Fluid mixer
AssigneeThe United States of America as represented by the Secretary of the Air Force
InventorDavid E. Barland
Life of this patent
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Abstract
A multi-entry fluid mixer is provided, e.g. for mixing and injecting liquid rocket propellants, which mixer has a first set of passages for receiving fluid A and a second set of passages for receiving fluid B, the passages being separated by porous walls for mixing of fluids A and B therethrough as the fluids flow through such passages and then through a porous end wall, for further mixing and then discharge, as in, say, fuel injection into the combustion chamber of a rocket. The inventive mixer can also be employed in filtrated mixing of gases or gas/liquid combinations as well as for liquid rocket propellant injection, jet engine propellant injection, chemical mixing, aerosol formation and numerous other mixing and dispersion operations.
Claims10
A fluid mixer comprising:
- a) an porous core having,
- a first set of passages for fluid A and a second set of passages for fluid B, at least some of said passages terminating in a porous endwall, said passages being separated by porous walls for mixing of fluids A and B therethrough as said fluids flow through said passages and through said porous end wall to discharge from said core and
- b) a casing with inlet and outlet ports enclosing said core.
Dependencies are inferred from the claim text.