Claims Analysis
Total Claims: 8
Claim 1
Independent Claim
218 words
In a process for the conversion of heat into work, an improved cycle for an external combustion engine including a heater, a turbine, and a compressor, said cycle comprising the steps of: (a) heating a liquid heat transfer fluid under pressure to provide a pressurized vapor, (b) expanding said pressurized vapor in functional flow communication with an impulse turbine to perform work and to provide a turbine-spent efflux vapor, (c) maintaining the efflux vapor from the impulse turbine at a pressure reduced to approximately 1/2 of a pressure of the pressurized vapor as introduced functionally into the impulse turbine, and (d) maintaining the temperature of the vapor in the engine at a level to preclude condensation of the vapor, (e) releasing efflux vapor from the impulse turbine, into a compressor, (f) compressing in the compressor the efflux vapor released from the impulse turbine, and simultaneously cooling the efflux vapor in the same compressor while maintaining the efflux vapor as a gaseous phase, (g) reheating the compressed efflux vapor to provide a superheated vapor, (h) directing the superheated vapor through the impulse turbine to perform work, and (i) repeating process steps (c) through (h) including repeatedly recycling vapor through the impulse turbine while obviating transition of the vapor through a liquid phase throughout the duration of the operating cycle.
Claim 2
Dependent Claim
218 words
In a process for the conversion of heat into work, an improved cycle for an external combustion engine including a heater, a turbine, and a compressor, said cycle comprising the steps of: (a) heating a liquid heat transfer fluid under pressure to provide a pressurized vapor, (b) expanding said pressurized vapor in functional flow communication with an impulse turbine to perform work and to provide a turbine-spent efflux vapor, (c) maintaining the efflux vapor from the impulse turbine at a pressure reduced to approximately 1/2 of a pressure of the pressurized vapor as introduced functionally into the impulse turbine, and (d) maintaining the temperature of the vapor in the engine at a level to preclude condensation of the vapor, (e) releasing efflux vapor from the impulse turbine, into a compressor, (f) compressing in the compressor the efflux vapor released from the impulse turbine, and simultaneously cooling the efflux vapor in the same compressor while maintaining the efflux vapor as a gaseous phase, (g) reheating the compressed efflux vapor to provide a superheated vapor, (h) directing the superheated vapor through the impulse turbine to perform work, and (i) repeating process steps (c) through (h) including repeatedly recycling vapor through the impulse turbine while obviating transition of the vapor through a liquid phase throughout the duration of the operating cycle.
Claim 3
Dependent Claim
20 words
The process as set forth in claim 1 wherein simultaneous compression and cooling are carried out in the compressor isothermally.
Claim 4
Dependent Claim
38 words
The process as set forth in claim 1 wherein the heating of the liquid heat transfer fluid is effected through the steps of electrolyzing water to produce hydrogen and oxygen gases, and burning the gases to produce heat.
Claim 5
Dependent Claim
57 words
The process as set forth in claim 1 wherein the impulse turbine is a multi-stage impulse turbine, and wherein during a final stage exhaust of the multi-stage impulse turbine, the turbine is operated at a value and under conditions such that the ratio of the final stage exhaust pressure to the stage input pressure is approximately 1:2.
Claim 6
Dependent Claim
33 words
The process as set forth in claim 4 wherein said turbine is a velocity compounded stage turbine, and wherein the pressurized efflux vapor is expanded and utilized through the velocity compounded stage turbine.
Claim 7
Dependent Claim
19 words
The method as set forth in claim 5 wherein the velocity compounded stage turbine is a Curtis type turbine.
Claim 8
Dependent Claim
27 words
The method as set forth in claim 1 wherein the turbine is a multi-stage turbine comprising, in combination, a Curtis velocity-compounded type turbine and an impulse turbine.