Gas turbine propulsion system

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 defined by the shroud 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.

What is claimed is: 
     
         1 . A gas turbine propulsion system, comprising:
 a shroud that defines a fluid flow path;   a gas turbine engine in said fluid flow path, wherein said gas turbine engine comprises a compressor, a combustor downstream from said compressor, and a turbine downstream from said combustor;   an electric generator 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   an electric motor operably coupled to said propulsor to rotate said propulsor;   wherein said propulsor is rotationally isolated from said gas turbine engine so that said propulsor rotates independently from operation of said gas turbine engine.   
     
     
         2 . The gas turbine propulsion system as in  claim 1 , wherein said turbine of said gas turbine engine comprises an integrally bladed rotor. 
     
     
         3 . The gas turbine propulsion system as in  claim 1 , wherein said electric motor is coaxially aligned with said electric generator. 
     
     
         4 . The gas turbine propulsion system as in  claim 1 , wherein said propulsor is coaxially aligned with said electric generator. 
     
     
         5 . The gas turbine propulsion system as in  claim 1 , wherein said gas turbine engine is a single-spool gas turbine engine. 
     
     
         6 . The gas turbine propulsion system as in  claim 1 , wherein said gas turbine engine comprises 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. 
     
     
         7 . The gas turbine propulsion system as in  claim 6 , further comprising a plurality of non-lubricated bearings that rotatably support said shaft. 
     
     
         8 . A gas turbine propulsion system, comprising:
 a gas turbine engine, 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;   an electric motor operably coupled to said propulsor to rotate said propulsor;   wherein said propulsor rotates independently from operation of said gas turbine engine.   
     
     
         9 . The gas turbine propulsion system as in  claim 8 , wherein said turbine of said gas turbine engine comprises an integrally bladed rotor. 
     
     
         10 . The gas turbine propulsion system as in  claim 8 , wherein said electric motor is coaxially aligned with said electric generator. 
     
     
         11 . The gas turbine propulsion system as in  claim 8 , wherein said propulsor is coaxially aligned with said electric generator. 
     
     
         12 . The gas turbine propulsion system as in  claim 8 , wherein said gas turbine engine is a single-spool gas turbine engine. 
     
     
         13 . The gas turbine propulsion system as in  claim 12 , further comprising a plurality of non-lubricated bearings that rotatably support said single-spool gas turbine engine. 
     
     
         14 . A gas turbine propulsion system, comprising:
 a shroud that defines a fluid flow path;   a gas turbine engine in said fluid flow path, 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   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 so that said propulsor rotates independently from operation of said gas turbine engine.   
     
     
         15 . The gas turbine propulsion system as in  claim 14 , wherein said turbine of said gas turbine engine comprises an integrally bladed rotor. 
     
     
         16 . The gas turbine propulsion system as in  claim 14 , wherein said rotor is coaxially aligned with said compressor. 
     
     
         17 . The gas turbine propulsion system as in  claim 14 , wherein said electric motor is coaxially aligned with said electric generator. 
     
     
         18 . The gas turbine propulsion system as in  claim 14 , further comprising a plurality of non-lubricated bearings that rotatably support said shaft. 
     
     
         19 . The gas turbine propulsion system as in  claim 14 , wherein said gas turbine engine is a single-spool gas turbine engine.