KR20190045789A - A Vertical take-off and landing aircraft - Google Patents

Abstract

The present invention relates to an aircraft able to vertically take off and land with drone functions, which is able to make a centrifugal compression spray apparatus by power of a super-efficient power generation apparatus using a freezing cycle, to install an airfoil on the front side and rear side of the spray apparatus, to generate lift, to vertically take off or land, and to fly by a separate super-efficient engine. The aviation engine, which is currently the most widely used, has a centrifugal compressor on the front side unit to burn compressed air, to drive a turbine with burned mixed gas, to generate power, to spray the combustion gas with a strong pressure, to form on the front side of an aircraft by negative pressure, to spray a strong pressure towards the rear side of the aircraft, and to transfer the aircraft by the propulsion force. However, since the conventional internal combustion engine and flight engine drive by using fossil fuel, there has been a huge problem of polluting the environment. Accordingly, the present invention aims to provide an aircraft able to vertically take off and land with drone functions while preventing environment pollution by using free energy and super-efficient energy as power, installing an airfoil on the front and rear sides of the centrifugal compression spray apparatus, enabling the aircraft to vertically take off and land, and converging the drone functions with the functions of a fast aircraft.

Description

A vertical take-off and landing aircraft,

The present invention relates to a centrifugal compression injection device using power of a refrigeration cycle-based super-efficiency power generation device, and an airfoil is installed before and after the air injection device to generate lifting force for vertical takeoff and landing, Landing aircraft that combines a drones function.

Vertical takeoff and landing aircraft based on rotor blades, such as helicopters and drones, have the advantage of not requiring separate takeoff and landing facilities and equipment, but they are inferior in performance to high-flying, long-haul and high-altitude aircraft.

In general, aircraft and drones that take off and land vertically have a method of taking off from the ground by spinning a helicopter propeller in the main march of the British march that takes off the ground vertically by injecting strong pressure into the nozzle, There is a way to generate lift by transferring the wind from the center of the drone's round airfoil to the outside.

The former has a difficulty in using at home due to dust on the ground, and the latter has a disadvantage that the flying speed is slow.

Compared to a fixed-wing aircraft capable of selecting various propulsion systems from electric motors to jet engines, vertical takeoff and landing aircraft, which depend only on the axial horsepower of the engine, have a limited choice of propulsion system as the weight of the aircraft decreases.

In particular, the output-to-weight ratio of the reciprocating engine, which is widely used for a small aircraft with a maximum take-off weight (MTOW) of about 10 to 300 kg, is very small.

Therefore, in order to supply the power required for vertical takeoff and landing, the volume and weight of the engine is much larger than that of a fixed-wing aircraft of the same class, and the weight of the propulsion system to the aircraft's empty weight is excessively large, it is difficult to secure payload and endurance time.

Therefore, although a propulsion system using a battery and an electric motor is widely used for a small aircraft, due to the limitation of current battery technology having a low energy density, it is not possible to provide a sufficient time required for a mission.

In order to construct a long-term space, energy sources with high specific energy and power units capable of converting them are required. However, for vertical takeoff and landing, energy sources with high specific power and devices capable of converting them are required .

However, since there is no energy source or power generating device having both a non-energy and a non-power, there is an ongoing effort to provide a longer running time.

On the other hand, the most used aviation engine has a centrifugal compressor in the first half and burns compressed air; The turbine is driven by the combusted gas mixture and the power is generated. The combustion gas is injected at a strong pressure, so that the first half of the airplane forms a negative pressure and injects a strong pressure to the rear of the boat to transfer it to the driving force.

However, conventional internal combustion engines, aviation engines, and the like are driven by using them as fossil fuels, which has caused a great problem of polluting the environment.

Therefore, it is an object of the present invention to provide a diesel engine capable of preventing environment pollution by using free energy and ultra-efficient energy as a power source and installing an airfoil before and after the centrifugal compression injection device, It is to provide a vertical takeoff and landing aircraft that combines functions of an aircraft and serves as a drones function.

In order to achieve the above-mentioned object, the present invention provides a method for generating electricity by using a thermoelectric power generator to generate electrons generated between a high temperature part and a low temperature part by generating a pressure difference in a refrigeration cycle using a turbine, A power section; A second power section that is powered by a force that rotates by the force of a magnet; A third power section using gravity and magnetic force; A power generating motor unit driven by receiving the electric energy generated by the first power unit; A compressor is driven by a speed control unit for shifting and transmitting the rotational force of the power generation motor; An airfoil installed before and after the compressor; And the lift is determined by the speed of the air sucked into the compressor and the air injected into the compressor.

In addition, when the aircraft is not operated by the second power unit and the third power unit, the air is cooled and warmed, and the surplus electricity is charged to the battery, so that the start- The power unit and the third power unit provide energy, and when the first power unit performs a normal operation after a predetermined time, the first power unit performs all the power, and the reverse propulsion unit is installed at the center to take- City, and when you want to stop the flight.

As described above, the vertical takeoff and landing aircraft serving as the drone function of the present invention produces the following effects.

In the vertical take-off and landing aircraft serving as the drone function of the present invention,

1. It is not a method of spraying to ground by using pressure, so it can be used conveniently regardless of home or place.

2. After take-off, the flight speed is fast, it can be rotated in place, and it can be combined with the drones and aviation functions.

3. It can fly for a long time without supplying fuel, and can also navigate at sea by combining aircraft and ship functions.

4. It can be combined with functions such as housing and camper

)는 공기 또는 유체의 흐름과 항공기 이동방향.
표시 없는 사각은 공간과 같은 목적의 부품임.1 is a view showing the construction of a lifting device of the present invention;
2 is a front view of a vertical take-off and landing aircraft serving also as a drone function of the present invention.
FIG. 3 is a cross-sectional view of an embodiment of the present invention. FIG.
4 shows a "hollow" - "hollow" cross section and thrust force explanatory view of the present invention.
5 is a front view of the airplane of the present invention.
6 is a front elevational view of an aircraft in an emergency falling state of the present invention.
7 is a side elevational view of an aircraft in an emergency falling state of the present invention.
DESCRIPTION OF REFERENCE NUMERALS
01) Lift and propulsion generator 03) Airfoil
05) Air guide tube 07) Centrifugal compressor 09) Speed adjuster
11) Power generator motor 13) Ultra-efficient power generator 15) Power generator motor
17) Speed adjuster 19) Centrifugal compressor 21) Airfoil
31) Auxiliary parachute 33) Main parachute 35) Reverse propulsion unit
37) Magnetic rotating device 38) Gravity and magnetic rotating device
39) Propulsion power generation device 43) Bonding device 45) Energy storage device
47) Interior space 49) Battery 51) Support
61) Lifting blades 63) Lifting blades 65) Angle adjusting device
66) Boarding ladder
* arrow(

) Air or fluid flow and direction of aircraft movement.
The square without mark is a space-like part.

The construction of the present invention will now be described in detail with reference to the drawings from FIG. 1 to FIG. 7.

A super efficient power generation device 13 is installed in the middle part of the refrigerator to generate a refrigeration cycle using air heat and pressure; Power generators 11 and 15 are installed on both sides of the super efficient power generator 13; Speed adjusting devices 09 and 17 are installed on the other side of the power generating motors 11 and 15; An air guide pipe 05 is installed outside the installed devices; A plurality of lift and propulsive force generating devices 01 each having an airfoil 03 on one side of the air guide pipe 05 and an airfoil 21 on the other side are prepared.

At this time, the direction of installation of the airfoil 03 and the airfoil 21 should be the same, and each of the airfoils should be capable of adjusting the lift by providing each angle adjusting device. The side to which the air is sucked is referred to as the front, and the side to which the air is sucked is referred to as the suffix.

On the other hand, in the case where the lift generating vane 61 is installed in front of the propulsion generating device 39 having a large size of the super efficiency generating device 13 and the large super efficiency generating device 13, The propellant-spraying device 35 is prepared.

Subsequently, a plurality of lift and propulsive force generators (01) are horizontally installed on both sides of a cylinder having both sides opened and having an oval cross section and a length, is referred to as a small unit wing; The small unit wings are arranged in a multi-layered manner on both sides along the outer circumferential surface of the ellipse.

Then, the small unit wing is fixed by the binding device 43. [

Subsequently, the propulsion generating device 39 is installed at the four corners of the small unit wing, the reverse propulsion injecting device 35 is installed on the center line of the short radius of the ellipse, and on the outer side of the upper and lower parts; A magnetic force rotating device (37) is installed on both sides of the reverse propulsion injecting device (35).

On the other hand, a rotating device 38 of gravity and magnetic force is installed in the indoor space 47,

The energy storage device 45 is installed on the outer surface of the installed propulsion power generation device 39 and the battery 49 is installed on the outer surface of the reverse propulsion device 35.

Here, the magnetic force rotating device 13, the super efficient power generating device 13, the gravity and magnetic force rotating device 38 and the like should be referred to in detail.

Subsequently, a sub-parachute 31 is installed on both sides of the propulsion generating device 39 installed at the upper part, a main parachute 33 is installed at the center of the reverse propulsion injecting device 35, The support pedestal 51 is installed on the inside of the device 39 and the ladder 66 is installed on the rear side of the device 39. The support pedestal 51 is folded when taking off the ladder 66, 47, the construction of the present invention is completed.

The operation state of the present invention will now be described in detail with reference to FIGS. 1 to 7.

The power generation motor 11 and the power generation motor 15 are rotated by the energy generated in the super efficient power generation device 13 of the lift and propulsive force generation device 01 and the centrifugal compressor 11, (07) and (19) are rotated, air is generated in the air guide (03) in the process of sucking air into the air guide pipe (05), and lift is generated in the air foil , Lift is generated in the entire portion of the small unit wing, the air of the aircraft is raised, and forward movement is simultaneously generated.

At this time, the reverse propulsion injecting apparatus 35 is operated together to generate lifting force in the lift generating vane 61 and the lift generating vane 63, and the air flow is caused to be conveyed in the opposite direction to that in the case of the small unit vane.

Therefore, the forward force and the backward force are canceled, and only the lift is generated, and the body of the aircraft is taken off vertically.

The airplane body that has taken off to the target point operates the propulsion power generator 39 to freely move in straight, regular, revolving, rising, and falling directions.

At this time, the angle of operation of the air foils 03 and 21, the lift generating vane 61 and the lift generating vane 63 is adjusted by the angle adjusting device 65 to generate lift or suppress the lift.

When an emergency situation occurs and the descending speed exceeds a predetermined speed in a fall, the auxiliary parachute 31 and the main parachute 33 are deployed, so that the descending speed is slowed down to be safely landed.

On the other hand, when the aircraft lands and stops the flight, all functions except the magnetic force rotating device 37, the gravity and the magnetic force rotating device 38 are stopped; The cooling and heating of the indoor space 47 and the energy storage device 45 and the battery 49 are charged by the power generated by the magnetic force rotating device 37 and the gravity and the magnetic force rotating device 38.

On the other hand, when landing on the sea, a power source and propulsion force using the water temperature can be generated in the lower propulsion generating device 39 and the reverse propulsion injecting device 35, so that it can be used both at sea and in the air.

Further, the vertical takeoff and landing aircraft serving as the drone function of the present invention can also be used as a mobile house, and can be used as a camper.

The present invention is not limited to the above-described embodiment, but may be applied to other types of vertical takeoff and landing aircraft having a drone function. It will be understood by those skilled in the art that various changes in form and details may be made therein without departing from the scope of the present invention.

Claims (4)

A super efficient power generation device 13 is installed in the middle part of the refrigerator to generate a refrigeration cycle using air heat and pressure; Generation motors 11 and 15 are installed on both sides of the super efficient power generation device 13; Speed adjusting devices 09 and 17 are installed on the other side of the power generating motors 11 and 15; An air guide pipe 05 is installed outside the installed devices; Means for preparing a lift and propulsion generating apparatus 01 provided with an airfoil 03 on one side of the air guide pipe 05 and an airfoil 21 on the other side,
A plurality of lifting and propulsive force generators (01) are horizontally installed on both sides of a cylinder having both sides opened in an elliptical shape and having a length, is referred to as a small unit wing; Means for arranging the small unit wings in a double layer in symmetry on both sides along the outer circumferential surface of the ellipse,
A propulsion generating device 39 is installed at the four corners of the small unit wing, the reverse propulsion jetting device 35 is provided on the center line of the short radius of the ellipse, and on the outside of the upper and lower portions; Means for installing a magnetic force rotating device (37) on both sides of the reverse propulsion injecting device (35)
A gravity and magnetic force rotating device 38 is installed in the indoor space 47 and an energy storage device 45 is attached to the outer surface of the installed propulsion power generation device 39 on the outer surface of the reverse propulsion device 35, And means
The main parachute 33 is provided at the central portion of the inverted spraying device 35 and the small unit wing portion at the bottom and the propulsion power generating device 39 , And a means for installing a ladder (66) on the main body at the rear end, the vertical take-off and landing aircraft also serving as a drone function. The drones according to claim 1, characterized in that the super efficient power generation device (13) and the power generation motor (11) that generate electricity in a freezing cycle using air heat and pressure in the middle portion are replaced by a general aviation engine and a cylinder reciprocating engine Vertical takeoff and landing aircraft combined with functions. The airbag device according to claim 1, wherein a plurality of lift and propulsive force generators (01) provided with airfoils (03) on one side and airfoils (21) on the other side are provided, A vertical takeoff and landing aircraft that combines a drones feature that is installed. The vertical take-off airplane of claim 2, wherein the super-efficiency power generation device (13) and the power generation motor (11) are replaced by a general motor to generate a refrigeration cycle using air heat and pressure at the intermediate portion.

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