Gas turbine engine driven by sCO2 cycle with advanced heat rejection
First Claim
1. A gas turbine engine, comprising:
- a shaft having mounted thereto a first compressor, a second compressor, a turbine, and a fan assembly;
a power circuit that provides power to the shaft in a closed-loop system that includes a working fluid heated by a combustor, the power circuit comprising the turbine and the second compressor;
an inner housing that houses;
at least a portion of the shaft;
the second compressor;
the turbine;
the first compressor for compressing a core stream of air; and
the combustor to heat the working fluid when it enters the combustor;
a baffle that encloses a portion of the inner housing and forms a first air passageway therebetween;
a nacelle that encloses a portion of the baffle and forms a second air passageway therebetween; and
a heat exchanger positioned in the second air passageway that rejects heat from the working fluid into a heat rejection stream of air passing through the second air passageway;
wherein air is accelerated as streams in parallel and via the fan assembly;
as the core stream into the inner housing;
as a bypass flow stream of air through a first volume; and
as the heat rejection stream.
1 Assignment
0 Petitions
Accused Products
Abstract
A gas turbine engine includes a shaft comprising a first compressor, a fan assembly, and a power circuit that provides power to the shaft in a closed-loop system. An inner housing houses at least a portion of the shaft, the first compressor for compressing a core stream of air, and a combustor. A baffle encloses a portion of the inner housing and forms a first air passageway therebetween. A nacelle encloses a portion of the baffle and forms a second air passageway therebetween. A heat exchanger is positioned in the second air passageway that rejects heat from the power circuit into a heat rejection stream of air passing through the second air passageway. Air is accelerated as streams in parallel and via the fan assembly as the core stream into the inner housing, as a bypass flow stream of air through the first volume, and as the heat rejection stream.
-
Citations
22 Claims
-
1. A gas turbine engine, comprising:
-
a shaft having mounted thereto a first compressor, a second compressor, a turbine, and a fan assembly; a power circuit that provides power to the shaft in a closed-loop system that includes a working fluid heated by a combustor, the power circuit comprising the turbine and the second compressor; an inner housing that houses; at least a portion of the shaft; the second compressor; the turbine; the first compressor for compressing a core stream of air; and the combustor to heat the working fluid when it enters the combustor; a baffle that encloses a portion of the inner housing and forms a first air passageway therebetween; a nacelle that encloses a portion of the baffle and forms a second air passageway therebetween; and a heat exchanger positioned in the second air passageway that rejects heat from the working fluid into a heat rejection stream of air passing through the second air passageway; wherein air is accelerated as streams in parallel and via the fan assembly; as the core stream into the inner housing; as a bypass flow stream of air through a first volume; and as the heat rejection stream. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9)
-
-
10. A method of powering a gas turbine engine, comprising:
-
accelerating air as streams in parallel and via a fan assembly, the streams comprising; a core stream; a bypass flow stream; and a heat rejection stream; passing the core stream into an inner housing that houses; at least a portion of a shaft, the shaft having mounted thereto a first compressor, a second compressor, a turbine, and the fan assembly; the second compressor; the turbine; the first compressor for compressing the core stream; and a combustor that provides a power input directly to a working fluid of a power circuit in a closed-loop arrangement by heating the working fluid; passing the bypass flow stream external to the inner housing and into a first air passageway that is formed between a baffle and the inner housing; passing the heat rejection stream through a heat exchanger that is positioned in a second air passageway that is formed by a nacelle, that encloses at least a portion of the baffle; providing power to the shaft via the working fluid of the power circuit; and cooling the working fluid in the heat rejection stream with the heat exchanger; wherein the power circuit includes the turbine and the second compressor. - View Dependent Claims (11, 12, 13, 14, 15, 16, 17, 18)
-
-
19. A power-producing device, comprising:
-
an inner housing for passing a core stream of air, the inner housing houses; at least a portion of a shaft having mounted thereto a first compressor, a second compressor, a turbine, and a fan assembly; the second compressor; the turbine; the first compressor for compressing a core stream of air; and a combustor that receives a working fluid of a power circuit and provides a power input to the working fluid, the power circuit comprising the turbine and the second compressor; a nacelle that encloses a portion of the inner housing and forms a first air passageway therebetween for passing a heat rejection stream of air; and a heat exchanger positioned in the first air passageway that rejects heat from the power circuit into a heat rejection stream of air passing through the second air passageway; wherein the core stream and the heat rejection stream are accelerated in parallel and via the fan assembly; and wherein the power circuit includes carbon dioxide as at least a portion of the working fluid and is configured to operate as a super-critical (s-CO2) system. - View Dependent Claims (20, 21, 22)
-
Specification