Gas-to-hydraulic power converter
AssigneeThe United States of America as represented by the Administrator of the National Aeronautics and Space Administration
InventorCharles W. Galloway
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AssigneeThe United States of America as represented by the Administrator of the National Aeronautics and Space Administration
InventorCharles W. Galloway
Estimating the term…
A gas piston driven hydraulic piston pump in which the gas cycle is of high efficiency by injecting the gas in slugs at the beginning of each power stroke. The hydraulic piston (40) is disposed to operate inside the gas piston (30), and the two pistons, both slidably but non-rotatably mounted, are coupled together with a rotating but non-sliding motion transfer ring (50) extending into antifriction grooves (46 and 37) in the sidewalls (42 and 32) of the two pistons. To make the hydraulic piston move at a constant speed during constant hydraulic horsepower demand and thus exert a constant pressure on the hydraulic fluid, these grooves are machined with variable pitches and one is the opposite of the other, i.e., the gas piston groove (37) increases in pitch during its power stroke while the hydraulic piston groove (46) decreases. Thus the motion transfer ring (50) is properly denominated a force multiplier ring. Any number of piston assembly sets may be used to obtain desired hydraulic horsepower.
A gas-to-hydraulic power converter comprising:
A gas-to-hydraulic power converter comprising an outer piston and cylinder assembly, an inner piston and cylinder assembly disposed within and coaxial with said outer assembly, and a motion transfer ring rotatably but not translatably mounted between the two assemblies and having opposed antifriction bearing surface portions engaging helical grooves in the sidewalls of the two pistons, in the inner surface of the outer portion and in the outer surface of the inner piston, each of such grooves varying in pitch from one end to the other, said outer assembly having opposed gas closure and hydraulic closure ends and the pitch of its helical groove decreasing from a maximum at its end nearer to said gas closure end to a minimum pitch at the other end of such groove while the pitch of the helical groove of the inner piston increases between its corresponding ends, each of said pistons being mounted within its cylinder to be translatable but not rotatable with respect thereto.
Dependencies are inferred from the claim text.