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US3908517A Expired / Lapsed US ⏱️ 0.0 years remaining

Hydrostatic engine control

Assignee: Twin Disc Inc
•
Filing: 1973-05-11
•
Granted: 1975-09-30
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Expires: 1993-05-11
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Abstract

Abstract A multipiston hydrostatic engine of the radial cylinder type is equipped with a variable throw crankshaft. The radial piston thrusts of the engine act upon a cam ring which is rotatably centered on a radially in and out shiftable slideblock on the crankpin of the crankshaft. An oblong aperture of the slideblock extends radially of the crankpin and provides a space to which pressure fluid is admitted selectively at one side or the other of the crankpin so as to shift the slideblock in or out and thereby increase or decrease the radial spacing of the cam ring center from the journal axis of the crankshaft.

Inventors

  • 👤 Alan E G Wenbourne

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-01 16:11
CPC Classifications
F; F04; F04B; F04B1/00; F04B1/04; F04B1/053; F04B49/00; F04B49/12; F04B49/123; F04B49/125; F04B1/06; F04B1/07

Claims Analysis

Total Claims: 2
Claim 1
Independent Claim 282 words
In a multipiston hydrostatic engine of the radial cylinder type the combination of a crank case, a crank shaft rotatably mounted in said crank case and having a pair of axially spaced radial flanges therein and a crankpin extending axially between said flanges, said crank pin having a pair of plane side surfaces at opposite sides of and in parallel relation to a radial plan through the journal axis of said crankshaft, and diametrically opposite arcuately convex surfaces extending axially between said flanges and transversely between said plane side surfaces; an annular slide block surrounding said crank pin in radially back and forth shiftable relation thereto, said slide block having a pair of parallel diametrically opposite plane internal surfaces in contacting relation with said plane parallel side surfaces of said crank pin, axially opposite radial end faces in contacting relation, respectively, with adjacent radial surfaces of said flanges and radially opposite arcuately concave internal surfaces extending axially between said end faces and circumferentially between said parallel internal surfaces whereby a pair of radially expandable and contractable fluid chambers are provided at diametrically opposite sides of said crank pin between the latter and said slide block; annular sealing means operatively interposed between each of said axially opposite radial end faces of said slide block and the adjacent radial surfaces of said flanges; and linear sealing means extending axially of said crank pin and operatively interposed between each of said side surfaces of the latter and the adjacent plane internal surface of said slide block, said crankshaft being provided with internal fluid passages communicating, respectively, with said fluid chambers; and thrust transmitting means operatively interposed between radially reciprocable engine pistons and said slide block.
Claim 2
Dependent Claim 282 words
In a multipiston hydrostatic engine of the radial cylinder type the combination of a crank case, a crank shaft rotatably mounted in said crank case and having a pair of axially spaced radial flanges therein and a crankpin extending axially between said flanges, said crank pin having a pair of plane side surfaces at opposite sides of and in parallel relation to a radial plan through the journal axis of said crankshaft, and diametrically opposite arcuately convex surfaces extending axially between said flanges and transversely between said plane side surfaces; an annular slide block surrounding said crank pin in radially back and forth shiftable relation thereto, said slide block having a pair of parallel diametrically opposite plane internal surfaces in contacting relation with said plane parallel side surfaces of said crank pin, axially opposite radial end faces in contacting relation, respectively, with adjacent radial surfaces of said flanges and radially opposite arcuately concave internal surfaces extending axially between said end faces and circumferentially between said parallel internal surfaces whereby a pair of radially expandable and contractable fluid chambers are provided at diametrically opposite sides of said crank pin between the latter and said slide block; annular sealing means operatively interposed between each of said axially opposite radial end faces of said slide block and the adjacent radial surfaces of said flanges; and linear sealing means extending axially of said crank pin and operatively interposed between each of said side surfaces of the latter and the adjacent plane internal surface of said slide block, said crankshaft being provided with internal fluid passages communicating, respectively, with said fluid chambers; and thrust transmitting means operatively interposed between radially reciprocable engine pistons and said slide block.

References Cited (Backward Citations)

US1453417A Cited
US2013468A Cited
US2404175A Cited
US2345125A Cited
US2356993A Cited
US3255707A Cited
US3828400A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1978-09-29 1979-03-31 1979-09-30 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1982-09-29 1983-03-31 1983-09-30 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1986-09-29 1987-03-31 1987-09-30 $7700.00 Window Closed / Lapsed

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