公开(公告)号：EP2758308B1

公开(公告)日：2017-05-31

申请号：EP12740435.8

申请日：2012-07-10

申请人： The Boeing Company

发明人： ARMATORIO, Andrew ,  BURCH, Daniel, A. ,  NUYDA, Justin ,  OLIVIER, Roland, J. ,  SHENKORU, Yared ,  LOFTIS, Richard, J.

IPC分类号： B64F5/00

CPC分类号： B64D15/14 ,  B64D15/00 ,  B64D15/12 ,  B64F5/20 ,  H05B2214/02

公开(公告)号：EP2758308A1

公开(公告)日：2014-07-30

申请号：EP12740435.8

申请日：2012-07-10

申请人： The Boeing Company

发明人： ARMATORIO, Andrew ,  BURCH, Daniel, A. ,  NUYDA, Justin ,  OLIVIER, Roland, J. ,  SHENKORU, Yared ,  LOFTIS, Richard, J.

IPC分类号： B64D15/12

CPC分类号： B64D15/14 ,  B64D15/00 ,  B64D15/12 ,  B64F5/20 ,  H05B2214/02

摘要： A system and method to apply heat to an aircraft surface are disclosed. The composite aircraft structure comprises a base comprising a plurality of resin impregnated plies 212,214,216,218,220,222), heating layer (230) adjacent the base, wherein the heating layer com prises at least one heater, an adhesive layer (240a, 240b) adjacent the heating layer, a lightning protection layer (250) adjacent the heating layer, and an exterior surface layer (260) adjacent the lightning protection layer.