JPS6373302A - Propultion device for flying body - Google Patents

Abstract

PURPOSE:To realize sudden propelling, sudden stop, and orthogonal turn, by generating and controlling electromagnetic energy to give the variation of a curvature component in the neighborhood of a flying body, and setting a spatial distortion force generated in a space as the driving force of the flying body. CONSTITUTION:The flying body 1 is constituted of a disk-shaped body, and propelling parts 21-26 are provided at four of outer peripheral positions where the outer periphery of a disk is divided equally into four portions, and in the center position of the upper and the lower planes of the disk. Each of the propelling parts 21-26 is constituted by corresponding an electromagnetic energy generating means and a control means to control the above means to one to one. The electromagnetic energy generating means generates a magnetic field required to give the variation on the curvature component of the space in the neighborhood of the flying body 1, by a superconduction technology, etc. The control means controls the generating status of the electromagnetic energy, and controls the variation of the curvature component of the space locally, and sets the spatial distortion force generated in the space, as the driving force of the flying body 1. In this way, it is possible to perform the sudden propelling, the sudden stop, and the orthogonal turn, etc., for all of the directions from a state ceasing in the space.

Description

[Detailed Description of the Invention] (Industrial Application Field) The present invention relates to a propulsion device for flying objects (aircraft, manned rockets, etc.), and in particular, it controls the curvature component of space by powerful electromagnetic energy, and This invention relates to a new propulsion device that uses the generated space distortion force as a propulsion force.

(Prior art) Conventionally, the propulsion methods for flying objects include a method using the reaction of air flow by a propeller, a method using the reaction of the jet gas flow from an internal combustion engine such as a jet engine or a rocket engine, and a method using the reaction of plasma flow and ion flow. There are electric propulsion methods, etc.

(Problems to be Solved by the Invention) The conventional propulsion system for a flying object described above has the following problems.

(1) Although the amount of fuel consumed is large, the resulting propulsion speed is slow; for example, propulsion using a propellant gas flow (chemical rocket) is several tens of kilometers per second, and electric propulsion is several tens of kilometers per second.
The limit is +o/sec to 00, and the propulsion efficiency is poor. In addition,
In terms of thrust-to-weight ratio, it is 100 for chemical rockets, while it is 10-' to 10-3 for electric propulsion systems.
Very weak.

(2) As is clear from rockets, space shuttles, etc., most of the volume of a flying object (70-90%) is occupied by the propulsion device containing fuel, and the weight of the object (human, artificial satellite, etc.) to be flown is , the volume is limited.

(3) Propulsion methods using internal combustion fuel injection (excluding electric propulsion methods) are propulsion methods that utilize fuel explosion, which poses safety problems.

(4) It generates noise and propellant gas, which is harmful to the environment.

(5) Not only is it technically impossible to perform sudden starts, sudden stops, or right-angle turns in all directions from a stationary state, but the inertial force may destroy the crew.

In short, conventional propulsion systems for flying objects are based on primitive principles, and can be said to have reached their theoretical limits.

The present invention has been made in view of these conventional problems, and its purpose is to provide a propulsion device for a flying object based on a novel principle.

(Means for Solving the Problems) In order to achieve the above object, a propulsion device for a flying object according to the present invention has the following configuration.

That is, the propulsion device for a flying object of the present invention includes: an electromagnetic energy generating means for generating electromagnetic energy for changing the curvature component of a space around the flying object; and controlling the manner in which electromagnetic energy is generated by the electromagnetic energy generating means. a control means for locally controlling a change in the curvature component of the space, and using a spatial distortion force generated in the space as a propulsive force of the flying object; It is a propulsion device.

(Function) Next, the function of the flying object propulsion device of the present invention having the above configuration will be explained.

The present invention is based on the mechanical structure of space shown by Riemannian geometry. The mechanical structure of space follows Riemannian geometry, but if we assume that space is an infinite continuum, the following holds.

That is, when an infinitesimal line element that defines the distance between two points changes due to a certain physical action, the change is continuous, and space remains a continuum even after the change.

Space is distorted by external physical action,
When all external physical effects are removed, it always returns to its natural, undistorted state.

Distortion of space is caused by the curvature of space, so when distortion occurs in space, it causes changes in the local geometry of space. Since the curvature of space is represented by curvature, changes in the geometrical structure of space can be represented by changes in the curvature components of space.

Therefore, if we express the geometric properties of the space using curvature components, the value of the curvature component of a curved space (Riemann space) that is not flat is not O, and the value of the curvature component of a flat space (Minkowski space) is The value can be said to be O.

By the way, the starting point of Riemannian geometry is the metric tensor 9p
v, which makes the infinitesimal line element d S 2 between two points
=g)-rvdx'''dxv is defined, and this 9μ
From the combination of υ, the Riemann connection coefficient r% and further the Riemann curvature tensor R'', k are defined, and the geometry of the entire space is determined.

The following shows what kind of distortion is caused by the curvature of space, and what kind of body force is generated by this distortion.

The distortion of the space is given by the following equation (1) using the curvature indicating the curvature of the space and the closed surface of the space.

e uv= Rpvkl d A ” --
−−−−””'−−− (1) Here, eμυ is the strain tensor, Rpvbt is the Riemann curvature tensor, and dA
kt indicates an area component.

In other words, distortion occurs due to the bending of space.

Then, when a field of strain is created, a field of stress is generated, and due to the equilibrium condition in the continuum, σl J == EI J"Vepυ-(2)-χ1=
σl J ′J , , , , , , ,
, , , , , , -, , , (3> holds true.

As a result, from equations (1) to (3),
A kL (4) is obtained. Here, xi is the body force acting on the spatial region, σ is the stress tensor, and EIJJIlj is the fourth-order tensor that defines the properties of the space. Note that the Riemann curvature tensor is shown in the following equation (5).

Rμνkt=fu(gμl, Vlf 9υt, JJk
To 9μ + ν1 + 9ν, μl) + “1 for β” '3x
r' s pJ" Ct ----------(
5) In short, when distortion occurs in space, area force (stress)
is generated, and this area force is converted into a body force (spatial distortion force) that acts on the spatial region.

This spatial distortion force is transmitted to objects existing in the spatial region by the proximity effect of the spatial field, and the effect is equivalent to the effect of gravity.

That is, the present invention attempts to utilize spatial distortion force as a propulsion force for a flying object, and uses electromagnetic energy as an external physical action.

Next, the relationship between the curvature of space and energy is as follows.

The energy that affects the curvature of space is material energy and electromagnetic energy, so the material energy tensor is expressed as Y“0
, the electromagnetic energy tensor is Mμm, then the Ricci tensor R"1, which is a contraction of the Riemann curvature tensor, is the following (
6) It is given by Eq.

Here, considering only electromagnetic energy from a technical point of view, by setting the electromagnetic energy tensor M"1 to be, the following is obtained. However, fpP=9μcf 9pBfaβ.

Here, an antisymmetric tensor fμν is used as a quantity representing the strength of the electromagnetic field. Note that the scalar curvature R, Ricci tensor RpV, and Riemann curvature tensor R9aa.

The relationship is shown in the following equation (9).

R“”=1? ""g"Ras, Ra, = R', β = 9
”R,,,β.

R= Rca-9cII3Ra a −
------- (9) By the way, the relationship between the curvature component of space and the electromagnetic energy tensor is given by the above equation (6), and the particularly dominant component is. The electromagnetic energy tensor M” is MOO= (↓
εoE2+upper B2) ---111-(12)2
2μ0, but in reality the magnetic field energy is dominant, so
Practically speaking, it becomes 2μ0, where M""=, -UB2. Here, G is the universal gravitational constant, B is the magnetic flux density (w
b/m”=:T), μo is the magnetic permeability of vacuum, and C is the speed of light.

Therefore, in the present invention, the curvature component of the spatial region around the flying object is changed by the electromagnetic energy generated by the electromagnetic energy generating means, that is, the value of the curvature component is increased from 0 to a certain value.

Then, this change in the curvature component results in a change from a flat spatial region to a curved spatial region, that is, a spatial distortion. This spatial distortion penetrates into a nearby spatial region including the flying object as a distortion stress as an area force, that is, a body force, and a spatial distortion force as a proximity effect of the spatial field acts directly on the flying object.

At this time, the control means controls the manner in which electromagnetic energy is generated by the electromagnetic energy generation means so that the change in curvature of the spatial region becomes local, and controls the flight direction of the flying object.

That is, since the main propulsion force is not generated by a static magnetic field, the control means controls the electromagnetic energy generation means so that the magnetic field changes in a pulsed manner, or so that a dynamic change in the curvature component is obtained by rotating the magnetic field. I will do it.

Next, how much acceleration can be obtained depending on the curvature of space will be explained using a specific numerical example.

The amount of deviation of space on the earth's surface from a flat space hoo is hoo = 20M/♂R1 The curvature of space ROO is Roo = (
■hoo)/R2, the acceleration α generated by this is α=
(Case C” hoo) /R, so the mass of the earth M
(M = 5.974xl Okg), the earth radius R (R = 6.378x 103fan),
GM-3,986X 10 (kIII) /s
, C=3X 105km/s and calculate, h
00=1.389X10, Roo=1.71X
10 m, α=9.8 m/S.

In other words, the magnitude of the curvature of space is a small value of 10 m, but the acceleration obtained by the bending of space is 9
．． 8 m/'s2, which is large.

From this, it is predicted that if the curvature of the space is increased by 2 to B orders of magnitude, a considerable acceleration due to body force can be obtained. By the way, the magnetic energy, that is, the strength of the magnetic field that generates the value of the spatial curvature 10-''m-2 is the curvature component R00, that is, the above (
It can be determined from equation 4), and the magnetic flux density B is approximately 1. ．． 4
This is a large value of X 1.0'Tesler 1.4 x 10'' Gauss.The strength of this magnetic field exceeds the magnetic field that can be generated by current superconducting technology (2X 1.0 Gauss). It is hoped that future technological advances will enable us to obtain the desired strong magnetic field.

As explained above, according to the projectile propulsion device of the present invention, the propulsion force of the projectile is a body force that permeates the entire spatial region including the projectile, that is, a direct action from the space around the projectile. Since body force (spatial distortion force) is used, all material points, including the flying object and the crew inside the flying vehicle, are accelerated by the same force, and there is no inertial force, so there is no destruction of the crew, etc. Therefore, according to the present invention, navigation such as sudden start, sudden stop, right angle turn, zigzag turn, etc. in all directions from a stationary state in the air is possible.

Further, since the propulsive force according to the present invention is equivalent to gravity, the final velocity obtained can in principle be close to the speed of light.

Furthermore, since the present invention does not use the propulsion force from an internal combustion engine, it does not generate noise (propeller sound, gas injection sound, etc.) or jet gas, and the navigation is stable (from stationary in the air to low speed to high speed is optional). It is highly safe because it does not carry explosive fuel.

In addition, according to the present invention, since the propulsive force acts on the entire spatial region including the flying object, the air on the outer surface of the flying object is similarly accelerated and moves, reducing the occurrence of aerodynamic heating due to air friction heat. can.

In other words, there is only friction between air molecules, and the flying object moves through the atmosphere at high speed (for example, several kilometers per second).
It can move at a speed of ~10 kTQ/s).

Finally, since the propulsive force according to the present invention acts on the entire spatial region that includes (or surrounds) the flying object, from a different perspective, the entire flying object becomes a force field.
It is protected by something like ld). Therefore, during navigation in outer space, even if interstitial materials or stone fragments are floating in the direction of travel of the projectile, they will receive the same force as the projectile due to the main propulsion force, and will be blown away in the direction of travel. .

In other words, head-on collision with objects floating in space can be prevented,
This allows for safe navigation in outer space.

As described above, various excellent effects can be expected from the propulsion device of the present invention.

<Example> Hereinafter, an example of the present invention will be described with reference to the drawings. 1st
The figure shows the appearance of a flying object according to an embodiment of the present invention.
FIG. 1(A) is a schematic top cross-sectional view, and FIG. 1(B) is a schematic side cross-sectional view.

The flying object 1 according to this embodiment is disc-shaped, and propulsion parts (21 to 26) are provided at four outer circumferential positions obtained by dividing the outer circumference of the disc into four equal parts and at a central position on the upper and lower surfaces of the disc.

In this embodiment, each of the propulsion units 21 to 26 has an electromagnetic energy generation means and a control means for controlling the same on a one-to-one basis.
It is configured in association with .

In addition, one control means may be provided as a whole, and all the electromagnetic energy generation means may be collectively controlled.

The electromagnetic energy generating means generates a necessary magnetic field using superconducting technology or the like to cause a change in the curvature component of the space around the flying object 1, that is, to increase the value of the curvature component from 0 to a certain value. arise.

The control means changes the curvature component dynamically by changing the magnetic field in a pulsed manner, for example, or by rotating the magnetic field, in order to localize and at the same time promote the change in the curvature component of the space caused by the electromagnetic energy. The electromagnetic energy generating means is controlled in such a manner.

As a result, if the curvature component of the spatial region near the propulsion section 26 is changed by strong electromagnetic energy from the propulsion section 26, which is installed on the lower surface side of the flying object 1 (J), for example, as shown in FIG. The spatial region changes from a flat spatial region to a curved spatial region.This change results in spatial distortion, and distorted stress as an area force, or in other words, as a body force, penetrates into the neighboring spatial region including the flying object 1. , the spatial distortion force F acts directly on the flying object 1.

Since this spatial distortion force F becomes a force that pushes the lower surface of the flying object 1 upward, the propulsive force obtained by the propulsion unit 26 is a vertical upward force.

For example, when a strong magnetic field of 2 billion Tesla is generated by an electromagnetic energy generating means, the spatial distortion force F becomes F≠100G, and the resulting acceleration is approximately 1 km/s.
It becomes 2. In other words, if you generate F in a stationary state, you will be at a point that has moved 1 km after 1 second.

The same applies to the other propulsion units 21 to 25, and the propulsion unit 25 obtains the propulsion force for vertical descent, and the propulsion units 21 to 24 obtain the propulsion force for horizontal movement in mutually orthogonal directions in the horizontal plane. Propulsive force in any direction can be obtained depending on the combination.

Therefore, as shown in Fig. 3, a sudden start or sudden stop in any direction from a stationary state in the air (Fig. 3 (A)).

Any navigation that cannot be achieved with conventional propulsion methods, such as navigation that combines horizontal movement and vertical ascent (descent) (Fig. 3 (B)), zigzag navigation, etc., becomes possible.

Here, the propulsive force obtained by the present invention is not an electromagnetic force such as the Lorentz force, but a propulsive force due to the action of space itself, and this is equivalent to gravity, so the final velocity obtained by this is in principle In fact, it is possible to achieve speeds close to the speed of light. However, since it is limited by the Lorentz contraction effect due to special relativity, it is expected that in practical terms the speed will be about 10 to 30% of the speed of light.

The reason for this can be explained as follows.

That is, at 10% of the speed of light, the Lorentz coefficient increases by 0.5%, and the time delay and mass increase can be almost ignored. The Lorentz coefficient increases by 4.8% at 30% of the speed of light, increases by 15% at 50% of the speed of light, increases by 40% or 1.4 times at 70% of the speed of light, and increases by 2.29 times at 90% of the speed of light, the speed of light 3.2 times at 95%.

For example, when flying at 95% of the speed of light, the time delay is 3.2 times 1 f, so the passage of 1 hour corresponds to the passage of 3.2 hours, and a long flight at this speed becomes a problem.

Furthermore, although the outer surface of the flying object increases 3.2 times when it is at rest, since the main propulsive force is body force, an increase in mass directly results in an increase in propulsive force, so there is no effect.

Therefore, 10 to 30% of the speed of light is considered to be an appropriate value since the time delay can be ignored.

In addition, high-speed flight in the atmosphere is due to aerodynamic friction and heat.

Although the projectile is heated to a high temperature, the main propulsion force acts on the entire spatial region including the projectile, so the air on the outer surface of the projectile is similarly accelerated and moves, reducing the generation of aerodynamic frictional heat. In other words, it is only friction between air molecules, and the flying object can move in the atmosphere at high speed (for example, several km/s to several tens of km/s). However, the entire projectile is surrounded by highly heated, ionized air (plasma).

Furthermore, the propulsion force obtained by the present invention acts on the entire spatial region containing (or surrounding) the flying object.

If you look at this from a different perspective, the entire flying object is a field of propulsion (for
ce field). Therefore, during navigation in outer space, even if inter-leg materials, stone fragments, etc. are floating in the direction of travel of the projectile, they will receive the same force as the projectile due to the main propulsion force, and will be blown away in the direction of travel.

In other words, it can prevent a head-on collision with a floating object in outer space and allow safe navigation in outer space.

By the way, as shown in FIG. 4, if there is a yield point in the space itself due to the spatial distortion force, then the propulsive force explained above can be said to be used in the linear region (2).

In area ■, rather than the movement of an object by propulsive force, it is an infinite displacement in space (mathematically speaking, in reality it has a finite length)
It is expected that there will be a possibility of navigation by instantaneous movement of objects. In this case, propulsion is not due to acceleration, so the wall of light speed due to special relativity does not occur.

In the embodiments described above, the flying object 6 is in the shape of a disk, but it may also be in the shape of a sphere, for example.

(Effects of the Invention) As explained above, according to the flying object propulsion device of the present invention, the propulsion force of the flying object is the body force that permeates the entire spatial region including the flying object, that is, the space around the flying object. Since the body force (spatial distortion force) which is a direct effect from the air is used, all material points including the flying object and the occupants inside the flying object are accelerated by the same force, and there is no inertial force. There was no damage to the crew.

According to the invention, therefore, sudden starts, sudden stops and right-angle turns in all directions from rest in the air.

Navigation such as zigzag turns becomes possible.

Further, since the propulsive force according to the present invention is equivalent to gravity, the final velocity obtained can in principle be close to the speed of light.

Furthermore, since the present invention does not use the propulsion force from an internal combustion engine, it does not generate noise (propeller sound, gas injection sound, etc.) or jet gas, and the navigation is stable (from stationary in the air to low speed to high speed is optional). It is highly safe because it does not carry explosive fuel.

In addition, according to the present invention, since the propulsive force acts on the entire spatial region including the flying object, the air on the outer surface of the flying object is similarly accelerated and moves, so that the generation of air friction heat can be reduced. In other words, there is only friction between air molecules, and the flying object moves through the atmosphere at high speeds (for example, several kilometers per second).
s ~ number 1. It can move at a speed of 0km/s).

Finally, since the propulsive force according to the present invention acts on the entire spatial region that includes (or surrounds) the projectile, if we look at it differently, the entire projectile becomes a force field.
It is protected by something like eld). Therefore, during navigation in outer space, even if interstitial materials or stone fragments are floating in the direction of travel of the projectile, they will receive the same force as the projectile due to the main propulsion force, and will be blown away in the direction of travel. .

In other words, head-on collisions with floating objects in outer space can be prevented, and navigation in outer space can be achieved safely.

As described above, according to the propulsion device of the present invention, various excellent effects can be expected.

[Brief explanation of the drawing]

FIG. 1 shows the appearance of a flying object according to an embodiment of the present invention,
Figure 1 (A) is a schematic top cross-sectional view, Figure 1 (B) is a schematic side cross-sectional view, Figure 2 is an explanatory diagram of the principle of propulsion generation, Figure 3 is an explanatory diagram of navigation, and Figure 4 is a spatial distortion diagram. It is a predicted characteristic diagram of force. 1... 1 body, 21-26... Propulsion section, F... Spatial distortion force. Agent Patent attorney Yoshi Yahata Hirokomaku (, 4) 7---F Chilled ice 2/~21-----Ichi-kyo I
-Kabutoaki n Kishorin 4 Gaiban / Figure 7, l Hayabusa 2 Zuku = p stillness 5/) Emenren (Ewo Masa) (A) Horizontal f-stroke and right-angled keishi-ji (B) Dagdegu f stroke (C) -fff Shell supply / @ side number Kohiro example 3 Figure all questions 1 company power with dry lips / solid layer Figure 4 procedural amendment (voluntary) October 27, 1986 2, Title of the invention Projectile propulsion device 3, Relationship to the case of the person making the amendment Patent applicant address 5-33-1 Shiba, Minato-ku, Tokyo Name (423) NEC Corporation Representative Tadahiro Sekimoto 6, amendment Contents of the amendment in the detailed description of the invention in the specification (1) In the 14th line of page 2 of the specification, the phrase [100] has been replaced with [about 100] ” he corrected. (2) ' d S 2'' g on page 5, line 11 of the specification
pvdx" dxVJ, 'd s2=';
Correct it as jpvd x “dxv”. (3) Equation (6) stated on page 7, line 14 of the specification is corrected as follows. (4) In the 6th line of page 11 of the specification, ``the above formula (4)'' is corrected to ``the above formula (13)''. (5) In the 9th line of page 15 of the specification, the statement "The spatial distortion force F is" is corrected to "The acceleration due to the spatial distortion force F is". (6) On page 15, line 12 of the specification, the text "rlkm" is corrected to '0.5km.'that's all

Claims (1)

[Claims] an electromagnetic energy generating means for generating electromagnetic energy for changing the curvature component of the space around the flying object; controlling the manner in which the electromagnetic energy is generated by the electromagnetic energy generating means to locally change the curvature component of the space; 1. A propulsion device for a flying object, comprising: a control means for controlling the spatial distortion force generated in the space as a propulsion force for the flying object.