Gas turbine engine with water recovery system
An engine system is provided that includes an open propulsor rotor, an engine core assembly, a bypass flowpath and a condenser. The engine core assembly is configured to drive rotation of the open propulsor rotor. The engine core assembly includes a core flowpath, a compressor section, a combustor section and a turbine section. The core flowpath extends through the compressor section, the combustor section and the turbine section from an inlet into the core flowpath to an exhaust from the core flowpath. The bypass flowpath bypasses the engine core assembly. The condenser is configured to exchange heat energy between combustion products flowing within the core flowpath downstream of the combustor section and bypass air flowing within the bypass flowpath.
1. An engine system, comprising:
an open propulsor rotor;
an inlet duct upstream of and fluidly coupled in parallel with a core inlet and a bypass inlet;
an engine core assembly configured to drive rotation of the open propulsor rotor, the engine core assembly including a core flowpath, a compressor section, a combustor section and a turbine section, and the core flowpath extending through the compressor section, the combustor section and the turbine section from the core inlet into the core flowpath to an exhaust from the core flowpath;
a bypass flowpath bypassing the engine core assembly and extending along a length of the core engine assembly;
a condenser configured to exchange heat energy between combustion products flowing within the core flowpath downstream of the combustor section and bypass air flowing within the bypass flowpath; and
a housing, wherein the engine core assembly and the bypass flowpath are disposed in the housing, the bypass flowpath extending from the bypass inlet, internally through the engine system, to a bypass exhaust, the housing extending along the length of the core engine assembly, and the open propulsor rotor is configured to propel additional air outside of and along the housing to provide thrust.
2. The engine system of claim 1 , further comprising:
a water separator;
the condenser configured to condenser water vapor flowing through the core flowpath into water; and
the water separator configured to collect the water within the core flowpath.
3. The engine system of claim 2 , further comprising:
a water reservoir fluidly coupled with the water separator;
the water reservoir configured to store at least some of the water.
4. The engine system of claim 2 , further comprising:
a water recovery system including the condenser and the water separator;
the water recovery system configured to direct at least some of the water to the engine core assembly.
5. The engine system of claim 2 , further comprising:
a water recovery system including the condenser, the water separator and an evaporator;
the evaporator configured to evaporate at least some of the water into steam; and
the water recovery system configured to direct at least some of the steam to the engine core assembly.
6. The engine system of claim 2 , further comprising an evaporator configured to exchange heat energy between the combustion products flowing within the core flowpath and at least some of the water to evaporate the at least some of the water into steam.
7. The engine system of claim 6 , further comprising a turboexpander section comprising a turboexpander rotor;
the turboexpander section configured to expand at least some of the steam across the turboexpander rotor to drive rotation of the turboexpander rotor.
8. The engine system of claim 7 , wherein the turboexpander rotor is configured to further drive rotation of the open propulsor rotor.
9. The engine system of claim 7 , further comprising a mechanical load mechanically powered by the turboexpander section.
10. The engine system of claim 1 , further comprising:
a fuel system including a fuel reservoir, a fuel flowpath and a fuel injector;
the fuel flowpath configured to direct hydrogen fuel, received from the fuel reservoir, to the fuel injector; and
the fuel injector configured to introduce the hydrogen fuel into a combustor of the combustor section.
11. The engine system of claim 1 , further comprising:
a fuel system including a fuel flowpath, a fuel-cooling air heat exchanger and a fuel injector, the fuel flowpath configured to direct fuel through the fuel-cooling air heat exchanger to the fuel injector, and the fuel injector configured to introduce the fuel into a combustor of the combustor section; and
a cooling circuit configured to direct cooling air through the fuel-cooling air heat exchanger to the engine core assembly;
the fuel-cooling air heat exchanger configured to exchange heat energy between the fuel flowing within the fuel flowpath and the cooling air flowing within the cooling circuit.
12. The engine system of claim 1 , further comprising:
a fuel system including a fuel flowpath, a fuel-combustion products heat exchanger and a fuel injector, the fuel flowpath configured to direct fuel through the fuel-combustion products heat exchanger to the fuel injector, and the fuel injector configured to introduce the fuel into a combustor of the combustor section; and
the fuel-combustion products heat exchanger configured to exchange heat energy between the fuel flowing within the fuel flowpath and the combustion products flowing within the core flowpath.
13. The engine system of claim 1 , further comprising:
a fuel system including a fuel flowpath, a fuel injector and a turboexpander section;
the fuel flowpath configured to direct fuel through the turboexpander section to the fuel injector;
the fuel injector configured to introduce the fuel into a combustor of the combustor section;
the turboexpander section comprising a turboexpander rotor, and the fuel system configured to expand the fuel flowing within the fuel flowpath across the turboexpander section to drive rotation of the turboexpander rotor.
14. The engine system of claim 13 , wherein the turboexpander rotor is configured to further drive rotation of the open propulsor rotor.
15. The engine system of claim 13 , further comprising a mechanical load mechanically powered by the turboexpander section.
16. The engine system of claim 1 , further comprising a fuel system including a fuel flowpath, an accumulator and a fuel injector, the fuel flowpath configured to direct fuel through the accumulator to the fuel injector, and the fuel injector configured to introduce the fuel into a combustor of the combustor section.
17. The engine system of claim 1 , wherein the open propulsor rotor comprises a propeller rotor.
18. An engine system, comprising:
an un-ducted propulsor rotor;
an engine core assembly configured to drive rotation of the un-ducted propulsor rotor, the engine core assembly including a core flowpath, a compressor section, a combustor section and a turbine section, the core flowpath extending through the compressor section, the combustor section and the turbine section from an inlet into the core flowpath to an exhaust from the core flowpath, and the combustor section comprising a combustor;
a fuel system including a fuel flowpath and a fuel injector, the fuel flowpath configured to direct hydrogen fuel to the fuel injector, and the fuel injector configured to introduce the hydrogen fuel into the combustor;
an internal second flowpath extending around the engine core assembly and along a length of the core engine assembly, the internal second flowpath disposed within an engine housing, the engine housing disposed radially outboard of and extending along a length of the core engine assembly, and the internal second flowpath including an internal second flowpath inlet disposed in parallel with the inlet into the core flowpath; and
a heat exchanger configured to exchange heat energy between a working fluid and air flowing within the internal second flowpath;
wherein the un-ducted propulsor rotor is configured to propel air outside of the engine system axially along the engine core assembly and the internal second flowpath.
19. An engine system, comprising:
an open propulsor rotor;
an engine core assembly configured to drive rotation of the open propulsor rotor, the engine core assembly including a core flowpath, a compressor section, a combustor section and a turbine section, and the core flowpath extending through the compressor section, the combustor section and the turbine section from an inlet into the core flowpath to an exhaust from the core flowpath;
a bypass flowpath bypassing the engine core assembly and extending along a length of the core engine assembly;
a water recovery system including a condenser, a water separator, a water reservoir, an evaporator, a first flow regulator and a second flow regulator, the condenser configured to exchange heat energy between combustion products flowing within the core flowpath downstream of the combustor section and bypass air flowing within the bypass flowpath, the condenser configured to condense water vapor flowing through the core flowpath into water, the water separator configured to collect the water within the core flowpath, the water reservoir fluidly coupled with the water separator, the water reservoir configured to store at least some of the water, the evaporator configured to evaporate at least some of the water into steam, an outlet of the water reservoir fluidly coupled with one or more components of the core engine assembly through the first flow regulator, the outlet of the water reservoir fluidly coupled with the evaporator through the second flow regulator, and the water recovery system configured to direct at least some of the steam to the engine core assembly; and
a housing, wherein the engine core assembly and the bypass flowpath are disposed in the housing, the housing extending along the length of the core engine assembly, and the open propulsor rotor is configured to propel additional air outside of and along the housing to provide thrust.