AIRCRAFT ENVIRONMENT CONDITIONING SYSTEM AND METHOD FOR OPERATING THE SAME

Japanese Patent JP2016026950

A

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

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WILLIAM H LUKENS
LYUNN M ROG
PAUL M D ORLANDO
FRANCESCO A DEVITA
JOHN T GATZURAS
WILLIAM D HOYT

JP2015094111A

February 18, 2016

May 01, 2015

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HAMILTON SUNDSTRAND CORP

B64D13/02; B64D25/00; B64D45/00; F02C1/05

JPH06312698A	1994-11-08
JP2001294028A	2001-10-23
JPH08240406A	1996-09-17
JP2010203433A	2010-09-16
JP2006231974A	2006-09-07
JP2005067356A	2005-03-17
JP2005014745A	2005-01-20
JP2004090778A	2004-03-25
JP2002515113A	2002-05-21

US20040231350A1	2004-11-25
US20030042362A1	2003-03-06
US5586065A	1996-12-17
US5461882A	1995-10-31
US4430867A	1984-02-14

Hiromichi Kobayashi
Tomioka Kiyoshi

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