Oxyhydrogen pulse and rotary detonation combustion pump
A pump capable of producing both positive pressure and a vacuum. The pump utilizes a combustion chamber and various valve assemblies. The pump operates via a process of internal gas combustion combined with the movement of fluid within a combustion chamber and various valve assemblies. The combustion of gas and fluid movement creates a force that is harnessed to generate vacuum or pressure from the combustion process.
1. A process for generating a pumping force comprising:
introducing a volume of a fluid into a vessel defining a volume, the vessel having at least one fluid inlet and one fluid outlet, wherein the fluid includes at least water and is at least unreactive to hydrogen and oxygen;
introducing and igniting a detonation gas comprising an approximately stoichiometric mixture of hydrogen and oxygen within the vessel to induce a detonation of the detonation mixture, wherein the detonation produces a superheated steam and a hypersonic shockwave within the vessel, and wherein the superheated steam expands producing a pressure wave within the pressure vessel;
expelling via the pressure wave and hypersonic shockwave substantially all of the fluid from the vessel through the at least one fluid outlet such that only the superheated steam remains in the vessel after the expulsion;
condensing the superheated steam such that a vacuum state is created within the vessel; and
repeating the introducing, igniting, expelling, and condensing steps such that an oscillating pressure is created within the vessel whereby a system pressure within the vessel increases during the igniting step to a high pressure state greater than atmospheric pressure and asymptotically decreases during the expelling and condensing steps to a vacuum state wherein the pressure within the vessel is lower than atmospheric pressure such that by the oscillation between high pressure and vacuum states the pumping force is produced.
2. The process of claim 1 , wherein at least a portion of the water undergoes thermolysis to produce additional detonation mixture.
3. The process of claim 1 , wherein the pumping force generated by the vacuum state within the vessel introduces the fluid into the vessel from a source.
4. The process of claim 1 , wherein the fluid includes acids or bases.
5. The process of claim 1 , wherein the mixture has a 2 to 1 ratio of hydrogen to oxygen.
6. The process of claim 1 , wherein the pumping force is configured to act as a vacuum pump to lower pressure in an external volume.
7. The process of claim 1 , wherein the pumping force is configured to act as a pressurizing pump to increase pressure in an external volume.
8. The process of claim 1 , wherein the pumping force is configured to act as a fluid transfer pump to move the fluid between first and second external volumes.
9. The process of claim 1 , wherein the process is distributed across a plurality of vessels.
10. The process of claim 1 , wherein the introduction of the fluid pressurizes the detonation mixture prior to ignition and detonation.
11. The process of claim 10 , wherein the expelled steam has at least a supersonic velocity; and
further comprising, directing the expelled steam at a source of molten metal such that the molten metal is atomized to a plurality of metal particles.
12. The process of claim 11 , further comprising applying a magnetic field to the atomized plurality of metal particles.
13. The process of claim 1 , wherein the fluid includes gaseous water.
14. The process of claim 1 , wherein the hypersonic shockwave has a speed of up to Mach 4.5 and a temperature of up to 2800° C.
15. The process of claim 1 , wherein the superheated steam expands in volume up to 2000 times the original volume of the detonation gas.
16. The process of claim 1 , wherein the pressure vessel forms a portion of a rotary detonation pump such that a continuous thrust vector can be induced from the pump force.
17. The process of claim 1 , wherein the fluid ejected from the pump is selected from the group of steam, water, hydrogen and oxygen.
18. The process of claim 1 , further comprising, prior to the introducing the fluid into the vessel, priming the vessel, the priming comprising:
introducing a detonation gas comprising an approximately stoichiometric mixture of hydrogen and oxygen into the vessel;
igniting the detonation gas to induce a detonation of the detonation gas, wherein the detonation produces a superheated steam and a hypersonic shockwave within the vessel, and wherein the superheated steam expands producing a pressure wave within the pressure vessel;
expelling via the pressure wave and hypersonic shockwave substantially all of a gaseous atmosphere from the vessel through the at least one fluid outlet such that only the superheated steam remains in the vessel after the expulsion; and
condensing the superheated steam such that a vacuum state is created within the vessel.
19. A process of generating vacuum comprising:
receiving a determined amount of a detonation gas comprising an approximately stoichiometric mixture of hydrogen and oxygen into a chamber; and
igniting the detonation gas producing a detonation in the chamber, such that at least superheated steam and a hypersonic shockwave are produced, thereby generating an increasing pressure wave within the chamber expelling any fluid within the chamber out of an exit valve such that only the superheated steam remains in the chamber after the expulsion; and
condensing the superheated steam such that the pressure inside the chamber asymptotically decreases below the pressure outside the chamber thereby creating a vacuum within the chamber.
20. A process of pumping fluids comprising:
providing a pump wherein the pump comprises a chamber having an exterior portion and an interior portion wherein the interior portion forms an internal space,
at least one fluid inlet assembly in fluid communication with the interior portion of the chamber having a portion thereof connected to the exterior portion of the chamber;
a gas inlet assembly in fluid communication with the interior portion of the chamber and connected to the exterior portion and configured to transfer a detonation gas comprising an approximately stoichiometric mixture of hydrogen and oxygen into the internal portion of the chamber;
an ignitor assembly connected to the exterior portion of the chamber and wherein a section of the ignitor assembly is exposed to the interior portion of the chamber and wherein the ignitor assembly contains an ignitor;
receiving a fluid into the chamber through the fluid inlet assembly;
receiving the detonation gas into the chamber through the gas inlet assembly;
igniting the detonation gas by activation of the ignitor thereby producing a detonation of the detonation gas such that at least superheated steam and a hypersonic shockwave are produced, thereby generating an increasing pressure wave within the chamber thereby expelling the fluid out of the chamber through an outlet valve connected to a portion of the chamber such that only the superheated steam remains in the chamber after the expulsion; and
condensing the superheated steam, wherein the detonation of the detonation gas, expulsion of the fluid, and condensation of the superheated steam within the chamber asymptotically decreases the pressure generating a vacuum within the chamber thereby impelling additional fluid into the chamber through the at least one fluid inlet assembly.