An intercostal for an aircraft for dissipating a load from a first frame onto a second frame and/or a skin of the aircraft, the intercostal having a framework.
申请公布号
US7481398(B2)
申请公布日期
2009.01.27
申请号
US20050064661
申请日期
2005.02.24
申请人
AIRBUS DEUTSCHLAND GMBH
发明人
SCHIMMLER MARC;GRAUERHOLZ THOMAS;TUCKER ALASTAIR;KROG LARS
