DE102015016604A1 - Mass loss free electromechanical satellite propulsion - Google Patents

Abstract

The present invention relates to a zero-loss electromechanical satellite drive. In this case, in a closed tube, a rocket nozzle is attached at one end, and a shock absorber unit at the opposite end. The energy for the rocket nozzle is provided by solar energy by electrical or thermal energy for splitting water into hydrogen and oxygen or steam generation. Alternatively, energy can be harnessed by nuclear decay energy. In the shock absorber, part of the impinging impact energy is converted into internal energy and drained out of the system. This creates an imbalance in the movements that causes locomotion with the satellite unit coupled to the drive.

Description

Technical area

The present invention relates to a zero-loss electromechanical satellite drive.

Such drives are known from the prior art. In this case, microwaves are used in a body in such a way that a propulsion arises. However, these drives have the disadvantage of low propulsion of sometimes less than a Newton. See the EM drive U.S. Patent 5,543,801 or WO 2007089284 ,

Based on the knowledge of the wave-particle dualism, which is proven in numerous double-slit experiments also with molecules (Buckminster fullerenes), it should therefore be possible to build a particle drive without mass loss, which allows higher thrusts.

This object according to the invention is achieved as follows.

Presentation of the invention

The lossless electromechanical satellite propulsion system consists of a closed tube in which a missile nozzle is located at one end and an absorber unit for converting the kinetic energy into internal energy of the overall system at the other end of a tube of multiple length of diameter.

For propulsion, the impulse of an explosive reaction of hydrogen and oxygen is used, which is ignited in a pressure chamber and then ejected from a rocket nozzle.

This drive unit is located at a pipe end of the closed tube, which is broken only by cables but closed.

After ignition, the entire system moves in the opposite direction of the exiting water molecules until the particles impinge on the other side of the pipe. Then the whole system comes to action according to action equal to standstill but is changed by an amount capable.

So that the entire system does not come to a standstill, an absorber unit is provided on the side opposite to the drive unit, shortly before the end of the tube, which converts the impact energy into internal energy.

The absorber unit is a concave circular sheet having a porous, permeable coating for trapping the water molecules.

The impact forces acting thereby convert one or more shock absorbers with which the absorber disk is mounted at a distance from the back into heat by the media flowing in the shock absorbers. The flowing media flow through an adjustable BEZW. fully lockable throttle / kickback assembly.

The heat is radiated via a radiator, which is preferably attached to the back of a photovoltaic panels.

This energy is no longer available for completely decelerating the entire system and the overall system is accelerated by discharging it from the missile nozzle at intervals.

This phenomenon can also be observed in everyday life when a dropped rubber ball (even in a vacuum) no longer reaches its initial height, because part of the kinetic energy has gone into deformation work and thus heat of the rubber ball. If the ball reached its initial height and warmed up, the energy conservation rate would be violated.

Likewise, a steel bolt can heat up to red-hot by hammer blows. Part of the hammering energy is transformed into internal energy of the steel and thus no longer hits the anvil.

The water accumulates due to the acceleration experienced by the entire system at the tuber-lying location of the concave absorber disc. There it is passed via a telescopic line to an electrolysis unit. This converts the water from the panels into hydrogen and oxygen using solar energy. These gases are passed separately to the pressure chamber and fed there again to the cycle.

The energy can also be supplied by other energy sources such as radioactive decay energy or a battery.

There is no loss of water.

A variant of the drive unit consisting of pressure chamber and nozzle provides that therein steam, which was heated with solar thermal solar collectors under high pressure leaves the nozzle at intervals.

The absorber plate becomes active during the expulsion of the molecules through the closed throttle hindered from moving. Only a moment later, the throttle opens so that the absorber plate can move towards the back. The then used impact energy now allows it with a spring to push this absorber plate in the initial position. The next ignition follows.

Brief description of the drawings

Embodiments of the invention, from which further inventive features result are shown in the schematic representations.

Show it:

1
A schematic view of the invention from the side

2
Another schematic representation of a variant of the invention.

Embodiment of the invention

With 1 is a lossless electromechanical satellite propulsion unit that uses solar energy (electrical, thermal) to accelerate a coupled unit.

This has a pressure chamber 2 with rocket nozzle 3 in which an oxygen / hydrogen mixture is cyclically exploded and via the nozzle 3 generates a feed.

In 2 takes the pressure chamber on pressurized steam, which is also ejected clocked.

The ejected molecules measure the tube closed all around 1.1 until impact on the absorber disk 4 with porous permeable structure and give their impact energy to the absorber disc 4 from, until the impact of the particles through the closed throttle 12 or by eddy current brake in the rotating bodies (counter-rotating) is held and released at the moment of impact of the molecules.

The absorber disc 4 is in 1 against the shock absorbers 12 pressed, with the circulating medium contained in the shock absorbers (oil, gas) via the adjustable throttle 12.2 flows and the medium is heated by friction.

The medium is preferably passed to a radiating surface located at the back of the solar panels and cooled.

The feather 14 conveys the absorber plate 4 back to the starting position and in the throttle / check system, the cooled medium flows again with little friction from the solar panels / radiation unit 6 back into the shock absorber.

The condensing water in the absorber plate, which has a structurally achievable temperature, collects at the lowest point of the concave disk and flows through the telescopic tube 11 via a check valve 11.1 to the electrolysis unit 5 ,

The electrolysis unit 5 is via lines 7 and 8th supplied with power from the photovoltaic panel.

The gases generated there are hydrogen and oxygen via lines 8th and 9 separated from the pressure chamber 2 fed and re-clocked brought to the explosion.

This creates a mass loss-free material cycle.

In the variant off 2 high-pressure steam flows out of the steam generator 5.1 via wire 9.1 in pressure chamber 2 and is also clocked there by rocket nozzle 3 pushed out.

The steam generator 5.1 gets its thermal energy via wire 8.1 from the solar panels 6.1 eg. a gutter parabolic mirror with absorber.

The administration 8.1 a heat pipe is commonly referred to as a heat pipe.

The rotation body 12.1 , from the double-sided rack 13 By means of gears offset in opposite rotation convert part of the absorber disc 4 incoming energy into rotational energy. They have a freewheel and are during the return travel of the absorber disc by an eddy current brake, which in turn via the cooling line 12.3 be cooled, braked.

The drive unit according to the invention 1 and 2 is not limited to the illustrated embodiments.

Rather, other embodiments are conceivable that the impact energy in zb. transform an angular momentum through several rotors into internal energy of the whole system.

LIST OF REFERENCE NUMBERS

1

lossless electromechanical drive system

2

pressure chamber

3

rocket

4

Absorber plate with porous-permeable structure

5

Electrolysis unit

5.1

steam generator

6

Photovoltaic module with radiator on the back

6.1

Thermal solar collector also with backside radiator

6.2

Photovoltaic panel for powering the control and regulation units

6.3

Power line in the circuit of the drive system

7 and 8

 power line

8.1

Heat-pipe

9 and 10

Hydrogen and oxygen lines

11

Telescopic water pipe

12

Shock absorber with throttle check system (electrically adjustable)

 12.1

Rotational masses with eddy current brake

 12.2

throttle

12.3

Heat-pipe for unspecified cooling of the eddy current brakes

 13

double-sided rack

14

 Return spring

QUOTES INCLUDE IN THE DESCRIPTION

This list of the documents listed by the applicant has been generated automatically and is included solely for the better information of the reader. The list is not part of the German patent or utility model application. The DPMA assumes no liability for any errors or omissions.

Cited patent literature

• US 5543801 [0002]
• WO 2007089284 [0002]

Claims (8)

Mass loss electromechanical satellite drive, which is provided by a pressure chamber / nozzle unit impact energy for driving in a closed tube. The closed tube on the opposite side of the drive unit has an absorber unit which converts impact energy into internal energy of the overall system. The drive power is extracted from the explosion of hydrogen and oxygen, and the water is reused in an electrolysis unit. The drive power consists of heated water at high pressure which is obtained in a steam generator from solar thermal or nuclear decay energy. The drive system has solar panels for electrical and thermal energy. That the conversion of the impact energy into internal energy of the entire system is effected by a plurality of rotors The internal energy is derived from the overall system by heat-pipes. The absorber disc is movably attached to the shock absorber and telescopic tube.

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