|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||62/402 ; 62/172|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 39 인용 특허 : 0|
This invention relates to an airconditioning system to provide environmental control for an aircraft\s cabin or cockpit. The system cooling cycle includes in combination: a rotary power supply and a turbomachine which includes a power compressor secured to a power shaft for providing compressed air. The rotary power supply is drivingly coupled to the power shaft to operate at a given speed. An expansion cooling turbine is mounted on a shaft concentric to the power shaft. A power driven fan is provided for directing a source of ambient air to and through ...
An airconditioning control system for an enclosure, the environment of which is to be controlled, including in combination; a rotary power supply, a turbomachine including a power compressor for providing compressed air secured to a power shaft, said rotary power supply drivingly coupled to said power shaft to operate at a given speed; an expansion cooling turbine mounted on a shaft concentric to said power shaft, means for directing a source of ambient air to and through a heat exchanger, said power compressor coupled to said enclosure and through said ...