Raytheon technologies corporation (20240301823). HEAT EXCHANGER(S) FOR RECOVERING WATER AND/OR HEAT ENERGY FROM TURBINE ENGINE COMBUSTION PRODUCTS simplified abstract

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HEAT EXCHANGER(S) FOR RECOVERING WATER AND/OR HEAT ENERGY FROM TURBINE ENGINE COMBUSTION PRODUCTS

Organization Name

raytheon technologies corporation

Inventor(s)

Jon E. Sobanski of Glastonbury CT (US)

Jacob C. Snyder of East Haddam CT (US)

Neil J. Terwilliger of Cheshire CT (US)

HEAT EXCHANGER(S) FOR RECOVERING WATER AND/OR HEAT ENERGY FROM TURBINE ENGINE COMBUSTION PRODUCTS - A simplified explanation of the abstract

This abstract first appeared for US patent application 20240301823 titled 'HEAT EXCHANGER(S) FOR RECOVERING WATER AND/OR HEAT ENERGY FROM TURBINE ENGINE COMBUSTION PRODUCTS

Simplified Explanation:

This patent application describes a turbine engine with an axis that includes a fan section, a turbine engine core, a bypass flowpath, a recovery system, and a core flowpath. The core compresses the fan section and includes a core compressor section, a core combustor section, and a core turbine section. The recovery system consists of an evaporator module and a condenser module, with the condenser module overlapping the bypass flowpath.

  • The turbine engine core powers the fan section.
  • The recovery system includes an evaporator module and a condenser module.
  • The condenser module is positioned radially outboard of the bypass flowpath.
  • The core flowpath extends through various sections of the turbine engine core and the recovery system.

Key Features and Innovation:

  • Integration of a recovery system into a turbine engine design.
  • Efficient power generation for the fan section.
  • Optimization of airflow through the core and bypass flowpaths.
  • Enhanced cooling and energy recovery capabilities.

Potential Applications:

This technology could be applied in aircraft engines, power generation systems, and other industrial applications requiring efficient turbine engines with recovery systems.

Problems Solved:

This technology addresses the need for improved energy efficiency and cooling in turbine engines, as well as the recovery of waste heat for additional power generation.

Benefits:

  • Increased fuel efficiency.
  • Enhanced power generation capabilities.
  • Improved overall performance and reliability of turbine engines.

Commercial Applications:

Potential commercial applications include aircraft propulsion systems, power plants, and marine propulsion systems. This technology could significantly impact the aerospace and energy industries.

Questions about Turbine Engine with Recovery System:

1. How does the recovery system in this turbine engine improve overall efficiency? 2. What are the key advantages of integrating a recovery system into a turbine engine design?


Original Abstract Submitted

a turbine engine with an axis is provided. this turbine engine includes a fan section, a turbine engine core, a bypass flowpath, a recovery system and a core flowpath. the turbine engine core is configured to power the fan section. the turbine engine core includes a core compressor section, a core combustor section and a core turbine section. the bypass flowpath is fluidly coupled with and downstream of the fan section. the recovery system includes an evaporator module and a condenser module. the condenser module is arranged radially outboard of and axially overlaps the bypass flowpath. the core flowpath extends sequentially through the core compressor section, the core combustor section, the core turbine section, the evaporator module and the condenser module.

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