SE2000238A1 - Vortex Propeller - Google Patents

Abstract

This document is a patent application and covers an overview of Vortex Propulsion which is an overview of a previously unknown and undocumented functional acceleration manipulation device which is a new concept. After reading this document you will basically understand mechanism of how to build a functional modeled propulsion device and have a understanding of functionality. Vortex Propulsion is entirely an innovation invention. This device is a rational functional aerospace propulsion concept which introduces a new innovation in methodology unexpressed prior to this application to the Swedish patent authority body PRV. This innovation is not a gift or token purchase; nor collaboration from any collective with which I have collaborated; data was subsequently collected and interpreted. The resulting device is an acceleration manipulation device and is a new innovation. I present here manipulation which covers its capability in manipulation of acceleration as well as elaborated proposal of use as a motorized propulsion device. This document should be reviewed by a physicist or engineer for interpolation assessment.

Description

Vortex Pronulsion - Aerosnace Provulsion Brief : This document is a patent application and covers an overview of Vortex Propulsionwhich is an overview of a previously unknown and undocumented functional accelerationmanipulation device which is a new concept. After reading this document you willbasically understand mechanism of how to build a functional modeled propulsion deviceand have a understanding of functionality. Vortex Propulsion is entirely an innovationinvention. This device is a rational functional aerospace propulsion concept whichintroduces a new innovation in methodology unexpressed prior to this application to theSwedish patent authority body PRV. This innovation is not a gift or token purchase; norcollaboration from any collective with which I have collaborated; data was subsequentlycollected and interpreted. The resulting device is an acceleration manipulation deviceand is a new innovation. l present here inaniptilation which covers its capability inmanipulation of acceleration as well as elaborated proposal of use as a motorizedpropulsion device. This document should be reviewed by a physicist or engineer forinterpolation assessment. lllustrated below is an enclosure medium /gas filled with an inner shaft fitted with adownward force motorized clockwise propeller above and a motorized stir rotationanticlockwise propeller plane within the shaft to stir the devices medium. Verticalvelocities combine with horizontal rotation to result in a longer distance fusion of velocities and vector acceleration for the propeller plane.

This configuration is a closed loop propulsion system propelling in this schematic producing thrust upwards for the vehicle when fitted to a vehicle for use in space where thereis no medium for a conventional propeller/ turbine. The medium used in this example calls forxenon gas a medium which has compression property including other than gas and a higher density than carbon dioxide gas like compressed xenon. f \ E Propeller j PropellerPlane i|||||i|||||||| enteri I c Illl Illl J Overview of rotation filter: Overview \ The rotation filter is used to a null rotation of the medium thereby releasing inertial dark matter surface of rotation energy. This fulfills the conventional propulsion requirementargument that matter needs to be released by a body at rest to effect propulsion.Validity requirement of matter release is further eroded when considering that inertialmass decays when interacted with as a surface This rotation filter is static. lt is assumedthat rotation forces generated by the device would require the use of two modulescountering each other in torque and rotation forces what is shown thus far is one module which could be either right or left module.

Propulsive argument: Rotation of the medium within the sliaft increases the thrust created by the propeller turbine by inducihg a complimenting energy surface of inomenttim and inertia against which to propel (vortex) similar to ground effect vortices further to which the exhaustvelocity of the shaft is decreased when compared to a shaft without a rotation filter. Whileproviding resistance to the velocity of thrust from the propeller as inertial mass; the rotatedmedium of the propeller plane does not counter against the chassis of the vehicle hence wehave an opportunity of free space resistance without cost thereby facilitating propulsion. Thecombined velocities plus accelerations within the shaft exceed the velocities in the returnshaft of medium to the propeller intake for closed loop recycle. The rotated plane within the shaft illustrates that matter and inertia are interchangeable for a given volume Lorentz Force s2(sin s cos)/\s2(cos s sin)=Ve Distance traveled by the medium within the inner shaft as exceed distance traveled onreturn to intake. lvlanifolds can be used to decrease undesired rotations on the outer shaft ofthe device shell as well as a null momentum energy rotations prior to impacting the modulefioor from an optimized height.

Recursive argument: Sums of shaft velocities evidence a propulsive argument taking sum potential of five (i)velocities where there is gain component posed by a decelerating module floor relative outershaft that requires includes with residing vector velocities where a bar value is exceeded toeffect an acceleration impulse valued by vehicle mass variables including floor decelerationrelative to outer shaft propeller velocity - employed mass versus load. We find that thisdynamic is overcome by the vector velocities being independent of propeller thrust resultingin a ratio of propeller thrust in conjunction the vector variables of this logarithmic algorithmof systemic flow being relative of vehicle chassis distances.

Magneto-hydro dynamic Hg medium template : Cathode Anode Spatial propeller (+l Conical Magnet Diamagnetic lnner shaft Rotation Filter t 1 Il t l ll i J Rotation Manifold Here is a template for a vortex propeller using magneto hydrodynamic and mercury medium; Wecan see that here use of the outer ring for rotation propelling With a spatial propeller at the topof the image for the outer ring. A shielded conical magnet sheath is used to shield the innershaft from magneto-hydro dynamic rotation.

Recursive arqument continued: In the diagram below we see an addition of torsion dynamic angular momentum which iscompounded for the rotated length. A vortex event accumulation which translates into usabletemporal mornentum with Velocity transfer due to higher veiocities as thrust dynamic moves further out from focal. t llll llll 1 Nanotube for platform microboard: Taking advantage property of magnetic field vector being a field linear field strength for spatialdistribution paradigm we have a nanotube example; preferred for an entirely magnetohydrodynamic functioned module with a Chassis mounted propeller.

Cathode Anode Electromagnetic Conlcal / Propell Vanez/(-l Diamagnetic Shielding Permanent Conlcal Magnet _ m Inner Shaft" ii i in iiuiiiii _ Rotation rutert iii i iii i , Rotation Manifold ln this template we have a propeller vane which is a deflector frame mounted propeller forrotation downwards generating a propelling force with thrust energy being transferred to theplatform /vehicle Chassis. There is diamagnetic Shielding to prevent undesired rotation in theinner Shaft of this module. The electromagnet variable conical magnet is a permanent conicalmagnet functioning induced rotation a dynamic of magneto hydro dynamics. Below, a rotationfilter functions to a null rotation in the wash return cycle of this templates algorithmic flow.

Rotation manifolds are included in the module floor to a null rotation prior to impacting themodule floor.

Vortex Propeller : Cathode .

H I InI-Iilšlí llllll eLLLi, Anode HH e!ï!äš Propeller Vane N/S Electromagnet S/N MagnetDiamagnetic ShieldingInner Shaft Rotation Filter Rotation Manifolds ln order to optimize the propellers vortex values we change it's overall shape trorn a basic tube configuration to a conical one. This allows us to extend the rotation planes increasing the rotational forces produced in this propeller thereby increasing propulsion force produced. Conical magnets are arranged so that spin versus each other is reversed noted as north /south and south / north with power variance where an electromagnet is ernployed for magneto hydro dynamic spin.

Reguirement: This is a breakthrough of process and methodology as well as state of accelerationcomponent potential for aerospace logistics propulsion complementary. The technologiesemployed exist Where the practice, usage and conception did not; I claim ownership aspropohent and originator of this concept step towards propulsion methodology havingresearched solutions. This type of acceleration device does not exist and l am theoriginator of this concept. This device is available and justified in what can be called a demonstration of anomaly in the commonly assumed physics of motion.

Stefan Tubman