阅读说明：本技术 一种安全性极佳的陆海空全能型飞行汽车 (Land, sea and air all-round type hovercar with excellent safety ) 是由 孙林青 于 2019-11-08 设计创作，主要内容包括：本发明公布了一种安全性极佳的陆海空全能型飞行汽车,包括车身、船体、共轴反转双旋翼、固定翼、尾翼、降落伞。所述车身的纵剖面是机翼形状；车身中部的上方设有共轴反转双旋翼；车身中部共轴反转双旋翼的上方设有降落伞舱,降落伞舱内设有降落伞；车身尾部设有尾翼,尾翼上设有空中推进螺旋桨；车身两侧对称设有船体；所述船体外侧设有固定翼；船体下面设有车轮；船体后端设有水中推进螺旋桨。本发明将飞翼、旋翼、双体船与汽车有机地结合在一起,可以实现本发明在海陆空全能应用,且安全性能极佳。(The invention discloses an all-round aerocar in land, sea and air with excellent safety, which comprises a car body, a ship body, coaxial counter-rotating double rotors, fixed wings, a tail wing and a parachute. The longitudinal section of the vehicle body is in the shape of an airfoil; coaxial reverse dual rotors are arranged above the middle part of the vehicle body; a parachute cabin is arranged above the coaxial reverse double rotors in the middle of the vehicle body, and a parachute is arranged in the parachute cabin; the tail part of the vehicle body is provided with a tail wing, and the tail wing is provided with an aerial propulsion propeller; the two sides of the vehicle body are symmetrically provided with the ship bodies; the outer side of the ship body is provided with a fixed wing; wheels are arranged below the ship body; the rear end of the ship body is provided with an underwater propulsion propeller. The invention organically combines the flying wings, the rotor wings, the catamaran and the automobile together, can realize the full-functional application of the invention in sea, land and air, and has excellent safety performance.)

1. A land, sea and air all-round type hovercar with excellent safety is characterized in that: the multifunctional boat comprises a boat body, coaxial reversing double rotors, fixed wings, a tail wing and a parachute, wherein the coaxial reversing double rotors are arranged above the middle part of the boat body; a parachute cabin is arranged above the coaxial reverse double rotors in the middle of the vehicle body, and a parachute is arranged in the parachute cabin; the two sides of the vehicle body are symmetrically provided with the ship body, and the outer side of the ship body is provided with the fixed wings.

2. The flying car of the all-purpose type in land, sea and air with excellent safety as claimed in claim 1, wherein: the longitudinal section of the vehicle body is in the shape of an airfoil.

3. The all-terrain aerocar with excellent safety according to claim 2, wherein: the two sides of the vehicle body are symmetrically provided with ship bodies.

4. The all-terrain aerocar with excellent safety according to claim 3, wherein: the hull is a small waterline hull.

5. The flying car of the land, sea and air all-round type with excellent safety as claimed in claim 4, wherein: the ship is characterized in that a cabin is arranged on the front part of the ship body, wheels are arranged below the cabin, and an underwater propulsion propeller is arranged at the rear end of the ship body.

6. The flying car of the all-purpose type in land, sea and air with excellent safety as claimed in claim 1, wherein: the empennage comprises two side vertical tails, a middle vertical tail and a horizontal tail, the lower ends of the two side vertical tails are symmetrically arranged at the tail part of the ship body, the lower end of the middle vertical tail is arranged at the tail part of the automobile body, and the horizontal tail is arranged at the upper ends of the three vertical tails.

7. The flying car of claim 6, which is of all-purpose type, including: an aerial propulsion propeller is arranged behind the combination part of the horizontal tail and the middle vertical tail, a pitching control propeller is arranged above the middle part of the horizontal tail, pitching control rudders with aileron functions are symmetrically arranged at the two ends of the horizontal tail, and a direction control propeller is arranged at the upper part of the middle vertical tail.

Technical Field

The invention relates to an aircraft, in particular to a land, sea and air all-round flying automobile with excellent safety.

Background

With the development of technology and the demand of market, the flying automobile facing the public has become a pet for new product development. The fixed wing aircraft type flying automobile has the advantages of high speed, long range and strong carrying capacity, but needs runway takeoff and landing. The helicopter type aerocar can vertically lift and flexibly and conveniently use, but has low flying speed, short endurance time and larger vibration and noise. The two types of flying automobiles which are not specially designed or modified cannot be safely lifted, descended and parked on the water surface. In particular, the prior product has ideal flight performance but insufficient anti-falling safety performance.

Disclosure of Invention

In order to solve the technical problems, the invention provides the all-purpose aerocar in land, sea and air with long endurance time, flexible use, high anti-falling safety and excellent safety.

The technical scheme adopted by the invention is as follows: an all-round aerocar in the land, sea and air with excellent safety comprises a car body, a ship body, coaxial reverse dual rotors, fixed wings, a tail wing and a parachute. The longitudinal section of the vehicle body is in a flat wing shape; coaxial reverse dual rotors are arranged above the middle part of the vehicle body; a parachute cabin is arranged above the coaxial reverse double rotors in the middle of the vehicle body, and a parachute is arranged in the parachute cabin; the tail part of the vehicle body is provided with a tail wing, and the tail wing is provided with an aerial propulsion propeller; the two sides of the vehicle body are symmetrically provided with the ship bodies; and fixed wings are arranged on the outer sides of the ship bodies.

In the all-purpose aerocar in land, sea and air with excellent safety, the cabin is arranged on the front part of the ship body.

In the all-purpose aerocar in land, sea and air with excellent safety, wheels are arranged below the ship body.

In the all-purpose aerocar in land, sea and air with excellent safety, the rear end of the ship body is provided with an underwater propulsion propeller.

In the above-mentioned all-round type hovercar in land, sea and air that security is splendid, hull and automobile body afterbody be equipped with the fin, the fin include two side vertical tails, a well vertical tail and a horizontal tail, two side vertical tail lower extremes symmetry sets up the afterbody at the hull, well vertical tail lower extreme sets up the afterbody at the automobile body, the horizontal tail sets up the upper end at three vertical tails.

In the all-purpose aerocar in land, sea and air with excellent safety, an air propulsion propeller is arranged behind the joint part of the horizontal tail and the vertical tail.

In the all-purpose aerocar in land, sea and air with excellent safety, the pitching control propeller is arranged above the middle part of the horizontal tail.

In the all-purpose aerocar in land, sea and air with excellent safety, the upper part of the middle vertical tail is provided with the direction control propeller.

In the all-purpose aerocar in land, sea and air with excellent safety, the two ends of the horizontal tail are symmetrically provided with the pitching control rudders with the aileron function.

Compared with the prior art, the invention has the beneficial effects that:

1. the invention organically combines the flying wings, the rotor wings, the catamaran and the automobile together, has the advantages of high speed, long voyage and strong carrying capacity of a fixed wing aircraft, has the advantages of capability of vertically taking off and landing a helicopter without a runway, and can take off, land, sail and park on the water surface and also can run on a road. Therefore, the invention has comprehensive and flexible use performance.

2. The vehicle body is in a flat wing shape, and can play the roles of the vehicle body and the wing at the same time, so that the structural weight is reduced.

3. The cabin is completely separated from the vehicle body and is positioned on the side surface, so that the damage of an engine, a transmission and the like in the vehicle body to drivers and passengers when the vehicle falls or collides can be avoided, and the damage of a fire which is easy to occur in the vehicle body to the drivers and passengers can also be avoided.

4. When the forced landing is needed, the invention can be safely forced to land on the water surface, and can avoid the injury to ground personnel and self drivers and passengers when the ground is forced to land.

5. The pitch control propeller and the direction control propeller can be mutually backed up with the corresponding pitch rudder and direction rudder, so that the problem that the safe flight and landing cannot be realized due to the loss of related control is avoided.

6. The parachute of the invention can ensure that the parachute can land safely when falling, and the life of drivers and passengers is prevented from being injured.

Drawings

Fig. 1 is a front view of the present invention.

Fig. 2 is a left side view of the present invention.

Fig. 3 is a top view of the present invention.

Fig. 4 is a cross-sectional view of the present invention.

Fig. 5 is a front view of embodiment 2 of the present invention.

Fig. 6 is a left side view of embodiment 2 of the present invention.

Fig. 7 is a top view of embodiment 2 of the present invention.

Fig. 8 is a front view of embodiment 2 of the present invention.

Fig. 9 is a left side view of embodiment 2 of the present invention.

Fig. 10 is a top view of embodiment 2 of the present invention.

Fig. 11 is a sectional view of embodiment 2 of the present invention.

In the figure: 1, an upper rotor wing; 2 a lower rotor; 3, a vehicle body; 4, hanging the tail at the side; 5 pitching the control propeller; 6, propelling a propeller in the air; 7 parachute bay; 8, pitching a rudder; 9, flattening the tail; 10 a hull; 11 cabin; a 12-direction rudder; 13 propelling a propeller in water; 14 direction control propeller; 15 middle vertical tails; 16 wheels; 17 the fixed wing.

Detailed Description

The invention will be further explained with reference to the drawings.

As shown in fig. 1 to 4, the vehicle body 3 of the present invention has a flat wing shape, and also functions as a wing, so that the structural weight can be reduced.

The helicopter comprises a vehicle body 3 and coaxial reverse dual rotors, wherein the coaxial reverse dual rotors are arranged above the middle part of the vehicle body 3 and comprise an upper rotor 1 and a lower rotor 2, so that the helicopter can vertically lift like a helicopter.

A parachute cabin 7 is arranged above the coaxial reverse double rotors of the vehicle body 3, and a parachute is arranged in the parachute 7. The parachute can be opened in the falling process of the invention, the falling speed of the invention is greatly reduced, and the injury of personnel and the damage degree of the invention are greatly reduced.

The two sides of the vehicle body 3 are symmetrically provided with the ship bodies 10, so that the invention can be lifted, descended and parked on the water surface, and has good transverse stability.

The ship body 10 is a small water line ship body, and the rear end of the ship body is provided with an underwater propulsion propeller 13, so that the ship can sail in water, and the sailing resistance is small.

Wheels 16 are provided under the hull 10 to enable the invention to be driven on a ground road.

The cabin 11 is arranged on the front part of the ship body, so that the cabin 11 is completely separated from the vehicle body 3, the harm of an engine and the like in the vehicle body 3 to personnel in the cabin when the ship falls or collides can be avoided, and the harm of flame and smoke generated when the engine or an oil tank and the like in the vehicle body 3 happen to the personnel in the cabin 11 can also be avoided.

Empennages are arranged on the rear parts of the vehicle body 3 and the ship body 11 and comprise two side vertical tails 4, a middle vertical tail 15 and a horizontal tail 9. The middle vertical tail is provided with a direction control propeller 14, and the horizontal tail is provided with a pitching control propeller 5, which can form backup with the rudder 12 and the pitching rudder 8. The outer side of the horizontal tail is provided with a pitching rudder 8 with the function of an aileron.

The outer side of the hull 11 is provided with a fixed wing 17, and the rear part of the empennage is provided with an air propulsion propeller 6, so that the invention can take off, land and fly like a fixed wing airplane.

As shown in fig. 5 to 7, as a second embodiment, when the area of the vehicle body having the function of the wing is large enough to meet the requirement of generating lift force, the fixed wing may not be provided outside the hull. The advantage of this aerodynamic configuration is that it makes it easier to select landing sites when necessary.

As a third embodiment, as shown in fig. 8 to 11, a coaxial counter-rotating twin rotor is provided in the vehicle body. The advantage of this aerodynamic layout is that the rotor is protected by the vehicle body and is not easily damaged by external obstacles, thus improving the safety of the invention.