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US3779216A Expired / Lapsed US ⏱️ 0.0 years remaining

Variable explosion-displacement rotary engine

Assignee: Individual
•
Filing: 1972-06-05
•
Granted: 1973-12-18
•
Expires: 1992-06-05
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Abstract

Abstract A variable explosion-displacement rotary engine, free of a fuel compression cycle, and specifically designed for use with pollution free fuels of the alkyne type; and others, having a cylindrical rotor revolving in an elliptical opening of a housing to define two annular spaces on two sides therebetween. The rotor having radial members which project to follow without sealing the contour of the elliptical opening to form volume expanding combustion areas behind said members. High speed tungsten poppet valves mounted in the fuel input ports which extend into the combustion areas open and close via differential in pressures to admit fuel periodically between explosions, the engine providing four explosions in one shaft revolution. Ignition timing cooperating with the position of said members and the volume of fuel displaced controls the explosive force, the explosion displacement, engine torque and shaft revolutions per minute. The volume of fuel exploded is in direct proportion to the amount of horsepower required at any moment with the fuel-air mixture precisely fixed for complete combustion and pollution free exhaust.

Inventors

  • 👤 R Britt

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-23 12:00
CPC Classifications
F; F01; F01C; F01C1/00; F01C1/30; F01C1/34; F01C1/344; F01C1/3446; F02; F02B; F02B53/00; F02B2730/00; F02B2730/01; F02B2730/012; Y; Y02; Y02T; Y02T10/00; Y02T10/10; Y02T10/12

Claims Analysis

Total Claims: 12
Claim 1
Independent Claim 244 words
A rotary engine comprising: a housing having an open space therein defined by an at least partially elliptical wall; a rotatable cylindrical rotor axially disposed within said space defining at least one substantially crescent shaped chamber; a radially movable blade means carried by said turbine rotor extending into contact with said wall for creating a low pressure in said crescent shaped chamber behind said blade means as said rotor is rotated in one direction; a source of combustible fixed fuel mixture; fuel intake means communicating with said source and with said crescent shaped chamber for introducing fuel inTo said crescent shaped chamber behind said blade means; exhaust means communicating with said crescent shaped chamber at a point spaced angularly from said intake means in the direction of rotation of said rotor; fuel ignition means positioned in communication with said crescent shaped chamber adjacent said intake means for burning the fuel therein creating a high pressure in said crescent shaped chamber; a valve carried by said fuel intake means for opening said fuel intake means responsive to a reduction in pressure in said crescent shaped chamber behind said blade means and closing said fuel intake means responsive to said high pressure in said crescent shaped chamber behind said blade means; and adjustable means for actuating said ignition means at selected positions of said blade in said crescent shaped chamber; whereby controlled volumes of a fixed fuel mixture may be ignited to meet varying power requirements.
Claim 2
Dependent Claim 244 words
A rotary engine comprising: a housing having an open space therein defined by an at least partially elliptical wall; a rotatable cylindrical rotor axially disposed within said space defining at least one substantially crescent shaped chamber; a radially movable blade means carried by said turbine rotor extending into contact with said wall for creating a low pressure in said crescent shaped chamber behind said blade means as said rotor is rotated in one direction; a source of combustible fixed fuel mixture; fuel intake means communicating with said source and with said crescent shaped chamber for introducing fuel inTo said crescent shaped chamber behind said blade means; exhaust means communicating with said crescent shaped chamber at a point spaced angularly from said intake means in the direction of rotation of said rotor; fuel ignition means positioned in communication with said crescent shaped chamber adjacent said intake means for burning the fuel therein creating a high pressure in said crescent shaped chamber; a valve carried by said fuel intake means for opening said fuel intake means responsive to a reduction in pressure in said crescent shaped chamber behind said blade means and closing said fuel intake means responsive to said high pressure in said crescent shaped chamber behind said blade means; and adjustable means for actuating said ignition means at selected positions of said blade in said crescent shaped chamber; whereby controlled volumes of a fixed fuel mixture may be ignited to meet varying power requirements.
Claim 3
Dependent Claim 43 words
The structure set forth in claim 1 including: a by-pass valve means effective at least during an initial portion of movement of the blade means through said crescent shaped chamber for reducing and thereby controlling said high pressure created behind said blade means.
Claim 4
Dependent Claim 35 words
The structure set forth in claim 2 wherein a pair of opposed crescent shaped chambers are defined in said housing, each such chamber having fuel intake means, exhaust means, a valve and fuel ignition means.
Claim 5
Dependent Claim 102 words
The structure set forth in claim 3 wherein said radially movable blade means includes: a plurality of stacked laminar blades having passageways spaced in staggered relationship in the outer edge of said blade from one blade to another forming said by-pass valve means; whereby a by-pass of diminishing proportions is created as said blade means moves through said crescent shaped chamber from a position near the minor axis of the elliptical wall toward the greater axis of the wall responsive to relative movement of the laminar blades with respect to each other as a result of their contact with the elliptical wall.
Claim 6
Dependent Claim 22 words
The structure set forth in claim 4 wherein said valve is poppet valve normally spring biased to close said fuel intake means.
Claim 7
Dependent Claim 186 words
A rotary engine comprising: a housing having an open space therein defined by an at least partially elliptical wall; a rotatable cylindrical rotor axially disposed within said space and defining at least one substantially crescent shaped chamber; a radially movable blade means carried by said rotor extending into contact with said wall for creating a low pressure in said crescent shaped chamber behind said blade means as said rotor is rotated in one direction; a source of a combustible fuel; fuel intake means communicating with said source and with said crescent shaped chamber for introducing fuel into said crescent shaped chamber behind said blade means; exhaust means communicating with said crescent shaped means chamber ahead of said blade means; fuel ignition means positioned in said crescent shaped chamber behind said blade means for burning the fuel therein creating a high pressure in said crescent shaped chamber behind said blade means; and a by-pass valve means effective at least during an initial portion of movement of the blade means through said crscent shaped chamber for reducing and thereby controlling said high pressure created behind said blade means.
Claim 8
Dependent Claim 186 words
A rotary engine comprising: a housing having an open space therein defined by an at least partially elliptical wall; a rotatable cylindrical rotor axially disposed within said space and defining at least one substantially crescent shaped chamber; a radially movable blade means carried by said rotor extending into contact with said wall for creating a low pressure in said crescent shaped chamber behind said blade means as said rotor is rotated in one direction; a source of a combustible fuel; fuel intake means communicating with said source and with said crescent shaped chamber for introducing fuel into said crescent shaped chamber behind said blade means; exhaust means communicating with said crescent shaped means chamber ahead of said blade means; fuel ignition means positioned in said crescent shaped chamber behind said blade means for burning the fuel therein creating a high pressure in said crescent shaped chamber behind said blade means; and a by-pass valve means effective at least during an initial portion of movement of the blade means through said crscent shaped chamber for reducing and thereby controlling said high pressure created behind said blade means.
Claim 9
Dependent Claim 94 words
The structure set forth in claim 6 wherein said radially movable blade means includes: a plurality of stacked laminar blades having spaced passageways in staggered relationship from one blade to another forming said by-pass valve means; said by-pass valve means having an opening of diminishing proportions as said blade means moves through an initial portion of said crescent shaped chamber responsive to movement of the blades with respect to each other as a result of their contact with the elliptical wall; and a poppet valve normally spring biases to close said fuel intake meanS.
Claim 10
Dependent Claim 187 words
In a rotary engine having a housing with an open space therein defined by an at least partially elliptical wall, a rotatable cylindrical rotor axially disposed within and space defining at least one substantially crescent shaped chamber; and a radially movable blade means carried by said rotor extending into contact with said wall for creating a low pressure in said crescent shaped chamber behind said blade means as said rotor is rotated in one direction; a source of a fixed fuel mixture; fuel intake means communicating with said source and with said crescent shaped chamber for introducing fuel into said crescent shaped chamber behind said blade means; exhaust means communicating with said crescent shaped means chamber ahead of said blade means; fuel ignition means positioned in said crescent shaped chamber behind said blade means for burning the fuel therein creating a high pressure in said crescent shaped chamber behind said blade means; and adjustable means for actuating said ignition means at selected positions of said blade in said crescent shaped chamber; whereby controlled volumes of a fixed fuel mixture may be ignited to meet varying power requirements.
Claim 11
Dependent Claim 187 words
In a rotary engine having a housing with an open space therein defined by an at least partially elliptical wall, a rotatable cylindrical rotor axially disposed within and space defining at least one substantially crescent shaped chamber; and a radially movable blade means carried by said rotor extending into contact with said wall for creating a low pressure in said crescent shaped chamber behind said blade means as said rotor is rotated in one direction; a source of a fixed fuel mixture; fuel intake means communicating with said source and with said crescent shaped chamber for introducing fuel into said crescent shaped chamber behind said blade means; exhaust means communicating with said crescent shaped means chamber ahead of said blade means; fuel ignition means positioned in said crescent shaped chamber behind said blade means for burning the fuel therein creating a high pressure in said crescent shaped chamber behind said blade means; and adjustable means for actuating said ignition means at selected positions of said blade in said crescent shaped chamber; whereby controlled volumes of a fixed fuel mixture may be ignited to meet varying power requirements.
Claim 12
Dependent Claim 56 words
The structure set forth in claim 8, including: a poppet valve carried adjacent said fuel intake means opening said fuel intake means responsive to said low pressure in said crescent shaped chamber behind said blade means and closing said fuel intake means responsive to said high pressure in said crescent shaped chamber behind said blade means.

References Cited (Backward Citations)

US1090021A Cited
US1167386A Cited
US2231440A Cited
US2224443A Cited
US2283433A Cited
US2547560A Cited
FR1361236A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1976-12-17 1977-06-18 1977-12-18 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1980-12-17 1981-06-18 1981-12-18 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1984-12-17 1985-06-18 1985-12-18 $7700.00 Window Closed / Lapsed

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