Spatial 3D Gravitational-Metric Interferometer Complex ("Volumetric Tetrahedron")
Unlike existing global 2D projects (LISA, TianQin, Taiji), which represent flat planar triangles, patent #1 establishes a closed spatial 3D tetrahedron truss of 3 GEO satellites ($L \approx 73,000\text{ km}$) and 1 polar satellite (SAT-4) with 6 mutual opto-RF chords in space vacuum.
Orthogonal Cartesian 3D Gravitational Interferometer with Polar-Equatorial Basis $(X \perp Y \perp Z)$
Essence of Patent #2 Improvement: Unlike the oblique tetrahedron of Patent #1, the new system deploys 4 spacecraft along the strictly orthogonal axes of the Cartesian coordinate system $(X \perp Y \perp Z)$ at mutual $90^\circ$ angles:
- • Two axial polar satellites (Z-Axis): SAT-1 (North Pole $+Z$, aligned with IC 1101 / "Axis of Evil") and SAT-2 (South Pole $-Z$, aligned with Phoenix A);
- • Two equatorial satellites (X and Y axes at 90°): SAT-3 (GEO, $0^\circ$ longitude, $+X$ axis) and SAT-4 (GEO, $90^\circ$ E longitude, $+Y$ axis);
- • 5 independent orthogonal communication links: 4 polar-equatorial beams (SAT-1 $\to$ SAT-3, SAT-1 $\to$ SAT-4, SAT-2 $\to$ SAT-3, SAT-2 $\to$ SAT-4) and 1 direct equatorial $90^\circ$ link (SAT-3 $\leftrightarrow$ SAT-4);
- • Digital downlink to the North Pole: All telemetry relays via SAT-1 to the Master Ground Station at Earth's North Pole;
- • Ground Calibration Station (North Pole): 1064 nm Laser + Ka-band RF measures vertical tidal and geodynamic oscillations of polar ice/rock to subtract local Earth noise from cosmological data.
Dual-Frequency Redundant Pipeline (Laser 1064 nm + Ka-band RF)
To resolve $2\pi$ phase ambiguity and achieve sub-picometer precision across giant baselines ($L \sim 73,000\text{ km}$), each edge of the 3D tetrahedron is equipped with a dual-frequency synchronous optoelectronic system:
1. Precision Laser Interferometer (1064 nm)
- • Wavelength: $\lambda = 1.064\text{ }\mu\text{m}$ (Nd:YAG with ultra-stable cavity).
- • Precision: Metric variations $\Delta L$ resolved down to $\sim 10^{-12} - 10^{-14}\text{ m}$ (picometers).
- • Plasma Immunity: $282\text{ THz}$ optical carrier unaffected by solar wind.
2. Coherent Ka-Band RF Link (30–40 GHz)
- • Wavelength: $\lambda \approx 8–10\text{ mm}$ (unmodulated carrier).
- • Absolute Ranging: Resolves $N \times 2\pi$ laser phase integer ambiguity.
- • Clock Synchronization: Inter-satellite atomic clock reading to $\sim 10^{-12}\text{ s}$.
Orientation Invariance & Superiority of SGDM Polar Axis Alignment
1. 3D-Tensor Invariance: The constellation is mathematically self-sufficient and fully operational under arbitrary spatial orientation, measuring the complete metric curvature tensor $h_{ij}$ across 6 differential phase channels without blind spots.
2. Recommended SGDM Polar Alignment: When aligning the tetrahedron's polar axis $Z$ along the Universal Polar Axis ($\vec{J}_0 \parallel \text{IC 1101} \longleftrightarrow \text{Phoenix A}$), the system unlocks unique scientific capabilities:
Direct Measurement of "Axis of Evil"
First local instrument in the Solar System to measure the Universal gravitational quadrupole, verifying Planck CMB alignment.
Multiverse Tidal Force Detection
Continuous monitoring of external tidal torque from Giant Universe $M_2$, confirming the $6^\circ$ spin precession.
Terrestrial Applications & Metrological Precision Table (Space vs Terrestrial)
The 3D tetrahedron architecture of SGDM is fully scalable, addressing high-tech challenges in both deep space and terrestrial industries:
High-Precision 3D Gravity Gradiometry
Direct mapping of rare metals, uranium, hydrocarbons, and subterranean cavities via full tensor gravity gradiometry $\Gamma_{ij}$ down to $0.001\text{ Eötvös}$.
Earthquake Early Warning & Stress Monitoring
Detection of tectonic stress accumulation in fault zones 6–48 hours before seismic events via differential metric strain between surface stations and borehole sensors.
Autonomous Navigation (GPS/GLONASS-Denied)
Absolute 3D navigation for submarines and subterranean boring complexes with $\pm 1.5\text{ m}$ accuracy via Earth's unique density tensor fingerprint without surfacing.
Relativistic Quantum Geodesy
Direct geopotential and geoid height measurements with $\pm 1\text{ mm}$ accuracy via gravitational redshift of optical atomic clocks ($\Delta f/f \sim 10^{-18}$).
Comparative Analysis: Invariants and Distinct Specifics of Space vs Terrestrial 3D Systems
Fundamental Invariants (Shared Core)
- • Topology: Volumetric 3D tetrahedron (4 nodes, 6 mutual links) eliminating planar blind spots.
- • Mathematics: Calculation of full 3D gravity tensor $\Gamma_{ij} = \partial^2 \Phi / \partial x_i \partial x_j$ across $4\pi$ steradians.
- • Dual-Frequency Pipeline: Laser 1064 nm (sub-picometer phase) + coherent RF/comb link ($2\pi$ ambiguity resolution).
- • Quantum Synchronization: Optical atomic clocks with $\Delta f/f \sim 10^{-18}$ stability.
Terrestrial Deployment Specifics (Poles / Equator)
- • Node Basing: 3 surface stations in a triangular grid + 1 borehole sensor ($-1\text{ km}$) or mountain station.
- • Polar Siting (Earth Poles): Deployment at geographic poles (e.g. Antarctica) aligns axis $Z$ parallel to Earth's rotation with minimal Coriolis noise.
- • Equatorial Polygon: Siting at the equator maximizes sensitivity to Laniakea superdisk dynamics and tidal waves.
- • Lightguides: Evacuated vacuum tubes to shield from atmospheric turbulence.
Metrological Parameters of SGDM 3D Complex (Space vs Terrestrial)
| Metrological Parameter | Traditional Systems (2026) | 3D SGDM: Space (GEO + Polar) | 3D SGDM: Terrestrial Network |
|---|---|---|---|
| Base Configuration | 2D planar triangle (LISA) / 1D | 3D Tetrahedron (6 links) | Tetrahedron (surface + shaft) |
| Interferometer Arm ($L$) | $220\text{ km}$ (GRACE) / $4\text{ km}$ (LIGO) | $L \approx 65,000 - 80,000\text{ km}$ | $L \approx 100\text{ m} - 10\text{ km}$ |
| Arm Strain Precision ($\Delta L$) | $10^{-9}\text{ m}$ (nanometers) | $10^{-12} - 10^{-15}\text{ m}$ (picometers) | $10^{-14} - 10^{-15}\text{ m}$ (femtometers) |
| Gravity Tensor Measurement ($\Gamma_{ij}$) | $5 - 10\text{ E}$ (1D $g_z$ only) | Complete 3D metric tensor $h_{ij}$ | $10^{-3} - 10^{-4}\text{ E}$ ($0.001\text{ E}$) |
| Absolute Ranging & Phase | $2\pi$ ambiguity | Redundant Ka-band (30 GHz) | Dual-frequency optical comb |
| Clock Synchronization | $10^{-9}\text{ s}$ (nanoseconds) | $\sim 10^{-12}\text{ s}$ (picoseconds) | $\sim 10^{-18}$ ($\Delta f/f$, optical clocks) |
| Primary Scientific & Practical Goal | Local Earth gravimetry | Universal Polar Axis (Axis of Evil) | Seismic early warning, 3D minerals |
Patent Claims (Patent Suite)
1. A spatial 3D gravitational-metric interferometer complex, comprising a constellation of spacecraft with laser and radio frequency communication links and phase detection equipment, characterized in that:
- The spacecraft are arranged in space to form a closed three-dimensional geometric tetrahedron, comprising three satellites in geostationary orbit (GEO) in the equatorial plane and at least one satellite in a high-elliptical polar orbit;
- All spacecraft are pairwise linked by six direct optical laser (1064 nm) and redundant radio frequency (Ka-band) inter-satellite links in space vacuum above Earth's atmosphere;
- The complex is equipped with a computational unit calculating the complete 3D metric tension tensor $h_{ij}$ from mutual carrier wave phase shifts with subsequent digital telemetry downlink to a ground station.
2. The complex according to claim 1, further characterized in that the polar axis of the tetrahedron $Z$ is aligned along the Universal Polar Axis towards supergiant galaxy IC 1101 (coordinates of Planck CMB quadrupole anisotropy / "Axis of Evil"), providing maximum sensitivity to cosmological quadrupole and external Multiverse tidal forces.
3. The complex according to claim 1 in a terrestrial embodiment, characterized in that:
- The reference stations of the tetrahedron are arranged on Earth's surface to form a triangular polygonal base ($X, Y$) of three surface quantum-optical stations, and at least one vertical reference station ($Z$) is deployed with an elevation offset — in a deep underground mine/borehole from $100\text{ m}$ to $3\text{ km}$ deep and/or at an elevated site (mountain summit or high mast);
- All six optical channels are implemented as shielded evacuated vacuum lightguides with coherent laser interferometers and optical frequency combs;
- The complex is located preferably in a geographic polar region of Earth to minimize centrifugal and Coriolis noise, and/or in an equatorial/seismically active zone, providing continuous measurement of the full 3D gravity gradient tensor $\Gamma_{ij}$ for early earthquake forecasting, high-precision 3D mineral exploration, and autonomous navigation.
4. An orthogonal Cartesian 3D gravitational interferometer complex with polar-equatorial basis $(X \perp Y \perp Z)$, characterized in that:
- Four spacecraft are positioned strictly along the mutually perpendicular axes of the Cartesian coordinate system at $90^\circ$ angles, comprising two axial polar spacecraft on polar orbits around Earth's geographical poles — SAT-1 (North Pole $+Z$, aligned towards IC 1101 / "Axis of Evil") and SAT-2 (South Pole $-Z$, aligned towards Phoenix A), and two equatorial spacecraft in geostationary orbit — SAT-3 ($+X$ axis, $0^\circ$ longitude) and SAT-4 ($+Y$ axis, $90^\circ$ E longitude);
- The spacecraft are connected via five independent direct optical-radio measurement communication links, including four polar-to-equatorial links (SAT-1 $\to$ SAT-3, SAT-1 $\to$ SAT-4, SAT-2 $\to$ SAT-3, SAT-2 $\to$ SAT-4) and one direct equatorial $90^\circ$ link (SAT-3 $\leftrightarrow$ SAT-4), eliminating cross-shadowing by planet Earth;
- Downlink of all digitized telemetry $\Delta\Phi$ is performed through the central relay gateway SAT-1 (North Pole $+Z$) to the master ground receiving complex located at Earth's North Pole.
5. The complex according to claim 4, further characterized in that the ground receiving complex at Earth's North Pole is additionally equipped with a vertical calibration laser (1064 nm) and Ka-band transceiver directed at zenith towards satellite SAT-1 for real-time measurement of local tidal and geodynamic oscillations of polar ice/rock and their software/hardware subtraction from cosmological 3D spacetime curvature data.
6. A closed-loop non-reactive precession graviton drive, comprising a sealed evacuated housing and rotor assemblies on electromagnetic bearings, characterized in that:
- It comprises a closed-loop system of four synchronized flywheel rotors, including a pair of vertical stabilizing rotors with coaxial rotation along the $Z$-axis and a pair of horizontal precession rotors along the $X$-axis;
- The horizontal rotors are configured for simultaneous high-speed intrinsic rotation ($\pm\omega_x$) and controlled orthogonal forced counter-precession ($\pm\Omega_p$) around the $Y$-axis, generating a dynamic phase shift of the quadrupole graviton ensemble of the rotor atoms relative to the external graviton field and producing a net propellantless thrust vector $F_{\Sigma} = F_3 + F_4$ along the $+Z$ axis;
- The counter-directed precession ($\pm\Omega_p$) of horizontal rotors ensures mutual cancellation of overturning gyroscopic moments ($\vec{M}_{\text{overturn}} \equiv 0$), while counter-rotation of the vertical stabilizer pair ($\pm\omega_z$) guarantees net zero angular momentum of the spacecraft body ($\vec{L}_{\Sigma} \equiv 0$).
7. The drive according to claim 6, further characterized in that steady-state power consumption is limited strictly to thermal power dissipation $P_{\text{dissip}} \sim 350 - 450\text{ W}$ arising from the finite phase relaxation time of graviton polarization ($\tau_{\text{rel}} \approx 10^{-5}\text{ s}$) inside the rotating rotors, rejected via radiative spacecraft heat pipes.
8. A universal triaxial non-reactive propulsion and protective complex for spacecraft, comprising three mutually perpendicular axes ($X \perp Y \perp Z$) with electromagnetic axis locks and a spherical vacuum gimbal, characterized in that:
- The rotor pair along the reference $Z$-axis is configured asymmetrically: the lower rotor 1 comprises a heavy mass (heavy tungsten/steel rim of radius $R_1$, rotating at speed $\omega_1$ clockwise along the graviton stream), receiving 100% of unshielded primary planetary/cosmic graviton flux for maximum lift generation $\Delta F_z$;
- The upper rotor 2 comprises a lightweight thin-walled shield of enlarged diameter $R_2 = (3-5) R_1$ (comparable to spacecraft hull diameter), rotating at ultra-high speed $\omega_2 = (5-10) \omega_1$ counter-clockwise, ensuring complete nulling of total angular momentum ($L_{\Sigma} = m_1 R_1^2 \omega_1 - m_2 R_2^2 \omega_2 \equiv 0$) with minimal shield mass $m_2 \ll m_1$;
- The outer rim of the upper ultra-high-speed rotor 2 ($v_{\text{rim}} \ge 25\text{ km/s}$) serves as an active centrifugal Whipple kinetic shield to disintegrate and radially repel incoming micrometeorites and space debris;
- Permanent rare-earth magnets or superconducting coils mounted along the periphery of rotor 2 generate a powerful rotating toroidal magnetic cocoon around the spacecraft hull for continuous deflection of cosmic rays and crew radiation protection.
9. Method for deterministic quantum-optical direction switching of light wave trains, comprising generating coherent optical radiation, transmitting it through a double-slit interferometric assembly, and detecting it on a position-sensitive detector, characterized in that:
- Radiation is generated by a pair of mutually focused micro-emitters operating in calibration mode with a mutual phase shift $\Delta\varphi = 180^\circ$ producing a compensated zero field ($E_{\Sigma} \equiv 0$);
- Phase and direction control of the quantum is executed via pulse modulation: independent activation of the first emitter generates a wave train with initial phase $\psi_1 = 0^\circ$, activation of the second emitter generates an inverted wave train with phase $\psi_2 = 180^\circ$, and simultaneous activation produces non-radiative cancellation;
- The receiver detector is configured as a two-section phased metasurface whose surface atoms are coherently pumped in mutual anti-phase: left half at $\varphi_L = 0^\circ$ and right half at $\varphi_R = 180^\circ$, ensuring 100% selective resonant capture of the wave train energy ($\hbar\omega$) on the in-phase detector half and destructive phase reflection on the opposite half without mechanical beam deflectors.
10. Device (quantum-optical photonic logic gate) according to claim 9, characterized in that it comprises two coaxial vertical laser micro-emitters with anti-phase modulation circuitry and a detector array with a phase synchronization bus, implementing an optical logic switch ('0' — left absorption, '1' — right absorption) at clock rates up to hundreds of gigahertz.
11. Method according to claim 9, characterized in that upon repetitive emission of pulses of identical phase, a deterministic interference pattern is formed, shifted as a single entity by an angle $\pm\theta_0$, establishing around the shifted primary interference wedge a symmetric system of sharply decaying lateral wedges ($\pm 1, \pm 2$), with potential geometric overlap of weak lateral orders onto the adjacent screen half depending on slit baseline $d$, slit width $b$, and distance $L$, while maintaining dominant energy concentration at the vertex of the primary wedge.
Non-Reactive 4-Rotor Precession Graviton Drive of Closed Type with Complete Gyroscopic Torque Cancellation
Generation of unidirectional propellantless thrust $F_{\text{thrust}}$ in space vacuum via dynamic phase interference of precessing rotors with the secular graviton background ($\vec{L}_{\Sigma} \equiv 0, \vec{M}_{\Sigma} \equiv 0$).
Physical Principle & Overcoming Tsiolkovsky's Rocket Equation: Unlike conventional rocket engines requiring chemical propellant expulsion (90–95% of initial launch mass), in Chesnokov's SGDM model space vacuum is a Graviton Ocean ($M_g \sim 10^{-68}\text{ kg}$).
High-speed rotor spin ($\omega$) combined with forced precession ($\Omega_p$) drives nuclear gravitons across external field lines at 90°, producing net thrust:
• Dual-Link Boom: Rotors are offset from the $Z$-axis via $L_1 \approx 1\text{ m}$ booms with small articulated levers $L_2$ ("up–norm–down" arc with physical thrust stop).
Complete elimination of parasitic moments and stress limits:
- 2 vertical stabilizers ($\pm Z$): counter-spin $\pm\omega_z$ nulls body angular momentum: $\vec{L}_z \equiv 0$;
- 2 horizontal rotors ($\pm X$): counter-precession $\pm\Omega_p$ doubles thrust and cancels overturning moment: $\vec{M}_{\text{overturn}} \equiv 0$;
- 4-Stroke Pulse Cycle: 1) Active spin-up to $\omega_{\text{crit}}$ $\to$ 2) Inertial cruise $v=\text{const}$ $\to$ 3) Regenerative brake-to-battery charging $\to$ 4) Re-spin for next $+\Delta v$ pulse.
• 1. Flight Polar Drop-Test: Synchronous drop of two identical sealed capsules ($\varnothing 30\text{ cm}$, 15 kg each, passive Z-axis gyro-stabilization) from an aircraft over the North Pole ($h=10–12\text{ km}$). Capsule 1 decelerates ($+\Omega_p$), Capsule 2 accelerates ($-\Omega_p$). Differential tracking $\Delta a = 2 a_{\text{SGDM}}$ yields clean vertical separation $\Delta h \approx 45\text{ m}$ in 15 s, cancelling aerodynamic drag and $g$.
• 2. Ground Polar V-Stand with Oil Integrators: The device in a spherical ring with dampeners is suspended via two symmetric beams (Beam 1 aligned to the North Star parallel to Earth's polar axis at latitude $\varphi$, Beam 2 mirrored South) to spring scales inside viscous oil flasks (100% absorption of high-frequency motor vibrations).
• 3. Diurnal (24h) & 12-Month Annual Ellipse: 10-minute cycles track the 23h 56m sidereal harmonic wave ($F_{\text{max}}$ at midnight, $F_{\text{min}}$ at noon), and 12 monthly runs register annual orbital modulation of $\pm 4.75\%$ ($v_{\text{orb}} = 30\text{ km/s}$ vs $v_{\text{MW}} = 627\text{ km/s}$), proving direct coupling to the Multiverse Graviton Ocean.
Summary Specifications and Operating Modes of the SGDM Drive
| Parameter | Mode 1: Lab Testbed | Mode 2: Space Probe (1.5 t) | Mode 3: Heavy Tug (10 t) |
|---|---|---|---|
| Rotor Active Mass ($m$) | 4 × 2.5 kg = 10 kg | 4 × 25 kg = 100 kg | 4 × 100 kg = 400 kg |
| Rotor Radius ($R$) | 0.20 m | 0.45 m | 0.85 m |
| Rotation Speed ($\omega$) | 60,000 RPM (6,283 rad/s) | 90,000 RPM (9,425 rad/s) | 120,000 RPM (12,566 rad/s) |
| Precession Speed ($\Omega_p$) | 300 RPM (31.4 rad/s) | 600 RPM (62.8 rad/s) | 1,200 RPM (125.6 rad/s) |
| Generated Thrust ($F_{\Sigma}$) | 42.5 N | 212.0 N (21.6 kgf) | 4,600.0 N (470 kgf) |
| Spin-up Energy ($E_{\text{spin}}$) | 3.9 MJ (1.1 kWh) | 85.0 MJ (23.6 kWh) | 910.0 MJ (252.8 kWh) |
| Thermal Dissipation ($P_{\text{heat}}$) | ~65 W | ~335 – 450 W | ~4.8 kW |
| Spacecraft Dynamics | Lab test bench / CubeSat | $a = 0.14\text{ m/s}^2$ (Mars transit in 35 days) | $a = 0.46\text{ m/s}^2$ (Jupiter transit in 90 days) |
Propellantless Interplanetary Graviton Drive: Earth — Mars Transit
Complete theoretical & engineering design: 1,324 t fuel saved, 99.88% energy savings, 4-rotor complex, and 3D tacking navigation.
Universal Triaxial Non-Reactive Propulsion & Attitude Control Complex with Commutable Degrees of Freedom and Spherical Gimbal
Complete spatial isotropy: symmetric 3-axis architecture ($X \perp Y \perp Z$, 6 rotors). Locking any axis transforms it into a rigid gyrovertical $Z$-axis, releasing 4 remaining rotors as precession thrust amplifiers within a vacuum spherical gimbal.
Essence of Patent #4 Invention: Unlike base Patent #3 (where the $Z$-axis has a fixed mechanical position), in the advanced architecture the system is fully isotropic and symmetric across all 3 spatial axes:
Each orthogonal axis ($X, Y, Z$) is equipped with a high-speed electromagnetic lock. Engaging the lock on any axis locks the rotor spin plane, creating an instant reference gyrovertical ($\vec{L} \equiv 0$).
Disengaging locks on the other two perpendicular axes allows four rotors to execute synchronized counter-precession ($\pm\Omega_p$), doubling Laithwaite thrust ($F_{\Sigma} \approx 2 \times F_{\text{pair}}$) with zero overturning torque.
The 6-rotor assembly is housed inside a sealed vacuum sphere on magnetic suspension. The reference $Z$-axis rotates at low angular velocity directly towards the maximum graviton polarization vector (Earth's pole or IC 1101) for maximum thrust resonance.
Method and Device for Deterministic Quantum-Optical Phase Switching of Wave Trains and Chesnokov Coherent Logic Gate
Elimination of quantum randomness: direct 100% deterministic routing of single-photon wave trains through two slits via anti-phase laser field synthesis ($\Delta\varphi = 180^\circ$) and a two-section phased detector metasurface ($\varphi_L = 0^\circ, \varphi_R = 180^\circ$).
Physical Principle & Overcoming Bohr's Statistical Postulate: In standard Copenhagen quantum mechanics, single photons are assumed to randomly select a detection point. In Chesnokov's SGDM model, a photon is a classical wave train ($E \perp B, \Delta\varphi = 0^\circ$), and absorption is strictly dictated by phase resonance with target atoms:
Generates a wave train with initial phase $\psi_1 = 0^\circ$. The wave covers both slits $S_1, S_2$, entering into 100% in-phase resonance with the left detector half ($\varphi_L = 0^\circ$). Photon is absorbed on the LEFT (Logical '0') with 100% certainty.
Generates an inverted wave train with phase $\psi_2 = 180^\circ$. A destructive barrier forms on the left, while perfect resonance occurs on the right ($\varphi_R = 180^\circ$). Photon is absorbed on the RIGHT (Logical '1') with 100% certainty.
Both lasers fire simultaneously in anti-phase ($E_1 + E_2 \equiv 0$). The field mutually annihilates at the focus, and no wave propagates into space. Complete darkness on screen (forbidden state).
• 1. Optoelectronic Method (InGaAs/GaAs Quantum Wells): Auxiliary pump laser illuminates the left half at phase $\varphi_L = 0^\circ$, and the right half via a $\text{LiNbO}_3$ electro-optic crystal with a $180^\circ$ ($\Delta\varphi = \pi$) shift.
• 2. Passive Plasmonic Metasurface: Gold nanorod array on silicon; the right half nanorod length is shifted by $\Delta L = \lambda/2$, creating a passive $180^\circ$ phase response without external power.
• 3. Atomic Layer with EIT (Electromagnetically Induced Transparency): Gas cell of cold $^{87}\text{Rb}$ atoms where $0^\circ$ phase opens resonant absorption and $180^\circ$ phase induces complete optical transparency.
• Unified Phase Tilt: Upon emitting a pulse with defined initial phase ($\psi = 0^\circ$), the unified wavefront encompasses both slits $S_1, S_2$ simultaneously, producing a synchronous angular tilt of wavevector $\vec{k}$ and steering the primary interference wedge toward $\pm\theta_0$.
• Bilateral Symmetry of Decay Orders: Relative to the shifted primary maximum vertex, sharply decaying secondary wedges ($\pm 1, \pm 2$) diverge symmetrically to the left and right. For a single quantum, their localized field density remains below the photoelectric threshold, ensuring localized absorption strictly at the primary vertex.
• Geometric Overlap ("Tails"): In physical setups, depending on slit baseline $d$, width $b$, screen distance $L$, and blade conductivity (Rubinowicz–Sommerfeld edge diffraction), the weak lateral wing may partially cross into the adjacent screen half, yet dominant energy concentration ($>95\%$) and primary peak remain strictly deterministic on the target side.
• Accumulation Experiment & Law of Ellipsoid Formation: Over millions of repeated pulses, the screen reveals not a probabilistic blur, but a cleanly shifted deterministic interference pattern in the shape of a luminous ellipsoid with peak brightness along the system horizon ($z=0$). In a physical source, dipole wave train emission angles vary within the aperture: under Lambert's cosine law and Poynting projection theorem, on-axis alignment ($\alpha = 0^\circ$) delivers 100% wave train energy into the slits (equatorial maximum), while angular misalignment $\alpha$ attenuates intercepted energy as $\cos^2\alpha$ (dropping to 0% at $90^\circ$). The biaxial Gaussian angular dispersion of the vertical slit ($H \gg b$) combined with cosine energy falloff naturally closes the interference fringes into an elongated ellipsoid, validating the deterministic wave nature of light.
Patent Information Search & World Novelty Report
Comprehensive comparative analysis of prior art (WIPO, USPTO, EPO, Rospatent, NASA NTRS, Nature 2026), 100% world novelty verification for Patents #1, #2 and fundamental novelty confirmation for the 4-rotor SGDM drive in Patent #3 for Chesnokov Yu. A. dated Oct 02, 2026.
The patent search includes a detailed comparative analysis of 20th–21st century physical experiments investigating anomalous rotational dynamics and asymmetric weight changes in Earth's gravitational field:
• Experimental Fact: Right-handed rotation (spin downward, Sendai, 38° N) of vacuum-enclosed gyroscopes (140–176 g) causes a repeatable weight loss $\Delta m$ up to $12\text{ mg}$ ($13,000\text{ RPM}$), linear with $\omega$. Left-handed rotation produces strictly zero change ($\Delta m \equiv 0$).
• SGDM Rationale: Confirms secular spin polarization of Earth's graviton background and generation of unidirectional $\Delta F_z$ force on the vertical $Z$-axis rotor pair.
• Experimental Fact: Forced circular precession ($\Omega_p$) of a spinning heavy flywheel ($20\text{ kg}$) generates a vertical gyroscopic dynamic lift, enabling single-handed lifting without bearing reaction fatigue.
• SGDM Rationale: The horizontal precession rotor acts as a dynamic thrust amplifier with gain $K_{\text{amp}} = \Omega_p / \Omega_{\text{Earth}} \approx 860,000$, scaling Hayasaka's milligrams into tens of kilograms of continuous thrust $F_{\Sigma}$.
• Latitude Dependence ($\propto \sin\varphi$): Gyroscope weight asymmetry increases from equator ($\varphi \to 0^\circ$, effect vanishes) towards the North Pole: in Pulkovo ($60^\circ\text{ N}$) and Arctic ($68^\circ-78^\circ\text{ N}$) the effect is maximal and stable.
• Axis Alignment: Tilting the gyro axis parallel to Earth's rotation axis (aiming at Polaris) maximizes the effect, proving coaxial coupling with the planet's polarized graviton vector.
Prior art lacked the synthesis of Laithwaite's precession amplifier with Hayasaka's spin-$Z$ compensators. Patent #3 introduces the world's first closed-loop 4-rotor architecture: 2 vertical stabilizers ($\pm\omega_z$) establish a rigid gyroscopic platform and guarantee net zero angular momentum ($\vec{L}_{\Sigma} \equiv 0$), while 2 horizontal counter-precessing rotors ($\pm\omega_x, \pm\Omega_p$) mutually cancel overturning torque ($\vec{M}_{\Sigma} \equiv 0$) and sum useful thrust $F_{\Sigma}$ along the $+Z$ axis.
Chesnokov Diurnal Polar V-Stand for Measuring Spatial Graviton Polarization and Calibrating Propellantless Propulsion Thrust
The apparatus solves the problem of direct terrestrial measurement of Earth's secular spin-graviton polarization and metrological calibration of propellantless thrusters (Patents #3, #4, #7), cleanly separating static mass $M_0$ from dynamic thrust $F_{\text{SGDM}}$:
Chesnokov Diurnal Polar V-Stand & Spin-Graviton Polarization
Postulate #4, 100 years of experiments (Miller, Kozyrev, GP-B, Planck), metrological equations, and thrust calibration.
Cyclic Quantum Membrane Graviton Drive with Reinforced Nanocanvas and Dynamic Angular Momentum Compensation
The invention relates to propellantless deep-space propulsion. The complex comprises a large-diameter 12-cable centrifugal membrane ($\varnothing 10.0\text{ m}$) and a coaxial compact tungsten counter-flywheel ($\varnothing 0.8\text{ m}$), guaranteeing strict zero net angular momentum $\vec{L}_{\Sigma} \equiv 0$:
Coupling a 20-meter membrane with a Patent #3 gyroscopic power amplifier generates $98.1\text{ kN}$ ($10\text{ tons}$) of continuous thrust, providing comfortable $1.0\,g$ Earth gravity on board: reaching Proxima Centauri in 3.5 years ship time, the Galactic Core in 20.5 years, and the Andromeda Galaxy in 28.6 years!
32-Qudit 256-Phase Quantum-Topological Computing Processor with Laser Commutation and Wave ALU at Room Temperature (+20°C)
The invention relates to quantum microelectronics and optical computing. The complex comprises 32 solid-state sapphire cells with Tantalum-181 ($^{181}\text{Ta}$, $J=7/2$) or Aluminum-27 ($^{27}\text{Al}$) centers, each encoding a full 8-bit machine byte ($2^8 = 256$ discrete phase states of the $137\,\lambda_C$ electron standing soliton with step $\Delta\varphi = 1.40625^\circ$). The register Hilbert space spans $256^{32} = 2^{256} \approx 1.158 \times 10^{77}$ parallel states per picosecond optical cycle:
32-Qudit Quantum-Topological Processor (2²⁵⁶)
Solid-state room-temperature chip: 256-phase encoding, optical ALU (1 ps), recirculation memory (1 ms), and Space-TMR '2 of 3'.
Method of Multidimensional High-Precision Quantum-Optical Measurement of Gravitational, Electric, and Magnetic Vacuum Fields and Chesnokov Vacuum Comparator on a Rotating Platform
Unprecedented zero-probing-energy metrological system: direct deterministic separation of gravitational potential $\Phi(r)$, electrodynamic polarizability $\pm E$, dual-axis magnetic precession $\pm B$ (horizontal/vertical), and Earth diurnal rotation velocity ($\pm V$) via transformation of a vertical light ellipsoid over a long baseline $L \gg 1$.
Essence of Invention & Overcoming the Casimir–Einstein Metrological Impasse: В классической физике измерение сверхслабого квантово-гравитационного взаимодействия фотонов на малых дистанциях блокировалось паразитными силами Казимира, контактной разностью потенциалов и случайными бликами. В Патенте №9 Чеснокова Ю. А. создан многомерный 4D-анализатор вакуума, где все паразитные силы обращены в независимые измерительные координаты, а само квантовое состояние фотонного волновода ($137\,\lambda_C$) считывается пассивно на дальнем экране без энергетических затрат:
Массивный шар $M$ ($0\text{ В}$) и сам шток микрометра покрыты поглощающим напылением (тёмное тело). Смещается вдоль щелей $S_1-S_2$, модулируя гравитационный потенциал $\Phi(r) = -GM/r$ и градиент показателя преломления вакуума.
Плавное сканирование потенциала шара от $-E$ до $+E$. Позволяет напрямую измерить поперечную дипольную поляризуемость светового цуга и точно скомпенсировать силы Казимира до абсолютного $0$.
Двухосное переключение (вертикальное и горизонтальное): экранированные катушки создают регулируемое поле $B \parallel (S_1-S_2)$ и $B \perp (S_1-S_2)$, напрямую воздействуя на спиновую компоненту фотона через эффект Ааронова — Бома.
Вращение стола на Восток ($+V$) и Запад ($-V$) регистрирует анизотропию суточного хода Земли ($v \approx 300\text{ м/с}$), а на Север ($+Z$) — вековую спиновую поляризацию Вселенной (IC 1101)!
• Масштабирование на дальней базе ($L = 10\dots 50\text{ м}$): Наноскопический фазовый сдвиг $\Delta\varphi \sim 10^{-6}\text{ рад}$ на дистанции $L=50\text{ м}$ трансформируется в макроскопическое линейное смещение эллипсоида $\Delta X = 50\text{ мм}$, считываемое ПЗС-матрицей с субпиксельной точностью без необходимости в мощных лазерах накачки!
• Формирование вертикального светового эллипсоида: При вертикальной щели ($H \gg b$) закон Ламбера и косинусный спад энергии $\cos^2\alpha$ замыкают интерференционную картину в вертикальный эллипсоид, а перекрытие щели шаром динамически срезает боковые лепестки под углом $60^\circ$ (геометрия тетраэдра SGDM).
Патент №9: Универсальный 4D Вакуумный Компаратор SGDM
Первый в истории комплекс на базе Патента №5, позволяющий пассивно и без затрат энергии с высокой точностью разделять гравитационный сдвиг, поляризацию $\pm E$, двухосный магнетизм $\pm B$ и суточный вектор Земли!
Method of Precision Optico-Gravitational Spectral Analysis and Dual-Lens Focal Gravispectrometer of Chesnokov with 10,000x Field Gradient Amplification
Direct laboratory measurement of gravitational field interaction with light quanta of varying energies (wavelengths): conical focusing of a vertical slit beam into a 10-micron caustic with insertion of a massive plate in the $x_0 \to 0$ gap, inverse collimation into a parallel beam, and dispersive prism decomposition.
Физический принцип и преодоление ограничения апертурного зазора: В стандартных схемах приближение массивного тела к широкому световому пучку ограничено поперечным сечением самого луча (зазор не менее $1\text{ мм}$), что делало лабораторный гравитационный фазовый набег исчезающе малым. В Патенте №10 Чеснокова Ю. А. реализован принцип конического пространственного сжатия энергии:
Сжимает вертикальную полосу белого света или трёх эталонных лазеров (Красный 700 нм, Зеленый 532 нм, Фиолетовый 400 нм) в субмикронную фокальную каустику толщиной $d_{\text{фокуса}} \approx 10\text{ мкм}$.
Заземлённая массивная вольфрамовая пластина ($0\text{ В}$) с поглощающим напылением «тёмное тело» вводится в зазор $x_0 \sim 10\text{ мкм}$. Сила гравитационного натяжения $1/x_0^2$ возрастает ровно в 10 000 РАЗ ($10^4$)!
Преобразует расходящийся из зоны гравитационного воздействия конус обратно в строго параллельный пучок, полностью исключая сферические аберрации на дисперсионной призме.
Раскладывает параллельный пучок в спектр на дальний экран. Фиксирует квантово-хроматическое расщепление расстояний $\Delta L(R-G)$ и $\Delta L(G-V)$ пропорционально частотам стоячих волн $\omega = c/\lambda$!
• Дифференциальный эталон трёх линий: Сравнение расстояний между Красным ($700\text{ нм}$), Зелёным ($532\text{ нм}$) и Фиолетовым ($400\text{ нм}$) до введения пластины и после её подведения в зазор $x_0 \to 0$ исключает систематические инструментальные погрешности, напрямую доказывая зависимость гравитационного фазового сдвига от собственной частоты кванта де Бройля.
• Вертикальные диафрагмы: Узкие диафрагмы на всех оптических переходах устраняют боковое паразитное рассеяние, оставляя чистый вертикальный срез фотонного фронта.
Essence of the Monolithic 1-Ton Implementation: The entire optical measuring system (entrance slit, lens $F=1.0\text{ m}$, focal zone with microgap $x_0 \to 0$, collimator, and prism) is mounted on a single monolithic platform (table-mass) weighing $1000\text{ kg}$ ($1\text{ ton}$) made of invar / modified high-damping cast iron. The opposite end of the platform is kinematically linked to the refracting apex of the dispersion prism via a rigid amplification lever with a $1:100$ transmission ratio, equipped with an elastic overload safety damper to prevent glass destruction and counter-acting invar rods for thermal drift compensation ($dL/dT \equiv 0$).
Direct gravitational phase pull of the 1-meter wedge on de Broglie standing wave photons. Induces quantum wavelength divergence strictly according to frequencies ($\Delta X_{\text{violet}} = 1.75 \times \Delta X_{\text{red}}$) under a static prism angle.
Gravitational tidal tension of space or Earth causes sub-nanometer elastic strain of the 1-ton table ($\Delta L \sim 10^{-11}\text{ m}$), amplified 100-fold by the $1:100$ lever to elastically squeeze/expand the prism angle, expanding the overall spectral baseline up to $0.1–0.2\text{ mm}$ on screen!
• "Factor 1 Only" Mode (Lever disengaged): direct measurement of quantum chromatic gravitational spectrum shift;
• "Factor 2 Only" Mode (Wedge retracted to $x_0 \gg 1\text{ mm}$): pure measurement of tidal elastic strain of the 1-ton mass by Earth/cosmic bodies;
• "In-Phase Mutual Amplification (1 + 2)" Mode: simultaneous optico-gravitational beam deflection and lever expansion of the spectrum base, mutually multiplying the measurement signal by $3–4$ orders of sensitivity!
Patent #10: Dual-Lens Gravispectrometer of Chesnokov (10⁴ Gain)
Первый в истории науки спектрометр, напрямую измеряющий квантовую хроматическую гравитационную дисперсию вакуума без сверхтяжёлых космических масс — чисто на 10-микронном клине в лабораторных условиях!
Quantum-Topological Reactor-Generator SGDM-10⁸ with Linear CRT Injector for Hydrogen (¹H) Cold Neutronization and Direct Power Extraction
Linear time-of-flight injector: CRT electron gun with magnetic lock $B_z$, nanoporous stripper ($0.5\text{ Å}$), grazing-incidence cone ($\alpha_{\text{in}} = \alpha_{\text{out}}$), 3-laser optical anvil, and tungsten-rhenium core W-25Re ($750\text{ }^\circ\text{C}$). Direct 200 kW mechanical shaft power extraction via sCO₂ Brayton turbine at 0.027 ml H₂O/hour with zero nuclear waste!
Quantum-Topological 128 Core Foundation
In SGDM, the electron torus ($137.036$) consists of a rigid binary core $2^7 = 128$ and 9 field lobes. When passing through a nanoporous stripper ($0.5\text{ Å}$), the electron tori ($1.06\text{ Å}$) strip away, while bare nuclei ($1+4$) collapse in 3-laser focus into a stable neutronium cell ($1+2 \to 8*16 = 128$) releasing a deionization quantum:
Energy & Power Balance (COP ≈ 14.8)
- Self-Consumption Input: $13.5\text{ kW}$ (lasers, pumps, grids).
- Thermal Core Output (W-25Re): $400.0\text{ kW}$ ($750\text{ }^\circ\text{C}$).
- Useful Mechanical Shaft Power: $200.0\text{ kW}$ ($272\text{ hp}$, $\text{sCO}_2$ turbine).
- Fuel Consumption: $0.027\text{ ml}$ H₂O/hour ($15\text{ ml}$ per 11.5 days!).
- Radiation and Nuclear Waste: STRICTLY 0% (Zero Waste).
Piezo H₂ pulse + field emission + magnetic lock $B_z$ (torus disks 1.06 Å $\perp$ axis).
Membrane $0.5\text{ Å}$ strips tori, passing bare nuclei $1+4$ ($v = 2400\text{ km/s}$).
Grazing reflection ($\alpha_{\text{in}} = \alpha_{\text{out}}$) + Patent #10 wedge (confinement to 30 nm).
3 counter-lasers (120°) brake $v \to 100\text{ m/s}$ + Zeno strobe phase collapse to 128 core.
Cluster impact ➔ Heat to 750 °C ➔ Microchannel dump into $\text{sCO}_2$ turbine ($200\text{ kW}$).
Method for Quantum-Topological Synthesis of Supermaterials, Additive 3D-Graviton Printing and Sub-Angstrom Jet Processing via Embedding of Stable Neutronium (1+2) Nodes
Deep bulk hardening of crystal matrices (W, Ti, Steel, Cu, Nd, Si, Au) with stable neutral 1+2 clusters: density up to $45\text{–}50\text{ g/cm}^3$, hardness $> 120\text{ GPa}$, thermal limit $> 5000\text{ }^\circ\text{C}$, dry super-slipping ($\mu \approx 0.001$). Additive 3D-graviton printing of complex gradient parts and sub-Angstrom jet drilling of calibrated nanopores ($0.5\text{–}3.0\text{ Å}$) for water desalination, DNA sequencing, and planetary defense.
1. Bulk Hardening W-SGDM
Core saturation: density $45\text{–}50\text{ g/cm}^3$, hardness $> 120\text{ GPa}$, $T_{\text{melt}} > 5000\text{ }^\circ\text{C}$. Ideal for 1.0g gyro-thruster rotors, 20 km ultra-deep drilling bits, and armor.
2. Surface Cladding
Scanning 1+2 beam creates a $5\text{–}50\text{ \mu m}$ nanolayer with dry friction $\mu \approx 0.001$. Oil-free engine life $> 50\text{ years}$, eternal turbine blades, and surgical scalpels.
3. Sub-Angstrom Drilling
Neutral graviton needle ($0.5\text{ \AA}$) drills $0.5\text{–}3.0\text{ \AA}$ pores without Coulomb broadening (Aspect Ratio $> 100,000 : 1$). Gravity-flow water desalination and DNA sequencer chips.
Density x2.5, strength x15, $T_{\text{melt}} > 5000\text{ }^\circ\text{C}$ (thruster rotors, aerocraft frames).
Conductivity x100 at $+20\text{ }^\circ\text{C}$, currents up to $10^9\text{ A/cm}^2$ (lossless power lines, space RF).
Induction $B = 25\text{–}40\text{ T}$ at $+20\text{ }^\circ\text{C}$, limits to $800\text{ }^\circ\text{C}$ (matchbox-sized 50 kW motors).
1 THz clock rate, zero heat dissipation, magnetless phase turbines on `[111]` cuts.
Method and Apparatus for Remote Quantum-Topological Decontamination and Transmutation of Nuclear Waste via Neutral Neutronium (8+16) Clusters with a Dynamic Tesla Valve
Non-contact in-situ remediation of SNF fuel assemblies (Cesium-137, Plutonium-239, Strontium-90, Americium-241) in storage pools: dynamic Tesla valve retaining 10⁻⁷ Torr vacuum without foils, water irrigation cone (30–50 cm), 1.25 MeV beam energy operating safely below environmental activation thresholds. Nuclear core completion into the symmetric 128 octave forcing transmutation into stable lead and barium within 2–5 hours while co-generating 200 kW clean power!
Absolute Environmental Safety
- Beam Energy: $1.25\text{ MeV/nucleon}$ (12x below $^{16}\text{O} \to 15.66\text{ MeV}$ threshold).
- Induced Radioactivity: STRICTLY 0% (Physical conservation law).
- Fission Chain Suppression: 8+16 cluster acts as a topological damper.
- Tesla Valve: Vortex hydrodynamic seal without foil degradation.
Nuclear Plant Remediation Output
- Fuel Assembly Decontamination Time: $2\text{–}5\text{ hours}$ (vs 100,000 years in repository).
- End Product: Stable industrial metals (Lead $^{208}\text{Pb}$, Barium $^{138}\text{Ba}$).
- Co-generation Power: $+200\text{ kW}$ clean electricity via $\text{sCO}_2$ turbine loop.
- Treatment Cost: $\$0$ (Self-offsetting energy production).
Collimated 8+16 beam generation in $10^{-7}\text{ Torr}$ vacuum.
Non-contact beam discharge with hydrodynamic vortex barrier.
Water scattering ($3^\circ\text{–}5^\circ$) expands beam into $\varnothing 30\text{–}50\text{ cm}$ cone.
Lattice completion ➔ Core stabilization ➔ Clean lead & barium!
Inventor Credentials & Contact Information
Inventor: Chesnokov Yuri Alexandrovich • Physics & Technology Faculty, DSU (1984) • Author of the fundamental SGDM Cosmological Model.
Tel: +7 (903) 652-90-14 • E-mail: europo1@yandex.ru