Device for generating directed thrust force by means of an asymmetric electromagnetic field pulse control unit
The propulsion system addresses inefficiencies in mass-ejection systems by generating momentum flux asymmetries within an electromagnetic field to achieve efficient and precise thrust conversion.
Patent Information
- Authority / Receiving Office
- DE · DE
- Patent Type
- Utility models
- Current Assignee / Owner
- KHAN MUHAMMAD ZOHAIB
- Filing Date
- 2026-03-04
- Publication Date
- 2026-06-11
Smart Images
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Abstract
Description
[0001] Technical field: The invention relates to a propulsion system for aircraft, spacecraft, and other mobile platforms. The invention utilizes the generation of momentum flux asymmetries within a localized electromagnetic field to effect a directed kinetic displacement without the ejection of supporting mass.
[0002] Disclosure of the invention: The system comprises means for generating a localized electromagnetic field pulse density within a defined volume. By applying non-reciprocal time modulation (asymmetric duty cycle), the field pulse density built up in the system is discharged directed into the surrounding physical vacuum (localized field).
[0003] This process causes a momentum transfer between the system's internal field and the external metric field, resulting in a net acceleration of the overall system. Here, stored electromagnetic energy is directly converted into kinetic energy of the carrier system according to the momentum theorem.
[0004] To ensure the physical integrity of the system during operation, the control unit has an integrated symplectic audit logic. This ensures that the energy conservation laws are maintained and that thrust generation is precisely isolated from internal numerical drift effects. Reference symbol list 1 Distance travelled (meters) 2 Lateral Oscillation (Meters) 3 Speed limitation width 4 Force (Newton) 5 Force input (asymmetry ratio 0.75) 6 Speed 7 Time (seconds) 8 Generator (black dot at the origin of the coordinate system) 9 Object (starting point of the trajectory)
Claims
Device for generating thrust, comprising: a) means for generating a variable electromagnetic field pulse density within a carrier system; b) a control unit configured to effect a temporally asymmetric modulation of the field pulse density in order to emit a directed pulse flux into a localized ambient field; c) wherein the control unit is configured such that the asymmetry of the modulation cycle generates a net reaction force on the device. Device according to claim 1, characterized in that the modulation cycle comprises a build-up phase with a first temporal rate of change of the pulse and a discharge phase with a second, higher temporal rate of change. Device according to claim 1 or 2, characterized in that the control unit is configured to force a non-reciprocal interaction between the internal energy storage and the external field pulse exchange, so that the internal electromagnetic energy is directly converted into kinetic energy of the device. Device according to one of the preceding claims, characterized by a control unit with an integrated numerical audit logic, which preferably comprises a symplectic integration logic to validate the conservation laws of the total pulse with a precision of at least 10-9 and to isolate the directed pulse flow from numerical artifacts.