High speed propulsion system with inlet cooling

A cooling system for a turbine engine, the turbine engine comprising a core engine and a bypass flow turbomachine, the core engine having a compressor, a combustor, and a turbine and the bypass flow turbomachine having a plurality of rotor blades, the plurality of rotor blades having an inboard portion defining a bypass flow turbomachine compressor and an outboard portion defining a bypass flow turbomachine turbine, the cooling system comprising:

• a heat exchanger in fluid communication with a first fluid inlet stream and disposed upstream and in fluid communication with the core engine, the heat exchanger operative to cool the first fluid inlet stream, the heat exchanger comprising:
• a heat exchanger inlet for input of a heat exchanging medium for exchange of heat from the first fluid inlet stream to the heat exchanging medium;
• and
• a heat exchanger outlet for discharge of a heated output stream onto an the outboard portion of the plurality of rotor blades of the bypass flow turbomachine, wherein the heated output stream comprises steam, the plurality of rotor blades defining a plurality of turbine stages of the bypass flow turbomachine turbine, whereby the steam bypasses the compressor, the combustor, and the turbine of the core engine and provides an additional flow to the bypass flow turbomachine.

A turbine engine including a cooling system, the turbine engine comprising:

• a core engine comprising an intake side and an exhaust side, the core engine configured to receive a first fluid stream and discharge a primary exhaust flow stream, the core engine comprising a compressor, a combustor, and a turbine;
• a bypass flow turbomachine comprising a plurality of rotor blades, an inboard portion of the plurality of rotor blades defining a bypass flow turbomachine compressor disposed to receive a second fluid stream and an outboard portion of the plurality of rotor blades defining a plurality of turbine stages disposed to receive the primary exhaust flow stream from the core engine and discharge a secondary exhaust flow stream, the bypass flow turbomachine including an augmentor;
• and
• an inlet heat exchanger in fluid communication with the first fluid stream and disposed upstream and in fluid communication with the core engine, the inlet heat exchanger operative to cool the first fluid stream, the inlet heat exchanger comprising:
• a heat exchanger inlet for input of a heat exchanging medium for exchange of heat from the first fluid stream to the heat exchanging medium;
• and
• a heat exchanger outlet for discharge of a heated output stream, wherein at least a portion of the heated output stream bypasses the compressor, the combustor, and the turbine of the core engine and is output to at least one of the plurality of turbine stages of the bypass flow turbomachine or an injector of the augmentor.