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US5429083A Expired / Lapsed US ⏱️ 0.0 years remaining

Rotary internal combustion twin engine

Assignee: Individual
•
Filing: 1994-09-07
•
Granted: 1995-07-04
•
Expires: 2014-09-07
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Abstract

Abstract A rotary internal combustion twin engine includes matching pairs of multilobed interengaging compression rotors compressing gas and air mixtures into compression chambers defined by concavities of transfer rotors. With a 180 degree rotation of transfer rotors, compression chambers become combustion chambers containing intermittent ignition devices. Ignited and expanded gasses impel lobes of matching pairs of multilobed interengaging expansion rotors providing rotational energy and exhausting burned gasses.

Inventors

  • 👤 Robert W. Becker

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-28 23:23
CPC Classifications
F; F02; F02B; F02B53/00; F02B53/02; F02B2053/005; Y; Y02; Y02T; Y02T10/00; Y02T10/10; Y02T10/12

Claims Analysis

Total Claims: 8
Claim 1
Independent Claim 108 words
A rotary internal combustion engine comprising: a housing of intersecting circular chambers, matching pairs of multilobed interengaging compression rotors mounted on shafts supported in said housing, a circular gas and air transfer rotor with concavities diametrically located on the periphery of said rotor defining alternating rotating compression and combustion chambers mounted on a drive shaft supported in said housing, a recessed ignition device in said housing, matching pairs of multilobed interengaging expansion rotors mounted on shafts supported in said housing, and rotary transmission means mounted on said shafts to transfer rotational energy between said rotors and to provide desired compression, desired expansion and sufficient exhaust of burned gasses.
Claim 2
Dependent Claim 108 words
A rotary internal combustion engine comprising: a housing of intersecting circular chambers, matching pairs of multilobed interengaging compression rotors mounted on shafts supported in said housing, a circular gas and air transfer rotor with concavities diametrically located on the periphery of said rotor defining alternating rotating compression and combustion chambers mounted on a drive shaft supported in said housing, a recessed ignition device in said housing, matching pairs of multilobed interengaging expansion rotors mounted on shafts supported in said housing, and rotary transmission means mounted on said shafts to transfer rotational energy between said rotors and to provide desired compression, desired expansion and sufficient exhaust of burned gasses.
Claim 3
Dependent Claim 24 words
The rotary engine defined in claim 1, wherein said transfer rotor concavities extend along 90 degrees of said transfer rotor's periphery on opposite sides.
Claim 4
Dependent Claim 33 words
The rotary engine defined in claim 1, wherein compression chamber opening to said transfer rotor is equal in length and width with respect to opening of adjacent transfer rotor concavity when aligned horizontally.
Claim 5
Dependent Claim 33 words
The rotary engine defined in claim 1, wherein combustion chamber opening to said transfer rotor is equal in length and width with respect to opening of adjacent transfer rotor concavity when aligned horizontally.
Claim 6
Dependent Claim 22 words
The rotary engine defined in claim 1, wherein said transmission means comprise gears changeable in diametric sizes to provide desired compression ratio.
Claim 7
Dependent Claim 22 words
The rotary engine defined in claim 1, wherein said transmission means comprise gears changeable in diametric sizes to provide desired expansion rate.
Claim 8
Dependent Claim 49 words
The rotary engine defined in claim 1, further including an identical twin engine comprising an identical housing, chambers, ignition device and rotors mounted on said rotor shafts extended through said transmission means, with said identical transfer rotor positioned on its axis 90 degrees from the first said transfer rotor.

References Cited (Backward Citations)

DE103086C Cited
US1046280A Cited
US1856011A Cited
US4825827A Cited
US4909208A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1998-07-03 1999-01-02 1999-07-04 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 2002-07-03 2003-01-02 2003-07-04 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 2006-07-03 2007-01-02 2007-07-04 $7700.00 Window Closed / Lapsed

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