New type one-man flight vehicle capable of vertically taking off and landing and with fixed wings

Abstract

The invention discloses a new type one-man flight vehicle capable of vertically taking off and landing and with fixed wings. The new type one-man flight vehicle comprises wings, a support frame, engines, a rotating bearing, braces, a flight control unit, a fuselage, batteries, holding arms, a solar cell panel, an escape parachute and a lifesaving air bag. The vertical taking off and landing, low-speed flight and transition towards horizontal flight can be realized by rotating the directions of the two engines, low-speed and flexible flight can be realized without the utilization of fixed wings, and also high-speed and remote flight can be realized by utilizing the fixed wings.

Description

Technical field

[0001] The invention relates to a single-person aircraft, in particular to a fixed-wing single-person aircraft with vertical take-off and landing and horizontal flight functions that can change the direction of an engine. Background technique

[0002] Flying freely like a bird is a dream of mankind for thousands of years. Existing aircraft capable of vertical take-off and landing include overhead coaxial dual-rotor solutions, overhead single-rotor solutions, jetpacks, rocket straps, etc. The common advantage of these solutions is vertical take-off and landing, but the main common disadvantage is that they have no fixed wings. Long-distance level flight cannot be realized, the flight time and range are very short, and the speed is slow, the flight cost is high, the control is complicated, and the safety is poor. The existing light single-person aircrafts that can fly horizontally, such as powered paragliders and powered deltas, are slow in speed and short in range...

Examples

Embodiment 1

[0016] It will be further explained by taking the motor 4 as an embodiment.

[0017] Attached figure 1 Among them, the wing 1 adopts a symmetrical design with the longitudinal axis of the aircraft as symmetrical. After being fixed to the fuselage 11 by a support frame 2, the wing 1 adopts a controllable folding design. When flying vertically, the wing 1 can be folded to reduce the size. Affected by the airflow, it makes the flight more stable. Two engines 4 are fixed at both ends of a support frame 2, two bearings 3 are fixed and distributed in the middle, the outer side of the bearing 3 is fixed on the fuselage 11, and the support frame 2 is fixed between the two engines 4. Two propellers 5 are respectively installed on the two engines 4, one of which rotates forward and the other rotates reversely, so as to cancel each other's torque. There are life-saving umbrellas and life-saving airbags on the aircraft for lifesaving. The flight controller 7 is installed on the arm 6. Sol...

Embodiment 2

[0020] Take a jet engine as an example for further explanation.

[0021] As attached figure 2 As shown, the engine 4 is two jet engines, the propeller 3 does not need to be installed on the engine 4, the energy storage tank 9 has a battery pack and fuel, and the energy storage tank 9 has a fuel supply device to ensure that no matter what state the aircraft is in, Fuel can be supplied to the engine. The other parts are the same as the first embodiment.

Technical field

[0001] The invention relates to a single-person aircraft, in particular to a fixed-wing single-person aircraft with vertical take-off and landing and horizontal flight functions that can change the direction of an engine. Background technique

[0002] Flying freely like a bird is a dream of mankind for thousands of years. Existing aircraft capable of vertical take-off and landing include overhead coaxial dual-rotor solutions, overhead single-rotor solutions, jetpacks, rocket straps, etc. The common advantage of these solutions is vertical take-off and landing, but the main common disadvantage is that they have no fixed wings. Long-distance level flight cannot be realized, the flight time and range are very short, and the speed is slow, the flight cost is high, the control is complicated, and the safety is poor. The existing light single-person aircrafts that can fly horizontally, such as powered paragliders and powered deltas, are slow in speed and short in range...

Examples

Embodiment 1

[0016] It will be further explained by taking the motor 4 as an embodiment.

[0017] Attached figure 1 Among them, the wing 1 adopts a symmetrical design with the longitudinal axis of the aircraft as symmetrical. After being fixed to the fuselage 11 by a support frame 2, the wing 1 adopts a controllable folding design. When flying vertically, the wing 1 can be folded to reduce the size. Affected by the airflow, it makes the flight more stable. Two engines 4 are fixed at both ends of a support frame 2, two bearings 3 are fixed and distributed in the middle, the outer side of the bearing 3 is fixed on the fuselage 11, and the support frame 2 is fixed between the two engines 4. Two propellers 5 are respectively installed on the two engines 4, one of which rotates forward and the other rotates reversely, so as to cancel each other's torque. There are life-saving umbrellas and life-saving airbags on the aircraft for lifesaving. The flight controller 7 is installed on the arm 6. Sol...

Embodiment 2

[0020] Take a jet engine as an example for further explanation.

[0021] As attached figure 2 As shown, the engine 4 is two jet engines, the propeller 3 does not need to be installed on the engine 4, the energy storage tank 9 has a battery pack and fuel, and the energy storage tank 9 has a fuel supply device to ensure that no matter what state the aircraft is in, Fuel can be supplied to the engine. The other parts are the same as the first embodiment.

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