JP2936858B2 - Flying object propulsion device - Google Patents

Description

DETAILED DESCRIPTION OF THE INVENTION

[0001]

BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a propulsion device for a flying object (aircraft, manned rocket, spacecraft, etc.), and more particularly to controlling a curvature component of a space by strong magnetic energy to generate a space distortion generated in the space itself. The present invention relates to a space-driven propulsion device that uses force as a driving force.

[0002]

2. Description of the Related Art A conventional propulsion system for a flying object includes a system based on a reaction of an air flow by a propeller, a system based on an injection gas flow from an internal combustion engine such as a jet engine or a rocket engine, and an electric propulsion based on a reaction of a plasma flow and an ion flow. Methods are known. In the rocket propulsion system,
In addition to the chemical rocket propulsion system that has already been put into practical use, the application of electric propulsion systems (electric heating propulsion, ion propulsion, plasma propulsion, etc.) that have been put into practical use for attitude control of artificial satellites has been studied for rocket propulsion. At the conceptual stage, there are nuclear propulsion systems (nuclear thermal propulsion, fission pulse propulsion, fusion pulse propulsion, etc.) and non-chemical rocket propulsion systems (solar heating propulsion, ramjet propulsion, laser propulsion, etc.).

[0003]

However, in all of the conventional propulsion systems for a flying object, a reaction thrust (momentum thrust) in which a working substance is jetted backward at a high speed and generates a thrust in a forward direction by the reaction. Therefore, there is a certain limit on the speed obtained.

That is, since the final arrival speed is theoretically determined from the injection speed and the mass ratio of the working material, the speed limit obtained is low, and an arbitrary high speed cannot be obtained.
For example, a chemical rocket (a propulsion method using a jet gas flow) has a limit of several tens of km / sec, and an electric propulsion has a limit of several hundred km / sec, and a higher speed cannot be obtained. However, the thrust-to-weight ratio (acceleration performance) is very low, about 100 for a chemical rocket, and 10 ^-5 to 10 ^-3 for electric propulsion. Therefore, chemical rockets are the only propulsion systems that can escape from the Earth's 1G gravitational sphere, although their operation time is short depending on the amount of fuel loaded.

In the operation of a flying object, it is necessary to perform various operations such as sudden start from a state of suspension in the air, sudden stop, and right-angle turning in all directions. It is technically impossible, and if executed, the occupants and the like may be destroyed due to the huge acceleration of the inertial force. This is because the inertial force cannot be theoretically eliminated.

[0006] Furthermore, the generation of noise is unavoidable and is harmful to the environment in conjunction with the emission of injected gas. In particular, in nuclear propulsion, scattering of radioactivity is inevitable. In addition, since the fuel explosion is used, there is a problem in safety.

Next, as is apparent from a rocket, a space shuttle, or the like, it is as if several crew members are loaded on a huge load of fuel, and the volume ratio occupied by the crew members is several percent. From 10 to about 10%, and there are restrictions on the weight and volume of objects (humans, cargo, etc.) to be made to fly.

[0008] Finally, the spacecraft has the ability to navigate in space at high speed (several hundred km / sec to tens of thousands km / sec to light speed) and the free horizontal and vertical attitude between the planet and atmosphere. It must have the ability to fly with ease, take off and land easily, and both, but this is not possible with conventional propulsion systems.

An object of the present invention is to provide a propulsion device based on a novel propulsion principle suitable for the propulsion of a flying object, that is, to control a curvature component of a space by strong magnetic energy to promote a space distortion force generated in the space itself. An object of the present invention is to provide a space-driven propulsion device that uses force.

[0010]

In order to achieve the above object, a flying object propulsion device according to the present invention has the following configuration. That is, the flying object propulsion device of the first invention generates a spherical magnetic field for generating a strong magnetic field for giving a change to the curvature component of the space inside the flying object (aircraft, manned rocket, spacecraft, etc.) and the space around the flying object. Main Superconducting Magnet that Generates a Magnetic Field
A magnetic energy generating means disposed inside a spherical body made of a superconducting material ; and controlling a mode of generation of a strong magnetic field by the magnetic energy generating means to locally change a curvature component of the space to be quasi-antisymmetric. A space distortion force equivalent to the gravity generated in the space as a propulsion force of the flying object.
Control means, one half of the main superconducting magnet
Auxiliary superconducting magnet that generates a magnetic field of opposite polarity in a spherical magnetic field
The magnets of both superconducting magnets
And magnetic control means for changing and controlling the repetition frequency .

A flying object propulsion device according to a second aspect of the present invention is a flying object
(Aircraft, manned rockets, spacecraft, etc.)
Strong magnetic field to change the curvature component of the space around the projectile
Means for generating magnetic energy; and said magnetic energy
Controlling the generation mode of the strong magnetic field by the
By controlling the change of the curvature component of the space locally to be quasi-antisymmetric,
Space distortion force equivalent to gravity generated in space
A flying object comprising: magnetic control means for providing propulsion;
Propulsion device, wherein the magnetic energy generating means,
Liquid metal storage container for storing liquid metal as a highly conductive fluid
And a spherical blanket as a container for generating a strong magnetic field;
The liquid metal from the liquid metal storage container is used as a fluid as it is.
The blanket as or as spray-like fluid particles
A nozzle for injecting into the blanket;
An initial magnetic field is generated inside the blanket placed opposite the wall.
A pair of superconducting magnets; and a pair of superconducting magnets.
The blanket on both sides perpendicular to the magnet placement direction
Fluid particles or streams that are placed opposite the
A pair of laser light sources for irradiating the body with pulsed laser light;
Bundling the unfluidized fluid particles or fluid with the liquid metal
An exhaust pump for refluxing to the storage container;
The magnetic control means controls the pair of superconducting magnets.
Exciting current control, asymmetric control of the pair of laser light sources, and
Fast process from fluid particle or fluid injection to exhaust
Performing repetitive control and the like .

[0012]

[0013]

Next, the operation of the flying object propulsion device of the present invention configured as described above will be described. Propulsion of the present invention, conventional jet engine, rather than by reaction thrust (momentum thrust) by gas fluid ejection such as rocket engines, the pressure difference type by field distortion of the space by the pressure differential thrust to thrust This is a space-driven propulsion system. The outline is as follows.

In continuum mechanics, a field-filling object is affected by the gradient of the field quantity. For example, large particles move under a net pressure due to the hydrostatic distance gradient. This quantity (hydrostatic pressure) as a field quantity is a function of the location, and this pressure gradient is an important driving force. An object in a pressure gradient field moves due to a net pressure difference. An object in a field of zero pressure does not move while continuing to stand still. It is assumed that this object generates a locally antisymmetric pressure field in one direction around the object. In this state, since the action of generating the pressure field in the space of the object and the action of the generated pressure field on the object are balanced, the object cannot move although the pressure from the field exists.

Next, the action of generating a pressure field in the space of the object is momentarily interrupted. Even if this effect is instantaneously removed from the space, it takes a finite time to return to the pressure 0, instead of returning to the original natural pressure 0 state instantaneously. That is, the space has a finite strain rate. In this finite time domain, the object and the space field are independent, the object is in the pressure field,
It moves under the pressure of the field. This pressure is equivalent to the net pressure difference in the pressure gradient. ON-O of this pressure field generation
Continuous thrust is obtained by repeating the FF process at high speed. In terms of energetics, the surrounding space is locally deformed by the pressure field generating action of the object, and the strain energy stored in the form of distortion in the space by this displacement action is released by the instantaneous interruption of the pressure field generating action However, the distortion energy of the space excluding a part of energy loss is given to the object as kinetic energy at the time of release. Here, the pressure of the space field is a surface force generated from the curvature of the space generated by a strong magnetic field.

This propulsion principle is derived from a new concept regarding space and a theory regarding the dynamic structure of space determined from the geometric properties of space. That is, the term "strain" as used herein means a strain defined in continuum mechanics. The distortion of space is generated by the curvature of space, and the curvature of space is generated by the mass or magnetic field of an object. The space distortion field due to the mass of the object is a gravitational field. The magnetic field is equivalent to the gravitational field through the medium of space curvature (distortion).

Therefore, in the present invention, the mode of generation of the strong magnetic field generated by the magnetic energy generation means is controlled by the magnetic control means so that the dynamic curvature change of the space area including the flying object becomes local, and the space itself is controlled. (Specifically, a force obtained from a field in a distorted space in a transition process in which a bent space returns to a flat space having zero curvature) is defined as a propulsive force. This will be described below from another point of view. Space is
When the vehicle turns, an acceleration field is formed in the bent space region.
The mass in the field of acceleration is estimated by Newton's second law.
Move under force.

Therefore, this propulsion system is a kind of pressure differential propulsion system utilizing the proximity action (concept that direct action is received from the field) due to the distortion of the space field, or the force generated by the distortion of the space. Is equivalent to gravity and can be called a gravitational field propulsion system . Since the thrust is a body force that permeates the entire space area including the flying object (a force distributed uniformly inside the volume element and proportional to the mass of the volume element, gravity and inertia force are also body forces), it is not affected by inertia force It has excellent characteristics as a propulsion system for flying objects, such as being able to theoretically achieve a quasi-light speed in a short time. Hereinafter, the mechanical structure of space (space distortion theory), the principle of propulsion operation, and the like necessary for understanding the background of the present invention will be described.

Spatial distortion theory Basic concepts of space (1) Space is an infinite continuum, and its structure is determined by the framework of Riemannian geometry. The space has only one natural state without distortion (flat space)
When all external physical effects that cause distortion are removed, the space always returns to its natural state without distortion. Then, adjacent points in the space remain as adjacent points under any physical action, and the change satisfies the basic condition of being continuous and being a continuum after the change. It is a continuum in the sense that it satisfies this hypothesis. The space as a continuum is a Riemann space, and its structure follows Riemann geometry.

(2) Spatial bends are purely geometric quantities. In order to relate this geometrical quantity to the real force, the concept of continuum mechanical strain is important. The field of distortion is the interface between geometric quantities and real dynamics.

(3) A change in the local geometric structure of the space is regarded as a state of space distortion. The change in the geometrical structure is a change in the curvature component, and indicates a transition from a flat space with a curvature component of 0 (Minkovsky space) to a fully curved space with a curvature component (Riemann space). The fact that space is bent and that space is distorted are essentially the same.

(4) The distortion of the space represents a kind of deformation of the space, and the material points filling the space are affected by the deformation of the space. An important analysis technique that relates the concept of continuum mechanics as deformation to the concept of Riemannian geometry is translation of vectors. If the curvature is not 0, the result of the parallel translation of the vector varies depending on the course of the space, and the vector does not return to the initial value even if the vector makes a round along the closed curve on the curved surface. When the curvature is 0, this phenomenon does not occur.

(5) The substance occupies an area in space in a continuous manner. Here, space and matter must be clearly distinguished. The substance fills the space and occupies an area of the space by moving. That is, the substance can move in the space, and fills the space by moving in the space.

[0024] (6) the continuity of space for one holding the moving speed of the material point of filling the space does not exceed the strain rate of space.

II. What is Riemannian geometry? Riemannian geometry is geometry that deals with curved spaces. That is, in this paper, a four-dimensional Riemann space as a curved space is targeted, and the curvature of the space is emphasized. The target physical space is represented by three spatial coordinates (x = x ¹ , y = x
² , z = x ³ ) and one axis of time coordinate (w = ct = x ⁰ ). This is called x ⁱ (i = 0, 1, 2,
Notation 3).

The square of the infinitesimal distance ds between the two points and the point x ⁱ in the four-dimensional Riemann space at the adjacent point x ⁱ + dx ⁱ is given by Equation 1. g _ij is called a metric tensor, is a quantity that defines all the geometric properties of space, and is generally a function of place. The starting point of the Riemann geometry is a metric tensor g _ij that defines an infinitesimal line element between two points. From the combination of g _ij , the Riemann connection coefficient (Equation 2)
Further, the Riemann curvature tensor (Equation 3) is defined, and the geometry of the entire space is determined.

[0027]

(Equation 1)

[0028]

(Equation 2)

[0029]

(Equation 3)

Next, the properties of the Riemann space are as follows. (1) In a flat (unbent) space, all components of the Riemann curvature tensor are zero. In a curved space, the component of the Riemann curvature tensor is not zero. Non-zero component is 1
If so, the space is essentially bent.

(2) A necessary and sufficient condition for the space to be flat is that all 20 independent components of the Riemann curvature tensor are zero.

(3) In a flat space, the metric tensor takes a constant value. In a curved space, the metric tensor is a function of location. That is, the metric tensor deviates from a flat value (Minkowski metric).

III. Basic structural formula of space A line element between any two points in the space area I before structural deformation is represented by ds
= G _i dx ⁱ , the infinitesimal distance is ds ² = g _ij d
the x ⁱ dx ^j (left in FIG. 1). Then, in the spatial region II after structural deformation of the space due to external physical action (influence due to the presence of matter or electromagnetic energy), the line element connecting the same two points in the same spatial region is newly changed, Ds ′ = g _i ′ dx ⁱ ′, and the infinitesimal distance is ds ′ ² = g _ij ′ dx ⁱ dx ^j (right side in FIG. 1). g _i ′ is a displacement of the basis vector g _i , and g _ij ′ is a metric tensor of the coordinate system after the deformation.

Since the degree of deformation can be expressed as a change in the distance between any two points, Equation 4 is obtained.

[0035]

(Equation 4)

That is, the degree of the geometric structural deformation of the space is described by the amount of change r _ij = g _ij ′ −g _ij of the metric tensor. This state of deformation can be expressed using a displacement vector u extending from the position before deformation to the position occupied by the same coordinate point after deformation for each point (Equations 5, 6).

[0037]

(Equation 5)

[0038]

(Equation 6)

Using the above equation, the square d of the deformed line element
When s ′ ² is created, Equation 7 is obtained.

[0040]

(Equation 7)

In Equation 7, the second-order minute term u ^k : _i u
_k : _j can be neglected sufficiently when the displacement is small. Here, the symbol “:” indicates a covariant derivative.

The covariant derivative is represented by Expression 8, and is different from the ordinary derivative A _i , _{j by} the quantity of the second term. In a flat space, since the Riemann connection coefficient Γ ^r _ij = 0, A _i : _j = A
_i , _j , that is, the covariant derivative of the first-order tensor (vector) A _i matches the ordinary derivative. In a curved space, the derivative usually needs to be corrected, and is described as a covariant derivative.
Therefore, when the derivative of the field quantity is included, it is generalized to express it as a covariant derivative.

[0043]

(Equation 8)

The actual physical space can be treated as a small displacement based on a trial calculation of the order of the distortion, and the secondary small term can be ignored.

[0045]

(Equation 9)

On the other hand, as a concept of distortion in continuum mechanics,
Since the distortion tensor e _ij is given by Expression 10, the relational expression of Expression 11 is obtained.

[0047]

(Equation 10)

[0048]

[Equation 11]

Equation 11 is an equation showing a certain deformation in the geometric structure of the space by the concept of distortion. This shows that the strain field e _ij is generated when the metric tensor shifts from g _ij to g _ij ′ due to the presence of a substance or the like.

IV. Basic equations of space An important analytical technique that relates the concept of continuum mechanics as a deformation to the concept of Riemannian geometry is the concept of vector translation. Equation 12 is obtained by extending the concept of vector translation on Riemann space.

[0051]

(Equation 12)

In Equation 12,

[0053]

[Outside 1]

Is the Riemann curvature tensor

[0055]

[Outside 2]

From the property of (1), it is an antisymmetric tensor, and becomes a rotation tensor indicating the rotation of the displacement field. When the space is bent, a rotation of the displacement (field) occurs within the area of the space.

Now, the rotation tensor and the strain tensor are expressed in continuum mechanics.

[0058]

[Outside 3]

Satisfies the following differential equation (Equation 13) for the displacement gradient in the direction perpendicular to the rotation plane. This equation holds because the order of differentiation is reversible in a flat space.

[0060]

(Equation 13)

In order to extend the differential equation of Equation 13 to a curved Riemann space, it is necessary to correct the equation to co-deformation. This can be performed under the condition that Equation 14 is satisfied. A covariant differential equation is obtained.

[0062]

[Equation 14]

[0063]

(Equation 15)

Next, this equation 15 shows that the displacement gradient of the rotation tensor corresponds to the difference between the displacement gradients of the strain tensor, and represents a fourth-order tensor defining the properties of space on both sides.

[0065]

[Outside 4]

Expressions 16 and 17 are obtained by formally multiplying In addition, the relational expression (Equation 18) between the stress (field) tensor σ ^ij and the strain (field) tensor _em1 on the continuum mechanics was used, and the above-mentioned fourth-order tensor was treated as a constant for the covariant derivative. . As described above, the symbol “:” indicates a covariant derivative.

[0067]

(Equation 16)

[0068]

[Equation 17]

[0069]

(Equation 18)

On the other hand, the body force X ⁱ and the stress (field) tensor e ^ij are given by Expression 19 according to the equilibrium conditions in the continuum.

[0071]

[Equation 19]

Therefore, Expression 17 shows the change ΔX ^{i in the} body force.
Therefore, Expression 20 is obtained from Expressions 16 and 17.

[0073]

(Equation 20)

Equation 20 shows that the spatial distortion force is generated by the gradient of the Riemann curvature tensor indicating the bending of the space. The space distortion force generated here is a body force that permeates a space and an object filling the space.

V. Structure of Space Curvature The curvature of a space is determined by the Riemann curvature tensor. The Riemann curvature tensor is given by Expressions 21 and 22.

[0076]

(Equation 21)

[0077]

(Equation 22)

The Riemann curvature tensor is a metric tensor

[0079]

[Outside 5]

Since the space is composed of, the structure of the space is determined by the metric tensor. The solution of this metric tensor is determined by the gravitational field equation.

Further, the scalar curvature R and the rich tensor are

[0082]

[Outside 6]

The Riemann curvature tensor has the following relationship (Equation 23).

[0084]

(Equation 23)

Represents the material energy tensor

[0086]

[Outside 7]

Applying this to the gravitational field equation yields Equation 24, which is finally expanded to give Equation 25.

[0088]

(Equation 24)

[0089]

(Equation 25)

On the other hand, the material energy tensor is given by
Given by

[0091]

(Equation 26)

In equation (26), ρ is the static mass density,

[0093]

[Outside 8]

Along with

[0095]

[Outside 9]

[0096] shows a four-yuan rate.

[0097] Now, the speed of the material is assumed to sufficiently small compared to the speed of light c, 4-way velocity is given by Equation 27. Therefore, the largest component of the matter energy tensor is μ =
Since ν = 0, Y ⁰⁰ is given by Expression 28.

[0098]

[Equation 27]

[0099]

[Equation 28]

[0100] Thus, by substituting Equation 28 into Equation 25, material energy tensor, that is, the maximum component R ⁰⁰ curvature due rest mass density is obtained (equation 29).

[0101]

(Equation 29)

Equation 29 shows that the static mass density ρ controls the curvature of the space. The magnetic field B also controls the curvature of the space similarly as described later. In other words, the mass density and the magnetic field generate the curvature of space (Space Curvature).

Now, considering a space that can be approximated by a static and spherically symmetric Schwarzschild space-time, the scalar curvature R is given by Equation 30.

[0104]

[Equation 30]

The Riemann curvature tensor on the Riemann space and the Gaussian curvature K on the two-dimensional sub-space embedded in the Riemann space have the relationship of Equation 31, and the scalar curvature R and the Gaussian curvature K are represented by Equation 32. Have a relationship. Therefore,
From Equation 31, Equation 33 is obtained for the two-dimensional Riemann space.

[0106]

(Equation 31)

[0107]

(Equation 32)

[0108]

[Equation 33]

VI. Curvature control of space by magnetic field The electromagnetic energy tensor M ^ij is applied to the gravitational field equation. In this case, the metric tensor g _ij is given by Expression 34.

[0110]

(Equation 34)

Equation (34) is an equation for determining the structure of the space due to electromagnetic energy. By multiplying Equation (34) by g _ij to obtain Equation (35), Equation (35) is obtained. can get.

[0112]

(Equation 35)

[0113]

[Equation 36]

The antisymmetric tensor f _ij indicating the magnitude of the electromagnetic field
By using the electromagnetic energy tensor M
^{Since ij} is given by Equations 37 and 38, the value of M is obtained as follows (Equation 39).

[0115]

(37)

[0116]

(38)

[0117]

[Equation 39]

By substituting M = 0 into Equation 36,
Equation 40 is obtained.

[0119]

(Equation 40)

The rich tensor R ^ij has ten independent components, but the main component is i = j = 0, that is, R ⁰⁰ . Therefore, Equation 41 is obtained from Equation 40.

[0121]

[Equation 41]

On the other hand, the antisymmetric tensor f _ij = −f _ji is given by an electric field E and a magnetic field B in relation to Maxwell's electromagnetic equation (Equation 42).

[0123]

(Equation 42)

Equation 42 is substituted into Equations 37 and 38 to obtain Equation 43, and finally Equation 44 is obtained. In addition,
In both formulas, μ ₀ is 4π × 10 ⁻⁷ (H / m), ε ₀ is 1 / 36π × 10 ⁻⁹ (F / m), and c is 3 × 10 ⁸ (m / m).
s), B is a magnetic field (Tesla), G is 6.672 × 10 ^-11 (N
^{· M 2 / kg 2),} R 00 is curvature components of the spatial (1 / m ^2).

[0125]

[Equation 43]

[0126]

[Equation 44]

Equation 44 shows that the main curvature component of the space is controlled by the magnetic field B. Control is also possible by the electric field E, but for E and B of similar magnitude, 1 /
About 1 Compared value of ² · ε ₀ E 2 is the value of 1 / 2μ ₀ · B ²
Since it is about seven orders of magnitude smaller, the contribution of the electric field E to the curvature is sufficiently negligible compared to the magnetic field B.

On the other hand , the principal curvature component based on the material energy tensor Y ^ij is given by Expression 45.

[0129]

[Equation 45]

[0130] Since the curvature component R ⁰⁰ space is independent of the cause of material energy or electromagnetic energy tensor as its source, becomes Equation 46, the formula 47 is derived.

[0131]

[Equation 46]

[0132]

[Equation 47]

[0133] B ² / 2μ ₀ = W identifies that a magnetic field energy density (J / m ^3), the following relationship is the rest mass density ρ (kg / m ³⁾ (Equation 48). Equation 48 guarantees the relational expression between mass and energy, E = mc ² .

[0134]

[Equation 48]

VII. Field pressure due to space curvature (surface force)
Since the basic structure of the generated three-dimensional space is determined by the quadric surface structure, the Gaussian curvature K in the two-dimensional Riemann space gives a practical concept (Equation 49).

[0136]

[Equation 49]

The following equilibrium condition equation is obtained by applying the film theory to the quadratic surface (Equation 50).

[0138]

[Equation 50]

Note that in equation 50,

[0140]

[Outside 10]

Is the film force (linear stress),

[0142]

[Outside 11]

Is the second basic metric of the curved surface, and P ³ is the normal stress (surface force) on the curved surface.

The second basic metric of a surface has the following relationship between the principal curvature of the surface and the metric tensor (Equation 51, 5).
2).

[0145]

(Equation 51)

[0146]

(Equation 52)

Therefore, Equation 50 is replaced by Equation 53.

[0148]

(Equation 53)

Since α and i are binary with respect to the quadratic surface, Equation 54 is obtained. Note that in Expression 54, K
₍₁₎ and K ₍₂₎ are the principal curvatures of the curved surface, and the principal curvature radii R ₁ ,
It is the reciprocal of the R _2.

[0150]

(Equation 54)

[0151] Further, since the Gaussian curvature K is given by equation 55, the equation 56 assumes the membrane force ^{_{N 1 1 = N 2 2 =}} N.

[0152]

[Equation 55]

[0153]

[Equation 56]

That is, the film force and the principal curvature on the curved surface generate a vertical stress P ³ (N / m ³ ) as a surface force on the curved surface.
The direction is toward the inside of the curved surface.

Now, consider a curved surface of a thin layer in a spherical space in which both the main curvature radii R ₁ and R ₂ are equal to the radius R. Since the Gaussian curvature K is given by Expression 49 and Expression 55 from Expression 57,
By substituting 1 / R = (R ^00/2 ) ^1/2 into Expression 56, Expression 58 is obtained, and Expression 59 is obtained.

[0156]

[Equation 57]

[0157]

[Equation 58]

[0158]

[Equation 59]

Since the film force N of the space as the linear stress is considered to be a unique constant value under certain conditions,
From the curvature of the R ⁰⁰ are generating a normal stress P ³ as the surface force of the space towards the inside of the curved surface. The inward normal stress P ³ curved is namely situ pressure, the accumulation of a large number of curved surfaces in the region of the space, to form a one-way pressure field.
Here, the surface force of the curved surface of the thin layer in the space = the vertical pressure in the inward direction of the curved surface = the pressure of the field = −P ³ (N / m ² ).
It's just a difference in perspective. The surface force field is a kind of force field, which gives an acceleration to a substance in the area of space, so that an acceleration field is generated. From the above, the curvature of the space (Curvature) is the surface force (Surface Force) on the space itself
And a unidirectional acceleration field is formed in the spatial region.

VIII. The curvature of space and the field of acceleration Due to the curvature of space, a surface force directed inward is generated in the curved thin film layer itself, and an acceleration field is formed in a certain space region by the integration of these thin film layers. The principal curvature component R ⁰⁰ field strength α and space of the acceleration caused by the geometrical structure of the space, weak field distortion is relatively small curvature of space, and this field is temporally , Are given by Equations 60 and 61, respectively, from comparison with Newtonian mechanics.

[0161]

[Equation 60]

[0162]

[Equation 61]

[0163] Here, h ₀₀ represents the deviation between the Minkowski metric eta ₀₀ = -1 flat space and the metric tensor g ₀₀ of curved space, Equation 62, a relationship of the 63.

[0164]

(Equation 62)

[0165]

[Equation 63]

From Equations 62 and 63, the relationship between the curvature of the space and the acceleration field is given by Equations 64 and 65.

[0167]

[Equation 64]

[0168]

[Equation 65]

From Expressions 60 and 61, Expression 66 is obtained.

[0170]

[Equation 66]

Equation 66 shows the spatial distortion e ₀₀ (= １ ／ · ・).
h ₀₀ ) produces a field of acceleration α. Also, it can be seen that the geometric quantity of the Riemann connection coefficient Γ ⁱ ₀₀ corresponds to a physical quantity indicating a gradient of distortion of e ₀₀ : _i .

[0172] space in static spherically symmetric Schwarzschild spacetime components gamma ⁱ ₀₀ is a Riemannian connection coefficient is not 0, the component of the i = 3 toward the radial direction of the sphere, i.e., gamma ³ ₀₀ Only. Therefore, R ⁰⁰ is given by Expression 67, and the acceleration α ³ = α is given by Expression 68.

[0173]

[Equation 67]

[0174]

[Equation 68]

[0175] Equation 68, the acceleration α for receiving an object in play of the acceleration shown to be proportional to the distance integrations of curvature R ⁰⁰ of the space.

In Newtonian mechanics, the acceleration α is given by a potential Φ: _i . Here, Φ is given by Expression 69, however, since α = Φ: _i and Expression 60 become Expression 70, h ₀₀ becomes Expression 71. Therefore, R ⁰⁰ is given by Expression 72.

[0177]

[Equation 69]

[0178]

[Equation 70]

[0179]

[Equation 71]

[0180]

[Equation 72]

On the other hand, the acceleration is obtained by the following equation (Equation 73), and the value on the earth surface is obtained by substituting the radius and mass of the earth (Equation 74).

[0182]

[Equation 73]

[0183]

[Equation 74]

The relational expression between the magnetic field and the curvature (Equation 75)
Therefore, the strength of the magnetic field that generates the space curvature of 3.42 × 10 ⁻²³ is 20 million Tesla.

[0185]

[Equation 75]

Next, the relationship between the curvature of the space and the acceleration field will be examined. It has already been mentioned that the surface force of the space field generated by the space curvature R ⁰⁰ is given by P ³ = N · (2R ⁰⁰ ) ^1/2 . Curvature R ⁰⁰ of the space on the Earth's surface,
Given by 3.42 × 10 ^-23 , an object in the space of the point receives 1 G of gravitational acceleration from the field. The value of the curvature is very small but large enough to cause a 1 G acceleration on the ground. Strictly speaking, although given the acceleration of the object with a gradient of surface forces, true essential for generating the acceleration field by considering a sufficiently small local area of current space
Correspondence between the acceleration is obtained approximately by surface forces P ³ is a factor.

[0187] curvature of space to produce a surface force P ³ to give acceleration field of 1G R ⁰⁰ is something that has been brought about by the mass density of the earth, but the curvature of the space is also effected by a magnetic field as described above. The curvature as a property of the space must have the same result independently of the factor of its occurrence. Therefore, 1G = P ³ = N · (2 * 3.42 * 10 ⁻²³ ) ^1/2 = N ·
^{(2 * 8.2 * 10 -38 ·} B 2) from ^1/2, B = 20M Tesla
Becomes

[0188] Now, if, when the size of the earth mass 100 times that is the density in intact is 100 times, the curvature of the space on the surface in the R ⁰⁰ = 3.42 * 10 ^-21, the corresponding acceleration field Is 100 G, and the corresponding magnetic field strength is 200 M Tesla in the same manner as above. The following table is obtained with the same idea.

[0189]

[Table 1]

Here, it should be noted that:
This means that the value of the curvature ^{R00 and} the value of the acceleration α do not correspond one-to-one. As can be seen from Equation 65, the curvature, that is, how much the space bends, does not correspond to the acceleration value itself, but to the degree of change in the acceleration, that is, the gradient of the acceleration field.

Alternatively, the equation 73 indicates that the acceleration corresponds to the integral with respect to the distance of the curvature, that is, the area (Volume) of the curved space.

The comparison here is a comparison on a spherical surface of a substance called the earth and a spherical surface when a magnetic field is confined in a spherical shell. It should be noted that the strain potential as a body distribution density function satisfies the Laplace equation at an outer point on the surface of the sphere, that is, in free space, so that it attenuates as a function of the distance r. The values in the table are for reference only.

IX. Gravity and inertia force The magnitude of both gravity and inertia force is proportional to the mass of the volume element, penetrates into each part of the object from the outside, is uniformly distributed inside, and acts equally on all material points inside And both exhibit the properties of body force. Inertial force as pseudo gravity is equivalent to gravity, and canceling gravity locally is a well-known fact as an equivalence principle. It has already been experienced because it is possible to temporarily achieve a zero gravity state by turning a flight of an aircraft.

In order for all the material points in the volume element to move under the same action, it is essential that a gradient of surface force (also called area force), that is, a kind of pressure difference gradient, exists in this region. That is, in order to uniformly move not only the movement of the outer shell of the volume element itself but also the storage of the volume element, a surface force difference of ΔP in the volume element is required as a driving force (see FIG. 2). . This mechanism creates an acceleration field.

Assuming that the space is a continuum, gravity and inertial force both generate a gradient of strain, and detailed equations are omitted. However, the gradient of this strain generates the above-mentioned distance gradient of surface force. Therefore, a body force acting equally on all material points is generated, and the mechanism is completely equivalent.

[0196] The essential difference of gravity and inertia, gravity whereas with a curvature R ⁰⁰ of the space, the inertial force is not accompanied by the curvature of space, is that that is, the curvature R ⁰⁰ = 0. In the case of the inertial force, the acceleration α is constant regardless of the location from the curvature R ⁰⁰ = 0 (Equation 76).

[0197]

[Equation 76]

However, in the case of gravity, the curvature α of the space is a function of the place, and is given by Expression 77, so that the acceleration α is a function of the place and is not constant. In other words, in gravity, the value of acceleration changes from place to place. Exactly, it has a distance gradient, and the degree of change in the acceleration corresponds to the curvature, that is, how much the space is bent.

[0199]

[Equation 77]

Although gravity and inertial force are distinguished by the presence or absence of curvature, a distortion gradient due to the bending of the space and a linear distortion gradient in the space accompanying the acceleration motion of the object are generated, and a surface force gradient is generated. It will exhibit the properties of body force.

Principle of Propulsion Operation In summary of the above description, space bending causes space distortion. The distortion force of the space penetrates and acts on the space and the object filling the space as a field. Such a bending of the space is generated not only by the object mass but also by the magnetic field. That can control the main curvature component R ⁰⁰ space by a magnetic field (Equation 78). The curvature of the space R ⁰⁰ are unidirectional pressure field in a space region including the object as a place pressure space -
Generate P ³ (Equation 79) or the curvature of the space is
An acceleration field is formed in the specified space area (Equation 68).
An object in a unidirectional pressure field moves by receiving this pressure , or an object of mass m in a field of acceleration α
Moves by receiving a thrust of f = mα from this place. This pressure is equivalent to the net pressure difference experienced by an object in the pressure gradient field. This gives the propulsion principle of the present invention.

[0202]

[Equation 78]

[0203]

[Expression 79]

That is, a bend is generated by a strong magnetic field in a space area near the arrangement area (propulsion section) of the magnetic energy generation means mounted on an object (flying object). However, in a static magnetic field, the action of changing the curvature of the space and the action of the distortion of the space are balanced, so that even if thrust is generated, there is no propulsion (movement) of the flying object. Therefore, in order to propel the flying object, it is necessary to unilaterally break the equilibrium between the action of the magnetic field on the space and the reverse action from the space. For this purpose, a magnetic control means is provided. At this time, the action on the space is performed in a quasi-static process while slowly maintaining an equilibrium state, and the reverse action from the space is performed instantaneously. It is important to control the rate of energy release. It is like a bow and arrow, and is gradually stored as the strain energy of the elastic body, almost giving instant energy to the arrow. Therefore, when a magnetic field is generated, reverse thrust cannot be obtained.

The magnetic control means controls the mode of generation such that the strong magnetic field generated by the magnetic energy generating means changes in a pulsed manner or rotates the magnetic field (30 GHz), and the dynamics of the curvature component of the space are controlled. It generates a dynamic change and gains continuous thrust from the space field to propel it.

The space has a finite strain speed (light speed) as a continuum, and it takes a finite time for the distorted (bent) space to return to a flat space even if the magnetic field is momentarily interrupted. . During the transition process to return to a flat space, the projectile is independently present in a curved space field and can be propelled by the action of this space field.

That is, since the equilibrium state is broken by instantaneously interrupting the action of bending the space, the bent space returns to a flat space without bending for a very short time in the transition process.
The projectile is independent of the field of the curved space, and the projectile can be propelled by the adverse effect of the field from the space.

In general, it is not possible to propel while dragging a place created by the place. In other words, unless the thing to be promoted and the place are independent, it cannot be promoted by the place. This is because the action on the field and the reaction from the field are balanced. At this time, it is important in principle to delay the reaction from the action in time.

Characteristics of the flying object (1) Since the thrust is body force, all the material points including the occupant inside the flying object (spacecraft) and the occupant inside the flying object (spacecraft) are accelerated by receiving the same force. There is no force action.

(2) Navigation such as sudden start in all directions, sudden stop, right angle turning, zigzag turning, etc. is possible from the stationary state in the air.

(3) The magnetic field energy acting on the space and
Since the power source is built in the projectile (spacecraft), it can be used for both planetary atmosphere and space navigation.

(4) The propulsion acceleration can be freely varied from several μG to 100 G by controlling the pulse magnetic field. That is, the navigation is stable (air suspension to low speed to high speed is arbitrary).

(5) Since the thrust is proportional to the increase in mass due to the increase in speed, the propulsion acceleration is always constant. In addition, since there is no limitation on the propulsion operation time, the final arrival speed of the flying object (spacecraft) is a quasi-light speed.

(6) Since it is not an internal combustion engine, it does not generate noise (propeller sound, gas injection sound) or injection gas. Also,
High safety because it does not carry explosive fuel.

(7) Since thrust acts on the entire space area including the flying object (spacecraft), the flying object (spacecraft) in the atmosphere
Similarly, the air on the outer surface is also accelerated and moves, so that the occurrence of aerodynamic heating can be reduced. In other words, only the friction between air molecules occurs, and the flying object (spacecraft) can move in the atmosphere at high speed (several km / s to several tens of km / s). However, it is expected that the air (plasma) ionized by the high heat wraps the entire flying object (spacecraft).

(8) The shape of a flying object (spacecraft) can be said to be a sphere or an ellipsoid having the highest functional efficiency from the operating principle and omnidirectionality.

(9) The space area around the flying object (spacecraft)
Since it is locally bent, it will fly due to the gravitational lens effect.
The shape of the projectile (spacecraft) changes, or observations on the ground
Blind spot that is completely invisible due to the position with the person, ie, distance and azimuth angle
Could be possible.(10) When the propulsion acceleration of the spacecraft is 100G and it is necessary to reach Mars
The duration is about 11 hours, and the period required for manned planetary exploration is
Decrease dramatically. (11) Space control by timing control to turn off the magnetic field
It is possible to suck and release objects under the ship.

[0218]

Embodiments of the present invention will be described below with reference to the drawings. 3A and 3B show the appearance of a flying object according to one embodiment of the present invention, wherein FIG. 3A is a schematic top cross-sectional view, and FIG. 3B is a schematic side cross-sectional view.

The flying object 1 according to this embodiment is of an elliptical shape, and the propulsion engines (21 to 26) are provided at four outer peripheral positions obtained by dividing the outer periphery of the disk into four equal parts and at the center positions of the upper and lower surfaces of the disk. It is.

Each of the propulsion engines (21 to 26) has a magnetic energy generating means and a magnetic control means for controlling the magnetic energy generating means in a one-to-one correspondence. It is to be noted that one magnetic control means may be provided as a whole so as to control all the magnetic energy generating means as a whole.

The magnetic energy generating means generates a strong magnetic field to increase the value of the curvature component of the space around the flying object 1 from 0 or a certain value to a certain value. To generate a field. The magnetic control means,
The change in the curvature component of the space caused by the strong magnetic energy is made quasi-antisymmetric locally, and at the same time, in order to obtain the propulsive force, the magnetic field changes in a pulsed manner, or the rotation of the magnetic field changes the space. The magnetic energy generating means is controlled so that the curvature component changes dynamically.

FIG. 4 shows a state in which the propulsion engine 24 shown in FIG. 3B is operated. The flying object 1 receives an external force (pressure difference) PP ′ from an asymmetrical strain field in space and is propelled rightward (in the direction of P ′) in the figure. The same applies to other propulsion engines. Propulsion forces are obtained in directions perpendicular to each other in the vertical direction and the horizontal plane, and movement control in any direction can be performed by a combination of these.

For example, in the flying object shown in FIG.
If the engine is shaped as shown in FIG. 5, the four propulsion engines allow the vehicle to suddenly start and stop in any direction from the stationary state in the air as shown in FIG. 6 (FIG. 6A). , Combination of horizontal movement and vertical ascent (descent) (Fig. 6
(B)), zigzag-like navigation (FIG. 6 (C)), and other arbitrary navigations that cannot be obtained by the conventional propulsion system are possible.

Next, the principle of the propulsion operation has been described above, but in order to facilitate understanding, a practical propulsion concept will be described first, and then the arrangement and configuration of the propulsion engine and the motion of the flying object (spacecraft) will be described. The structural model of a propulsion engine that generates a quasi-antisymmetric space with respect to propulsion, propulsion efficiency, is described.

Conceptual explanation of the principle of propulsion For example, an object in a space around the earth moves (falls) toward the center of the earth. The direct cause of the movement of the object is the effect due to the distortion field due to the bending of the space around the earth, not the effect of the earth itself.
However, since the existence of the earth's mass (density) bends the space, it is an indirect cause for the movement of an object.

The object moves toward the earth center because the gradient of the strain field is generated in the direction of the curvature of the space (vertical direction of the curved surface) generated by the mass (density) of the earth and coincides with the direction of the earth center. (Fig. 7). It should be noted that the curved space and the object are independent and have no interaction.

Now, as a virtual experiment, it is assumed that the earth does not exist, and that only the bending of the space exists in the same region as the above in outer space. An object in a curved field in space will move in exactly the same way (FIG. 8). The curved space and the object are independent without interaction.

This means that in the earth revolving around the sun, even if the sun disappears instantaneously, its influence will reach the earth 8 minutes and 32 seconds later, and until that time, Is a similar interpretation to the fact that it is still revolving around the sun that has already disappeared.

[0229] The principle of this propulsion is that an object (spacecraft) in outer space artificially generates the above-described unidirectional space bend around the object and instantaneously interrupts the generation action. , To create a state of curved space equivalent to the above. However, the state immediately after the generation action is refused is a transition state in which the bent space returns to a flat space, and the bent space and the object (spacecraft) are independent from each other in this process, and there is no interaction ( (FIG. 9).

The acceleration α generated in the curved space area is given by Equation 80, where R ⁰⁰ is the curvature, the light speed is c, and the integral constant indicating the curved area is r.

[0231]

[Equation 80]

If the curvature of the space is uniform (constant value) in the area (FIG. 9), the acceleration α is given by the following equation 81, where s is the area length. Then, the curvature of the space is generated by the mass density ρ or the magnetic field B (Equation 82). That is, the mass field or the magnetic field creates an acceleration field in a space region.

[0233]

[Equation 81]

[0234]

(Equation 82)

The disappearance of an object is impossible unless a virtual experiment is established or an explosion actually occurs. However, the equivalent of annihilation of an object can be easily achieved by OFF control in a magnetic field.

In order to propel the spacecraft, a space distortion surface as shown in FIG. 10 is ideal. That is, the area A 'is a flat space having a curvature R ⁰⁰ = 0, and the area A is a space having an antisymmetric curvature such as a curved space (a distorted space) having a curvature R ⁰⁰ ≠ 0. . The magnitude of the acceleration field generated in the curved space area A, that is, the acceleration α
Is the universal gravitational constant, μ, assuming R ⁰⁰ is uniform.
_{As described above, 0} is given by Equation 83 as the magnetic permeability of vacuum, and the magnetic field B generates an acceleration field in the space region.

[0237]

[Equation 83]

However, practically, as shown in FIG.
The distortion surface of the space is spherically symmetric around the spacecraft engine.
It does not affect promotion. Within a finite time during which the spacecraft moves under the thrust of the acceleration field in the area A, the distorted surface of the curved space in the area A 'has already returned to a flat space (R ⁰⁰ = 0 ). There is no reverse thrust due to the 'acceleration field.

Time τ at which a bent space returns to a flat space
Is given by τ = 1 since the space distortion speed is the light speed c.
/ C is constant. This thrust received from the acceleration field is a body force equivalent to gravity, and is proportional to the mass of the volume element. Therefore, in the state of FIG. 'There is no reverse thrust.

Further, in practice, as shown in FIG. 12, the space where the strained surface of the region A ′ is weaker than the strained surface of the region A, that is, (the curvature R ⁰⁰ ′ of the space of the region A ′) ) <
It may be a space having a quasi-antisymmetric curvature such that (the curvature R ⁰⁰ of the space of the region A). The space having this quasi-antisymmetric curvature is generated by controlling the magnetic field distribution in the spacecraft engine.

Assuming that the magnetic fields of the engine whose distributions are antisymmetrically controlled are B and B ', respectively, the curvature of the space in the area A is represented by Equation 84, and the curvature of the space in the area A' is represented by Equation 85. Therefore, when controlling to B '= (1/10 to 1/40) × B,
The curvature R ⁰⁰ ′ of the space of the region A ′ is R ⁰⁰ ′ = (1/100
~1 / 1600) × R ⁰⁰ next, as a numerical order, R ⁰⁰ '"R ⁰⁰ to be able to quasi-anti-symmetric space.

[0242]

[Equation 84]

[0243]

[Equation 85]

[0244] 'While masses not spacecraft, the region A' region A acceleration α in 'The formula 86, Although the acceleration α in the region A is a formula 87, R ^00' from "R ⁰⁰ , Α '<< α
Thus, the spacecraft can propel the quasi-antisymmetric space shown in FIG.

[0245]

[Equation 86]

[0246]

[Equation 87]

Further, the time τ in which the curved space in both the region A and the region A 'returns to the flat space is the same, and the space curved while the spacecraft accelerated in the region A moves to the region A'. It has already disappeared, and α ′ = 0. In addition, since the mass body (mass m) of the spacecraft is not in the region A 'and most of the spacecraft is in the region A, the thrust due to acceleration f _A = mα and f _A ′ ≒
Since 0 × α ′ = 0, the reverse thrust by the area A ′ can be treated as a minute amount from the beginning.

Engine Arrangement and Flying Object (Spacecraft) Mobility FIG. 13A shows six engines arranged as shown in FIG. 3. In this arrangement, movement in all directions is possible. It is possible. Activate the front engine for forward, activate the rear engine for reverse, activate the right engine for rightward, activate the left engine for leftward, and upper for climb The engine is operated, and the lower engine is operated for descent. However, since the propulsion direction is a vector composition of the propulsion direction of each engine unit, the flying object can move in all directions.

For example, a left-right turn is performed as follows. At an acceleration of 100G ≒ 1km / s ^2, the operation for one second of the front engine, uniform linear motion of the 0 → 1km / s after one second. That
After that, after 1 second of operation of the rear engine, 1 km / s after 1 second
→ Stop at 0. Then, the left engine operates for 1 second
One second later, at 0 → 1 km / s, go left at a right angle (constant speed linear
Move).

Then, the engine is formed in the sphere,
As shown in FIG. 13 (B), if the type of the engine is formed by connecting two spheres (small and large spheres) from one sphere into a bowling pin shape, the number of engines is reduced. Can be reduced. In the figure, the upper small ball corresponds to the upper engine and the lower large ball corresponds to the lower engine.

Even if four such pin-shaped engines are arranged as shown in FIG. 13 (C), they can be moved in all directions. Even if three of the pin-shaped engines are arranged in a regular triangular shape, they can be moved in all directions by changing the engine control performance.

Structural Model of Propulsion Engine As a function of the engine, it is required to form a unidirectional surface force field as a space pressure by giving a curvature to the space. The quadratic curved surface of the thin layer in the space where the surface force is generated is called the space distortion surface. The surface force is directed inside the distorted surface.

The curvature component of the space controlled by the magnetic field B is given by Equation 88. This strong magnetic field is generated by a superconducting magnet confined within a shell of a perfect diamagnetic material (superconducting material) having a spherical strength. Caused by The reason for using a completely diamagnetic material is to obtain only the curvature of the space purely without confining the magnetic field in the engine inside and exposing it to the external space. In the space around the engine, a spherical distortion surface is generated as a spherically symmetric field (FIG. 14).

[0254]

[Equation 88]

Since the engine receives a surface force toward its center in a spherically symmetric manner from the distorted surface of the space, the surface force is balanced and the engine cannot move. However, other substances in the field of the distortion around the engine move toward the center of the engine under the surface force in the direction of the spherical center.

For propulsion, the engine is required to generate an antisymmetric unidirectional strain field in a space region. That is, the curvature R in one half area of the space around the engine
⁰⁰ ≠ 0 (curved space), R ⁰⁰ =
It is necessary to generate an antisymmetric field of 0 (flat space) by controlling the direction of the magnetic field.

Therefore, the principle structure of the magnetic energy generating means in the propulsion engine is as shown in FIG.
A main superconducting magnet 31 for generating a spherically symmetric magnetic field, and an auxiliary superconducting magnet 3 arranged in a hemispherical magnetic field on one side of the main superconducting magnet 31 so that the polarity of the magnetic field is reversed.
And 2. Since the magnetic field required for propulsion is several tens of billions of Tesla and cannot be realized by ordinary magnetic field generating means, a superconducting magnet is used.

As a result, an antisymmetric one-way distortion field shown in FIG. 16 is generated. Since the engine receives an antisymmetric surface force, it moves in one direction toward a flat space region having zero curvature. Other substances in the space region on one side of the engine (curvature ≠ 0) likewise move toward the flat space region with zero curvature. Therefore, if the generation of the magnetic field is ON / OFF controlled, the flying object (spacecraft) can be propelled.

Note that the magnitude of the magnetic field is B ² = B · B = |
B | ² , two different magnetic fields B ₁ and B
_2. Assuming that the combined magnetic field is B _T , Expression 89 is obtained. When the two magnetic fields have the same magnitude, Equation 90 is obtained when the direction of the magnetic field is forward, and Equation 91 is obtained when the direction of the magnetic field is reverse.

[0260]

[Equation 89]

[0261]

[Equation 90]

[0262]

[Equation 91]

Propulsion Efficiency and Energy Formula Next, the propulsion efficiency of the propulsion engine will be examined from the viewpoint of energy conversion for explaining the magnetic control means. The conversion flow is as follows: supply power energy (P _WE ) → superconducting magnetic field energy (E _MAG ) → curvature of space (R ⁰⁰ ) → strain energy stored in space (U _STRAIN ): = engine output energy (E _NG P _WR ) →
Release of spatial distortion energy → Effective propulsion energy (E _EFP )
+ Reactive propulsion energy (E _LOS ) + radiant energy (E _RAD ). The efficiency in each phase is as shown in Equations 92 to 95,
The efficiency η of the whole engine is expressed by Expression 96.

[0264]

(Equation 92)

[0265]

[Equation 93]

[0266]

[Equation 94]

[0267]

[Equation 95]

[0268]

[Equation 96]

The distortion energy U stored in the space
_STRAIN (engine output energy) is given by equation (97), and (effective propulsion energy + ineffective propulsion energy + radiant energy) is given by equation (98).

[0270]

(97)

[0271]

[Equation 98]

In equation (98), V ₁ and ρ ₁ are the volume and average density of the flying object, V ₂ and ρ ₂ are the volume of the finite region around the flying object and its average density (atmospheric density if in the atmosphere), h And ν are Planck's constant and radiant energy frequency. In other words, the reactive propulsion energy means an energy loss for accelerating the surrounding atmosphere in the same manner because the thrust is body force. Further, it is considered that not all of the space distortion energy is converted as propulsion energy, and a part is emitted as radiant energy.

The overall efficiency of the engine is given by Expression 99 from the viewpoint of the power.

[0274]

[Equation 99]

In Equation 99, f is the body force of the field (N /
m ³ ), V is the working area (m ³ ), fV = F is the thrust (N), v is the propulsion speed (m / s), ν is the number of superconducting engine excitation cycles,
E is the superconducting coil exciting voltage (V), I is the superconducting coil exciting current (A), and τ is the current pulse width (s).

In short, from equation (99), the propulsion speed can be controlled by varying the number of engine excitation cycles ν, and the thrust basically depends on the power EI of the power source, and is controlled by varying the excitation current I.

As a result, the magnetic control means is configured to control the repetition frequency of the exciting current pulse. As a result, the magnetic field changes in a pulsed manner, and a dynamic change in the curvature of the space is obtained with the ON / OFF of the magnetic field, and the projectile (spacecraft) flattens the curved space when the magnetic field is cut off. As a result of the transition process returning to a natural space, the thrust as an action from the space field can be instantaneously received and propelled.

Now, a specific example of the magnetic field generating means will be described.
In this method, a strong magnetic field is obtained by freezing magnetic flux and laser beam implosion (FIGS. 17, 18, and 19).

First, the freezing of magnetic flux will be described briefly. Flux freezing is also called magnetic field freezing, which is a phenomenon in which when a highly conductive fluid moves in a magnetic field, magnetic flux (lines of magnetic force) adhere to the fluid and try to move together. In principle, when there is a relative motion between the highly conductive fluid and the magnetic field, a current is induced by electromagnetic induction, and the current and the magnetic field interact to try to cancel the relative motion between the fluid and the magnetic field. As a result, the fluid and the magnetic field move together as if the lines of magnetic force were attached to the fluid. Since the magnetic field is attached (frozen) to the fluid, the line of magnetic force is dragged and deformed or strengthened by the movement of the fluid.

This phenomenon has been proposed as a hypothesis to explain the magnetic field of celestial bodies as a fossil mechanism. In other words, when a star is born by the contraction of the interstellar gas and the magnetic field lines are frozen in the gas, the magnetic field lines are concentrated with the gas contraction, and the star has a poloidal magnetic field. It is estimated to be about 500 million Tesla for a neutron star, which corresponds to the observation result.

In FIG. 17, (a) shows a state where the magnetic flux (lines of magnetic force) is frozen in the highly conductive fluid particles.
(B) shows a state in which the fluid particles are contracted by the action of an external force or the like, and the lines of magnetic force are also contracted accordingly, and (c) shows a state in which the fluid particles are further contracted to have a poloidal type. Since the magnetic flux frozen in the fluid particles also undergoes the same contracting motion with the contraction of the fluid particles, only the magnetic flux passage area S (m ² ) contracts and decreases while the magnetic flux φ (Wb) is preserved. Therefore, the magnetic flux density, that is, the magnetic flux intensity B (Tesla) is B = φ / S, and the value increases and the magnetic field is concentrated.

FIG. 18 shows the principle of strong magnetic field concentration.
An initial magnetic field is applied to the sprayed liquid particles of the highly conductive liquid metal or the liquid metal that has been poured as it is in advance, and the magnetic flux is frozen. Thereafter, laser light is applied to the region of the fluid particles or liquid metal whose magnetic flux has been frozen from the four sides. The surface of the irradiated fluid particles or liquid metal is heated and plasma emission starts, and the fluid particles or liquid metal
The genus is compressed toward the center by the reaction of the plasma blast.
The so-called implosion effect is achieved, and plays a role to further enhance the contraction effect of the optical pressure by the laser beam. It should be noted that an asymmetric distribution of the magnetic field can be obtained by controlling the left and right laser beam intensities (for example, right intensity> left intensity).
The auxiliary superconducting magnet 32 shown in FIG.

As described above, the fluid particles or liquid metal contracts rapidly due to the light pressure of the laser beam and the ablation (spouting) pressure generated by the reaction of the high-temperature plasma gas, so that the magnetic flux frozen by the fluid particles also contracts. , A magnetic field enrichment is achieved.

The laser light power density S (W / m ² ) is given by S = u · C, where u is the light pressure (Pa: = N / m ² ) and C is the speed of light. Considering the area ratio (1 / r) due to concentration, the laser light power density is S = u · C · (1 /
r).

Since the power density of the laser beam currently in practical use is about 10 ¹⁷ to 10 ¹⁸ (W / cm ² ), assuming a radius ratio of 1/1000 due to concentration, the area ratio is 1 / r = 1/10
⁶ From S = 10 ¹⁷ (W / cm ² ) = 10 ²¹ (W / m ² ), the laser light pressure u becomes 10 trillion atm. Due to the light pressure including the implosion effect of the laser light, the magnetically frozen good-conductivity fluid particles are rapidly contracted, and a strong magnetic field is concentrated.

FIG. 19 shows a strong magnetic field generator.
This strong magnetic field generator generates a magnetic field (seed magnetic field) in the nozzle 42 by spraying and injecting the liquid metal as a good conductive fluid into the blanket 41 as a fluid or as sprayed fluid particles. superconducting mug nets 43 to be, the same 44, the laser light source 45 to provide light pressure and implosion effect fluid particles or liquid metal and flux frozen in the blanket 41, the same 46, the fluid flux freeze is released Exhaust pump 4 for exhausting particles or liquid metal
7 and a liquid metal storage container 48, and is a device capable of continuously generating a pulse magnetic field of several hundred thousand Tesla to several hundred billion Tesla.

In FIG. 19, the initial magnetic field (seed magnetic field) is 5
An operation of continuously generating a pulse magnetic field of 500,000 Tesla at 0 Tesla will be described. First, a highly conductive liquid metal is sprayed from the liquid metal storage container 48 by the nozzle 42 as atomized particles.
Alternatively, the liquid metal is sprayed and injected into the blanket 41. Then, the upper and lower superconducting magnets (43, 4
4), the initial magnetic field (5
0 Tesla). The magnetic field is frozen into the injected fluid particles or liquid metal .

Next, a pulse laser beam is applied to the fluid particles or liquid metal from the laser light sources (45, 46). The power density of this pulse laser beam is 10 ¹⁸ W / cm ² = 10 ²² (W / m ² )
It is. At this time, light pressure is ^{10 22/3 * 10 8 =} 3 * 10 13 Pa
Which is equivalent to 300 million atmospheres. Then, by a laser beam implosion effect, assuming a radius ratio 1/100, 1/10 ⁴ Area Ratio Since the fluid particles or at a pressure of 3 trillion atmospheres in light of the present effect
Or shrink the liquid metal . In this case, since the area ratio is 1/10 ⁴ , the initial magnetic field of 50 Tesla is 50 * 10 ⁴
= Concentrated to a magnetic field of 500,000 Tesla. In addition, 500,000 Tesla
Has a magnetic pressure of 1 trillion atmospheres.

This magnetic field concentration process proceeds until the magnetic pressure and the laser beam pressure are balanced. When the pulse irradiation of the laser beam is completed, the light pressure decreases, so that the contracted fluid particles or liquid metal attempts to expand and explode due to the magnetic pressure. At this point, the superconducting magnets (43, 4)
The magnetic field generation operation of 4) is stopped. Fluid particles that are frozen and released in the blanket 41 due to the stop of the magnetic field
Alternatively, the liquid metal is exhausted by the exhaust pump 47 and returned to the liquid metal storage container 48 again. In this process, a demagnetizing action is performed as necessary.

The above process is defined as one cycle, and is repeated several thousand cycles per second. That is, a strong magnetic field of 500,000 Tesla is generated by a continuous pulse of several KHz. Then, as described above, the intensity of the left and right laser light sources (45, 46) is controlled. That is, the present apparatus includes the magnetic energy generating means and the magnetic control means.

Although the generation of a strong magnetic field of about 500,000 Tesla, which is the most feasible with the existing technology, has been described above, the intensity of the generated magnetic field depends on the laser beam power density and the radius ratio obtained by the implosion effect. The difference can be understood from the above description.

That is, the present apparatus freezes a magnetic flux of 50 Tesla to 500 Tesla from a magnetic field of 50 Tesla into a spray-like particle or liquid metal of a highly conductive fluid (liquid metal), and laser light (power density: 10 ¹⁴ (W / cm ² 〜10 ¹⁸ W / cm ² )
An initial magnetic field of 50 Tesla to 500 Tesla is concentrated to 1 / 10,000 to 1 / 100,000,000 times by fluid contraction of 10,000, and therefore 1 / 10,000 to 1 / 100,000,000 by area ratio.
An ultra-strong magnetic field of 10,000 Tesla to 5 million Tesla to 50 billion Tesla can be generated in pulses.

Also, spraying of spray-like particles or liquid metal
Since the pouring and laser beam irradiation can be controlled mechanically and electrically, a continuous pulse operation of several KHz to several tens of MHz can be easily performed. Note that a structure such as a liner for concentrating the magnetic field is unnecessary, and there is a feature that the structure is not destroyed by a giant magnetic pressure accompanying the generation of the magnetic field. In addition, as a laser light source
Uses an organic dye laser by forced mode locking.
This organic dye laser has a large power density pico pulse.
Because the laser can be realized by repetition of several MHz to several GHz.
is there.

Table 2 shows the expected main performance data of the flying object according to the present invention.

[0295]

[Table 2]

For reference, the book on space-driven propulsion spacecraft
The formula for calculating the body is expressed as
Equations 101 and 102 are shown in FIG.
21).

[0297]

[Equation 100]

[0298]

[Equation 101]

[0299]Note that in equation 100, R ⁰⁰ : Space
Curvature (1 / m ^Two ), B: magnetic field (Tesla), c: speed of light (of space
Strain propagation speed) (m / s), S: Area length of curved space
(M), L : Spacecraft body length (m), N: Propulsion pulse repetition
Frequency (Hz): = Number of propulsion pulses per second, α
_NET : Net acceleration received by the spacecraft (m / s ^Two ), Τ: thrust
Effective time (propulsion pulse width) (s), t: acceleration time (engine
Operating time) (s), M: spacecraft mass (Kg), V: spacecraft
Speed (m / s), F: Spacecraft thrust (N).

In equation 101, ε: propulsion pal
Laser energy (J) for one cycle (T = 1 / N), k:
Number of inertia holding pulses, ε _s : Ray per inertia holding pulse
The irradiation energy (J), S _D : laser power density (W /
m ² ), t _L : laser irradiation time (s), A: laser irradiation area
( M ² ), χ: Implosion radius ratio (≪1), u: Implosion laser light pressure
(N / m ² : = Pa), _Pu : magnetic pressure (N / m ² : = Pa), E:
Energy supplied per second (J / s: = W): = Engine
This is the supply power P _E (W).

As a calculation example, the length of the spacecraft
Diameter) L = 15m, curved space area S (= 3L) = 45
m, magnetic field B = 80 billion Tesla
Shown below. Investigation on laser implosion engine started
Immediately after, I want to keep it as a guide only. τ =
t ₂ = L / c = 50 ns, t ₁ = S / c = 150 ns, t ₃ = 0 ns.
Set the maximum value of N = 1 / t ₁ and N = 6.7 MHz. R ⁰⁰ = 5.3 ×
10 ^-16 (1 / m ² ), α = 2146 m / s ² = 219G, α _NET = 36G. P
_u = 2.5 × 10 ²⁷ Pa. ε = 10MJ, k = 10, t _L = 0.1Ps
, A = 0.0314 cm ² , χ = 0.2 × 10 ⁻⁵ and S _D = 3.2
^{× 10 24 W / m 2,} u = 2.7 × 10 27 Pa , and the I and u ≒ P _u
You. E = P _E = 67 TW. Maximum propulsion acceleration of one engine 3
6G, supply power 67TW. Spacecraft propulsion direction 3 engines
With a maximum propulsion acceleration of 108 G and a supply power of 200 TW.
You. Control of spacecraft speed and thrust is based on repeated propulsion pulses.
The propulsion acceleration by 108G
~ 36G ~ 1G ~ 0G can be reduced. For example, 1G
In the case, the spacecraft's body height L = 5 m and the curved space area S
= L = 5m, magnetic field 80 billion Tesla, N = 4.9MHz,
τ = t ₂ = L / c = 17 ns, t ₁ = S / c = 17 ns, t ₃ = 170 n
s, R ⁰⁰ = 5.3 × 10 ^-16 , α = 236 m / s ² = 24G, α _NET
= 1 G, E = P _E = 4.9 TW. Power is laser irradiation time
If t _L is set to 0.01ps (10f _S ), each calculation example becomes 1/10
Become.

[0302] In addition, the electric power required for the propulsion device is generated.
Power source is a small liquid
Genus MHD generator (MHD power generation using liquid metal as working fluid)
), The anti-proton-proton pair annihilation reaction
The used anti-particle annihilation reactor is used.

[0303]

【The invention's effect】 As described above, the flying object of the present invention
According to the propulsion device, the propulsion force of the flying object is
Force equivalent to gravity that penetrates the entire interspace (space distortion
Power), including the flying object and the crew inside the flying object
The mass is accelerated by the same force, and the inertial force
There is no use, and crew members are not destroyed.

[0304] It is a propulsion system that theoretically eliminates inertial force,
Therefore, sudden start in all directions from sudden stop in the air, sudden
Arbitrary navigation, such as stopping, right angle turning, zigzag turning and V-shaped turning
Law becomes possible.

[0305] Also, since the propulsion is equivalent to gravity,
In principle, the final speed is about the speed of light (quasi-light speed).
Is possible.

[0306] Furthermore, the propulsion device of the present invention
Noise (propeller sound, gas injection sound, etc.)
It is possible to fly quietly without generating noise. Also, the navigation
Stable (arbitrary in the air to low speed to high speed)
High safety because no fuel is loaded.

[0307] In addition, the propulsion power is
Since it acts on the body, the air on the outer surface of the flying object is also accelerated
Therefore, the occurrence of aerodynamic heating can be reduced. Toes
Sky It only causes friction between gas molecules and air molecules,
Flying objects travel in the atmosphere at high speed (several km / s to several hundred km / s)
You can move with.

[0308] From the above, navigation in outer space at the speed of light
Ability to fly and at high speed in the atmosphere with any flight pattern
Expect various excellent effects in combination with the ability to navigate
And further reduce navigation time for planetary exploration (for example, to Mars
One-way half day) has a great effect.

[Brief description of the drawings]

FIG. 1 is an explanatory diagram of a basic structure of a space.

FIG. 2 is an explanatory diagram of a surface force difference as a driving force.

FIG. 3 shows the appearance of a flying object according to an embodiment of the present invention,
(A) is a schematic top sectional view, (B) is a schematic side sectional view.

FIG. 4 is a diagram illustrating the principle of a spatial distortion propulsion mechanism.

FIG. 5 is a layout diagram of four propulsion engines.

[6] Ri navigation illustration Der by propulsion engines of six or four, the (A) is sudden acceleration and stopping from hover shows
(B) shows a right-angle flight, and (C) shows a zigzag flight.
Indicates a row.

FIG. 7 shows spatial distortion around the earth and an object M in this space.
FIG.

FIG. 8 shows an object M in the case where there is a unidirectional spatial distortion similar to the space around the earth in a space such as the earth where there is no mass body.
FIG.

FIG. 9 is an explanatory diagram of a propulsion principle of the present invention.

FIG. 10 is an explanatory diagram of an ideal space distortion surface for propelling a spacecraft.

FIG. 11 is an explanatory view of a practical space distortion surface for propelling a spacecraft.

FIG. 12 is an explanatory view of a practical space distortion surface for propelling a spacecraft.

13A and 13B are explanatory diagrams of a layout configuration of a propulsion engine and motility of a spacecraft. FIG. 13A shows a case of six engines,
(B) shows the type of engine, and (C) shows the case of four engines.

FIG. 14 is an explanatory diagram of a spatially distorted surface formed by one superconducting magnet.

FIG. 15 is an explanatory view of the principle structure of the propulsion engine of the present invention.

FIG. 16 is an explanatory diagram of a spatially distorted surface formed by the propulsion engine of the present invention.

FIG. 17 is a conceptual diagram of magnetic field concentration by magnetic flux freezing,
(A) is a state diagram in which the magnetic flux is frozen in the highly conductive fluid particles,
(B) is a state diagram in which the fluid particles contract due to the action of an external force or the like, and the magnetic flux is also contracted accordingly, and (c) is a state diagram in which the fluid particles are further contracted.

FIG. 18 is a diagram illustrating the principle of a strong magnetic field generator according to one embodiment of the present invention.

FIG. 19 is a configuration block diagram of a strong magnetic field generator according to one embodiment of the present invention.

FIG. In operation state diagram by engine ON / OFF
is there.

FIG. 21 FIG. 4 is an explanatory diagram of operation pulses.

[Description of Signs] 1 Flying object 21 to 26 Propulsion engine 31 Main superconducting magnet 32 Auxiliary superconducting magnet 41 Blanket 42 Nozzle 43 to 44 Superconducting magnet 45 to 46 Laser light source 47 Exhaust pump 48 Liquid metal storage container

Claims (2)

(57) [Claims] 1. A spherical magnetic field is generated to generate a strong magnetic field for changing the curvature component of the space inside a flying object (aircraft, manned rocket, spacecraft, etc.) and the space around the flying object.
The main superconducting magnet produced is a spherical body made of superconducting material.
A magnetic energy generating means disposed in the space; controlling a mode of generation of a strong magnetic field by the magnetic energy generating means to locally control a change in a curvature component of the space in a quasi-antisymmetric manner, and generating gravity in the space; Control means for setting a spatial distortion force equivalent to the propulsion force of the flying object,
A magnetic field of opposite polarity is placed in a hemispherical magnetic field on one side of the conducting magnet.
The generated auxiliary superconducting magnet is placed, and both superconducting magnets are
Change and control the repetition frequency of the excitation current pulse of the net
And a magnetic control means. 2. A flying object (aircraft, manned rocket, spacecraft)
Change in the curvature component of the space inside and around the projectile
Magnetic energy generator that generates a strong magnetic field to give
Generating a strong magnetic field by the magnetic energy generating means.
Controlling the raw aspect to locally change the curvature component of the space
Space controlled by quasi-antisymmetric and equivalent to gravity generated in the space
Magnetic control means for using the distortion force as the propulsion force of the flying object
And a propulsion device for a flying object comprising:
Energy generation means contains liquid metal, which is a highly conductive fluid
Liquid metal storage container and a spherical container that generates a strong magnetic field
A liquid from the liquid metal storage container;
Metal as a fluid or with spray-like fluid particles
And a nozzle for injecting into the blanket;
The blanket is placed on the opposite wall of the racket
A pair of superconducting magnets that generate an initial magnetic field in the unit
And orthogonal to the arrangement direction of the pair of superconducting magnets.
Placed on opposite sides of the blanket wall on both sides to freeze magnetic flux
Irradiates pulsed laser light to the fluid particles or fluid
A pair of laser light sources; and the fluid particles unfrozen
Or to recirculate fluid to said liquid metal storage vessel
And an exhaust pump; wherein the magnetic control means comprises:
Excitation current control for a pair of superconducting magnets,
Asymmetric control of laser light source and injection of fluid particles or fluids
It performs control, etc., which repeats the process from exhaust to exhaust at high speed.
A propulsion device for a flying object, characterized in that: