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1.
公开(公告)号:US20060273221A1
公开(公告)日:2006-12-07
申请号:US11397208
申请日:2006-04-04
申请人: Kirk Olsen , Gerald Whiteford , Pat Sheridan , Scott Thompson
发明人: Kirk Olsen , Gerald Whiteford , Pat Sheridan , Scott Thompson
IPC分类号: B64D41/00
CPC分类号: B64D41/00 , B64D2041/002 , Y10T29/49826
摘要: The invention provides an aircraft with an auxiliary power unit isolated from the aircraft. An auxiliary power unit suspension system includes at least one suspension linkage. The suspension linkage terminates with a first low stiffness elastomeric rod end. The low stiffness elastomeric rod end has a low spring rate with the aircraft auxiliary power unit suspension system providing the aircraft auxiliary power unit with a suspended auxiliary power unit natural frequency, the suspended auxiliary power unit natural frequency below the aircraft auxiliary power unit operation frequency.