WO1991019105A1

WO1991019105A1 - Deflection accelerated mass propulser conveyance gravity override craft

Info

Publication number: WO1991019105A1
Application number: PCT/US1991/003923
Authority: WO
Inventors: Friedrich Ottokar Wilhelm Arntz
Original assignee: Arntz Friedrich Ottokar Wilhel
Priority date: 1990-06-05
Filing date: 1991-06-04
Publication date: 1991-12-12
Also published as: CA2018234A1; AU8217791A

Abstract

Object of this invention is to create a personnel, passenger, or freight carrier conveyance gravity override craft (109) installed within which are certain gravity override propulsers. Certain energy input (92) is converted into forward respectively upwards momentum. Unidirectional propulsive moments are obtained by keeping pairs of eccentrically loaded contrarotated capsulation cavity accelerator wheels (48), aligned and loaded most effectively whereby the eccentric mass is a suitable liquid (55) in recirculating circuit, such liquid mass constantly being accelerated through appropriate segments of arc of preferably somewhat less than 180 degrees (one hundred and eighty degrees). This invention is distinguishable from other inventions of prior art of some similarity in that this has at least seven elementary differences and applied co-operative functions.

Description

FIELD OF INVENTION __j__

DEFLECTION ACCE---LERATED MASS PROPDLSER CONVEYANCE GRAVITY OVERRIDE CRAFT

This invention endeavors to provide a new transport system that would greatly alleviate traffic congestion as we know it today and would revolutionize transportation and travel in general and also space travel in particular.

The concept applied here is based on Newton's Laws of Thermo¬ dynamics ( energy is never used up only transformed ) and laws relating to the performance of kinetic energy.

Two questions have to be answered in the affirmative - if this concept is to work and perform as predicted. They are:

1 ) Does the machine react on an outside force?

2) Does the machine either change it's mass or it's speed ' constantly all the time? The answer to the first question is: Yes, the machine reacts on the outside/inside force of gravity.

The answer to the second question is: Yes, the machine changes it's speed constantly all the time that is to say a

PART of the machine " namely the liquid mass contained in semi-circular rotation in semi-revolvive excentric confin- ^■ ed accelleration, is constantly changing it s speed.

Though several people over the years have tried to utilize the excentric and centrifugal force effects and convert these forces into unidirectional movement moments it never succeeded until this researched technological development as will be explained in the following disclosure, specification and descrip¬ tion.

DISCLOSURE, DESCRIPTION AND SPECIFICATION.

I have found that in this machine, while operating, a great number of co-relating functions have to take place in on-going manner in overlapping time-frame connection and subsequence, in order to make it work.

Forces and effects created here involve different forms of energy channeling or ducting and conversion after maindrive energy input is engaged thereby creating unidirectional lift and propulsive moments.

The main objective is to obtain lift and unidirectional moment and in such manner as to cancel out sidedrift and unwanted torque moments. Propulsion drive units are preferably always installed in twin configuration and in counterrotating assembly. Transport vehicles using this propulsion system are equipped with at least one vertical lift propulsion module and one horizontal propulsion module. A propulsion module consists of and is comprised of one clockwise and one counterclockwise rotation accellerator capsul¬ ation wheel and confiner-deflector-collider assembly.

Essentially vertical lift moments can be effected in an operating plane varying from 0° to 45° inclined towards the perpendicular orientation axis of the vertical lift propulsion module assembly. And horizontal lift and propulsion moments can be effected in an operating plane varying from 0° to 45° inclination towards the horizontal orientation plane of the horizontal propulsion module assembly. Reacting on the outside/inside force of gravity, the device is working based on functions acting on

1 ) a certain mass - in form of a suitable liquid such as Hg (mercury) in a state of accelleration and

2) acting on a certain mass - in form of the suitable liquid in a state of relative rest in a real time frame setting.

It will be evident that the higher (RPM) the speed of the mass accelleration is and the heavier the accellerated mass is, the more lift or propulsive moment is created. I have found that in order to achieve the desired effect of unidirectional lift and propulsive moment, I have to have the machine act as follows:

A suitable heavy mass liquid is from an appropriate area of injection in partial rotation through preferably NO more than an arc of confinement of 180° ( onehundredandeighty) degrees ) 3

1 ACCEI-LERATED

2 CONFINED IN CURVILINEAR ACCELLERATION

3 EJECTED 4 INTERCEPTED BY ENERGY RECOVERY TURBINES

5 DEFLECTED AND SPLIT INTO AT LEAST TWO EJECTION JET STREAMS

6 INTERCEPTED BY ENERGY RECOVERY TURBINES

7 COLLIDED IN A SUITABLE COLLIDER

8 COLLECTED ( slow Hg, containing NO Kinetic energy ) 9 RECIRCULATED

10 COOLED

11 PUMPBOOSTED AND

12 INJECTED at start point area of Acceleration Sequence in ONGOING, OVERLAPPING AND REPEAT MANNER, thusly:

The mass liquid used here as functional medium, preferably Hg ( mercury ) is being in a state of relative rest, that is to say containing kinetic energy of a very low level, if any, injected into a powerdriven rotated capsulation cavity ACCELLERATOR WHEEL at an injection port area extending from TOP-DEAD-CENTER TDC or right thereof in CLOCKWISE rotated capsulation cavity accelerat¬ or wheels / or in case of COUNTERCLOCKWISE rotated capsulation cavity ACCELLERATOR wheels extending from TOP-DEAD-CENTER or left thereof in such a way as to ensure that the effective loading of cavity capsules BEGINS at TOP-DEAD-CENTER TDC, or to the right thereof in clockwise units and the effective loading of cavity capsules BEGINS at TOP-DEAD-CENTER TDC, or to the left thereof in counterclockwise rotated units.

After mass liquid is injected and is picked up by accellerator wheel capsulation cavity baffles, it is being INSTANTLY INFUSED with very HIGH LEVELS OF KINETIC ENERGY —- and while constantly being kept in accelleration it is also confined and being deflect¬ ed in a curvilinear path of accellerated travel by a SUITABLE CONFINER which consists of a suitably curved part of a suitable material, installed rigidly in such a way as to ascertain and assure free and unencumbered rotation and revolvive ability of capsulation cavity accellerator wheel while maintaining the closest practical distance and even gap from the outer rim of said capsulation cavity accellerator wheels — measurable in ten-thousands of an inch — and maintaining in even close-gap adjacency desired most effective gap tolerance between and along outer accellerator wheel perimeter and along inner curvature rim of confiner in hugging manner, and also observing a like oper¬ ational close gap adjustment between outer injector stem assembly perimeter and inner perimeter of aforesaid capsulation cavity accellerator wheel, whereby said accellerated mass liquid is kept in near semi-circular accellerated rotation for a span of prefer- ably absolutely no more than 180 ° ( onehundredandeighty degrees) of partial accellerated rotation to a suitable ejection port built into the respective confiner-deflector part said respective ejection port located at BOTTOM-DEAD-CENTER BDC mark and extend¬ ing to the left thereof for the most appropriate distance in order to obtain the highest efficiency in such alignment as to ensure an ejection jet stream direction at point of exit perpen¬ dicular to North/South axis through center of capsulation wheel assembly in case of clockwise rotation, or in the case of counter¬ clockwise rotation respective ejection port located at BOTTOM- DEAD-CENTER mark and extending to the right thereof for the most appropriate distance in order to obtain the highest possible efficiency in such alignment as to ensure an ejection jet stream direction at point of exit perpendicular to North/South axis through center of capsulation cavity wheel assembly and from which respective ejection ports for such mass liquid, such mass liquid is ejected as a jet stream by centrifugal force and guided into respective appropriate Energy Recovery Interceptor Turbine which is mated to a suitable power generator such as an alternator, hydraulic pump, electric generator or some such energy converter, whereinthen after expending much of it's ejection-jet-stream flow contained kinetic energy, in this stage considered waste- or nuisance energy, respective jet stream is guided into a splitter-T-divider duct, from where, now split into two, the jetstreams are again ducted through appropriate second stage energy recovery interceptor turbines after which sequence the ejection jet streams, now containing kinetic energy of very little significanace, are suitably ducted into a suitable COLLIDER housing whereinwhich said jetstreams are collided against each other through a suitable collision cushion cartridge, resulting in a PROGRESSIVELY INELASTIC COLLISION, and following this, after said collision sequence, causing the complete exhaustion of remaining kinetic energy and it's transformation into heat or thermal energy, have the now stilled but hot mass liquid remaining, fall into and collect in an appropriate recirculating-collector-sump vessel from where the hot and now STILL MASS liquid containing zero kinetic energy; containing however a high amnount of thermal energy; is pumped through a suitable recirculation and heatexchanger segment whereinwhich said mass liquid is appropriately cooled and from where then said mass liquid, now cold, is pressure-pump-boosted towards the injector feed supply port, from where it is then re-injected into the appropriate respective capsulation cavity accellerator wheel capsulation cavities formed by suitable baffles in-said capsul¬ ation accellerator wheel, in order to repeat in continuing and ongoing manner the above depicted functions-sequence-cycle thereby creating and sustaining the desired lift and forward propulsive moments.

Following up this general outline described here is a vertically disposed propulser module ( for lift moments ), whereinwhich in appropriate match one clockwise and one counterclockwise rotated capsulation cavity accellerator wheel is working in unison, however in contrarotative revolution in a specific pro- grammed operation encompassing many different co-relative functions, whereinwhich in describing the details in Figure 1 disclosing the construction of the clockwise rotated capsulation cavity accellerator wheel segment are depicted essentials of this invention to later be acted on in appropriate fashion as depicted in attendant apparatus as seen in Figure 2, followed by further explanatory drawings in Figure 3, through Figure 9, relating to further other parts and necessary suitable components and functions.

DESCRIPTION OF THE DRAWINGS. There are a total of nine drawings.

In describing those drawings FIGURE 1 is a partly schematic cross-sectional frontview of the CLOCKWISE-ROTATED capsulation cavity accellerator wheel segment of the vertically disposed propulser which consists of a pair of contra-rotated capsulation accellerator wheels, disclosing the essential functions of that part segment of said propulser in it's arrangement to create desired lift and propulsive moments.

£IGURE_B2 is a partly schematic, cross-sectional side view of the attendant apparatus of FIGURE 1 disclosing the recirculating function and the kinetic-energy-conversion function of said apparatus.

ElfiϋδE_..---- i^{s a} partly schematic, cross-sectional frontview of the COUNTERCLOCKWISE rotated capsulation cavity accellerator wheel segment of the vertically disposed propulser complementary to CLOCKWISE rotated wheel segment.

fI§ §E_βjJ is a partly schematic, cross-sectional sideview of the attendant apparatus of Figure 3 disclosing the recirculating function and the kinetic energy conversion function of said apparatus.

F ■I■G■U■R■E■■5■ is a partly schematic cross-sectional sideview of the

COUNTERCLOCKWISE operated high-efficiency propulser segment, showing the vastly improved high-volume mass-liquid transfer capability.

FIGURE 6 is a partly schematic, partly fragmentary cross-section- ■-■■------------■ al frontview of the collider housing-collider cartridge assembly, recirculative collection sump vessel, with attendant apparatus such as ejection Jetstream funneling chute and ducts, Jetstream splitter and energy recovery interceptor turbines, recirculating pumps and partial heatexchanger.

F ■I■G■U■R■E■■7■ is a partly schematic partly functional cross-sectional sideview of the hollow main injector support stem assembly showing a very heavily reinforced lattice grid structural support screen within the main injection port area, and the driveshaft bearing mount end -cap-plate and supply feed port supply duct coupling means. FIGURE 8 is a partly schematic cross-sectional sideview of a

■■■■■■■--I typical one-baffle row ( as opposed to two-baffle row ) capsulation cavity accellerator wheel assembly together with power-drive input means.

FIGURE 9 is a schematic cross-sectional front-view of a gravity craft transporter showing a viable arrangement of both vertical lift propulser and horizontal propulser units installed within and mated to it, wherein also shown is alternate operational capability by said gravity craft shown equipped to be capable to operate as aircraft, a wheeled vehicle, and as an amphibious vehicle or combinations thereof.

DETAILED DESCRIPTION OF THE INVENTION.

Beginning the detailed description with primary CLOCKWISE ROTATED component 1 in Figure 1 , it is shown to be composed of an accel- erator wheel affixed with appropriate capsulation cavities 15 which are formed by capsule separation wall baffles 10. This capsulation cavity accellerator wheel is suitably installed within an outer deflector-confiner casing mantle consisting of inner casing liner 2, outer casing shell 11 interspersed with reinforcement gussets 14v On this module segment, position mark 30 denotes north or 12 o'clock or Top-Dead-Center TDC position of 1, whereas position mark 31 denotes south or 6o'clock or Bottom-Dead-Center BDC position of segment 1. Brackets 90 serve to install and appropriately mate to it's opposite match unit the here described clockwise rotated capsulation cavity wheel unit segment. As is evident said capsulation cavity accellerator wheel is rotated within aforesaid deflector-confiner casing 2-11-14 in close gap adjacency and is at the same time rotated appropriately around a suitable inner hollow main injector support stem assembly 9 consisting of main injector stem inject¬ ion port segment 6 and solid segment 16 of maininjector support stem assembly 9, which here also is shown affixed with mass liquid injector feed supply portflange 5 surrounding mass liquid maininjector supply port 7 showing within it's perimeter a partial schematic rendition of pressurized—cold recirculated injection mass liquid 28. Also indicated by small stipled indi¬ cator arrows ( not numbered ) is shown mass liquid 28 about to be pushed into the inside openings of those capsulation cavities 15, that at this appropriate instant are in accessability align¬ ment with aforementioned main injector stem support assembly injection port 6. 8 denotes the appropriately contained and confined mass liquid in CURVILINEAR ACCELLERATION while it's volume is increased incrementally as each individual capsulation cavity, DURING the appropriate interface fluid transfer cavity feed sequence, is supplied with more and more MASS LIQUID in cumulative fashion from position point to position point. In other words - at start of interface fluid transfer sequence - relatively little mass liquid is pushed into the cavity closest . to the start line of interface fluid transfer sequence but in a rising curve in relation to transfer interface arc covered, coinciding with injection port area 6, each capsulation cavity is filled with m ■o■r■e■ and m■o■r■e■ mass liquid 8, whereinwhich at the end of the fluid transfer interface arc each respective cavity is at that point in time or at that instant filled-to capacity. Arrow 12 indicates clockwise rotation. Figure 2 showing attendan apparatus to aforementioned clockwise rotated capsulation cavity accellerator wheel 1. 13 is arrow indicating direction of eject ion jet stream, funnelling reducer fitting 17 and duct connector flanges 3 for ejection jet guidance duct 18 conducting Jetstream 21 through a suitable ENERGY RECOVERY INTERCEPTOR TURBINE 19 whose matching powergenerator unit is suitably connected to powe drive unit 25 of recirculation pump 24. Jetstream conductor duct 18 is conducting 21 towards a suitable collider housing assembly containing a suitable collider cushion cartridge arrangement 20, from where the now hot but stilled mass liquid 22, now contain¬ ing very little kinetic energy, if any, falls into an appropriat recirculation collector sump vessel 23. From there pump 24 pushes hot mass liquid 22 through a suitable heatexchanger 26, cooling 22 to an acceptable temperature whereinfurther the now cooled mass liquid 28 is further pressure boosted by booster pump 27 to be routed towards and into main injector supply port 7 depicted in figure 1. Arrow 29 indicates direction of travel of 28.

In bringing the description to the primary COUNTERCLOCKWISE ROTATED component as shown in figure 3, 48 is composed of an accelerator wheel affixed with appropriate capsulation cavities 37 which are formed by capsule separation wall baffles 38. This capsulation cavity accellerator wheel is suitably installed within an outer deflector-confiner casing mantle consisting of inner casing liner 47, outer casing shell 46 interspersed with reinforcement gussets 45. On this module segment position mark 40 denotes north or the 12 o'clock position or TOP-DEAD-CENTER TDC position of 48 and marker arrow 41 indicates the south or 6 o'clock or BOTTOM-DEAD-CENTER BDC position of 48. Brackets 90 here also serve to install and appropriately mate to it's oppos¬ ite match unit, here described COUNTERCLOCKWISE ROTATED ACCELL- ERATOR CAVITY WHEEL unit segment.

As is evident said capsulation cavity accellerator wheel is rotated within aforesaid deflector-confiner casing 47-45-46 in close gap adjacency and is at the same time rotated appropriatel around a suitable inner hollow main injector support stem assemb ly 35 consisting of main injector stem injection port segment 34 and solid segment 39 of main injector support stem assembly.. In this frontview also can be seen the suitably perforated shape retention reinforcing ring 32 for aforesaid main injector suppor stem assembly 35 which here also is shown affixed with mass liquid injector feed supply port flange 33, surrounding mass liquid main injector supply port 49 showing within it's perimete a partial schematic rendition of pressurized - cold — recircul¬ ated injection mass liquid 58. Also indicated by small stipled indicator arrows ( not numbered ) is shown Mass Liquid 58 about to be pushed into the inside openings of those capsulation cavi¬ ties 37 that at appropriate instant are in accessability align¬ ment with aforementioned main-injector-stem-support-assembly- injection port 34. 36 denotes the appropriately contained and confined MASS LIQUID IN CURVILINEAR ACCELLERATION while it's volume is increased incrementally from capsulation cavity to capsulation cavity as each individual capsulation cavity, DURING the appropriate interface fluid transfer cavity feed sequence, is supplied with more and more MASS LIQUID IN CUMULATIVE FASHION from position point to position point to position point. In othe words, at START of interface fluid transfer sequence relatively little mass liquid is pushed into the cavity CLOSEST to the start line of interface fluid transfer sequence, but in a rising curve in relation to transfer interface arc covered, coinciding with injection port area 34, each capsulation cavity is filled with more and more mass liquid whereinwhich, at the end of the fluid transfer interface arc, each respective cavity is at that point in time or at that instant filled to capacity. Arrow 42 indicates counterclockwise rotation.

Regarding Figure 4 showing attendant apparatus to a foredescribed COUNTERCLOCKWISE ROTATED capsulation cavity accellerator wheel 48, 43 is arrow indicating direction of ejection Jetstream, funneling reducerfitting 61 and duct connector 52 for ejection jet guidance duct 62, conducting Jetstream 44 through a suitable ENERGY RE¬ COVERY INTERCEPTOR TURBINE 51 whose matching power generator unit is suitably connected to powerdrive unit 56 of recirculation pump 54. Jetstream conductor 62 is conducting 44 towards a suitable collider housing assembly containing a suitable collider cushion cartridge arrangement 50 from where the now hot but stilled mass liquid 55, now containing very little kinetic energy falls into an appropriate recirculation collector sump vessel.53.

From there pump 54 pushes hot mass liquid 55 through a suitable heatexchanger 57, cooling 55 to an acceptable temperature where- infurther the now cooled mass liquid is further pressure boosted by booster pump 59 to be routed towards and into the main inject- or supply port 49 depicted in module segment 48. Arrow 60 indi¬ cates direction of travel of 58.

In Figure 5 is described a preferred arrangement of a high-effi¬ ciency capsulation cavity accellerator wheel, in this case representing a COUNTERCLOCKWISE rotated capsulation cavity accellerator wheel segment wherein said cavity capsulation accell¬ erator wheel consists of a centerspine segment 77 of said wheel wherein said part 77 is suitably affixed and locked to shaft 69 which in turn is securely fixed in revolvive manner and suitably installed in appropriate centershaft bearings 74 and lateral shift lock flange bearing 67. As is apparent centerspine segment of said cavity capsulation wheel has suitably attached to it suitable appropriate cavity vanes 38 essentially perpendicularly affixed to it's axis shaft body in even distribution on each side to aforesaid part 77, which vanes at their respective outer- most vertical edges are mated to a suitable retainer keel segment end ring part 78 at each outer side thereby connecting individual vane blades at the respective outer sides and keeping them in secure operational position, all respective vane blades also thereby forming back and front wall ring segments for the format¬ ion of suitable capsulation cavities 37. 80 denotes appropriate weight reduction cavities of 77. 75 are special injection mass liquid supply header perforations suitably cut into the hollow main injector support stem/assembly stem 35 on the driven side of aforesaid cavity capsulation accellerator wheel segment where¬ in 75 are suitably shrouded by special injection mass liquid supply port shroud module assembly 76. 39 denotes the solid seg¬ ment of 35. 68 is the drive power connection means attached to shaft 69. 73 are lateral shift lock dowels. 66 are suitable supply lines feed couplings affixed to 76. Propulser unit accell¬ erator wheel segment side cap plate 65 on the driven side of typical 35 is suitably affixed to said hollow main injector support stem assembly 35 which also at it's inner end section is mated to a suitable bearing mount 89 for shaft 69.

In the simpler non-driven side 35 segment 70 is a suitable end plate. 63 are the supply ports alternate means for the high- efficiency unit propulser. 79 are suitable assembly weld seams. 64 is the respective propulser unit typical side cap plate for typical 35 non-driven side. 46 denotes the casings for counter¬ clockwise unit segment. 81 are the side plates of centerspine segment 77. 61 are EJECTION JET-STREAM outlet flange frames for coupling to further suitable ducting. 34 denotes the actual injection interface injection port area of 39.

Figure 6 is a partly schematic partial function-depicting-view of the suitable collider sump and attendant apparatus wherein 31 is an arrow indicating the flow direction of the mass fluid 21, which containing a large amount of kinetic energy is split into at least two jet streams by jet stream splitter 86.19 are suitably placed appropriate energy recovery interceptor turbines with energy converter and energy ducting assembly ocn-pc-nent far ptup 24 drive.After recovering and converting most of the here as nuisance considered kinetic energy contained in 21, the EMAINING much lesser kinetic energy contained in 21, after having 21 ducted suitably through 19 is then expended and converted by colliding the two split branches of the primary ejection jet stream against each other in a suitable collider housing of sump assembly 23 whereinwhich said Jetstream branches are collided against each other through a suitable collider cushion cartridge assembly 20 which is filled with a suitable collision retarder means such as steel balls, metallic shaving curls, gravel pebbles or the like causing a suitable, increasing¬ ly INELASTIC COLLISION to take place in ongoing manner. 20 is held in position by cartridge holder frame 88. 87 is a frame flange coverplate making for easy exchangeability when necessary. 85 are the support brackets for 88. 22 is the now hot but still mass liquid collected in the sump vessel 23 to be ducted into recirculation mode by pump 24 and through heatexchanger 26.

In Figure 7 is shown a typical partial cross-sectional side view. of the clockwise capsulation cavity accellerator wheel showing a reinforced lattice screen structure that injector port area 6 is equipped with in order to maintain structural rigidity of hollow maininjector support stem 9. 83 are suitable fasteners holding confiner casing 2-11-14 securely to propulser .unit side- ^" cap-plate 64. In Figure 8 is shown in typical, partly schematic cross-sectional side view how a typical single baffle row clockwise rotated rotor is matched to a suitable power drive input means. Also shown is an alternate reinforcing lattice screen 108 for 6 allowing for always unimpeded injection flow at the same time however provid- ing the preferred utmost possible structural rigidity.

Figure 9 is a typical, schematic rendition of a passenger, personnell conveyance or freight transporter 109 equipped with a gravity-override propulsion system comprised of vertical plane and horizontal plane centrifugal guidance propulsers, wherein- which such aforesaid transporter is capable of operating in amphibious mode, as a wheeled conveyance, as flying aircraft or as a gravity override gravity craft or in desired combinations thereof.

Typical clockwise rotated rotor unit, that is to say clockwise rotated capsulation cavity accellerator unit 1 is suitably mated to counterclockwise rotated rotor unit 48 by mating yoke assembly 102 which is affixed securely to attitude control mechanism 101. 92 are variable speed and power input ( for propulsive control ) main drive engines of a suitable nature such as turbine engines, diesel engines, combustion engines, hydraulic motors or electric motors. 23 and 53 are respective collider sumps for 1 and 48. 107 is a suitable vertical control airfoil. 93 are suitable lighting banks. 95 are fuel tanks. 96 is a suitable shroudway for the horizontally operated propulser unit module 99 with it's collider sump recirculator 100, and showing suitable swing anchorpin cylinder 97 assembly holding support arm assembly 98 which has 99 suitably mounted to it. 106 denotes waterline when in amphibious mode. 94 are suitable wheels for wheeled operation, 104 are retractable airfoils for aircraft operation mode supported by swing support pins 105.

Claims

CLAIMS .

What I claim as new and try to secure under the Patent Co-oper¬ ation Treaty PCT and WIPO is:

1 ) A PERSONNELL, PASSENGER or FREIGHT TRANSPORT CONVEYANCE operable in either aircraft, amphibious, wheeled, or gravity craft mode, or combinations of above, which is mainly propelled in horizontal, and / or vertical planes or combinations therof by having certain ( subsequently to be described in more detail with respect to aforesaid ) gravity override propulser units or banks of such units, installed within or appropriately affixed to such craft, respective propulser units intended for mainly horizontal forward propulsion and certain respective propulsers intended for mainly vertical and lift-moments-inducing propulsion and hovering capability, said propulsers operated in a suitable combination of operating planes and in appropriate combination with suitable variations of energy throughput intensity and revol vive speed, and also operated in controlled guidance, wherein- further such propulser units, working on the basis of suitably and preferably most effectively guided mass centrifugal excentric partial circular path accelleration, induced by appropriate energy input obtained by way of having appropriately coupled suitable engines attached to certain capsulation cavity liquid mass accelleration wheels, preferably installed in matched but counterrotative pairs per propulser unit module, which are appropriately spinning and rotating a suitable mass liquid through a partial circular path of curvilinear accelleration of preferably no more than 180° ( onehundredandeighty degrees ) of arc, wherein-further said arc path is aligned and programmed in preferably the most effective way alignment and orientation frame with reference to desired direction of desired propulsive moments in conjunction with having suitable mass liquid suitably recirculated and appropriately injected in preferably the most efficient programming and operation whereby the appropriate interface fluid transfer injection port area is so fashioned as to supply respective capsulation cavities with more and more mas liquid in cumulative fashion from position point to position point to position point, whereinwhichfurther in other words, at start of interface fluid transfer sequence relatively little mass liquid is pushed into the cavity closest to the start-line of interface fluid transfer sequence area, but in a rising curve manner in relation to transfer interface arc covered, coinciding with injection port area, each capsulation cavity is filled with more and more mass liquid whereinwhich at the end of the fluid transfer interface arc each respective cavity is at that poin in time or at that instant filled to capacity furtherwhereinwhich subsequently at the preferably six o'clock position of revolution of mass liquid it is allowed to eject by centrifugal force to have subsequently it's ejection Jetstream or jetstreams appropriately divided and subsequently have respective individual jetstreams of preferably like and balanced kinetic energy content suitably collided against each other in preferably balanced kinetic collision in order to transform kinetic energy here con¬ sidered as nuisance energy, into thermal that is heat energy and also furtherwhereinwhich aforesaid ejection jetstreams, before they enter collisionchamber (s) are suitably intercepted by suitable interceptor energy recovery turbines coupled to suitable energy converters whereby most of aforesaid waste or nuisance kinetic energy is usefully converted and only relatively little kinetic energy reaches the appropriate collision process, all such functions and processes taking place in correllated and ongoing synchronization.

2) A personnell, passenger or freight transport conveyance according to claim 1 , whose suitably installed appropriate propulsive moment inducers consist of mainly DEFLECTION-ACCELLER- ATED MASS PROPULSERS installed in suitably assembled matched together units of adequate numbers, whereinwhich one propulser unit module consists of at least one CLOCKWISE and one COUNTER¬ CLOCKWISE rotated capsulation cavity accelleration wheel, rotated in contrarotative unison; whereinwhich each wheel respectively is comprised of suitable capsulation cavity means affixed to a respective wheel keel strongback piece either positioned centrally or to a side, mated to an appropriate driveshaft contained in suitable bearings, said driveshaft mated to an appropriate power transmission means such as suitable gearing, pulleys or the like or directly coupled to a suitable appropriate engine or prime mover-power input device, whereinfurther respective cavity capsulation accellerator wheel is securely and appropriately mounted in close-gap but free-wheeling proxi- mity essentially within a suitable preferably most effective and suitably shaped CONFINER-DEFLECTOR-CASING equipped with an appro¬ priate EJECTION-JET-STREAM-PORT-NOZZLE-DUCT and furtherwherein suitable driveshaft bearings are partly mounted suitably within appropriate bearing mounting depressions or other suitable bear¬ ing mounting means at the respective outer end side of the cap- plate ends suitably affixed to appropriate injector mounting stem assembly that is extending into the center void of the respective capsulation cavity accellerator wheel and wherein- further a suitable injector port contained in the injector mount¬ ing stem appropriately incorporates the preferably longest appropriate close-gap interface fluid transfer contact arc path with respect to desired most efficient performance.

3) A conveyance according to claim 1 equipped with certain propulsion devices whereinwhich claimed as novelty is the use of mercury as applicable mass liquid in operational application.

4) A conveyance equipped with propulsion devices according to claim 1 which claims as novelty the use of a suitable oil and metallic powder mixture as a mass liquid in operational application.

5) A conveyance equipped with propulsion devices according to claim 1 which claims as novelty the use of water as an appropri¬ ate mass liquid in operational application provided metal parts used in this case for the construction of this machine are of corrosion-resistant alloy.

6) A conveyance equipped with propulsion devices according to claim 1 which claims as novelty the use of molten liquid tin as a mass liquid in operational application wherein aforesaid liquid tin is suitably kept hot enough and in an adequate state of flux by being kept suitably hot and in molten condition being kept suitably hot and in molten condition by being operated immersed suitably in a suitable gas atmosphere such as argon or other suitable mixture of gases or gas of an inert nature.

7) A conveyance according to claim 1 equipped with propulsion devices as in claim 1 in which respective clockwise and respect¬ ive counterclockwise rotated cavity capsulation accellerator wheels have respective or applicable resulting ejection jet streams ducted appropriately thusly that respective jet streams containing kinetic energy of essentially equal force and content are suitably collided against each other for the conversion of kinetic energy into thermal energy.

8) A conveyance equipped with propulsion devices according to claim 1 in which CLOCKWISE ROTATED CAPSULATION CAVITY ACCELLER¬ ATOR WHEELS have their MOST EFFECTIVE by far functional quadrant segment activity take place IN THE THREE 0"CLOCK QUADRANT TO SIX 0"CLOCK QUADRANT wherein south-north line equals six o'clock to twelve o'clock line and also equals propulsive moment direct- ion line.

9) A conveyance equipped with propulsion devices according to Claim 1 in Which COUNTERCLOCKWISE ROTATED CAPSULATION CAVITY ACCELLERATOR WHEELS have their MOST EFFECTIVE by far functional QUADRANT segment activity take place in the NINE O'CLOCK TO SIX O'CLOCK QUADRANT, wherein south-north line equals, six o'clock to twelve o'clock line and also equals propulsive moment direction line.

10) A conveyance equipped with propulsion devices according to claim 1 in which a suitable heavy mass liquid is from an appro- priate injection port area preferably in the most efficient design possible, in partial rotation through preferably no more than 180° ( onehundredandeighty degrees ) in ongoing sequence accellerated, confined in curvilinear accelleration, ejected, deflected and ducted as suitable ejection jet streams, suitably intercepted by energy recovery interceptor turbines, suitably collided in a suitable collider, collected, suitably cooled, re¬ circulated, cooled, pumpboosted or vice versa and reinjected at suitable injection area ports in ongoing, overlapping and repeat manner wherein the mass liquid before injection being in a state of relative rest is then suitably picked up by appropriate capsulation cavity baffles at which instant it is instantly INFUSED with very high levels of KINETIC ENERGY thereby over - riding the innate INERTIA of the mass liquid before the instant of injection and pickup.