JP3191468U - Reaction flight propulsion control machine - Google Patents

Abstract

PROBLEM TO BE SOLVED: To easily operate anyone without difficult flight training, to facilitate lifesaving and fire extinguishing activities even in an emergency such as a fire on a higher floor, and to reduce congestion and traffic accidents caused by ground traveling. We provide a flying aircraft that uses the principle of reaction flight propulsion. SOLUTION: This machine body 1 is installed inside the front and rear of a cockpit in which horizontal electric motors 2 and 4 and horizontal rotary blades 3 and 5 for directly achieving horizontal levitation are located at the center of gravity. Immediately after ascending directly from the rotating wind force, the vertical electric motors 6 and 7 mounted on the left and right sides of the cockpit can be indirectly forwarded and raised by the simultaneous left and right rear rotations 6a and 7a, and the left and right simultaneous forwards. Indirect backward climbing is performed by rotations 6b and 7b, and four indirect direction changes are performed from rotations 7a, 6a, 7b and 6b on one side of the vertical electric motors 6 and 7 on the left and right sides of the cockpit to perform four indirect direction changes. It is also useful for saving lives on the floor and solving traffic problems on the ground. [Selection diagram] Fig. 1

Description

  The present invention is a propulsion method for a flying type aircraft that flies in the sky with wind power from a horizontal electric motor and rotor blades, in addition to direct lift by wind power, in order to simplify take-off rise and direction change during air flight. The method of indirect rise and indirect direction change by reaction power of the reaction drawn from the rotation of the vertical type motor is proposed. The present invention relates to the principle of reaction flight propulsion control for performing propulsion control during flight by utilizing reaction force of reaction from rotation, so that a person can actually get on a flying aircraft and fly freely.

  In the present invention, an example of a flying type aircraft is presented as a form for flying in the sky, but the flight propulsion method of this aircraft is different from that of conventional airplanes and helicopter airplanes, as in the case of maneuvering them. It is intended to make it easy for anyone to fly and fly without any complicated and difficult knowledge or special training.In other words, after the direct rise by the wind power of the rotor blades, Using the reaction force of the reaction from the rotation of the vertical electric motors on the left and right, it is easier to tilt the aircraft freely in the air and indirectly move forward and backward and change direction during flight propulsion. Made possible by reaction flight propulsion control.

  Although the flight propulsion method of this aircraft seems to have the potential to reduce traffic congestion and traffic accidents on the ground by passenger cars, airplanes and helicopters have significant disadvantages as well as the advantages of flying in the air. Airplanes can not take off and land without a runway and cannot stop in the air, and helicopters can take off and land without a runway and can hover in the air When trying to save lives even in the event of a fire, etc., the rotating wings that protrude horizontally from the aircraft approach the side of the building etc. directly from the side against the life that the propeller disturbs and seeks rescue There are disadvantages that cannot save lives, but this is also possible if the rotating wings are rotating inside the flying aircraft.

  If the helicopter has the current structure, if the major axis of the rotor blade is shortened, there is a problem that direct flight of the airframe and direct direction change are structurally difficult and the original flight activity becomes difficult. If the aircraft itself can be lifted by the wind force, the reaction force of the reaction is extracted from the rotation of the vertical electric motors installed on the left and right of the cockpit at the center of gravity, and the aircraft is tilted to move forward. Indirect climbing such as climbing and retreating is possible, and the reaction force of the reaction is extracted from the rotation of one of the left and right sides of the vertical electric motor, and the right turn forward, right turn backward, left turn forward and left turn during flight Indirect direction change such as retreat is also possible, and reaction flight propulsion control can solve the problem.

  As described above, using the principle of reaction flight propulsion control of the present invention, the aircraft can be tilted freely forward and backward, left and right in the air to achieve indirect rise and reverse rise, and from this principle Although it is easy for anyone to perform indirect direction change and fly freely in the sky, although there is a history of flying cars etc. overseas, there are no flying aircraft using the principle of the present invention until now, The technology of flight propulsion control as a flying car is actually blocked worldwide, and the principle of the reaction flight propulsion control of the present invention is the flight type aircraft that adopts this invention in the state of waiting for technology, If it is possible to spread throughout the world in a wide area, humans will be greatly freed from the problems of traffic congestion and traffic accidents on the ground, and as a problem for high-rise fires from outside the sky Fire fighting A flight created from the principle of reaction flight propulsion control of the present invention as a next-generation flying vehicle that can respond quickly to life and lifesaving, and also considers the natural environment by using electric energy as the power source The type aircraft can greatly help.

  The flying aircraft of the present invention basically has the center of gravity in the cockpit, but there are horizontal electric motors and rotor blades in the front and rear of the aircraft. The aircraft will rise directly and rotate the rotor blades in the opposite direction in order to stabilize the aircraft from side effects due to the effects of the law of action and reaction. Immediately after this, starting from the center of gravity position of the cockpit, the reaction force of the reaction from the rotation of the vertical electric motor on the extension line of the left and right horizontal axis is pulled out, It tilts backward and rises, and the left and right sides are tilted diagonally, and this is the position where the aircraft tries to stay when it is tilted diagonally by the reaction force of the reaction, which was stable horizontally in the air. Part of the energy is reduced, and the power moves in an instant The momentary acceleration in this case is equivalent to the fall acceleration principle of the constant acceleration free fall motion, and even when decelerating from the air resistance, it is intermittently vertical. If the electric motor of the type is rotated repeatedly, the reaction force of the reaction will be drawn out as many times as possible, and the aircraft will rise and accelerate. We need enough wind power to stay.

  Hereinafter, an embodiment will be described with reference to the accompanying drawings. As the first step, the reaction aircraft propulsion control direct ascent of the aircraft 1 and the second step of the indirect forward rise 11 and reverse rise 12, the reaction of one aircraft is formed of a strong lightweight material on the outside. The entire body 1 of the flight propulsion control, the left side is the front of the aircraft and the right side is the rear. First, in order to raise the aircraft 1 directly, From the simultaneous rotation with the front and rear rotating directions of the horizontal electric motor 4 in the rear, the airframe of the front horizontal rotary blade 3 and the rear horizontal rotary blade 5 floats horizontally, and immediately after that the center of gravity position 9 The reaction force of the reaction is derived from the rotation of the simultaneous rearward rotations 6a and 7a of the left vertical electric motor 6 and the right vertical electric motor 7 on the extension line of the left and right horizontal axis of the cockpit 10 which is Tilt diagonally Either the forward lift 11 is achieved, or the reaction force of the reaction is derived from the simultaneous forward rotation 6b, 7b of the left and right vertical electric motors 6, 7, and the vehicle body is tilted rearward and tilted backward indirectly 12 The battery 8 is basically installed at the bottom of the cockpit 10 at the center of gravity 9.

  After the main body 1 inclines the airframe obliquely in the second stage and indirectly performs forward ascent 11 and reverse ascent 12, the center of gravity position 9 is used to indirectly change direction during air propulsion as the third stage. By rotating one side of the left and right vertical electric motors 6 and 7 on the extension line of the left and right horizontal axis of the cockpit 10, four indirect direction changes 13, 14, 15 and 16 can be achieved. That is, the reaction force of the reaction is drawn from the rotation of the rearward rotation 6a of the left vertical electric motor 6 of the cockpit 10, and the airframe is tilted forward to the right to indirectly perform the right turn forward 14, and the left vertical electric motor 6 The reaction force of the reaction is extracted from the rotation of the front rotation 6b of the vehicle, and the airframe is tilted rearward to the right to indirectly perform the right turn 16 and the reaction from the rotation of the rear rotation 7a of the right vertical electric motor 7 of the cockpit 10 Pull out the reaction force of Inclining the airframe forward to the left and indirectly making a left turn forward 13, pulling back reaction force from the rotation of the forward rotation 7 b of the right vertical electric motor 7, and inclining the airframe to the left rear and turning left indirectly The aerial stop during the flight propulsion 15 is performed while the aerial stop is performed by simultaneously rotating the vertical electric motors 6 and 7 installed on the left and right sides of the cockpit 10 in the same direction. The forward rotation 6b of the vertical electric motor 6 and the forward rotation 7b of the right vertical electric motor 7 are simultaneously rotated to incline the main body obliquely backward to stop in the air. By simultaneously rotating the rear rotation 6a and the rear vertical rotation 7a of the right vertical electric motor 7, the main body is tilted forward and the air stop is achieved.

  The direct descent as the fourth stage of the main body 1 of the reaction flight propulsion control suppresses the outputs of the horizontal electric motors 2 and 4 installed inside the front and rear of the cockpit 10 at the same time, Directly descends while lowering the wind power of the installed rotor blades 3 and 5.

It is a bird's-eye view top view which shows one Example of the reaction flight propulsion control machine of this invention. It is side surface sectional drawing which looked at this airframe which uses the reaction flight propulsion principle of this invention from the side. It is each schematic diagram of the flight propulsion method using the reaction flight propulsion control of this invention.

DESCRIPTION OF SYMBOLS 1 Body of reaction flight propulsion control 2 Front horizontal electric motor 3 Front horizontal rotor 4 Rear horizontal motor 5 Rear horizontal rotor 6 Left vertical motor 7 Right vertical motor 8 Battery 9 Center of gravity 10 Pilot's seat 11 Side view of ascending forward 12 Side view of ascending backward 13 Plan view of left turn forward during flight propulsion 14 Plan view of right turn forward during flight propulsion 15 Plan view of left turn backward during flight propulsion 16 Flight propulsion Top view of right turn backward

Claims (2)

  The present invention is for a flying type aircraft propelled by wind power of rotor blades to fly freely in the sky, and presents a flight propulsion method using the reaction force of the reaction of a rotating electric motor, that is, The principle of reaction flight propulsion control is to control the propulsion rise and change of direction of the flying aircraft focusing on the law of action and reaction, which is the effect on the natural law of a rotating electric motor. From take-off to landing 4 The aircraft flies in the sky with two stages, and the shape and design of the aircraft can be freely created, but the present invention explains this principle by taking one flying type aircraft as an example, and it has a cockpit seat in the center of the aircraft There are horizontal motors and rotors for floating the fuselage in the front and rear interiors of the center of gravity, and the right inner part overlaps the extension of the left and right horizontal axis of the cockpit. And the left side of the aircraft Vertical electric motors are fixedly mounted one by one, using the reaction force of the reaction drawn from the rotation of the left and right vertical electric motors after a direct rise in the wind power of the rotor blades. Starting from the cockpit at the center of gravity, the aircraft is tilted forward, backward, left and right to perform forward ascent, backward ascent and direction change during flight, facilitating indirect propulsion and indirect direction change Left and right vertical electric motor equipment installed for flying aircraft using the principle of reaction flight propulsion control.   By using the principle of reaction flight propulsion control of the present invention, it is intended that the flying type aircraft can be freely propelled from this principle regardless of the shape or design, but basically it is controlled to the center of gravity position in the center of the aircraft An indirect flight principle in which a seat is set and propulsion is controlled, and the reaction force of the reaction is extracted from the rotation of the vertical electric motor installed on the left and right from the center of gravity immediately after the aircraft floats, and the lift and direction change The take-off, flight, and landing of this flying type aircraft are from the first stage to the fourth stage, and the first stage is the first step by the horizontal electric motor and the direct rise by the wind power of the rotor blades, and the second stage This is an indirect rise due to the reaction force of the rotation reaction of the vertical electric motor located on the left and right from the center of gravity, which is caused by tilting the aircraft pushed upward by wind force with the reaction reaction force. Because the potential energy to stay in place is instantly transferred to kinetic energy, the aircraft rises diagonally so that it can be lifted from bottom to top in a natural law. It is also used for aerial stop of forward and backward during propulsion, and as a third stage, it performs indirect direction change by extracting reaction reaction force from one side rotation of the vertical electric motor on the left and right, that is, flight propulsion It enables middle right turn forward, right turn backward, left turn forward, left turn backward, etc., and as a fourth step, the output of the horizontal electric motor is suppressed for landing and the wind power of the front and rear rotors is lowered at the same output However, the purpose of this section is the reaction for the flying type aircraft to fly freely in the sky using the reaction force of the reaction drawn from the rotation of this vertical electric motor How the rows propulsion control.

Images