CN103303477A - Novel unidentified flying object (UFO)-like aircraft - Google Patents

Abstract

The invention relates to an uncommon aircraft in the field of aerospace. The aircraft is completely different from conventional aircrafts in the principle of generating ascending power, and the weight of the aircraft is overcome by completely depending on the spinning centrifugal force relative to the earth generated by high-speed rotation of a power shell layer. Therefore, the aircraft does not need aerostatic buoyancy, a screw propeller or an air injection (or rocket) engine nozzle. The whole aircraft body is totally closed, and the shape can be made into the dish-shaped UFO in the legends. In addition, the aircraft can employ various fuels and is particularly suitable for employing nuclear fuels. In order to allow the aircraft to have high maneuverability, multiple recoil nozzles can be additionally arranged. Compared with the traditional aircraft, the aircraft has the advantages that the fuel service efficiency is higher, even the aircraft can be taken as the dish-shaped UFO in the legends.

Description

The course of new aircraft of a kind of " class UFO "

Technical field:

The present invention relates to a kind of course of new aircraft of space industry, and be a kind of the generation aspect the principle of lift and the diverse aircraft of present existing mode.In addition, aircraft of the present invention can use various fuel, especially is more suitable for using atomic fuel.Even can think that the present invention is a kind of dish shape UFO aircraft.

Background technology 1:

The common principle of classification of conventional aircraft driving engine has two kinds [1]: the principle of whether participating in engine operation and driving engine generation thrust power by air.

Whether must work by air by driving engine, aircraft engine can be divided into air breathing engine, rocket jet formula driving engine two classes.

Air breathing engine is called for short airbreathing motor, the oxidizer (ignition promotor) that it must suck air acts as a fuel, thus can not arrive space work outside the dense atmosphere, can only be as the driving engine of aerocraft.General said aero-engine namely refers to this class driving engine.As the difference according to the airbreathing motor principle of work, airbreathing motor is divided into piston engine, gas turbine engine, ramjet driving engine and pulsation jet engine etc. again.

Rocket jet formula driving engine is a kind of driving engine that does not rely on air work, and spacecraft is owing to flying to the exoatmosphere, so this driving engine must be installed.It also can be used as the boosting power of aerocraft.By the energy difference that forms gaseous blast kinetic energy, rocket engine is divided into chemical rocket engine, electric engine and nuclear rocket engine etc. again.

By the principle difference that produces thrust power, the driving engine of aircraft can be divided into direct antagonistic force driving engine, indirect antagonistic force driving engine two classes again.

Directly the antagonistic force driving engine is to utilize to spray high velocity air backward, and the antagonistic force that produces forward advances aircraft.Directly the antagonistic force driving engine is jet engine again, and this class driving engine has turbojet, ramjet driving engine, pulsation jet engine, rocket jet formula driving engine etc.

Indirectly the antagonistic force driving engine be drive wind stick, helicopter by driving engine the rotor rotation to the air work done, when making air accelerate that (downwards) flows backward, air advances aircraft to screw propeller (rotor) generation antagonistic force.This class driving engine has piston engine, propeller turbine, turboaxle motor, turbo-propeller Duct-Burning Turbofan etc.Turbofan engine is existing direct antagonistic force then, and indirect antagonistic force is also arranged, but often it is incorporated into direct antagonistic force driving engine one class, so also be called turbofan.

By above-mentioned introduction, our can be perfectly clear type and flight theory thereof of conventional aircraft driving engine.

Background technology 2:

Compare with above-mentioned traditional aircraft, what I designed is a kind of course of new aircraft of various conventional, and this aircraft has sufficient theoretical foundation, and the discovery of this theoretical foundation is because an accidental inspiration fully, this is a theory of being ignored by people, and particular content is as follows:

[" theorem "]: on earth, an object (also can be placed on it in the artificial vacuum vessel) that is parallel to the horizontal surface rotation, if the rotating speed of the particle of the suitable quality in this object all surpasses the first cosmic velocity of the earth, the result of this high speed rotating of this object just necessarily can produce the rising phenomenon of built on stilts so.

[definition]: in order to come with the difference of translation centnifugal force, I am called the spin centnifugal force to the object parallel, horizontal face described in top " theorem " because rotating this centnifugal force with respect to the earth that produces the rising phenomenon at a high speed.

[proof]:

At first above-mentioned " theorem " specialized, description thes contents are as follows:

Found a vacuum environment at ground level, a CD (card of CD is parallel to horizontal surface) of rotation is at a high speed wherein arranged, the centnifugal force summation F that each particle produces with respect to the earth on this CD is asked in examination _CWhat are? does examination ask centnifugal force summation that each particle on this CD produces with respect to the earth and the ratio λ of the weight of CD what are again in addition? (relative parameters setting of this problem is as follows)

Topic establishes 1: the quality of CD is m in this topic, and disk thickness (or claiming height) is h, and the outer radius of CD is r ₂, the interior pore radius of CD is r ₁, the density of CD material is ρ; Acceleration due to gravity is g, and earth radius is R, and the first cosmic velocity is V ₀Pi

Topic establishes 2: 52 times of fast CD maximum speed ω ≈ 180 * 2 π=1.1 * 10 in the reality ³(radian per second), the CD radius r ₂=6.0 * 10 ^-2(rice), the interior pore radius of CD is r ₁=7.5 * 10 ^-3(rice), the first cosmic velocity of the earth is V ₀=7.9 * 10 ³(meter per second)

(top " theorem " specific problem is calculated, and process is as follows):

(1), CD can be regarded a hollow cylinder (being commonly called as " pipe ") as, and be the hollow cylinder that highly less, wall thickness is bigger.We can downcut a hollow cylinder κ coaxial with CD arbitrarily on CD, the inner radius of supposing κ is r, and wall thickness is Δ x, makes Δ x → 0, and the volume of κ is exactly 2 π r h Δ x so, and its quality is exactly 2 π r h ρ Δ x, and the linear velocity of κ is υ _κ, further, we can obtain κ with respect to the centnifugal force of the earth

$f_{\mathrm{\κ}}=m\frac{{\mathrm{\υ}}_{\mathrm{\κ}}^2}{R}=m\frac{{\left(\mathrm{\ωr}\right)}^2}{R}=2\mathrm{\πrh\ρ}\frac{{\left(\mathrm{\ωr}\right)}^2}{R}\mathrm{\Δx}$

After the arrangement: $f_{\mathrm{\κ}}=\frac{2\mathrm{\πh\ρ}{\mathrm{\ω}}^2{r}^3}{R}\mathrm{\Δx}$

Utilize the way of integration, we just can obtain whole Zhang Guangpan with respect to the centnifugal force F of the earth _CIntegral formula:

$F_C=\underset{\backslash x\→0}{\lim }\underset{r_1\≤r\≤r_2,x\∈r}{\mathrm{\Σ}}{f}_{\mathrm{\κ}}=\underset{r_1}{\overset{r_2}{\∫}}\frac{2\mathrm{\πh\ρ}{\mathrm{\ω}}^2{x}^3}{R}\mathrm{\Δx}=\frac{2\mathrm{\πh\ρ}{\mathrm{\ω}}^2}{R}\underset{r_1}{\overset{r_2}{\∫}}{x}^3\mathrm{\Δx}$

Try to achieve at last: $F_C=\frac{\mathrm{\πh\η}{\mathrm{\ω}}^2}{2R}(r_2^4-r_1^4)$ ……①

(2), the weight G=mg when CD is static, also can represent with following conversion relation:

$G=\mathrm{mg}=m-\frac{{V_0}^2}{R}=\frac{\mathrm{\πh\ρ}{V}_0^2}{R}(r_2^2-r_1^2)$ ……②

The ratio of the weight when (3), whole Zhang Guangpan is static with CD with respect to the centnifugal force of the earth 3.

1., 2. two formula substitutions 3. abbreviation get:

4.

The data substitution in " topic establishes 2 " 4. formula calculate and can obtain: λ ≈ 3.5 * 10 ^-55.

(4), the above-mentioned process of solving has obtained two important results F that we need _CAnd λ, especially λ, observe this numerical value of λ (λ ≈ 3.5 * 10 ^-5), we can obtain as drawing a conclusion:

[inference 1]: on earth horizontal surface, 52 times of fast CDs when vacuum environment high speed is rotated, 4/100000ths of the weight during generation static not as good as it with respect to the spin centnifugal force of the earth.

[inference 2]: the disk of a radius r is parallel to horizontal surface and rotates at a high speed, as rotational speed omega 〉=0.226V ₀During/r, the spin centnifugal force of this disk will be greater than the gravity of himself.(V wherein ₀Be the first cosmic velocity)

[inference 3]: the size of supposing CD enlarges 170 times (namely in proportion, radius reaches 10 meters), rotating speed remains 52 times of speed (get its maxim: 180 revolutions per seconds), so, the lift that this moment, this huge CD produced just can overcome the gravity of the earth, slowly leaves the earth.If allow this huge CD radius and rotating speed comprehensively increase, namely the product of radius and rotating speed increases, so it leave the earth will become be more prone to, more fast.

[inference 4]: " theorem " described principle is fit to make butterfly-shaped UFO aircraft very much.

[inference 5]: what dish shape UFO overcame that the main mode of celestial body gravitation utilizes should be exactly " theorem " described principle.

[inference 6]: it is little of microcosmic particle to arrive celestial body greatly, as long as they have spin motion, the interaction force between them (no matter being attractive force or repulsive force) just is bound to be weakened, and the degree that weakens is relevant with the intensity of spin.Therefore, our physics can consider to recomputate the big object of which movement equation of spin intensity from now on, make theoretical conclusion accurate more.

Summary of the invention:

Utilize above-mentioned " theorem ", we can design this conventional aircraft that is different from---and rely on the power shell of aircraft self to rotate at a high speed fully, and then generating the spin centnifugal force of the relative earth, this special lift can help aircraft to overcome the strength that self gravitation forms upward movement.Therefore, this aircraft does not need air lift force, does not need screw propeller, does not need jet (or rocket) engine nozzle yet, and entire body is totally-enclosed, and profile can be forged into legendary dish-shaped UFO shape.Certainly, if in order to allow this aircraft have more manoevreability, can set up the spout of several recoils.

The specific embodiment:

Annotate: make this aircraft, key is to manage to allow this aircraft self rotate at a high speed! Can realize with following two kinds of schemes.

The parts that [scheme 1] produces rising power all are solid materials.

Make the aircraft of this high speed rotation, need to pay close attention to following three technical essentials at least:

1, to adopt high-intensity material

In order to prevent that this aircraft from causing disintegrating because rotating the powerful centnifugal force of generation at a high speed, just must the high-intensity material of employing.

2, two of this aircraft power shells must mutual adhesion---" outer moving " shell and " interior moving " shell

I am called " outer moving " shell and " interior moving " shell to this NA two power shells mutually of this aircraft respectively.Can use between these two power shells certain fuel discharge (or conversion) thus energy these two power shells are formed repulsive interactions produce power and realize its two rotatablely moves, if for example aircraft uses atomic fuel, can at first change into electric energy to nuclear energy and then between the conductive coil of these two power shells, form the electromagnetism repulsive interaction, allow these two shells produce backward rotation.In addition, in order to allow these two shells realize rotation at a high speed, just need the mode of motion of inboard " interior moving " shell that two kinds of forms will be arranged simultaneously: the one, rotate in same plane with " outer moving " shell in its outside, the 2nd, to carry out repeatedly 180 ° flip-flop movement with respect to previous plane of movement in good time.Just can finally realize the high speed rotation of two power shells so that accelerate repeatedly between these two power shells by the way.In addition, by the superconductor technology that nowadays reaches its maturity, can realize mutual adhesion fully between the shell.

3, be necessary two shells increasing---" kernel " shell and " vacuum " shell

If manned or Sheng is carried other biology, must increase a shell again---" kernel " shell (also can be called " operating room " shell or " kernel operations chamber " shell), its main characteristics is: can not rotate.

In addition, with the violent friction of air generation, can a shell that does not rotate be set at outermost, and for the power shell of inboard provides vacuum environment, can be called this one deck visually " vacuum " shell when rotating at a high speed for anti-stopping power shell.Certainly, if do not take windage into account and do not think to increase separately this " vacuum " shell, regarding above-mentioned " outer moving " shell here, said " vacuum " shell also is a kind of all well and good design.

The parts that [scheme 2] produces rising power mainly are fluent materials, for example: mercury, aviation oil.

Make the aircraft of this high speed rotation, need to pay close attention to following three technical essentials at least:

1, first main points of same " scheme 1 "

2, fluent material is as power " shell " layer (definite saying be called the flow at high speed layer)

Utilize express pump that the liquid of this " shell " layer the inside is carried out the in good time acceleration repeatedly of same direction, allow these liquid at high speed flow, thereby can allow this power " shell " layer produce the effect of rotation at a high speed.

Also can use for reference the electromagnetic induction technology (the perhaps electromagnetic induction technology of cyclotron) of electrical motor liquid is carried out the acceleration repeatedly in good time of same direction, allow these liquid at high speed flow, can make this power " shell " layer produce the effect of rotation at a high speed equally.

3, the 3rd main points of same " scheme 1 "

[prospect]

1, advantage is obvious: compare with conventional aircraft, and fuel service efficiency height, energy consumption is low, has at least following two aspects to find out:

(1), entire body can be designed to full-closed structure, like this, violent friction just can not take place with air in the parts of this aircraft the inside; In addition, because adhesion between the shell does not have frictional loss yet.

(2), the fuel of conventional aircraft is burden, and fuel can be used for producing the power of rising in aircraft of the present invention.

2, this aircraft is with after any the creating in top two kinds of schemes, and we mankind just can stride into the brand-new air age of similar UFO.

List of references:

[1] Baidu library " aero-engine classification and brief introduction ".

Claims (8)

1. Independent claims

   1. a course of new aircraft relies on the power shell of aircraft self to rotate the spin centnifugal force that generates the relative earth at a high speed fully, and this special lift can help aircraft to overcome the strength that self gravitation forms upward movement; This aircraft does not need air lift force, does not need screw propeller, does not need jet (or rocket) engine nozzle yet, and entire body is totally-enclosed, and profile can be forged into legendary dish-shaped UFO shape; Certainly, if in order to allow this aircraft have more manoevreability, can set up the spout of several recoils.

   Dependent claims
2. 2. two of this lift device of aircraft kinds of schemes, one is to use NA two power shells mutually: " outer moving " shell and " interior moving " shell; Two are to use fluent material or fuel as power " shell " layer.
3. 3. the mode of motion of " interior moving " shell of this aircraft---have two kinds of mode of motion simultaneously: the one, rotate in same plane with " outer moving " shell in its outside, the 2nd, to carry out repeatedly 180 ° flip-flop movement with respect to previous plane of movement in good time.
4. 4. " kernel " shell of this aircraft, this is the shell that can match, it is in the innermost layer of aircraft, this one deck is if not being used for or containing to carry other biology manned, it can rotate, otherwise just this " kernel " shell is designed to non-rotary form, so that other biological and people such as can live or drive inside for a long time at behavior.
5. 5. " vacuum " shell of this aircraft; this also is the shell that can match; it is the shell of protecting aircraft; it is in the outermost layer of aircraft; for the power shell of inboard provides vacuum environment; can prevent when the stopping power shell rotates at a high speed and air produces violent friction, also can be designed to a kind of non-rotary shell to it.
6. 6. " theorem " of the theoretical institute foundation of this aircraft.
7. 7. the definition of spin centnifugal force.
8. 8. 6 " inferences " of " theorem " of the theoretical institute foundation of this aircraft.