Explosion / Implosion
If opposite a wall (grey, left side of picture) moves back from fluid, relative void comes up into which particles fall by own power, pure occasionally. Particle become rejected by back-stepping wall with some delay and particles fly back by reduced speed. So at the one hand results cold and at the other hand results reduced resistance. The faster wall steps back, the less resistance exists - however only up to sound speed.
At both cases flow becomes generated, once inclusive heat and increased resistance, second case inclusive cold and reduced resistance, i.e. demanding less input of power. Naturally previous back-stepping wall exists not within empty space, i.e. wall´s moving towards left will not be done without resistance. However, at first that wall must not stand right-angles to wanted flow, but also could be arranged diagonal like e.g. surface upside rear end of wing.
Secondly, front-side of wall could be ´hidden´ e.g. behind flow-conform bow of wing. For example, lifting force achieved by wings is ten times stronger than force demanded for drive, clear expressed by resistance-value Cw and lift-value Ca. Naturally similar relation is feasible, if suction-wall turns around circles, where front-side of wall is easy to ´hide within round edges´, like show below.
Static / Dynamic Pressure
Red arrow at A represents original motion, i.e. that flow shows increased (dynamic) pressure into direction ahead. Law of energy-constant inevitably determines, that flow same time must show less (static) pressure towards aside. Exactly same amount thus difference of static pressures (green arrow) right-angles to flow will show, so in total resulting diagonal flow from environment towards faster flow (blue arrow). The stronger original flow thus becomes accelerated, the stronger that pressure gradient (B) rises and the faster that diagonal flow (C) is moving - resulting e.g. these huge vortices systems of hurricanes and tornados with their spiral movement pattern.
Cone-Engine
Around cone-shaped rotor D (red) canal E (light- to dark-blue) is arranged, outside bordered by cone-shape hole of housing F (grey). Rotor moves faster within space at its large radius than at its ´thin end´. Fluid of relative thin border layer is dragged with rotor surface by friction, upside by faster speed than downside (see red arrows G resp. marked by different blue colours). Speed-differences between different flow-layers result corresponding pressure-gradient (see green arrows), so previous suction-process starts, resulting flow diagonal upward, more and more accelerated from downside up (see blue arrow H), all around rotor-cone.
Thus here no back-stepping wall is used but only friction-dragging at rotor-surface. With small input of power thus trigger-flows are initiated, even inclusive advantageous speed-differences. At outlet of canal, at large radius thus flow exits diagonal with much more kinetic energy than necessary for drive of rotor. These are practically likely processes Richard Clem used for driving his car or like Mazenauer achieved explosion of his machine. Within that cone-engine and its wide and barrier-free canal, fluid has much better conditions for autonomous acceleration.
Ultrasound-Acceleration
Within fluid exists average speed of molecular movements, which e.g. is measured as heat. Really however, all particles steady move by most different speeds, probably spread bell-shaped. One very interesting reader of my website gave me hints concerning ´Laval-Nozzle´, so first time I got conscious, also possibility for manipulation of that speed-spreading exists, also demanding nearby null energy-input and above this, advantageous spreading can be organized into special direction.
Even ahead of nozzles exists flow below sound-speed, speed within bottle-neck is accelerated up to sound-speed and particles within wider outlet area fly off by ultrasound-speed. Without input of external energy, but only by change of spreading of molecular speeds, accelerated throughput is achieved, i.e. at outlet increased kinetic energy of well ordered flow is available. That energy can be used by redirection at turbine blades, where no energy is ´consumed´, but only normal spreading of speeds and normal chaotic spreading of vectors are re-established.
At this picture downside, partial longitudinal cross-sectional view of an ´Ultra-Sound-Engine´ is sketched, which here for example is drawn as cone more flat and wide. Canal (blue) is running all around rotor, its cross-sectional surface decreases from inside towards outside, however not steady but by steps. Each relative ´bottle-neck´ (dark blue) represents Laval-nozzle. At least at outer end of canal, that effect of autonomous acceleration should once be used. Afterward, increased kinetic energy should immediately be transferred into turning momentum via redirection at blades. Never before I discussed that point of view, finally at these last chapters I discussed that most important effect in details.
Suction-Blades
As shown upside, flow well is achieved only by friction at rotor-surfaces, however these suction-sides achieve much stronger acceleration. Nevertheless these pumps merely affect pressure onto fluid, i.e. drive of rotor demands minimum power input. These pumps can be used for production of flows of open systems, however also within closed systems these pumps are most effective.
Picture 06.06.05 upside shows simple model of these ´horseshoe-blades´. In comparison with previous animation, here blades are not very long stretched backward (where turning sense of this pump-wheel is counter clock-wise). Suction-sides are relative low, nevertheless suction will affect into wide environment. These pumps are rather simple constructions and can run high revolutions. These pumps can serve for many applications, even that principle design could work as turbine.
Ring-Vortex-Engine
At picture 06.06.05 downside, principle design of corresponding Ring-Vortex-Engine is sketched by longitudinal cross-sectional view. Pump (red) shows half-circled depression, running all around system axis, within which previous suction-blades (light red) are embedded. Fluid (yellow) there is increasingly accelerated into flow diagonal-outward. That flow enters blades (light blue) of turbine (blue) and by narrowing in sense of Laval-nozzles flow becomes accelerated once more. Immediately afterwards, flow is redirected by turbine-blades and guided sharp inward, so turning momentum results. Flow is decelerated and moves back inward much slower.
Also fix connected with turbine is an inner set of blades (light blue), by which fluid is guided right-angles towards suction-sides of pump. Between both sets of blades, ring-shaped body (blue) is installed, thus also as fix part of turbine. Its contours are shaped that kind, canal running all around shows cross-sectional surfaces constant to each radius and adjusted to each speed of flows (probably some more asymmetric than sketched at this picture).
Based on these general principles for organization of fluid-movements and expedient manipulation of molecular movements concerning vectors and concerning spreading of speeds, engines for any performance can be constructed in great variety. Naturally still lots of jobs must be done for optimising and approving best technical solutions. Without any doubts however, problem of clean decentral power supply without consumption of common fuels can be solved, for stationary like mobile applications.
End and Start
Nevertheless that excursion was not in vain because I was able to point out much more distinct how energy of normal molecular movement of fluids becomes usable as free available energy. I well am conscious these chapters contradict common physics understand. However I would really be happy if also a reputed scientist for example would dare to state, each wing needs power for drive however delivers ten time stronger power for lifting airplane, i.e. naturally shows ´over-unity´ (while physicists use logic and mathematic tricks in order to approve wing won´t do real ´workload´).
That´s still that wrong interpretation of energy-constant physic sciences strangles themselves. Fluid still is practically handled like solid bodies and it´s not noticed fluid-internal movements are easy manipulated - and which huge energies thus become usable - without ever becoming consumed. Like any wing also fluid-engines must produce ten times larger benefits than costs. Naturally further researches must be done by physicists and engineers, however working solutions would soon be available if gigantic scientific facilities would be used without ´blinders´. However I hope, engaged handcrafts will sooner deliver approvals and real entrepreneurs will earlier take chance for production of quite new solutions.
I kindly ask not to ask me for further technical details. All I can deliver - as absolute layman - I delivered. I kindly ask not to ask me where which machine now is for sale. As soon as I am allowed, by sure I will publish at my website. At the very moment I only can say some first experiments are rather promising - however don´t ask for details. Any reader can state all that stuff is nonsense - or can convince himself it should work - and any specialist could realize machines, based at his understanding, much better than I ever could.
For me now that subject is closed and I start new workouts concerning ether. If some or even many readers now would start to realize dream of Free Energy - I would be glad.
At previous part 05. ´Particle-Movement´ essential criteria for manipulation of molecular movements and thus basis for usage of free available energy was described in details. Now this last part 06. ´Implosion-Machines´ presents some additional aspects and some conceptions even more effective. While common technologies prevailingly are based on application of pressures, e.g. ´explosion´ of fuel within combustion machines, implosion-technology prevailingly is based on usage of suction-effects. At picture 06.06.01 that difference is pointed out quite clear:
If a wall (grey, right side of picture) is pressed against fluid (blue and red points), fluid particles become accelerated and thus heat is produced, which mostly disappears unused into environment. Resulting are dam-up areas of increased density, into which that wall must be pushed with increased forces. Resistance rises with speed by square, so small efficiency of common pressure-technologies results.
In general, Perpetuum Mobile or usage of Free Energy are considered impossible based on general valid laws of energy-constant, like e.g. well known by lever-arm-law of mechanics. Different to solid bodies however, fluids exist by movable particles and internal flow e.g. is easy to generate by suction. Starting off originally small pressure-differences e.g. large hurricanes are ´born´ or by pure chance come up local whirlwinds. As soon as first motions are initiated, development of momentum of its own comes up, like roughly sketched upside of picture 06.06.02.
It´s common experience, pressure within fluid immediately spreads into all directions likely. Just as fast and inevitably, suction spread into environment, where particles fall by ´own drive´ into these areas of relative void. Force of that suction-movement in general is under-estimated, nevertheless motion occurs with kinetic energy of molecular speed resp. up to sound-speed. Just like relative void, faster flows affect ´suction´ towards neighbouring slower flows - and also these affecting forces in general are under-estimated. Like that simple graph shows, that force is just as strong as dynamic pressure of original flow by itself.
At chapter 05.10. ´Tornado-Engine´ of previous part these effects were discussed e.g. by analyse of Mazenauer- and Clem-Machine. There, movement processes occurred within canals more or less closed, while now at new conception these processes are organized within only one and much wider canal. At previous picture downside is sketched basic design of new and even more effective cone-engine.
Often I described manipulation of normal molecular movements, which practically result some ´sorting´ of vectors when applying suction. Within all flows still exist molecular motions into all directions, only distances until next collision is little bit longer into direction of flow. Just that occurrence is produced with few input of power by friction at rotor surface resp. by back-stepping wall.
Principle of these nozzles and decisive process is roughly sketched at picture 06.06.03 upside. Towards bottle-neck of nozzle comes up increased density and collisions there occur more frequent and after shorter distances. These frequent collisions increase probability of ´multiple-collisions´. So there often will meet e.g. two particles (yellow) same time with third particle (white). Both particles transfer energy onto that third, so that energized particle flies off outlet up to double sound-speed. Energy-delivering particles remain relative ´power-less´ (white) at area of bottle-neck, i.e. represent few resistance for following collisions.
Already often however I had described ´Suction-Blades´ which now I pointed out once more, because that design is very advantageous installed e.g. at ´Ring-Vortex-Engines´. This animation shows pretty well principle of these pumps: teeth-like blades are arranged long stretched and spiral at surface of rotor (which here e.g. is hyperbolic-shaped cone). Surfaces of these teeth showing parallel to general contours of rotor will merely affect pressure onto fluid. Opposite surfaces of these teeth are arranged right-angles to general contours of rotor and represent previous mentioned back-stepping walls (and their back-sides are ´hidden´ because ending smooth into bending of rotor surface).
Decisive effect and movement process of previous machines is easy to understand. However, also back-flow of fluid must be organized also precise. Round and most barrier-free circuit of working medium (advantageous some oil) must be achieved. Lastly, optimum shape will work like hydraulic coupling, where however drive and rotation of pump is necessary only as trigger for self-acceleration of fluids. Pump-wheel there must turn much faster than turbine-wheel, so movement process is even more like starting phase of torque-converter.
Now I finish that excursion into world of fluid- and implosion-technologies. These chapters were intended only as examples for complex movement pattern, so at the following I could better describe and point out differences of motions even more complex of ´my´ gapless ether. Now again, I want to concentrate completely at that ONE all other occurrences and appearances of any kind are based on.
Implosion-Machines