Aircraft cooling and heating systems and related methods are disclosed. An example apparatus includes an air compressor operatively coupled to a turbine engine. The air compressor is configured to generate compressed air at a first temperature. A vapor cycle system configured to reduce the first temperature of the compressed air provided by the air compressor to a second temperature that is less than the first temperature.
AIRCRAFT SYSTEMS AND RELATED METHODS
29.04.2021
Patent
Elektronische Ressource
Englisch
AIRCRAFT SPOILER ACTUATION SYSTEMS AND RELATED METHODS
Europäisches Patentamt | 2021
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