|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||62/236 ; 62/DIG.5|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 65 인용 특허 : 6|
An integrated air conditioning and power unit is provided for use with an aircraft. The system includes an air turbine 42 having air passages connected to an engine 10 of the aircraft for receiving bleed air and/or ram air for driving the air turbine 42. A motor/generator 104 is drivingly connected to the air turbine 42. The motor/generator 104 is capable of drawing electricity from an aircraft primary power system for driving the motor or generating electricity which is delivered to the primary power system 108. An air compressor 54 is drivingly connect...
[ What is claimed is:] [1.] An integrated air conditioning and power unit for use with an engine of an aircraft, comprising:an air turbine having an inlet air passage connected to the engine;a motor/generator drivingly attached to said air turbine;a primary power system capable of supplying electricity to said motor/generator for operation in a motor mode and capable of receiving electricity which is generated by said motor/generator in a generator mode;an air compressor drivingly attached to said air turbine and said motor/generator;a ram air duct for r...