发明名称 Load-reduction system for reducing load acting on fuselage of e.g. aircraft, includes at least one control unit which modifies amplitude characteristics and/or phase characteristics of loads acting on fuselage of aircraft
摘要 <p>#CMT# #/CMT# The system includes at least one control unit (11) which modifies the amplitude characteristics and/or phase characteristics of loads acting on the fuselage (5) of the aircraft (2) by regulating the ailerons (24-27) and the rudder (28) of the aircraft, through at least one actuators and based on the reduced load, such that the load acting on the fuselage reduces. #CMT# : #/CMT# The loads acting on the fuselage are detected by at least one sensor (6). The sensor can be e.g. strain gauge, extensometer, optical sensor, Bragg sensor, piezoelectric sensor, acceleration sensor, speed sensor. An independent claim is also included for a load-reduction method. #CMT#USE : #/CMT# For reducing load acting on fuselage of e.g. aircraft. #CMT#ADVANTAGE : #/CMT# Ensures reliable reduction of load acting on fuselage. #CMT#DESCRIPTION OF DRAWINGS : #/CMT# The figure shows the explanatory diagram of the load-reduction system. 2 : Aircraft 5 : Fuselage 6 : Sensor 11 : Control unit 24-27 : Ailerons 28 : Rudder.</p>
申请公布号 DE102004029196(A1) 申请公布日期 2006.01.12
申请号 DE20041029196 申请日期 2004.06.16
申请人 AIRBUS DEUTSCHLAND GMBH 发明人 ENZINGER, MICHAEL;KORDT, MICHAEL
分类号 B64C13/16 主分类号 B64C13/16
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