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US 2025/0376261 A1Published application
Environmental control system of an aircraft configured with a two-phase turbine encased with a compressor and motor
AssigneeHamilton Sundstrand Corporation
InventorViktor Kilchyk
Life of this patent
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Abstract
An environmental control system of an aircraft, having: a cooling circuit including: a sealed housing; a turbo-compressor sealed within the housing, wherein the turbo-compressor includes: a compressor fluidly coupled to the circuit; a turbine fluidly coupled to the circuit downstream of the compressor, wherein the turbine is a flash turbine; a shaft operably coupling the compressor and the turbine; and a motor generator operably coupled to the turbo-compressor and disposed within the housing.
Claims10
An environmental control system of an aircraft, comprising:
- a cooling circuit including:
- a sealed housing;
- a turbo-compressor sealed within the housing, wherein the turbo-compressor includes:
- a compressor fluidly coupled to the circuit;
- a turbine fluidly coupled to the circuit downstream of the compressor, wherein the turbine is a flash turbine;
- a shaft operably coupling the compressor and the turbine;
- and
- a motor generator operably coupled to the turbo-compressor and disposed within the housing.
5 more elements
Dependencies are inferred from the claim text.