JPS61234000A - Physical apparatus for interaction of electron and photon - Google Patents

Abstract

A physical instrument for electron-photon interactions and more particularly a physical instrument for production, recording, observation and transmission of temporospatially adjustable electron-photon interactions. The instrument comprises a ring-shaped vacuum tube with an electron injector, a linear accelerator, signal deflecting and collimating means operatively connected to the vacuum tube with free-flight intervals of the tube between adjacent means, interaction recording components associated with the tube in the free-flight intervals thereof, and a computer processing unit with a display, which is operatively connected to the accelerator and the interactton recording components.

Description

DETAILED DESCRIPTION OF THE INVENTION [Industrial Field of Application] The present invention provides a temporally and spatially adjustable (temporo-a
(patially adjustable) Physical devices for generating, recording, observing, and transmitting electron-photon interactions.

[Prior art and problems to be solved by the invention]
At present, the relativistic conditions of the rotating black hole Ipe/Tohorizon are based on the actual time/space, matter/radiation (temporo-
spatial matter-radiation
) is thought to be related to the transition of interactions between

On the other hand, space e-time is generally thought of as an established, fixed, and complete entity, or "block universe," which contains many equally well-ordered parallel or alternating realities.

It has been seriously proposed that one means of creating such a transition or transition between different regions of space and time is to travel to and pass through a black hole star. However, there is little chance that such a journey will lead to a successful return to the current observation coordinates or a signal back, and there is also little chance that they can be controlled and adjusted. Therefore, this would be an impractical and unfeasible method. Another unlikely method would be to have an unmanned observation vehicle pass through the black hole's event horizon and communicate with it after the time/space transition.
This is due to extremely large and physically destructive gravitational forces connected to currently known black holes. It is clear that the physical conditions correspond to the actual existence of matter-radiation interaction transitions in spacetime, and that the concrete equipment that actually performs such transitions is consistent with the speed of the rotating black hole event horizon. This can be achieved with rotation close to C (C is the speed of light),
It is also clear that it can be done. Therefore, it is possible to recreate and construct the physical mechanisms and the time-space, matter-radiation interaction transitions of the rotating black hole event horizon without destructive gravitational processes.

The aim of the invention is to provide a physical device it which produces interactive transitions by means of material components rotating with sufficiently high speed and which is detected and recorded by means of observation and processing components. This device is based on the current laws of physics and, by virtue of its own principle, avoids the need to enter into the gravitational traps that characterize black hole stars, and allows for a time-dependent response to the rotating black hole event horizon. Specifically execute and display spatial, material, and radiation transitions.

[Means for solving problems]

In order to achieve the above object, an apparatus based on the present invention includes an annular vacuum tube, an electron injector for supplying electrons to the tube, a linear accelerator for accelerating the electrons supplied to the tube, and an annular vacuum tube for supplying electrons to the tube. several deflection and parallel means connected to exert an effect on the tube with free-flight sections therebetween; and an interaction recording device connected to the tube within the free-flight section of the tube;
A computer processing device operatively connected to the accelerator and the interaction recording device, and a display connected to the computer processing device.

〔Example〕

The law governing all electron-photon interactions is the absolute velocity C of the photon relative to the electron. In normal perceptual observation, mutual aspects of interaction, radiating and receiving, occur within a complex system, each having reference coordinates. In the observed coordinates, this requires an adjustment of the apparent velocity of the object based on the well-known relativistic correction equation:

V:= (V1+y2),'+14(v, v2)
/c" 1 However, laws must be applied directly to electron-photon absorption or emission, respectively. In this case, the velocity components of a single photon and a single electron, and the discrete interaction process It is necessary to take a direct vector summation with the total velocity C.The idea of the invention is to combine a system of a single fast electron with a slower virtual photon, i.e. a correspondingly transitioned region of the surrounding proton universe. It is to use the addition of the fundamental velocity vectors as described above by direct interaction with slow virtual photons from the .

One practical method for producing and implementing the fast electrons is a synchrotron-type annular particle accelerator, with modifications based on the novel and special objectives and requirements of the present invention. Furthermore, we will connect devices for interaction detection, recording, observation, and transmission to create new and special devices.

The device shown in FIG. 1 extracts electrons into an orbital acceleration path, controls their speed, and holds them in the path at high speed.

The speed is controlled to a high speed very close to C.

Furthermore, the apparatus of FIG. 1 records the radiative interactions of these electrons with other regions of spacetime. This recording is performed at repeated locations of the target flight section of the electron orbit path in stages.

This device is an electron accelerator that is a modified synchrotron/electrosono-X tracing type.

An electron injector 10 is provided for injecting electrons. The electronic injector 10 is provided at one or more locations inside or outside the device frame. The device frame may be movable, fixed, or otherwise. Electron injector 10 injects electrons into toroidal vacuum tube 11 . The vacuum in the toroidal vacuum chamber 11 is created by a vacuum pump mechanism (not shown).

Electrons are linearly accelerated to and maintained at a desired speed within the annular tube by a steerable energy source within the radio frequency resonant cavity 12 or other linear accelerator device.

The electrons are accelerated (deflected) by the electromagnet 13 into a stepwise annular path trajectory. 1! , FBBi12, 0 placed at equal intervals around the tube's periphery.The number of electromagnets is variable and the power supply of the WL@stone is matched to the velocity of the electrons, i.e. the strength applied to the linear accelerator of the device. The orbital deflection electromagnet is combined with a focusing magnet 14 (magnetic lens or collimator) 4 to hold the child in a narrow aligned beam-like trajectory.

Between each combination of deflecting magnets 13 and focusing magnets 14, the shape of the free-flying electron path and the corresponding shape of the vacuum tube are straight. In all of these sections, the movement of electrons is not accelerated, except where the electron injector and linear accelerator are installed. Within this repeated free flight section, the interaction cone direction 15
is placed. The radiative interactions at visible and low radio frequency wavelengths, 1+ at high radio frequency wavelengths, are said to be oriented along the same relative action cone with respect to the direction of the electrons in the free flight path. In other words, when electrons are accelerated into orbit by a deflecting electromagnet, they are oriented in the same conical direction as synchrotron radiation, as shown at number 16, and at the point number 16, there is radiation from the deflected high-speed electrons. The direction and distribution of the synchronous radiation are shown.

The faster the electron moves, the more parallel the cone becomes along the electron's propagation axis. Therefore, as shown by number 17, the space-time direction of the electron-photon interaction in the free flight section is shown at the number 17, where the spatial position and direction of the interaction source are given, but i! It has a similar distribution and similar velocity to the child synchrotron radiation cone.

In the free flight section where high-speed electrons are neither accelerated nor deflected, the speed is slower than the speed of light and is 11 times faster than the speed of the electron.
Only slow photons can directly interact with electrons within the narrow cone. Same as all electron-photon interactions (,
A corresponding deceleration/acceleration of the electrons is necessarily produced in the interaction. These processes can be recorded as disturbances in the essentially uniform flow of electrons. There are several ways to measure the changes in the electric field that occur around the flow of electrons over part or all of the zero-free interval. Existing recording devices such as sufficiently sensitive interferometers, particle counters, electrostatic cathode ray oscilloscopes/oscillographs, or combinations thereof can be installed in the physical device. These recording devices are capable of tracking and displaying very small changes and can face the interior of straight free flight zones. In this way, the pattern of electron flow can be measured both in absolute terms and in comparison to records from other free-flight sections of the ring. By rotation about the vertical axis of the ring,
Said straight section can cover the entire horizontal circumference of the device. A slight rotation of the total vacuum tube or its support about the electron propagation axis also resolves the ambiguity in the corresponding direction due to the cross section of the interaction cone.

There are two types of interactions between electrons and photons. They are absorption and radiation. In this device, the absorption of a photon in the free-flight leg represents an interaction with a past region of space-time, and if this occurs for a sufficiently large number of electrons, the field recorder measures this as a corresponding deceleration of the electron flow. I can express it. The radial process in the direction of the interaction cone represents the communication with the future region and is measured and expressed as an acceleration.The magnitude of the deceleration and acceleration obtained from one recorder corresponds to the strength of the source, and the number of events is corresponds to source size and density.

Devices come in various sizes. The most practical size is a diameter of the electron orbital ring of 15 to 100 meters or more.

Electrons orbit inside a toroidal vacuum tube.

the vacuum tube is optically opaque or transparent;
Its center is an aperture, a hole, or capable of being apertured. The vacuum in the tube can be achieved and maintained by a pump mechanism, or it can be done automatically, for example in space, in which case the tube is replaced by a centripetal open slit and equally spaced electromagnets are used. , explodes a strong electromagnetic field and accelerates the electron on a stepwise orbit path □ Between the deflection Wl ship stones, the electron's trajectory is non-accelerated and straight n The electrons deflected in this stepwise orbit, etc. The basic features of the present invention are as follows: The accelerated electrons are collected as a pulse.
Due to the rotation of a large number of electrons gathered together,
A "front" or "horizon" is established at which several separate and independent direct electron-photon interactions occur together, so that they are synchronized and multiplexed so that they can be recorded. degree.

) Electrons are brought to a wide range of predetermined velocities in the accelerator by one or more resonant cavity radio frequency energy sources, up to a velocity very close to C, and the velocity of the electrons is therefore controlled by a simple energy controller. very precisely set,
(bl) Each time an electron is accelerated under the deflected tFa stone, so-called synchrotron radiation occurs. interaction, but simultaneous emission with deflection of electrons in a manner similar to electron emission in the Bohr orbital model of hydrogen spectroscopy.However, one important feature of synchrotronic emission is that the spatial There is a direction. This direction becomes parallel to the non-accelerated electron propagation axis as the velocity of the electron approaches C, as shown in number 16. Since other radiative interactions are also considered to take the same direction, , this direction depends on the direction and velocity of the electron at each moment of its path.

The only uncertainty is the continuously increasing cross section of the radiation cone along the electron path at low propagation speeds, but since the dimensions of this cross section can always be determined from said speeds, the exact direction of interaction is , for example, as shown in FIG. 2, is determined by rotating the electron path or storage ring or its support base over the same cross-sectional area about the electron propagation axis.

In short, the Zincrontron type particle accelerator modified and tuned according to the special conditions and characteristics of the present invention provides a practical device for maintaining the synchronous operation of electrons, can control a wide range of speed, and It can approach the speed of At this speed, direct electron-photon interactions with virtual photons from other space-time regions of the universe, which are correspondingly slower, occur, and the interaction known and performed in connection with the movement of electrons by synchrotronic radiation occurs. Directed along the cone of action.

Therefore, as shown in number 17, the closer the electron velocity is to C, the more the center of the electron flow is parallel to the direction of the interacting virtual photon. As explained in connection with Fig. 2, depending on the position of the virtual photon source and the slow electron speed,
It is determined by rotating the electron path (accelerator tube) around the propagation axis. In this way, since the direction and velocity of each electron can be determined at any point on the orbit, the velocity of the photon interacting with the electron, that is, the velocity of the photon added to C, can also be easily calculated. This velocity also gives the time transition of the interaction. If it is a head-on interaction and the speed of the electron is 172 C, then the speed of the virtual photon is also 172 C, and the source of the interaction is 9.5. If it is at a distance, the time transition coefficient is 2, that is, in the space-time coordinates based on the earth, the virtual photon comes from a point 2 years ago. The speed of the electron is 0
．． 99c, the coefficient is 10 and the time transition is 1
It is 2000. If the electron velocity is 0.999999c, the coefficient is 1,000,000 and the time displacement across the same pressure @ilc is 1.000,000 years. As described above, in the above example, the time transition caused by the change in electron velocity is exponential.

At low electron velocities, 0.2~. , □. Large velocity changes impart relatively inconspicuous time transitions, but at high electron velocities, small velocity instruments also impart relatively large time transitions. This is shown in Figure 3.

In other words, by controlling and detecting the velocity and position of electrons and the direction of the mainstream at all points in the electron path, the direction and time displacement coefficient of the virtual photon source can be easily calculated. However, there are two complementary forms of electron-photon interaction. That is, absorption and radiation.

These may equally be performed for electrons by other real space-time regions. In Figure 4, for example, if a virtual photon hits an electron moving forward at a speed of 0.99c, the speed of the photon is 0.01c, the photon is absorbed by the electron, and the observation standard on the left side of Figure 4 Emitted from the past region of space-time associated with the coordinates. If the electron emits a virtual photon, the photon leaves the back side (or possibly the front side) of the electron with a velocity of 0.01c, and the corresponding future point on the right side of Figure 4 is located on the opposite side of spacetime in the time direction. Interact with the realm. If there is a future region of spacetime in which the emission of a virtual photon is less active than the absorption of a virtual photon, but its relationship with a rapidly moving electron satisfies the conditions for virtual interaction, then
This is equally likely to occur.

The time displacement coefficient is exactly the same magnitude, but directed toward the future rather than the past. However, an interesting and measurable real-time effect of each absorption (past) and emission (future) interaction is that absorption involves a deceleration of the interacting electrons, whereas emission involves an acceleration. By measuring the presence, magnitude, and number of such decelerations or accelerations, these interactions and their more important properties can be recorded.

The magnitude of the deceleration/acceleration is proportional to the strength/wavelength of the photon source, and the number of interaction events, ie, the number of electrons affected by the photon within each pulse, is proportional to the density/size of the photon source. Therefore, the two directions of the radiation, its time displacement coefficient, its past or future nature, its strength and dimensions make it easy to calculate the measurable current time properties of the electron pulse mainstream in the accelerating ring. can get. These measurements include the deflection tTa
It is appropriate to use the free flight section of the electronic passageway.

Instruments are incorporated into the apparatus for detecting and recording the occurrence and nature of radiative interactions with moving electrons within repeated sections of the electron trajectory. This device is numbered 18 in Figure 1.
, and consists of a computer processing device. This computer processing device is operably connected to the accelerator IO and the interaction recorder 15, as shown in FIG. The output of the computer is connected to a cathode ray tube array or other observation display 19. The computer processing device and the parameters processed therein are shown in detail in FIG.

The hidden nature of the radiative interaction of rapidly moving electrons is that it is not naturally observed within the Earth's reference coordinates because the interaction occurs with other transitioned regions of space and time. That's true. The only simultaneous radiative interaction of electrons observed in this situation is the synchrotron radiation associated with electron orbital acceleration.

Interactions with other regions of spacetime are always carried out by virtual photons and are recorded only in the form of effects on fast electrons. The virtual photon first interacts with the high-speed electron, resulting in a deceleration/acceleration along the interaction direction axis, which reflects the actual absorption/emission process. Maskwell is
It has already been proposed that photons are transverse waves from changing electrical currents. First, in the case of isolated electron-photon processes occurring along the electron path direction, it resembles a longitudinal wave transverse to the axis of electron deceleration/acceleration. For high-speed electrons on a known narrow orbit in the direction of mainstream electron propagation, photon interaction occurs at t1! when the electron speed is high! However, the movement of electrons will be strongly opposed to the movement of electrons. One way to measure the absorption or emission of electrons/photons in the free-flight zone interaction between deflection-acceleration cap magnets is to detect and record the corresponding current time deceleration/acceleration of the electrons affected by the interaction. It is. A sufficiently large amount of electrons forms such a shadow V
If this happens, this process can be detected by particle recorders or Wt recorders placed in the free-flight section of the electron path in the accelerator ring.

In principle, a pulse of free-flying electrons passing through the device undisturbed will perfectly match the expected uniform pattern, but numerous decelerations and accelerations will cause corresponding disturbances in the electron flow and this Disturbances can be recorded as event type (deceleration or acceleration), intensity, amount, etc. Particle recorders or electrostatic field recorders of this type can span most of the free-flight path of the electronic storage link between bending magnets, and thus cover most of the accelerator circumference.

Since the velocity and main stream direction of each electron pulse within each linear free flight segment are known and adjustable, the direction of the radiation source can be easily calculated from these controllable factors. The information obtained from the device's electrostatic field detector, such as the past/future nature, strength and quantity of the source, is transferred directly to a computer where it can be easily calculated, as schematically shown in Figure 5. .

For this reason, the direction, the sign and magnitude of the temporal displacement coefficient, the wavelength, and the intensity of the interacting object (often a star at a very large spatiotemporal distance, or a correspondingly large stellar material) and exact information about the size can be instantly calculated and processed by the computer device of the invention.

The invention constitutes a novel combination of practical devices,
Coordinating, controlling, and maintaining the high-speed movement of electrons has never been achieved before. These deceleration and acceleration processes are due to the interaction of the electron with virtual photons from other regions of space-time, and the repeated freedom of the electron path is realized. It is detected, recorded, and calculated during the flight section. This device has a built-in computer system and provides a complex purpose and technique never before proposed: the recording and detailed calculation of electron-photon interaction transitions in space and time. The interaction transition is a mechanism similar to a rotating black hole. Combiator inputs and processing, such as object orientation, time displacement, intensity, and dimensions, are processed on-line by the computer and output to an optical or other display. For example, it is output as a visual image on a cathode ray screen along with the necessary spatio-temporal coordinates and other useful reference and coordinate indicators.

The assembled device is housed in various transportation vehicles for various purposes. For example, it may be installed on a space-time telescope stage on a fixed ground or satellite, or on the outer periphery of a mobile spacecraft. In this case, the visual cathode ray display device can be placed continuously or at intervals along the inside of the electron acceleration ring or observation horizon of the device. As shown in FIG. 6, the direction can be controlled around the vertical plane of the movable support base of the device to cover all spatial directions.

Also, from computer input and processing, processing of analog auditory processing, radar, and other communication methods is possible.

Based on the present invention, similar principles and mechanisms are used for reception only.
It can also be used to transmit and transmit analog impulses and signals to arbitrarily defined future or past regions of space and time. In other words, the linear acceleration of the electron pulses within each free-flight section of the electron trajectory controls the induction of deceleration.

[Brief explanation of the drawing]

Figure m1 is a schematic plan view of a device according to the invention built as a modification of the synchrotron/electron storage ring type electron accelerator; Figure 2 shows the rotation of the electron path/accelerator tube about the propagation axis; Figure 3 is a graph of the exponential time displacement coefficient with respect to the electron velocity of linear electron-photon interaction in the device of the present invention, and Figure 4 is a graph of the electron movement and the interaction between electron φ photons. FIG. 5 is a schematic diagram of the computer processing unit of the device, and FIG. 6 is a diagram showing the mobility of the storage ring or its support in the device. 10...Electron injector, 11...Vacuum tube, 12...Resonance cavity, 13...
・・Deflection-゛Magnet, 14 ・・Focusing magnet, 15・
... interaction recording device, 16 ... radiation method, 17 ... interaction source. 18
...Detection/recording device, 19...Display device.

Claims (2)

[Claims] (1) A physical device for generating, recording, observing, and transmitting electron-photon interactions that can be adjusted in space and time, which includes an annular vacuum tube or slit and an electron source for supplying electrons to the tube. an injector, a linear accelerator for accelerating the electrons supplied to the tube, and several deflection and parallel means operatively connected to the vacuum tube, between which a free flight section of the tube is provided. an interaction recording device coupled to the tube in the free flight section of the tube; and a computer processing device operatively connected to the accelerator and the interaction recording device. and a display connected to said computer processing device. (2) The apparatus according to claim 1, wherein the vacuum tube is adjustable.