发明名称 Fuel leakage detecting method for e.g. four-jet engine aircraft, involves determining surplus consumption ratio of engine having high consumption with respect to other engines and triggering alarm when surplus consumption is due to leakage
摘要 #CMT# #/CMT# The method involves determining the fuel consumption of each of the engines of an aircraft, comparing the consumption of each engine with the other engines and detecting the engine that has a high fuel consumption. The surplus consumption ratio of the detected engine is determined with respect to the other engines. The surplus consumption is verified to find if the consumption is due to a leakage and an alarm is triggered using an alarm triggering circuit (5) if the consumption is due to the leakage. #CMT# : #/CMT# Independent claims are also included for the following: (1) a system for detecting fuel leakage in an engine of a multi-engine type aircraft (2) a multi-engine type aircraft comprising a fuel leakage detecting system. #CMT#USE : #/CMT# Used for detecting fuel leakage in an engine of a multi-engine type aircraft (claimed) e.g. four-jet engine aircraft. #CMT#ADVANTAGE : #/CMT# The method detects the presence of leakages in the upstream of a flowmeter and identifies the leaking engine. #CMT#DESCRIPTION OF DRAWINGS : #/CMT# The drawing shows an electronic circuit for triggering an alarm. 5 : Alarm triggering circuit 38, 48 : Inputs 52 : Comparator 56 : OR logic gate `(Drawing contains non-English language text)`.
申请公布号 FR2887226(A1) 申请公布日期 2006.12.22
申请号 FR20050051696 申请日期 2005.06.21
申请人 AIRBUS FRANCE SOCIETE PAR ACTIONS SIMPLIFIEE 发明人 RIVOT JEAN LUC
分类号 B64D37/32 主分类号 B64D37/32
代理机构 代理人
主权项
地址