发明名称 AIRCRAFT ENVIRONMENT CONDITIONING SYSTEM AND METHOD FOR OPERATING THE SAME
摘要 PROBLEM TO BE SOLVED: To provide an aircraft environment conditioning system capable of detecting device failure.SOLUTION: An aircraft environment conditioning system having an air cycle machine, which decreases a temperature and a pressure of airflow including high temperature compressive air and thereby conditions the airflow, is disclosed. The air cycle machine is disposed in a housing 105 in a non-compression area of an aircraft, generates conditioned compressive air, and sends the conditioned compressive air to a compression area of the aircraft. The system further includes: vibration sensors 152, 154, 156, 158 disposed in the housing; and a controller 160 which is formed so as to respond to vibrations detected by the vibration sensors and communicates with the vibration sensors.SELECTED DRAWING: Figure 1
申请公布号 JP2016026950(A) 申请公布日期 2016.02.18
申请号 JP20150094111 申请日期 2015.05.01
申请人 HAMILTON SUNDSTRAND CORP 发明人 WILLIAM H LUKENS;LYUNN M ROG;PAUL M D'ORLANDO;FRANCESCO A DEVITA;JOHN T GATZURAS;WILLIAM D HOYT
分类号 B64D13/02;B64D25/00;B64D45/00;F02C1/05 主分类号 B64D13/02
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