|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||F02C-007/26 F02C-006/08 B64D-013/06|
|미국특허분류(USC)||060/778; 060/782; 060/786|
|우선권정보||DE-10 2010 047 971 (2010-10-08)|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 1 인용 특허 : 7|
An air conditioning system in an aircraft is provided. The system comprises at least one air cycle air-conditioning pack with a compressor comprising a bleed air outlet and with a compressed-air line connected to the bleed air connection, which compressed-air line is connectable to a starter turbine for a main engine. With the use of air from a compressor of an air conditioning pack it is not necessary to switch off the air conditioning pack; bleed air removal from the auxiliary power units becomes obsolete; and, since there is no unnecessary discharge o...
1. A method for starting engine of an aircraft, comprising: closing an air conditioning valve that separates an outlet of a compressor of an air conditioning pack from a delivery air inlet for a cabin;opening a start valve that connects the output of the compressor to a starter turbine;starting the engine by conveying compressed air from the compressor to the starter turbine;when the engine has reached an operating speed, closing the start valve;opening the air conditioning valve; andsupplying bleed air from at least the engine to the compressor. 2. An e...