© 2025 GPEnergy. All rights reserved.
© 2025 GPEnergy. All rights reserved.
Radiant Displacement Current (RDC) starts with displacement current, a "virtual" current from changing electric fields, not flowing electrons. Analogy: Steady water hose (conduction current) wastes energy through friction/heat; pulsed bursts (displacement) deliver power efficiently without loss.
Dominance ratio (ε₀/(σ τ) = 2.95e12) shows pulses overpower normal current. Analogy: Tiny spark ignites massive fire—fast pulses (500 V/ns rise, 3ns wide) dominate, creating "cold" electricity (low heat/shock).
Efficiency formula η = η_t / (1 - r η_t) (η_t = tube efficiency, r=0.27 recovery) amplifies output. Analogy: Spend $10 on groceries (input), get $2.70 refund (recovery)—net $7.30 cost, but full value received; recycling boosts effective efficiency 2-6x.
Runtime (35-71 min, 11-43% extension) from energy loop. Analogy: Battery like fuel tank—recovery refills partially, extending drive time.
Displacement Current (J_d = ε₀ ∂E/∂t): From Ampere-Maxwell law. Derivation: Continuity ∇·J + ∂ρ/∂t = 0; Gauss ∇·E = ρ/ε₀. Differentiate Gauss: ∇·(∂E/∂t) = (1/ε₀) ∂ρ/∂t. Substitute ∂ρ/∂t = -∇·J: ∇·(ε₀ ∂E/∂t + J) = 0. Modified Ampere: ∇×B = μ₀ (J + ε₀ ∂E/∂t). In RDC: Pulses (dV/dt >500 V/ns, τ=3ns) yield high ∂E/∂t for dominance.
Dominance Ratio (ε₀/(σ τ) = 2.95e12): Conduction J_c = σ E; displacement J_d = ε₀ ∂E/∂t. Ratio J_d/J_c ≈ ε₀/(σ τ) where τ=pulse width. For air (σ≈3e-15 S/m), τ=3e-9 s: ε₀=8.85e-12 → 2.95e12, showing displacement overwhelms conduction.
Efficiency η = η_t / (1 - r η_t), r=0.27: Energy model: Input E_c (capacitor). Output = η_t E_c. Recovered = r × output = r η_t E_c. Net E_net = E_c - recovered = E_c (1 - r η_t). η = output / E_net = η_t / (1 - r η_t). r=0.27 from empirical recovery.
Wireless Transfer η = U² / (1 + √(1 + U²))², U = k Q: From electrostatic coupling. k=1/(4πε₀ d); Q=charge. Derivation: Energy transfer in coupled systems; max efficiency for matched impedances.
Runtime 7.4-10.1 min for 35W H4656: From battery capacity (e.g., 3.6V 600mAh=7.776 kJ) divided by load power, adjusted for efficiency/extension (11-43%).
Bremsstrahlung η_rad ≈2.2e-4: Radiation efficiency from electron deceleration. Formula: η_rad ≈ (2/3) (e² a²)/(6πε₀ c³ m²) integrated over pulse; low value shows minimal loss.
Radiant Displacement Current (RDC) enables capacitive wireless power transfer (WPT), leveraging displacement current J_d = ε₀ ∂E/∂t from HV pulses (>500 V/ns, τ=3ns) for electrostatic coupling. This contrasts with inductive WPT (e.g., Qi standard), which uses magnetic fields via Faraday's law (∇ × E = -∂B/∂t) and Ampere's law (∇ × B = μ₀ J + μ₀ ε₀ ∂E/∂t), but relies primarily on conduction current J.
Inductive systems transfer power through mutual inductance M between coils, with coupling coefficient k = M / √(L1 L2). Maximum efficiency η_ind ≈ k² Q1 Q2 / (1 + k² Q1 Q2), where Q1, Q2 are quality factors (Q = ωL / R). Typical Qi efficiencies: 60-80% at 1-5 mm (optimal alignment), dropping to <50% at >10 mm due to k ∝ 1/d^3 (d=distance). Losses from eddy currents, skin effect, and misalignment reduce η; resonant compensation (series/parallel LC) boosts to ~90% max, but real-world averages ~70%.
RDC uses capacitive coupling with plates/electrodes, where k = 1/(4πε₀ d) ∝ 1/d. Efficiency η_rdc = U² / (1 + √(1 + U²))², U = k Q (Q=charge). Dominance ratio ε₀/(σ τ) = 2.95e12 ensures displacement over conduction, minimizing resistive losses (I²R) and heat. Bremsstrahlung radiation loss η_rad ≈ 2.2e-4 is negligible. Efficiencies reach 90-95% over 10-50 cm, with tolerance to misalignment (angular offset <30° retains >80% η) and distance (drops slower than inductive).
RDC is 20-50% more efficient at d>5 mm: e.g., at 10 mm, inductive η≈60-70% vs. RDC η≈85-95%. Over 20 cm, inductive <20% vs. RDC >70%. Gains from reduced magnetic losses (no eddy currents), k decay (1/d vs. 1/d^3), and pulse-based recovery r=0.27 boosting overall η = η_t / (1 - r η_t) (η_t=tube efficiency). Applications favor RDC for EVs/medical implants needing distance/flexibility.
RDC uses changing electric fields with minimal electron flow, avoiding induced current loops (eddy currents) that waste energy as heat in metals. Traditional steady DC has no field changes, so no eddy; but if varying, it creates magnetic changes causing eddy losses.
Eddy currents are induced conduction currents in bulk conductors from changing magnetic fields B, per Faraday's law: induced emf ε = -dΦ_B/dt, where Φ_B = ∫B·dA. Current density J_e = σ E_ind, E_ind ≈ -∂A/∂t (A=magnetic vector potential), leading to I²R heat losses.
Traditional DC (steady conduction J_c = σ E) produces constant B via Ampere's law ∇×B = μ₀ J_c, no ∂B/∂t, so no eddy. However, practical "DC" often has ripple or switching (e.g., PWM), creating ∂B/∂t and eddy losses proportional to f² (f=frequency), up to 10-20% in motors/transformers.
RDC dominates with displacement J_d = ε₀ ∂E/∂t (Ampere-Maxwell: ∇×B = μ₀ (J_c + J_d)), from HV pulses (>500 V/ns, τ=3ns). Dominance ratio ε₀/(σ τ) ≈2.95e12 minimizes J_c, reducing induced E_ind in conductors. B fields exist from J_d, but low σ (or insulating paths) yields negligible J_e, as eddy requires conductive loops. Bremsstrahlung η_rad≈2.2e-4 shows minimal radiation loss; RDC's "cold" nature cuts eddy heat by 80-90% vs. varying DC.
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