# US 10,119,399 B1 · Reverse vane engine extracting work from hot gas entering an engine at an ambient pressure > Agents: this data is available as JSON from the patentgrep API and MCP server — see https://patentgrep.com/llms.txt - Number: US 10,119,399 B1 - Document ID: US10119399B1 - Status: Granted - Kind: B1 - Application number: 14/962,965 - Filed: 2015-12-08 - Granted: 2018-11-06 - Earliest claimed: 2014-12-09 - Applicants: Brian Lee Davis - Inventors: Brian Lee Davis - Web page: https://patentgrep.com/patent/US10119399B1 ## CPC - F04C 29/04: Heating; Cooling (of machines or engines in general F01P); Heat insulation (heat insulation in general F16L59/00) - F01C 1/3441: {the inner and outer member being in contact along one line or continuous surface substantially parallel to the axis of rotation} - F01C 20/10: characterised by changing the positions of the inlet or outlet openings with respect to the working chamber - F01C 21/06: Heating; Cooling (of machines or engines in general F01P); Heat insulation (heat insulation in general F16L) - F01C 21/10: Outer members for co-operation with rotary pistons; Casings (casings for rotary engines or machines in general F16M) - F04C 2/3441: {the inner and outer member being in contact along one line or continuous surface substantially parallel to the axis of rotation} - F04C: ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS (engines F03C); ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS - F01C: ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES (internal-combustion aspects F02B53/00, F02B55/00) ## Abstract The present invention is an engine having a housing, a rotor and a plurality of vanes. The housing has a cavity with an outer wall that has an inlet region, an insulation or hot region, a thermal separator, a chill region, a work region and a return region. The vanes define cavities that rotate between the rotor and the housing. Hot gas enters in the inlet region, which can have a slot. The cavity is full of hot gas in the insulation region. The temperature is reduced in the chill region, which causes the pressure to likewise drop to a relative low pressure. In the work region, the diameter of the outer wall is reduced. The pressure differential between successive cavities causes the rotor to turn in the direction of the decreasing wall length, whereby work can then be extracted from the engine. ## Claims ### Claim 1 A reverse vane engine operable via a gas comprising: a housing with an outer wall; a rotor, said rotor having a center, said rotor rotating relative to said housing about said center; and a cavity defined by a first vane, a second vane, said rotor and said outer wall, said first vane and said second vane being supported by said rotor wherein said first vane and said second vane move relative to said outer wall, wherein said cavity moves through an inlet region with an inlet, a hot region with insulation on said outer wall, a chill region with a heat exchanger on said outer wall, and a work region wherein said outer wall has a decreasing radius relative to said center of said rotor within said work region, said work region having an exhaust port at a work region end, wherein: said hot region allows said cavity to be filled with said gas which is a hot gas prior to moving through said chill region, volume of said cavity is constant in said chill region whereby pressure of said gas drops as a cavity temperature drops, and work is performed within said work region as said first vane has a shorter length between said rotor and said outer wall than said second vane as said outer wall has said decreasing radius within said work region. ### Claim 2 (depends on 1) The reverse vane engine of claim 1 wherein said inlet region comprises a slot. ### Claim 3 (depends on 2) The reverse vane engine of claim 2 wherein: said inlet region has an inlet start and an inlet end; and said slot spans between said inlet start and said inlet end. ### Claim 4 (depends on 1) The reverse vane engine of claim 1 wherein said gas enters the assembly at an inlet pressure and exits the assembly at an outlet pressure, said inlet pressure and said outlet pressure being approximately equal. ### Claim 5 (depends on 1) The reverse vane engine vane engine of claim 1 wherein said exhaust port is an end exhaust port receiving an end plug that is removable from said end exhaust port if pressure within said cavity is greater than an ambient pressure when said cavity reaches said end exhaust port, said reverse vane engine further comprising an intermediate exhaust port receiving an intermediate plug that is removable from said intermediate exhaust port only when pressure within said cavity is greater than said ambient pressure when said cavity reaches said intermediate exhaust port, said intermediate exhaust port being located between a start of said work region and said end exhaust port. ### Claim 6 (depends on 5) The reverse vane engine of claim 5 wherein said intermediate plug releases towards an outside of said housing. ### Claim 7 (depends on 5) The reverse vane engine of claim 5 wherein said intermediate plug is wedge shaped whereby said intermediate plug does not extend into said cavity when pressure within said cavity is less than said ambient pressure when said cavity reaches said intermediate exhaust port. ### Claim 8 (depends on 1) The reverse vane engine of claim 1 wherein said work region has a length, said length being a variable length. ### Claim 9 (depends on 1) The reverse vane engine of claim 1 wherein: said cavity has an outer length; said hot region has a hot region length; and said outer length is approximately equal to said hot region length. ### Claim 10 (depends on 1) The reverse vane engine of claim 1 further comprising a thermal separator between said hot region and said chill region. ### Claim 11 (depends on 1) The reverse vane engine of claim 1 wherein said cavity has a constant volume when said cavity passes through said chill region. ### Claim 12 A reverse vane engine operable via a gas comprising: a housing with an outer wall; a rotor, said rotor having a center, said rotor rotating relative to said housing about said center; and a cavity defined by a first vane, a second vane, said rotor and said outer wall, said first vane and said second vane being supported by said rotor wherein said first vane and said second vane move relative to said outer wall, wherein said cavity moves through an inlet region with an inlet, a chill region wherein said gas within said cavity cools resulting in a reduction of a cavity pressure in said chill region, and a work region with a work region start and a work region end, said work region having an end exhaust port at said work region end and an intermediate exhaust port between said work region start and said work region end as determined by a rotational direction of travel of said cavity, said intermediate exhaust port removably receiving an intermediate plug, said intermediate plug being biased to a closed position, wherein, when said cavity reaches said intermediate exhaust port, said intermediate plug opens when said cavity pressure exceeds an ambient pressure outside of said housing to allow at least some of said gas to exit through said intermediate exhaust port, wherein work is performed within said work region as said first vane has a shorter length than said second vane as said outer wall has a decreasing radius within said work region. ### Claim 13 (depends on 12) The reverse vane engine of claim 12 wherein said intermediate plug is wedge shaped. ### Claim 14 A reverse vane engine operable via a gas comprising: a housing with an outer wall; a rotor, said rotor having a center, said rotor rotating relative to said housing about said center; and a cavity defined by a first vane and a second vane, said rotor and said outer wall, said first vane and said second vane being supported by said rotor wherein said first vane and said second vane move relative to said outer wall, wherein said cavity moves through an inlet region with an inlet, a chill region wherein said gas within said cavity cools resulting in a reduction of a cavity pressure in said chill region, and a work region wherein said outer wall has a decreasing radius relative to said center of said rotor, said work region having a work region start and a work region end as determined by a rotational direction of travel of said cavity, said work region radially having at least two exhaust ports each with a plug operably associated therewith, each of said plug operably associated therewith opening when said cavity pressure exceeds an ambient pressure outside of said housing and remaining closed when said cavity pressure is less than said ambient pressure when said cavity respectively passes each of said at least two exhaust ports, wherein said reverse engine has an effective work region that is variable in length defined radially starting at said work region start and terminating at the first one of said at least two exhaust ports wherein said plug operably associated therewith is open, and wherein work is performed within said work region as said first vane has a shorter length than said second vane as said outer wall has said decreasing radius within said work region.