a propeller, an electric motor, etc. is mounted approximately at the center of the left and right sides of the vehicle.
  • Such a car 100 can take off and land not only on roads but also at airports, farm roads, schoolyards, open spaces, rooftops, and the like.
  • the present invention has been described above based on the embodiments.
  • the embodiment is an exemplification, and various modifications can be made to the constituent elements and combinations of processing processes, and such modifications are also within the scope of the present invention.

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transportation (AREA)
  • Mechanical Engineering (AREA)
  • Motorcycle And Bicycle Frame (AREA)

Abstract

L'invention porte sur une automobile capable de rouler et de voler. Une automobile classique ayant une fonction de vol décolle d’une route et atterrit sur celle-ci difficilement, en raison du fait que la largeur et la hauteur de l'automobile sont importantes. La largeur et la hauteur d'une automobile selon la présente invention sont réduites par l'utilisation d'un ensemble d'ailes agencées de façon à générer une force de portance requise pour le vol, ce par quoi l'automobile est rendue capable de décoller d’une route et d'atterrir sur celle-ci. L'ensemble (158) d'ailes agencées est monté sur le corps (150) d'une manière telle que la direction de largeur de l'aile est amenée à être la direction droite-gauche de l'automobile, les ailes étant agencées sur un plan défini par la direction haut-bas et la direction avant-arrière de l'automobile, et l'angle de montage de chaque aile étant commandé de façon à constituer un angle d'attaque pour générer la même force de portance. Le corps (150) comprend une roue directrice gauche (152a) et une roue motrice gauche (153a) et roule à l'aide de ces roues. La partie propulsion (156) est constituée d'une hélice et génère une puissance de poussée requise pour le vol. Une gouverne d'élévation (124), une aile auxiliaire (126) et une gouverne de direction (128) assurent la commande de la posture pendant le vol.
PCT/JP2008/072227 2008-12-02 2008-12-02 Automobile volante WO2010064326A1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
JP2009545747A JPWO2010064326A1 (ja) 2008-12-02 2008-12-02 空飛ぶ自動車
PCT/JP2008/072227 WO2010064326A1 (fr) 2008-12-02 2008-12-02 Automobile volante

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/JP2008/072227 WO2010064326A1 (fr) 2008-12-02 2008-12-02 Automobile volante

Publications (1)

Publication Number Publication Date
WO2010064326A1 true WO2010064326A1 (fr) 2010-06-10

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ID=42232990

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/JP2008/072227 WO2010064326A1 (fr) 2008-12-02 2008-12-02 Automobile volante

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JP (1) JPWO2010064326A1 (fr)
WO (1) WO2010064326A1 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2015171881A (ja) * 2014-02-24 2015-10-01 浩 加納 空中浮遊車

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2848147A1 (fr) * 2002-12-09 2004-06-11 Laurent Fabre Vehicule automobile volant
JP2006213225A (ja) * 2005-02-04 2006-08-17 Kanazawa Inst Of Technology 飛行可能な自動車
JP3817591B2 (ja) * 2002-05-14 2006-09-06 学校法人金沢工業大学 自動車

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP3817591B2 (ja) * 2002-05-14 2006-09-06 学校法人金沢工業大学 自動車
FR2848147A1 (fr) * 2002-12-09 2004-06-11 Laurent Fabre Vehicule automobile volant
JP2006213225A (ja) * 2005-02-04 2006-08-17 Kanazawa Inst Of Technology 飛行可能な自動車

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