HELICOPTER REDUCED VIBRATION ISOLATOR AXIAL SUPPORT STRUT
摘要
Helicopter reduced vibration axial support struts and aircraft suspension system are disclosed with at least one vibration controlling fluid containing strut. The powered struts include an outer rigid housing containing an inner rigid member and first and second variable volume fluid chambers. Fluid pressure differentials are created between the first and second variable volume fluid chambers to control motion between the strut ends. The powered fluid containing struts, support isolators, suspension systems, and methods of operation provide reduced helicopter aircraft vibrations.
申请公布号
WO2008060681(A2)
申请公布日期
2008.05.22
申请号
WO2007US68377
申请日期
2007.05.07
申请人
LORD CORPORATION;MCGUIRE, DENNIS;MILLER, LANE, R.;JOLLY, MARK, R.;BADRE-ALAM, ASKARI