发明名称 Flapping hingeless multi-bladed rotor for rotary wing aircraft
摘要 The rotor hub plate(2) in the region of the flexible plate segments(16,18) is provided with deformation sensors(32,34) in the form of strain gauges recording the flexural movements of the blade connecting arms(4). Sensors(32A,32B) are located on the lower and upper sides of the plate to record the impact bending movements, and sensors(34A,34B) are located on the front and rear sides of the blade connecting arms to record pivotal bending movements.
申请公布号 DE19804717(A1) 申请公布日期 1999.08.19
申请号 DE19981004717 申请日期 1998.02.06
申请人 EUROCOPTER DEUTSCHLAND GMBH 发明人 BANSEMIR, HORST
分类号 B64C27/00;B64C27/32;(IPC1-7):B64C27/33;B64C27/35 主分类号 B64C27/00
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