KR20180003936A - Aircraft which is driven by combustion engine - Google Patents

Abstract

The present invention relates to an aircraft driven by a combustion engine. According to the present invention, a drone of which hot air is filled in an egg-shaped body such as an airship and in which wings, tail wings and the like are formed is formed with one vertical partition in a space of one sealed hexahedron back and with two big holes on a center of one surface of the hexahedron back located on a front side of the inside of a hull of the drone facing the partition such that if one of the two holes is opened, the other one is closed, and if the other one is opened, and the one is closed by a valve such as a solenoid valve or the like. On a wall surface without a big hole on the opposite side of the partition, at last one small exhaust hole for generating thrust of the aircraft is formed, and on the inside or the outside of the hexahedron, a heating unit formed with gas fire or a hot wire for heating the inside of the hexahedron is formed. In the heating unit, part or a whole material of the hexahedron back is made of a transparent material such as glass or the like to be heated by a greenhouse effect such that the inside of the hexahedron back is heated. A control unit for controlling the valve is formed at one side of the outside of the hexahedron such that when one side of the valve is opened, the other side is closed, and when the other side is opened, and the one side is closed. In addition, a wall surface without a big hole on the opposite side of the partition is formed at one side of the aircraft such that heated air of the heating unit except air discharged through the small exhaust hole is introduced into a body of the hot-air balloon-type aircraft.

Description

BACKGROUND OF THE INVENTION 1. Field of the Invention [0001]

The present invention relates to an aircraft propelled by a heat engine.

As a background of the present invention,

Hot air balloon

* Hot air is light because it has a smaller specific gravity than cold air and therefore synergizes in the atmosphere. Using this principle, when the air inside the apparatus is heated by fire, the weight becomes lighter, and it rises to the sky. Hot air balloons flying to the sky will fly along the wind.

tool

The goofy is generally made of spherical shape, and the shape balloon which makes various shapes according to the user's taste is also showing a lot of lines. There are A-type, O-type, V-type, N-type, and the like depending on the type of the mechanism. In addition, there are a side-bant type and a parallel type according to the way of discharging the inside air. Currently, parachute types are mostly used. The basket is made of rattan, which is intended to reduce weight and alleviate the impact on landing. A burner is a device that inserts hot air into a goofy.

The heat engine uses the heat engine of the application No. 10-2014-0082940 filed on July 3, 2014, and the present invention becomes the invention applying the heat engine

In addition, the greenhouse effect is also applied to the technique of the present invention.

Greenhouse effect

The short-wave radiant energy emitted by the sun passes through the greenhouse glass and is absorbed into the walls or the ground inside the greenhouse. The energy released from the heated floor or wall by the sunlight does not penetrate the glass of the greenhouse because it is a long wavelength infrared energy. Therefore, the temperature inside the greenhouse rises, which is called the greenhouse effect.

I'll explain the structure of the aircraft.

The configuration of the aircraft is divided into airframe, engine, main wing, tail wing, and landing gear.

The airplane's airframe is divided into an ordinary room and a cockpit (cockpit)

Main wings include flaps, front flaps, ailerons, air brakes ( spoilers) , and so on. On the main wing

It has a built-in fuel tank for fueling the aircraft.

The tail wing is divided into horizontal tail wing and vertical tail wing,

Vertical tail wing has rudder (rudder) which is responsible for combat play of aircraft,

There is an elevator (elevator) for the pitch of the aircraft in the horizontal tail wing.

The aircraft's primary control surface is divided into elevator, aileron, and rudder.

The flap is a high lifting device that lifts the aircraft's lift.

The trailing flap includes a flat flap, a fouler flap, a split flap, a jab flap, a slot flap,

The front flap has flap, slot and slat depending on the shape.

The flap changes the protrusion line of the wing of the aircraft or expands the wing to increase the lift when taking off

You can shorten the sliding distance and increase the drag on landing to reduce landing distance and landing speed.

The types of wings are divided into single, double, triple, and front wing, rear wing,

Rectangular wings, triangular wings, bowed wings, tapered wings, and elliptical wings.

Each has advantages and disadvantages, so use the wings that are appropriate for the applicable aircraft.

The engine (engine) type can be largely divided into a jet engine and a reciprocating engine

The reciprocating engine is divided into an opposing type and a forming engine, and is mainly used for small and medium-sized aircraft.

The jet engine has a jet fan engine, turbojet, ramjet, turboprop and so on.

The jet fan engine used in civil engines has less noise and fuel consumption than turbojets,

Jet engines are mainly used in military applications, and turboprop aircraft are mainly used in small- and medium-sized aircraft,

70% gain propulsion from the propeller, and 30% gain thrust by the exhaust gas.

The ramjet engine is not currently used because of the explosion hazard and high fuel consumption of the fuel.

To explain the landing gear of the aircraft, if the main landing gear is in front,

When the main landing gear is behind, it is front-wheel type.

There are two advantages and disadvantages.

Advantages of front wheel - Wide viewing angle, Easy to move on the ground

Advantages of the rear wheel - Landing is better. Disadvantages - Unstable movement on the ground.

And so on.

Landing gears are foldable and protruding, which is the drag force on the landing gear when the aircraft is in flight.

Because of fuel loss, speed reduction, and maneuverability, most aircraft, except for some light aircraft,

Use transplants and some light aircraft or ultra light aircraft use fixed landing gear.

Aileron

Summary: Small area wing surface (keying surface) that is hinged to the rear edge of the airplane wing.

It is moved directly from the cockpit or by a power tool. The aileron (auxiliary wing) serves to rotate the rotation axis of the airplane.

In other words, when the control rod is turned to the right, the right wing's auxiliary wing is raised, the left wing's auxiliary wing is moved down, and the right wing is reduced in camber of the wing section to reduce the lift, The plane is tilted to the right as it increases. At this time, the airplane turns largely as it slides sideways.

Flap [Listen to Flap]

It is a device that generates high lift by changing the shape of the main wing mounted on the back of the main wing of the aircraft. It is a kind of high lifting device. It has the same function as the flap, but what is mounted on the front of the main wing is called the slat.

Flap [flap]

Summary: A typical high lift device that increases the lift generated from an airplane wing.

It is mounted on the rear edge of the main wing or on both sides of the main wing for the purpose of shortening the take-off and landing distance and making the take-off and landing operations easier by taking off the airplane quickly from the ground, slowing down the landing speed, have.

Typical types of flaps are ① simple flap, ② split flap, ③ sluled flap, and ④ Fowler flap.

There is also an ejection flap and a jet flap using high-pressure air, and an ejection flap is used for some military aircraft.

Direction Key [rudder Listen to voice]

Summary: The moving part of the plane behind the vertical tail wing.

Also known as rudder. Operate with the directional pedal of the cockpit with the control wing surface fixed with a hinge on the back of the vertical stabilizer. For example, pressing the left direction key pedal causes the direction key to turn to the left, and the vertical tail wing to the right direction. Thus, the gas rotates with the rotational force in the left direction.

That is, by this operation, a camber is generated on the key surface in the blade surface of the vertical tail wing and a camber is generated in the blade surface in the vertical tail wing, thereby generating a lateral lift force on the camber side, thereby causing the airplane to slip or swivel or to stop it .

Lifting key

 Conversion by elevator

An elevator is a kind of adjustment surface, usually located behind the aircraft, which changes the pitch of the aircraft and adjusts the bearing to change the angle of attack of the wing. The increased angle of attack causes a large drag due to the shape of the wing, which slows down the speed. On the other hand, reducing the angle of attack increases the speed. There are lifts on both sides, but operation occurs at the same time. The elevator is attached to an adjustable adjustment surface which has only a pitch adjustment surface or is called a fixture or stabilizer. The elevator is hinged to the rear spar of the horizontal stabilizer, usually with the aircraft turning or stabilizing steering around the horizontal axis. The structure of the elevator is similar to that of ancillary wing and rudder, Static equilibrium is achieved by attaching a counterweight to the front part of the hinge line. Aerodynamic equilibrium is achieved by mounting the elevator behind the leading edge of the stabilizer. Usually, since the end of the elevator is extended several inches ahead of the hinge line, .

Pitch

Rotation relative to an axis (Y axis or transverse axis) connecting the wing tips of the aircraft through the center of gravity (CG) of the aircraft.

Horizontal stabilizer

Summary: The front half of a horizontal tail wing, which is mounted horizontally or nearly horizontally at the rear of the aircraft fuselage.

Sometimes the front part is installed. The elevator key [elevator] constitutes the horizontal tail wing and is not used alone.

Unlike fixed vertical stabilizers, horizontal stabilizers are highly mobile and raise or lower the aircraft's nose, maintaining vertical stability and stability. In this case, the horizontal stabilizer moves separately with the lift key, but there is also a horizontal tail wing which improves the maneuverability by the interlocking type.

Hydraulic pressure (hydraulic pressure) using a mechanical force Flying tail, man's power to move is called a stabilizer

Horizontal tail

1) The wings that run from side to side at the end of the fuselage.

2) Tail wing that is responsible for equilibrium, stabilization and steering of the species. It is called horizontal fist because it is installed almost horizontally.

Main wing [main wing]

Wing that is responsible for lifting the entire aircraft. As the structure of the wing becomes stronger and it can withstand a large wing face load, it can be all monotone now compared to the former which had more bamboo flute. The positional relationship between the wing and the fuselage is determined according to the main purpose of the gas as a result of long discussions. Some of the wings with adjustable wings or variable wings that are seen in supersonic military aircraft have been put to practical use.

A problem to be solved by the present invention is to provide an airplane in which a propeller is rotated by a heat engine in a hot air balloon to generate thrust, or air is heated by a rocket propulsion system to generate thrust.

The solution to this problem is to use a heat pipe of Patent No. 10-2014-0082940, filed on July 3, 2014, in which the propeller, which is formed integrally with the heat engine, rotates and generates thrust Or the air heated by the rocket propulsion system is injected to generate thrust.

The effect of the present invention can be achieved by using only electric power of a simple electronic operation so that a flight of a drone or the like can fly in a propeller type or a rocket type, and in the case of a rocket type, no noise is generated.

1 is a sectional view of a heat engine of the present invention.
2 is a sectional view of another heat engine of the present invention.
3 is a cross-sectional view of another heat engine of the present invention.
4 is a cross-sectional view of another heat engine of the present invention.
5 is a cross-sectional view of another heat engine of the present invention.
Figure 6 is a perspective view of the drones of the present invention.
7 is a perspective view of a dronion propelled by the heat engine of the present invention.
8 is a perspective view of a drones propelled by another heat engine of the present invention.

* Detailed contents for carrying out the present invention will be described with reference to the drawings.

FIG. 1 is a cross-sectional view of a heat engine according to the present invention, in which a first connecting rod of a piston and a piston is formed in one cylinder chamber, and a first connecting rod is reciprocated through a hole in one side wall of the cylinder chamber, Both ends of the inside of the cylinder chamber portion to be moved and the cylinder chamber to close the piston portion heat the valve portion cylinder in the hole where the air can be taken in and out and the valve in which the valve can be opened and closed by the gas fire And the valve is opened and closed by a control unit for opening and closing the cylinder chamber in which the valve is closed in the cylinder chamber on the side where the air in the cylinder chamber divided by the piston is heated and the cylinder chamber in which the air on the opposite side is opened alternately, I'm going to exercise.

FIG. 2 is a cross-sectional view of another heat pipe according to the present invention, in which a heat radiating plate is formed on a piston in a manner of applying heat to a cylinder chamber, and a heat shield plate in a piston is formed, And the gas nozzle, the heat sink, and the first connecting rod are formed as a gas pipe, a flexible gas pipe connects between the gas pipe and the first connecting rod, the locked state of the gas pipe and the open state of the gas pipe are input to the control unit, A control means for outputting a signal for opening and closing the gas pipe, and a shimming means for igniting the gas, such as a servo motor, which operates according to a signal outputted from the control means and opens and closes the gas pipe. While one of the valves is closed, the heat generated in the piston A valve is formed at both ends of the solenoid valve when the solenoid valve is formed in the piston so that the valve is opened to the side where the valve is closed and the valve is closed when one of the valves is opened. When the solenoid valves are formed at both sides of the piston, the valves are formed at the ends of the solenoid valves. While the valves of the ports formed at both ends of the cylinders are open, And the valve of the port formed at both ends of the cylinder is opened and closed to be inputted to the control unit as an electric signal and the control unit controls the valve of the piston as the cylinder, Of the valve Top and bottom faces outputs an electrical signal to be opened and closed, is closed in accordance with the output signals will be the opening and closing valve operating means

FIG. 3 is a cross-sectional view of another heat pipe according to the present invention, in which air heated by a heating unit blows hot air by a nozzle along a pipe to plant a plurality of blades or wings on the circumference of the rotating body, The turbo-type turbine is formed in an outer shape in which a nozzle is formed in an outer shape such as a cylindrical shape and a portion except for a portion where an air hole is formed in an upper portion or a portion where an exhaust pipe is formed in an air hole is closed,

FIG. 4 is a cross-sectional view of another heat pipe according to the present invention. FIG. 4 is a cross-sectional view of another heat pipe in which one partition wall is vertically formed in a space such as one closed hexahedron and the center of one surface of a hexahedron, to form large holes and two holes of each angle is open, the side of one of the valve such as a solenoid valve, the other is closed, and the structure other end is open, one side is closed wall without opposite the large holes in the partition wall of the drone One or more small exhaust holes for generating a thrust are formed, and a heating part in which a gas fire or a hot wire for heating the inside of the hexahedron is formed is formed inside or outside the hexahedron, or a part or all of the hexahedron Is formed of a transparent material such as glass to form a heating part in which the inside of the hexahedron is heated. When one side of the outer side of the hexahedron is opened, the other side is closed and the other side is closed. A control unit is formed,

5 is a sectional view of the solenoid valve when the solenoid valve is moved

Figure 6 is a perspective view of an aircraft of the present invention

FIG. 7 is a perspective view of an aircraft propelled by the heat engine of the present invention, and is a perspective view of the heat engine of FIG. 4 and FIG. 5 mounted thereon

FIG. 8 is a perspective view of an aircraft propelled by another heat engine of the present invention, and is a perspective view with a propeller mounted on the central axis of the heat engine of FIG. 3. FIG.

1: Closed cylinder 2: Piston
3: hole 5: valve
10: fire 11: electromagnetic coil
15: movable iron core 20: insulation
21: flexible gas pipe 25: gas cylinder
30: crankshaft 31: link joint
32: second connecting rod 33: first connecting rod
35: blade 50: piping
51: Nozzle 52: Turbine
53: Gas pipe 55: Exhaust hole
70: wheel 71: exhaust pipe
72: Rudder 73: Second Wing
75: solenoid valve 76: wing
77: heat sink 78: propeller

Claims (18)

The first connecting rod of the piston and the piston is formed inside the one cylinder chamber of the dron in which the wing and the tail wing are formed and the first connecting rod is connected to the cylinder chamber The cylinder chamber portion which reciprocates through a hole in the one side wall of the cylinder chamber and both end portions of the cylinder chamber in which the piston portion is closed form a hole through which air can be taken in and a valve capable of opening and closing the hole A portion of the cylinder chamber is made of a transparent material such as glass or the like so that the cylinder portion of the valve of the hole is formed by heating or heating by gas or gas or by a heat sink or the like or by the greenhouse effect A heating portion in which the inside of the cylinder chamber is heated is formed, and the valve is divided into two by the piston A piston is reciprocated by a valve opening and closing control unit which alternately opens the cylinder chamber on the side where the air in the cylinder chamber is heated and the cylinder chamber in which the air on the opposite side is opened alternately is connected to the crankshaft, Is formed on one side of the aircraft and the heated air of the heating unit is formed on one side of the aircraft so that it flows into the body of the old-fashioned airplane. 2. The aircraft as claimed in claim 1, wherein the end of the first connecting rod is linked to the second connecting rod and the other end of the second connecting rod is linked to the crank shaft. A valve according to any one of claims 1 to 3, wherein a valve capable of opening and closing a hole capable of allowing air to flow in and out at both ends of the closed cylinder chamber is formed, and a solenoid valve is formed, The cam of the camshaft is rotated by a timing chain or a timing belt on a gear or a belt pulley directly connected to the shaft, the push rod is reciprocated by the cam, and the rocker arm is rotatably fixed by the push rod to the rocker arm shaft To be opened and closed by means of a spring that is pressed against a port of the cylinder. The method as claimed in any one of claims 1 to 3, wherein, in the method of applying heat to the cylinder chamber, a heat line heated by electricity is formed in the piston, a blocking plate is formed on the left or right or upper and lower sides of the heat line formed in the piston, Wherein the blocking plate formed in the cylinder block is divided into two by a piston, the cylinder chamber is opened in the cylinder chamber on the side where the air is heated and the cylinder chamber on the opposite side is closed alternately so that the piston reciprocates. The method as claimed in any one of claims 1 to 4, wherein, in the method of applying heat to the cylinder chamber, when a heat radiating plate is formed on the piston and a blocking plate is formed on the left or right or upper and lower sides of the heat radiating plate formed on the piston, And the gas nozzle, the heat sink, and the first connecting rod are formed as a gas pipe, a flexible gas pipe connects between the gas pipe and the first connecting rod, the locked state of the gas pipe and the open state of the gas pipe are input to the control unit, A control means for outputting a signal for opening and closing a gas pipe, and an ignition means for igniting the gas and a shy means such as a servomotor operating according to a signal output from the control means for opening and closing the gas pipe. . The apparatus as claimed in any one of claims 1 to 5, wherein one of the valves of the ports formed at both ends of the cylinder is closed while the plate formed on both sides of the hot line formed in the piston is opened to the side where the valve is closed, And a solenoid valve is provided at both ends of the solenoid valve when the solenoid valve is formed in the piston. When the solenoid valve is formed at both sides of the piston, Each valve is formed at the end of the valve. While the valve of the port formed at both ends of the cylinder is open, the plate formed on both sides of the hot wire formed on the piston is closed to the side where the valve is opened, And relay or the like, The valve of the port formed at both ends of the cylinder is opened and closed by an electric signal to the control unit, the control unit closes the valve of the piston when the valve of the cylinder is opened and outputs an electric signal to open the valve, Wherein the airplane is driven by a heat engine. The valve according to claim 3, wherein when the solenoid valve is formed and the solenoid valve is opened and closed by a solenoid valve when a hole capable of allowing air to flow in and out at both ends of the cylinder chamber closed and a valve capable of opening and closing the hole are formed, Wherein a rotation angle of the shaft is sensed by a sensor and input to a control unit, and a control unit outputs an opening / closing timing of each of the valves at both ends to operate the solenoid valve to open / close the solenoid valve. The body of an egg-shaped body such as an airship is filled with hot air, and a part or all of a material such as a hexahedron or the like such as a glass or the like is made transparent so as to be heated by heat or gas or a greenhouse effect in a dron having a wing and a tail- And the heated air is heated by the heating unit to blow hot air by the nozzle along the pipe to form a plurality of blades or blades in the circumference of the rotating body. A turbine type turbine that rotates the turbine at high speed and rotates is formed in a cylindrical shape or the like and has an outer shape in which a nozzle is formed and a portion except an air hole is formed in an upper portion or a portion in which an exhaust pipe is formed in an air hole is closed, Is formed at one side of the drones and formed integrally with the center axis of the turbine, So that the air is introduced into the opening of the body fashioned drone aircraft it is propelled by a heat engine, characterized in that formed on one side of the drone. In the airplane where wings and tail wings are formed, hot air is filled in the body of an egg-shaped body such as an airship
A large hole is formed at the center of one surface of a hexahedron located at the front of the inside of the hull of the dron which forms one longitudinal bulkhead in a space such as one closed hexahedral, is formed in one side is open, the other is closed and the other end is open, one side is a closed structure, and the walls do not have opposite the large hole of the partition wall is a small air exit for generating the thrust of the aircraft at least one of the valve such as a solenoid valve And a part or all of a material such as a hexahedron is formed of a transparent material such as glass so that a heating part in which a gas fire or a hot wire for heating the inside of the hexahedron is formed is formed inside or outside of the hexahedron or is heated by the greenhouse effect A heating part in which the inside of a hexahedron is heated is formed, and when one side of the outside of the hexahedron is opened, Is closed and the other end is open, one side is closed, the control unit is formed and a wall heated air portion heating does not have opposite large hole in the partition wall of the air heated by heating element other than the air that is discharged to the small air exit opening fashioned aircraft Wherein the airplane is formed on one side of the drones so as to flow into the body. The aircraft as claimed in claim 9, wherein an exhaust pipe is formed in a small exhaust hole formed in a wall surface without a large hole. A large hole is formed in the center of one surface of a hexahedron or the like which forms one vertical partition in a space such as one closed hexahedron or the like and faces a partition wall, and each of the two holes has a solenoid When a solenoid valve is opened when one side is opened by the valve such as a valve and the other side is closed and the other side is opened, a large valve is formed at both ends of the solenoid valve. When the solenoid valve is opposed to the diaphragm A switch for outputting an electric signal interlocked with the operation of the switch for lighting the solenoid valve;
When the solenoid valve of the control unit opens one side of the hexahedron facing the partition and the other side of the partition, the time is outputted as an electric signal from the counter for calculating the time, And a valve controlling means such as a solenoid valve for outputting an electric signal so that one side is closed when the other is closed and the other is closed and operating according to a signal outputted from the control portion so as to close the valve. Aircraft. 12. An aircraft propelled by a heat engine according to any one of claims 1 to 11, characterized in that the valve is formed by a valve of an insulating material. The aircraft as set forth in any one of claims 1 to 12, wherein a wheel is formed on a lower side surface of a hexahedron or the like. The method as claimed in claim 8, 9, or 13, wherein hot air is blown by the nozzle along the tube to turn a turbo-type turbine into which a plurality of blades or blades are planted and rotated at a high speed around the circumference of the rotor Characterized in that the pipe connected to the nozzle is connected to the small exhaust hole with a large hole-free wall opposite the bulkhead of any one of claims 9 to 13. 15. The refrigerator according to any one of claims 1 to 14, wherein an upper part of an egg-shaped body such as an airship is provided with a large hole and a valve for releasing hot air, such as an upper part of a hot air balloon, And an electric signal for opening and closing the valve is outputted from the control unit, and the opening and closing means for opening and closing the valve by operating according to an electric signal for opening and closing the valve are formed. In the airplane where the wing and tail wing are formed, the upper part of the egg-shaped body such as an airfoil is provided with a large hole in which the hot air can escape and a valve A switch for outputting an electric signal in conjunction with the operation of the switch; An electric signal for lowering the altitude is input to the control unit and an electric signal for opening and closing the valve is outputted from the control unit. The electric signal is operated according to the electric signal for opening and closing the valve to open and close the valve. Wherein an operation signal of the motor is outputted from the control unit, and the motor is driven according to the output signal, so that the thrust is obtained by the motor. The method of any one of claims 1 to 16, wherein the adjustment of the wing and the tail wing is performed by GPS, the current position is input by the GPS, and the destination point is input to the control unit, and the control unit adjusts the angle, rudder, A control means for outputting a signal for adjusting the angle by calculating an adjustment angle, and a rudder for adjusting the angle of the rudder, the elevator and the auxiliary wing and the angle adjusting means for the elevator and the auxiliary wing, The aircraft being propelled by a heat engine. 18. An aircraft driven by a heat engine according to any one of claims 1 to 17, wherein a bottom part of an egg-shaped body such as an airship is formed with a structure capable of holding and fixing an object to be carried.

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