초록 ▼

The present invention provides an amphibious flying car, comprising: a casing, a chassis, a ship bottom body, a vehicle wheel, a drive system and an operating system; an upper airfoil and a rotor wing which are arranged on the top of the casing, are fixed on a bearing carrier located at the orthocen

The present invention provides an amphibious flying car, comprising: a casing, a chassis, a ship bottom body, a vehicle wheel, a drive system and an operating system; an upper airfoil and a rotor wing which are arranged on the top of the casing, are fixed on a bearing carrier located at the orthocenter of the fuselage; a strake wing is provided at the position where the casing, the chassis and the ship bottom body are combined; the horizontal wing comprises a stabilizing plane and an elevator, which are respectively located at the front end and the rear end of the fuselage; the vertical twin fins are arranged at both sides of the rear end of the fuselage, and its root segments are fixedly connected to the strake wing.

대표청구항 ▼

1. An amphibious flying car, comprising: a casing (3), a chassis (12), a ship bottom body (14), a vehicle wheel (11), an automotive engine (1), a drive system of the automotive engine (1), an aero-engine (8), a drive system of the aero-engine (8), a fuselage, and an operating system (2); characteriz

1. An amphibious flying car, comprising: a casing (3), a chassis (12), a ship bottom body (14), a vehicle wheel (11), an automotive engine (1), a drive system of the automotive engine (1), an aero-engine (8), a drive system of the aero-engine (8), a fuselage, and an operating system (2); characterized in that: the casing (3) is fixedly arranged on the chassis (12); an upper airfoil (6) and a rotor wing (5), which are arranged on the top of the casing (3), are affixed to a bearing carrier located at a orthocenter of the fuselage; the upper airfoil (6) is affixed to the casing (3) via a hinged shaft; the chassis (12) is connected with the ship bottom body (14); a strake wing (10) is provided at a position where the casing (3), the chassis (12) and the ship bottom body (14) are connected; a horizontal wing comprises a stabilizing plane (13) located at the front end of the fuselage and an elevator (9) located at the rear end of the fuselage; two vertical fins (7) are arranged the rear end of the fuselage, each having its root segment fixedly connected to the strake wing (10); the automobile engine (1) is arranged in the front of the chassis (12), and is connected to the vehicle wheel (11) and a thruster (16) by means of the drive system of the automobile engine (1); a water rudder (15) and the thruster (16) are arranged under the chassis (12) and at the rear of the fuselage; the aero-engine (8) is arranged at the rear end of the fuselage and is connected to the rotor wing (5) by means of the drive system of the aero-engine (8); the operating system (2) comprises a hydraulic rigid mechanical operating system and a quasi-active control system. 2. The amphibious flying car according to claim 1, characterized in that: each of said casing (3), the chassis (12) and the ship bottom body (14) are composed of carbon fiber reinforced composites and light alloy components integrated together; and said casing (3), the chassis (12) and the ship bottom body (14) are connected by a sealing glue. 3. The amphibious flying car according to claim 2, characterized in that: the chassis (12) of said amphibious flying car is further provided with an emergency sheltering device (21); said emergency sheltering device (21) comprises a storage battery and a motor, the storage battery is electrically connected to a motor. 4. The amphibious flying car according to claim 1, characterized in that: said aero-engine (8) is a turbocharged common rail injection diesel engine. 5. The amphibious flying car according to claim 4, characterized in that: the chassis (12) of said amphibious flying car is further provided with an emergency sheltering device (21); said emergency sheltering device (21) comprises a storage battery and a motor, the storage battery is electrically connected to a motor. 6. The amphibious flying car according to claim 1, characterized in that: said upper airfoil (6) comprises a leading edge flap, an aileron, and a trailing edge flap. 7. The amphibious flying car according to claim 6, characterized in that: the chassis (12) of said amphibious flying car is further provided with an emergency sheltering device (21); said emergency sheltering device (21) comprises a storage battery and a motor, the storage battery is electrically connected to a motor. 8. The amphibious flying car according to claim 1, characterized in that: under the control of the hydraulic rigid mechanical operating system, a rotation shaft of said rotor wing (5) tilts backwards in a range of 0.5°-3°. 9. The amphibious flying car according to claim 8, characterized in that: the chassis (12) of said amphibious flying car is further provided with an emergency sheltering device (21); said emergency sheltering device (21) comprises a storage battery and a motor, the storage battery is electrically connected to a motor. 10. The amphibious flying car according to claim 1, characterized in that: each of the two vertical fins (7) tilts outwards at a degree of 3°, and is provided with a rudder (17) and a navigation light (20). 11. The amphibious flying car according to claim 10, characterized in that: the chassis (12) of said amphibious flying car is further provided with an emergency sheltering device (21); said emergency sheltering device (21) comprises a storage battery and a motor, the storage battery is electrically connected to a motor. 12. The amphibious flying car according to claim 1, characterized in that: a coupler (4) is arranged between the drive system of said automobile engine (1) and the drive system of the aero-engine (8). 13. The amphibious flying car according to claim 12, characterized in that: the chassis (12) of said amphibious flying car is further provided with an emergency sheltering device (21); said emergency sheltering device (21) comprises a storage battery and a motor, the storage battery is electrically connected to a motor. 14. The amphibious flying car according to claim 1, characterized in that: a front face of said casing (3) is provided with an air inlet (19) of the automobile engine, and a rear portion of a side face of the casing (3) is provided with an inlet passage (18) of the aero-engine. 15. The amphibious flying car according to claim 14, characterized in that: the chassis (12) of said amphibious flying car is further provided with an emergency sheltering device (21); said emergency sheltering device (21) comprises a storage battery and a motor, the storage battery is electrically connected to a motor. 16. The amphibious flying car according to claim 1, characterized in that: said operating system (2) further comprises a navigation system, a communication system and/or a positioning system. 17. The amphibious flying car according to claim 16, characterized in that: the chassis (12) of said amphibious flying car is further provided with an emergency sheltering device (21); said emergency sheltering device (21) comprises a storage battery and a motor, the storage battery is electrically connected to a motor. 18. The amphibious flying car according to claim 1, characterized in that: the chassis (12) of said amphibious flying car is further provided with an emergency sheltering device (21); said emergency sheltering device (21) comprises a storage battery and a motor, the storage battery is electrically connected to a motor.