JPH09301289A - Flying body floating by reducing atmospheric pressure on airframe upper side - Google Patents

Abstract

PROBLEM TO BE SOLVED: To float a flying body by eliminating the air of the part of a rotating blade by its rotation to reduce the upper pressure. SOLUTION: This flying body is formed of an airframe 1 and rotating blades 2, 2', 2" of one stage or several stages. The rotating blades 2, 2', 2" have a shaft 3, and are rotated at high speed by an engine. By this action, a pressure of about 1kg/cm<2> is added to the whole body since the airframe 1 is in the atmosphere. Namely, the airframe 1 is pushed down in the upper part and pushed up in the lower part. This is mainly the weight of the air by the earth gravity. The upper air is wiped by the rotating blades 2, 2', 2'' to reduce the pressure, whereby the airframe can be raised or advanced by the pushup from the lower part. In order to slowly and rapidly move the rotating blades 2, 2', 2", an equipment or a computer is utilized. When the airframe 1 is advanced at high speed, a negative pressure is caused in the lower part to work a pressure for pulling it down. A soft sheet 4 or the like is mounted on the lower part to prevent this, whereby the air flow is smoothed.

Description

Detailed Description of the Invention

[0001]

BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a flying body that uses power to initially carry a small number of people, objects, etc. and fly freely in the sky.

[0002]

2. Description of the Related Art There are airplanes and helicopters.

[0003]

It is desirable to fly in the sky instead of a car. In addition, since the current flight body uses large wings and propellers, it has a large bulk. The present invention is directed to making a less bulky vehicle.

[0004]

[Structure and Action for Solving the Problems] The figure shows the main part of this flying body. It is called the flying body (1) and the following aircraft, and one or several stages of rotary wings (2) (2) '( 2) 'and other special elements are simply referred to as a rotary blade (2). The rotary blade (2) has a shaft (3) and is rotated at high speed by the engine. Since the fuselage (1) is in the atmosphere, the action exerts a pressure of about 1 Kg / cm ^{2 on} the whole. In other words, it is pushed down at the top and pushed up at the bottom. This is, of course, the weight of air due to earth gravity. If the air in the upper part is blown off by the rotary blades (2) to lower the pressure, it can be raised or advanced by pushing up from the lower part.

A person, an object, and a device are placed on the machine body (1), and the total weight is 500 kg, and the machine body (1) has a diameter of 15
If 0 cm, the atmospheric pressure above and below the fuselage (1) is (1
50 cm / 2) ² × π × 1 Kg / cm ² = 17t662
Since it is Kg, 50 is required to levitate this aircraft (1).
The upper air pressure of 0 kg or more should be eliminated by rotating the blade (2). In other words, if the upper pressure is set to 17t162Kg or less and the total weight of the airframe (1) is 500Kg, and the lower pressure becomes lighter than 17t662Kg, the airframe (1) will levitate, so if the rotation speed of the wing (2) is changed. , Ascending, flying and descending can be done freely.

[0006]

[Procedure] We will utilize the technology of equipment, computers, etc. that move the rotor blade (2) freely and slowly.
The central plane shape of the airframe (1) may be a spindle shape in the traveling direction. When the rotor blades (2) and (2) 'have two stages, they can be turned upside down to prevent the airframe (1) from interacting with the engine. When this machine body (1) travels at high speed, a negative pressure is generated in the lower part, and a downward force is exerted. To prevent this, if you attach a dotted flexible sheet (4),
The air flow becomes smooth. This sheet-like material (4) is made to naturally fold when landing. When the blade (2) is rotated at a high speed, air is scattered outward by centrifugal force, but the reaction can be used by changing it downward by attaching an appropriate cover (5). In order to increase the speed, the lower wing (2) 'may be oriented downward as shown in the figure, and the air may be ejected downward during the rotation, in addition to the acceleration of the engine. Although tilting the airframe (1) to change the direction is the same for other aircraft, the two-stage wing utilizes the sympathy phenomenon that occurs by accelerating one side. You may attach a rudder. The inventor can freely choose other changes and modifications.

[0007]

[Effects of the Invention] Nowadays, there are 10,000 deaths due to automobiles, 12 trillion yen / year due to traffic congestion, and 2.7 trillion yen in fiscal 1996 only for national budget for road improvement. The sky is hundreds of times larger than a road, and commute
Most of the above-mentioned defects can be prevented by using this for the purpose. Since the space is small, it is easy to store, and you can also use the roof of the building. You can reach your destination straight by pressing one button at the time of departure. And so on.

[Brief description of drawings]

FIG. 1 is a central cross-sectional view showing the main part of the aircraft.

2] Top plan view

[Figure 3] Top center outer view

[Explanation of symbols]

 1 Aircraft 2 Rotor 3 Rotor Axis 4 Sheet-like 5 Cover

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[Procedure amendment]

[Submission date] September 5, 1996

[Procedure amendment 1]

[Document name to be amended] Drawing

[Correction target item name] All figures

[Correction method] Change

[Correction contents]

FIG.

[Fig. 2]

[Figure 3]

Claims (1)

[Claims] 1. A rotor (2) comprising a flying body (1) on which a person, an object, etc. is placed, and one or several stages of powered rotors (2), (2) '(2)'. The air vehicle (1) that flies in the sky by eliminating the air in that part and lowering the upper pressure.