Advanced method and aircraft for pre-cooling an environmental control system using a dual compressor four wheel turbo-machine
Abstract:
A method and aircraft for providing bleed air to environmental control systems of an aircraft using a gas turbine engine, including determining a bleed air demand for the environmental control systems, selectively supplying low pressure and high pressure bleed air to the environmental control systems, wherein the selectively supplying is controlled such that the conditioned air stream satisfies the determined bleed air demand.
Information query
Patent Agency Ranking
0/0