RF Ion Propulsor Arrays for Fuel-Free Atmospheric Thrust
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Solution Overview
Problem
Conventional propulsion systems, such as jet engines and propeller-driven aircraft, require substantial liquid fuel and numerous moving parts, leading to high maintenance costs and inefficiencies, while non-combustion technologies like ion thrusters lack sufficient thrust and energy density for practical use in Earth's atmosphere.
Innovation Solution
A propulsion system utilizing Near Field Wave Mechanics (NFWM) to generate and control RF fields for ionizing and accelerating air molecules within a confined space, creating coherent ion bundles that produce thrust without fuel or moving parts, leveraging constructive and destructive interference to achieve high efficiency.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Force
If conventional combustion engines are used, then sufficient thrust is generated, but fuel consumption is high and maintenance requirements are extensive
Solution Approach 1:
The patent replaces the mechanical combustion system with an electromagnetic field-based ionization and acceleration system. RF antennas generate electromagnetic fields that ionize air molecules and accelerate ions to produce thrust, eliminating the need for combustion chambers, fuel injection systems, and moving mechanical parts.
Solution Approach 2:
The system uses ambient air as the working medium, ionizing and accelerating it directly to produce thrust. This eliminates the need for external fuel sources, as the air itself serves as both the propellant and the working fluid for the electromagnetic acceleration process.
2Use of energy by moving object
If ion thrusters are used, then fuel efficiency is improved, but thrust output is insufficient for Earth atmosphere flight
Solution Approach 1:
The patent changes the operating parameters by using RF electromagnetic fields instead of electrostatic fields, enabling much higher acceleration velocities. The system ionizes air molecules and accelerates them to hypersonic speeds, generating sufficient thrust for atmospheric flight while maintaining high efficiency.
Solution Approach 2:
The system uses continuous RF electromagnetic field oscillation to sustain ionization and acceleration. The periodic nature of RF fields allows for continuous ion production and acceleration, maintaining steady thrust output rather than the pulsed operation typical of electrostatic ion thrusters.
3Quantity of substance
If electrostatic ionization methods are used, then ionization efficiency is achieved, but spatial control and field precision are poor
Solution Approach 1:
The patent divides the electromagnetic field generation into multiple segmented RF antenna elements arranged in arrays. Each antenna element can be independently controlled in phase and amplitude, allowing precise spatial manipulation of the electromagnetic fields through constructive and destructive interference patterns.
Solution Approach 2:
The system incorporates feedback control mechanisms to monitor and adjust the RF field patterns in real-time. This allows for precise control of ionization regions and acceleration zones, maintaining optimal field configurations despite variations in ambient conditions or ion density.
Applied Scientific Principles
This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.
Function Achieved in This Case
The system generates thrust many times greater than conventional turbofan engines, with no fuel consumption and no mechanical components, enabling efficient air movement and potential applications in aircraft propulsion and levitation.
Implementation Method 1
A propulsion system utilizing Near Field Wave Mechanics (NFWM) to generate and control RF fields for ionizing and accelerating air molecules within a confined space
Implementation Method 2
ionizing and accelerating air molecules within a confined space, creating coherent ion bundles that produce thrust
Implementation Method 3
leveraging constructive and destructive interference to achieve high efficiency
Implementation Method 4
leveraging constructive and destructive interference to achieve high efficiency
Implementation Method 5
accelerating air molecules to high speeds, for high output thrust
Data Source
AI summary
An electric ion propulsor and method of using is provided comprising a substrate having an inner surface and outer surface. A plurality of antennae mounted adjacent to each other on the inner surface and are enabled to transmit RF energy, and a controller having a connection to each of the plurality of antennae, a digital signal processor (DSP) and software stored in memory enabling control of transmission of the RF energy by each of the plurality of antennae. The antennae are subdivided into a plurality of arrays, a first array of the plurality of arrays serves to ionize ambient air and trap the resulting ionized air into a plurality of individual voxels and each voxel is transferred to another adjacent array, subsequently and in a linear direction, until the voxel exits the substrate at a speed enabling air movement causing thrust.