Gas turbine propulsion system
AssigneeAntheon Research, Inc.
InventorsFrancis O'Neill, Anthony A. Hartzheim
Life of this patent
Estimating the term…
Abstract
A gas turbine propulsion system includes a shroud that defines a fluid flow path. A gas turbine engine in the fluid flow path includes a compressor, a combustor downstream from the compressor, and a turbine downstream from the combustor. An electric generator in the fluid flow path includes a rotor coaxially aligned with the turbine. A propulsor is upstream from the gas turbine engine, and an electric motor is operably coupled to the propulsor to rotate the propulsor. The propulsor is rotationally isolated from the gas turbine engine so that the propulsor rotates independently from operation of the gas turbine engine.
Claims18
A gas turbine propulsion system, comprising:
- a shroud that defines a fluid flow path;
- a gas turbine engine entirely in said fluid flow path defined by said shroud, wherein said gas turbine engine comprises a compressor, a combustor downstream from said compressor, and a turbine downstream from said combustor;
- an electric generator entirely in said fluid flow path defined by said shroud and upstream from said gas turbine engine, wherein said electric generator comprises a rotor coaxially aligned with said turbine;
- a propulsor upstream from said gas turbine engine and entirely in said fluid flow path defined by said shroud;
- and
- an electric motor operably coupled to said propulsor to rotate said propulsor;
- wherein said propulsor is rotationally isolated from said gas turbine engine during all operating conditions so that said propulsor rotates independently from operation of said gas turbine engine.
A gas turbine propulsion system, comprising:
- a shroud that defines a fluid flow path;
- a gas turbine engine entirely in said fluid flow path defined by said shroud, wherein said gas turbine engine comprises a compressor, a combustor downstream from said compressor, and a turbine downstream from said combustor;
- an electric generator operably connected upstream from said gas turbine engine, wherein said electric generator comprises a rotor coaxially aligned with said turbine;
- a shaft that rotatably connects said turbine to said rotor of said electric generator so that said turbine and said rotor rotate at the same speed;
- a propulsor upstream from said electric generator and entirely in said fluid flow path defined by said shroud;
- an electric motor operably coupled to said propulsor to rotate said propulsor;
- wherein said propulsor is rotationally isolated from said gas turbine engine during all operating conditions so that said propulsor rotates independently from operation of said gas turbine engine.
A gas turbine propulsion system, comprising:
- a shroud that defines a fluid flow path;
- a gas turbine engine entirely in said fluid flow path defined by said shroud, wherein said gas turbine engine comprises a compressor, a combustor downstream from said compressor, and a turbine downstream from said combustor;
- an electric generator operably connected upstream from said gas turbine engine, wherein said electric generator comprises a rotor;
- a shaft that rotatably connects said turbine to said rotor of said electric generator so that said turbine and said rotor rotate at the same speed;
- a propulsor upstream from said gas turbine engine and entirely in said fluid flow path defined by said shroud;
- and
- an electric motor operably coupled to said propulsor to rotate said propulsor;
- wherein said electric motor and said propulsor are rotationally isolated from said gas turbine engine during all operating conditions so that said propulsor rotates independently from operation of said gas turbine engine.
Dependencies are inferred from the claim text.