Compound combustion engines and methods of compounding same

Claim 2

A two rotor internal-combustion compound rotary engine comprising, in combination: a) a primary engine section and a secondary engine section operatively connected by an eccentric shaft as the power shaft common to both said sections, the primary section serving as the prime mover in the manner of a conventional single-rotor rotary engine operating according to the known four-event work cycle; b) a three-flanked rotor connected to said power shaft and rotatably contained in each said section for effecting work-cycle events; c) a two-lobed housing cavity contained in each said engine section serve as the operating chamber for the respective rotor during rotation thereof; d) an ignition system connected only to the primary section for ignition of rich fuel/air charges therein; e) means for supplying fuel and primary air only to the primary section; f) a recess in each of the three flanks of the primary rotor, each recess forming part of a moving combustion chamber; g) a secondary rotor with non-recessed flanks for substantially preventing transfer of gases between the lobes of the secondary rotor's two-lobed housing cavity; h) a short conduit for connecting and thereby compounding adjacent primary and secondary sections for transferring working medium exhausted by the primary section to the secondary section; i) eccentric shaft rotor journals oppositely positioned by a separation angle of 180° for rotors to be mounted thereon so as to be oppositely-phased in their operation; j) secondary rotor housing provided with an air intake port and an air outlet port disposed oppositely and peripherally in one lobe of said two-lobed housing cavity, said intake port connected to a conventional air-filter system and said outlet port connected to said conduit whereby the secondary engine section's rotor is enabled to induct supplemental secondary air through said air-filter system during each intake event in said one lobe and cause ejection of said air directly into said conduit and working medium during each compression event in said one lobe to support the burning of leftover combustibles in said medium; and said k) secondary rotor housing also provided with a peripheral inlet port in the other lobe of said cavity and connected to said conduit for admitting therefrom the air-treated said working medium during each expansion event in said other lobe; said housing additionally provided with a peripheral exhaust port disposed in the opposite side of said other lobe for release of the spent medium during successive exhaust events into an exhaust system connected to said exhaust port.

Claim 3

A four-rotor internal-combustion compound rotary engine comprising, in combination: a) primary engine sections and secondary engine sections operatively connected by an eccentric shaft as the power shaft common to all said sections, each primary section serving as a prime mover in the manner of a conventional single-rotor rotary engine operating according to the known four-event work cycle; b) a three-flanked rotor connected to said power shaft and rotatably contained in each said section for effecting work-cycle events; c) a two-lobed housing cavity contained in each said engine section to serve as the operating chamber for the respective rotor during rotation thereof; d) an ignition system connected only to each primary section for ignition of rich fuel/air charges therein; e) means for suppying fuel and primary air only to the primary sections; f) a recess in each of the three flanks of each primary rotor, each recess forming part of a moving combustion chamber; g) each secondary rotor with non-recessed flanks for substantially preventing transfer of gases between the lobes of the respective secondary rotor's two-lobed housing cavity; h) two short conduits each for connecting and thereby compounding one primary section and one adjacent secondary section to form one compound engine unit, and for transferring working medium exhausted by the primary section to the secondary section in the same unit; i) eccentric shaft rotor journals positioned radially around the axis of said eccentric shaft at 90° separation angles for the different rotors to be mounted alternately thereon whereby like rotors are oppositely phased in their operation; j) each secondary rotor housing provided with an air intake port and an air outlet port disposed oppositely and peripherally in one lobe of the respective said two-lobed housing cavity, said intake ports connected to a conventional air-filter system and each said outlet port connected to the respective said conduit whereby each secondary section's rotor is enabled to induct supplemental secondary air through said air-filter system during each intake event in the respective said one lobe, and cause ejection of said air directly into the respective said conduit and working medium during each successive compression event in that same lobe to support the burning of leftover combustibles in said medium; and k) each secondary rotor housing also provided with a peripheral inlet port in the other lobe of the respective said two-lobed cavity and connected to the respective conduit for admitting therefrom the air-treated working medium during each expansion event in the respective said other lobe; each said secondary housing additionally provided with a peripheral exhaust port disposed in the opposite side of the respective said other lobe for release of the spent medium during successive exhaust events into an exhaust system connected to said exhaust ports.

Claim 4

A four-rotor internal-combustion compound rotary engine comprising, in combination: a) primary engine sections and secondary engine sections operatively connected by an eccentric shaft as the power shaft common to all said sections, each primary section serving as a prime mover in the manner of a conventional single-rotor rotary engine operating according to the known four-event work cycle; b) a three-flanked rotor connected to said power shaft and rotatably contained in each said section for effecting work-cycle events; c) a two-lobed housing cavity contained in each said engine section to serve as the operating chamber for the respective rotor during rotation thereof; d) an ignition system connected only to each primary section for ignition of rich fuel/air charges therein; e) means for suppying fuel and primary air only to the primary sections; f) a recess in each of the three flanks of each primary rotor, each recess forming part of a moving combustion chamber; g) each secondary rotor with non-recessed flanks for substantially preventing transfer of gases between the lobes of the respective secondary rotor's two-lobed housing cavity; h) two short conduits each for connecting and thereby compounding one primary section and one adjacent secondary section to form one compound engine unit, and for transferring working medium exhausted by the primary section to the secondary section in the same unit; i) eccentric shaft rotor journals positioned radially around the axis of said eccentric shaft at 90° separation angles for the different rotors to be mounted alternately thereon whereby like rotors are oppositely phased in their operation; j) each secondary rotor housing provided with an air intake port and an air outlet port disposed oppositely and peripherally in one lobe of the respective said two-lobed housing cavity, said intake ports connected to a conventional air-filter system and each said outlet port connected to the respective said conduit whereby each secondary section's rotor is enabled to induct supplemental secondary air through said air-filter system during each intake event in the respective said one lobe, and cause ejection of said air directly into the respective said conduit and working medium during each successive compression event in that same lobe to support the burning of leftover combustibles in said medium; and k) each secondary rotor housing also provided with a peripheral inlet port in the other lobe of the respective said two-lobed cavity and connected to the respective conduit for admitting therefrom the air-treated working medium during each expansion event in the respective said other lobe; each said secondary housing additionally provided with a peripheral exhaust port disposed in the opposite side of the respective said other lobe for release of the spent medium during successive exhaust events into an exhaust system connected to said exhaust ports.

Claim 5

An internal combustion compound rotary engine containing at least two rotors and comprising, in combination: a) primary engine sections and secondary engine sections arranged side-by-side in pairs of unlike sections and operatively connected by an eccentric shaft serving as the power shaft common to all said sections, each primary section serving as a prime mover in the manner of a conventional single-rotor rotary engine operating according to the known four-event work cycle; b) a three-flanked rotor connected to said power shaft and rotatably contained in each said section for effecting work-cycle events; c) a two-lobed housing cavity contained in each said engine section to serve as the operating chamber for the respective rotor during rotation thereof; d) means for supplying primary air and fuel only to the primary sections, and in quantities effecting ignitable fuel-rich mixtures therein; e) ignition means for igniting said mixtures in said primary sections; f) each primary rotor having conventional design with a conventional recess in each flank, said recess forming part of a moving combustion chamber as that rotor rotates; g) each secondary rotor differing from primary rotors only by having non-recessed flanks which coactively participate with the peripheral surface of the respective said cavity in substantially preventing transfer of gases between the lobes of that cavity; h) short gas-transfer conduits each separately connecting and thereby compounding one primary section and one adjacent secondary section to form one compound engine unit thereof, each conduit serving as a passageway for direct transfer or working medium held at high temperature and pressure as it is exhausted by the primary section to the secondary section in the same unit; i) eccentrics of said eccentric shaft serving as rotor journals arranged for rotors to be rotatably mounted thereon and effect, during their rotation, equal spacing of the respectiive expansion events of the said four-event work cycle; j) each secondary rotor housing provided with an air intake port and an air outlet port disposed oppositely and peripherally in one lobe of the respective said two-lobed housing cavity, said intake ports connected to a conventional air-filter system and each said outlet port connected to the respective said conduit whereby each secondary section's rotor is enabled to induct supplemental secondary air through said air-filter system during each intake event in the respective said one lobe, and cause ejection of said air directly into the respective said conduit and working medium during each successive compression event in that same lobe to support the burning of leftover combustibles in said medium; and k) each secondary rotor housing also provided with a peripheral inlet port in the other lobe of the respective said two-lobed cavity and connected to the respective conduit for admitting therefrom the air-treated working medium during each expansion event in the respective said other lobe; each said secondary housing additionally provided with a peripheral exhaust port disposed in the opposite side of the respective said other lobe for release of the spent medium during successive exhaust events into an exhaust system connected to said exhaust ports.

Claim 6

An internal combustion compound rotary engine containing at least two rotors and comprising, in combination: a) primary engine sections and secondary engine sections arranged side-by-side in pairs of unlike sections and operatively connected by an eccentric shaft serving as the power shaft common to all said sections, each primary section serving as a prime mover in the manner of a conventional single-rotor rotary engine operating according to the known four-event work cycle; b) a three-flanked rotor connected to said power shaft and rotatably contained in each said section for effecting work-cycle events; c) a two-lobed housing cavity contained in each said engine section to serve as the operating chamber for the respective rotor during rotation thereof; d) means for supplying primary air and fuel only to the primary sections, and in quantities effecting ignitable fuel-rich mixtures therein; e) ignition means for igniting said mixtures in said primary sections; f) each primary rotor having conventional design with a conventional recess in each flank, said recess forming part of a moving combustion chamber as that rotor rotates; g) each secondary rotor differing from primary rotors only by having non-recessed flanks which coactively participate with the peripheral surface of the respective said cavity in substantially preventing transfer of gases between the lobes of that cavity; h) short gas-transfer conduits each separately connecting and thereby compounding one primary section and one adjacent secondary section to form one compound engine unit thereof, each conduit serving as a passageway for direct transfer or working medium held at high temperature and pressure as it is exhausted by the primary section to the secondary section in the same unit; i) eccentrics of said eccentric shaft serving as rotor journals arranged for rotors to be rotatably mounted thereon and effect, during their rotation, equal spacing of the respectiive expansion events of the said four-event work cycle; j) each secondary rotor housing provided with an air intake port and an air outlet port disposed oppositely and peripherally in one lobe of the respective said two-lobed housing cavity, said intake ports connected to a conventional air-filter system and each said outlet port connected to the respective said conduit whereby each secondary section's rotor is enabled to induct supplemental secondary air through said air-filter system during each intake event in the respective said one lobe, and cause ejection of said air directly into the respective said conduit and working medium during each successive compression event in that same lobe to support the burning of leftover combustibles in said medium; and k) each secondary rotor housing also provided with a peripheral inlet port in the other lobe of the respective said two-lobed cavity and connected to the respective conduit for admitting therefrom the air-treated working medium during each expansion event in the respective said other lobe; each said secondary housing additionally provided with a peripheral exhaust port disposed in the opposite side of the respective said other lobe for release of the spent medium during successive exhaust events into an exhaust system connected to said exhaust ports.