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US3298331A Expired / Lapsed US ⏱️ 0.0 years remaining

Rotary heat engine

Assignee: Individual
•
Filing: 1965-04-15
•
Granted: 1967-01-17
•
Expires: 1985-04-15
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Abstract

No abstract record available.

Inventors

  • 👤 James L Butler

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-02 11:04
CPC Classifications
F; F02; F02B; F02B53/00; F02B2730/00; F02B2730/01; Y; Y02; Y02T; Y02T10/00; Y02T10/10; Y02T10/12

Claims Analysis

Total Claims: 2
Claim 1
Independent Claim 238 words
IN A ROTARY ENGINE, A COMPRESSOR UNIT AND A POWER UNIT COUPLED TOGETHER FOR SIMULTANEOUS ROTATION IN THE SAME DIRECTION ABOUT A COMMON AXIS, EACH UNIT COMPRISING AN OUTER ROTOR HAVING A CYLINDRICAL CHAMBER AND A CYLINDRICAL INNER ROTOR OF LESS DIAMETER THAN THE CHAMBER AND TANGENTIALLY ENGAGING THE INNER CYLINDRICAL WALL OF SUCH CHAMBER CONSTANTLY, EACH UNIT HAVING A RADIAL BLADE COUPLING THE OUTER AND INNER ROTORS OF EACH UNIT TO CAUSE THE ROTORS OF EACH UNIT TO ROTATE IN UNISON, THE OUTER ROTOR OF EACH UNIT HAVING A SOCKET MOVABLY HOLDING THE BLADE, AND THE INNER ROTOR OF EACH UNIT HAVING A RADIAL SLOT TO RECEIVE MOVABLY A PORTION OF SUCH BLADE, THE BLADE OF THE COMPRESSOR UNIT EXTENDING ACROSS THE SPACE BETWEEN THE INNER AND OUTER ROTORS OF SUCH COMPRESSOR UNIT TO DIVIDE SUCH SPACE INTO INTAKE AND COMPRESSION CHAMBERS, THE BLADE OF THE POWER UNIT EXTENDING ACROSS THE SPACE BETWEEN THE INNER AND OUTER ROTORS OF SUCH POWER UNIT TO DIVIDE SUCH SPACE INTO EXPANSION AND EXHAUST CHAMBERS, A HOLLOW DRIVE SHAFT KEYED TO THE INNER ROTORS OF THE COMPRESSOR AND POWER UNITS AND ARRANGED ECCENTRICALLY TO THE COMMON AXIS OF THE COMPRESSOR AND POWER UNITS, A FUEL INDUCTION TUBE EXTENDING LOOSELY INSIDE THE SHAFT AND HAVING SEPARATED INLET AND OUTLET CHAMBERS, MEANS TO CONVEY A FUEL MIXTURE FROM THE INLET CHAMBER OF THE FUEL INDUCTION TUBE TO THE INTAKE CHAMBER OF THE COMPRESSOR
Claim 2
Dependent Claim 238 words
IN A ROTARY ENGINE, A COMPRESSOR UNIT AND A POWER UNIT COUPLED TOGETHER FOR SIMULTANEOUS ROTATION IN THE SAME DIRECTION ABOUT A COMMON AXIS, EACH UNIT COMPRISING AN OUTER ROTOR HAVING A CYLINDRICAL CHAMBER AND A CYLINDRICAL INNER ROTOR OF LESS DIAMETER THAN THE CHAMBER AND TANGENTIALLY ENGAGING THE INNER CYLINDRICAL WALL OF SUCH CHAMBER CONSTANTLY, EACH UNIT HAVING A RADIAL BLADE COUPLING THE OUTER AND INNER ROTORS OF EACH UNIT TO CAUSE THE ROTORS OF EACH UNIT TO ROTATE IN UNISON, THE OUTER ROTOR OF EACH UNIT HAVING A SOCKET MOVABLY HOLDING THE BLADE, AND THE INNER ROTOR OF EACH UNIT HAVING A RADIAL SLOT TO RECEIVE MOVABLY A PORTION OF SUCH BLADE, THE BLADE OF THE COMPRESSOR UNIT EXTENDING ACROSS THE SPACE BETWEEN THE INNER AND OUTER ROTORS OF SUCH COMPRESSOR UNIT TO DIVIDE SUCH SPACE INTO INTAKE AND COMPRESSION CHAMBERS, THE BLADE OF THE POWER UNIT EXTENDING ACROSS THE SPACE BETWEEN THE INNER AND OUTER ROTORS OF SUCH POWER UNIT TO DIVIDE SUCH SPACE INTO EXPANSION AND EXHAUST CHAMBERS, A HOLLOW DRIVE SHAFT KEYED TO THE INNER ROTORS OF THE COMPRESSOR AND POWER UNITS AND ARRANGED ECCENTRICALLY TO THE COMMON AXIS OF THE COMPRESSOR AND POWER UNITS, A FUEL INDUCTION TUBE EXTENDING LOOSELY INSIDE THE SHAFT AND HAVING SEPARATED INLET AND OUTLET CHAMBERS, MEANS TO CONVEY A FUEL MIXTURE FROM THE INLET CHAMBER OF THE FUEL INDUCTION TUBE TO THE INTAKE CHAMBER OF THE COMPRESSOR

References Cited (Backward Citations)

US791428A Cited
US969957A Cited
US1210042A Cited
US1410099A Cited
US1828245A Cited
AU924232A Cited
US2075561A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1970-01-16 1970-07-18 1971-01-17 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1974-01-16 1974-07-18 1975-01-17 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1978-01-16 1978-07-18 1979-01-17 $7700.00 Window Closed / Lapsed

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