High efficiency air cycle air conditioning system
AssigneeUnited Technologies Corporation
InventorGeorge C. Rannenberg
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AssigneeUnited Technologies Corporation
InventorGeorge C. Rannenberg
Estimating the term…
A high efficiency air cycle air conditioning system (10), driven and charged by a gas turbine engine (15), operates in a closed-loop, Brayton cycle. The system includes a main (bootstrap) compressor (75) discharging to a sink heat exchanger (85) which in turn discharges to a regenerative heat exchanger (110). Air is ducted from the regenerative heat exchanger to an expansion turbine (120) where the air is chilled and then ducted to load (20). Air exhausted from the load is again ducted through the regenerative heat exchanger where the load exhaust air precools turbine inlet air. The capacity (operating pressures) of, and input power to the system are controlled by modulation of charge air provided to the system from the gas turbine engine and if desired, may be further controlled by selective bleeding of air from the system, selective bypassing of the system turbine with refrigerant, or modulation of shaft input power to the main compressor.
In an air cycle refrigeration system for providing chilled refrigerant air to a load for the cooling thereof, said system being adapted for the supply thereto of compressed charge air from the compressor discharge section of a gas turbine engine and comprising a bootstrap compressor for increasing the pressure of said refrigerant air, airflow exhausted from said refrigerant compressor being directed to an expansion turbine for cooling thereby and discharge therefrom to said load, said expansion turbine and bootstrap compressor being mechanically interconnected whereby said expansion turbine provides, a measure of input power for driving said bootstrap compressor, said air cycle refrigeration system being characterized by:
A method of cooling a load with an air cycle refrigeration system, said method comprising the steps of providing charge air from the compressor discharge section of a gas turbine engine to the inlet of a main compressor of said refrigeration system, cooling said compressed supply air by heat transfer therefrom to a heat sink, chilling and expanding said compressed air in an expansion turbine and cooling said load by passing said chilled and expanded air therethrough, said method being characterized by the steps of:
Dependencies are inferred from the claim text.