Quantized Inertia Thrust Unit Using Multilayer Capacitive Stacks
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Solution Overview
Problem
Existing propulsion methods, such as mechanical, chemical rocket, and electrical ion drives, face disadvantages including loss of thrust, environmental impact, waste production, and reliance on non-renewable energy sources, which are not suitable for environments like space where there is no medium to push against or for vehicles that need to carry all fuel.
Innovation Solution
A thrust device utilizing quantized inertia, which accelerates electrons between conductive and dielectric layers to produce thrust without propellant or moving parts, using renewable energy sources and eliminating waste.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Force
If conventional propulsion methods (mechanical, chemical rocket, ion drives) are used, then thrust can be generated, but propellant is consumed and waste is produced
Solution Approach 1:
The patent replaces conventional mechanical and chemical propulsion systems with an electromagnetic field-based system. The thrust device uses oscillating electromagnetic fields to accelerate charged particles (electrons and ions) between conductive and dielectric layers, generating thrust through electromagnetic forces rather than mechanical action or chemical combustion. This substitution eliminates the need for consumable propellant while maintaining thrust generation capability
Solution Approach 2:
The patent changes the fundamental operating parameters of the propulsion system by using renewable energy sources (such as piezoelectric materials) to generate oscillating electromagnetic fields instead of chemical energy. The system operates by periodically reversing electric fields to accelerate charged particles back and forth, converting electrical energy directly into kinetic energy of particles and thrust, rather than relying on propellant mass ejection
2Force
If conventional propulsion methods are used, then thrust can be generated, but environmental harm and waste are caused
Solution Approach 1:
The patent replaces chemical combustion and mechanical propulsion systems with an electromagnetic field-based propulsion mechanism. By using oscillating electric fields to accelerate charged particles within a contained structure, the system eliminates exhaust emissions, chemical waste, and environmental pollution associated with conventional propulsion methods while generating the required thrust
Solution Approach 2:
The thrust device uses renewable energy sources such as piezoelectric materials that convert mechanical stress directly into electrical energy. The system is self-sufficient, generating its own operating energy without external fuel supply or waste production, thereby eliminating environmental harm while maintaining continuous thrust capability
3Force
If chemical rocket thrust is used, then propulsion in space can be achieved, but all fuel must be carried and mass increases
Solution Approach 1:
The patent replaces chemical rocket propulsion with an electromagnetic propulsion system that does not require carrying large masses of fuel. The thrust device uses renewable energy sources to generate oscillating electromagnetic fields that accelerate charged particles, producing thrust without consumable propellant. This dramatically reduces the mass that must be carried, enabling sustained space operations without the penalty of fuel mass
Solution Approach 2:
The patent fundamentally changes the energy source parameter from stored chemical energy (fuel) to renewable energy generation (piezoelectric or other sources). By converting mechanical or other forms of energy directly into electromagnetic fields for particle acceleration, the system eliminates the need to carry fuel mass while maintaining thrust capability for space propulsion
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 thrust device provides efficient propulsion without fuel or waste, suitable for space travel and other applications by leveraging the Unruh radiation effect to generate thrust proportional to electron acceleration, allowing for renewable energy use and reduced environmental impact.
Implementation Method 1
thrust is produced by the thrust device in a first direction when electrons accelerate in a second direction
Implementation Method 2
a thrust device that is configured to propel an object using quantized inertia
Data Source
AI summary
The present disclosure relates to a system and method that produces thrust without a propellant or any physically moving parts. The disclosed method produces thrust by accelerating electrons between a multilayer capacitive stack and taking advantage of a conductive dampener that makes up a single thrust unit. For example, as power is applied to a first conductive layer separated by a second conductive layer by at least one dielectric layer, the electrons accelerating from the first layer produce a thrust whose direction is determined by the presence of a cover layer. Multiple middle conductive layers with corresponding dielectric layers can provide thrust scalability. Stacked thrust units with a minimum of a calculated distance between said units can also scale the thrust observed. Specialty materials with built in dielectrics such as anodized aluminum can further improve the thrust unit.