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公开(公告)号：EP2219947B1
公开(公告)日：2013-02-27
申请号：EP08867872.7
申请日：2008-12-17
申请人： Goodrich Corporation , Rohr, Inc.
发明人： ZECCA, Joseph Christopher , BOTURA, Galdemir Cezar , BURKETT, Brian Bobby , HUBERT, Claude Marc , LAYLAND, Michael John , OLSON, Timothy Robert , ROMAN, James Michael
CPC分类号： B64D15/12 , B64D33/02 , B64D2033/0206 , B64D2033/0233 , F02C7/045 , F02C7/047 , F05D2250/132 , H05B3/06 , Y02T50/672 , Y10T29/49826
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公开(公告)号：EP3333081A1
公开(公告)日：2018-06-13
申请号：EP18151771.5
申请日：2008-12-17
申请人： Goodrich Corporation , Rohr, Inc.
发明人： ZECCA, Joseph Christopher , BOTURA, Galdemir Cezar , BURKETT, Brian Bobby , HUBERT, Claude Marc , LAYLAND, Michael John , OLSON, Timothy Robert , ROMAN, James Michael
CPC分类号： B64D15/12 , B64D33/02 , B64D2033/0206 , B64D2033/0233 , F02C7/045 , F02C7/047 , F05D2250/132 , H05B3/06 , Y02T50/672 , Y10T29/49826
摘要： An aircraft component (200) is disclosed which comprises a first segment (110) comprising a first exterior surface, a first end, and a first electric heater element (227) having a first edge proximate to the first end; a second segment (112) comprising a second exterior surface, a second end, and a second electric heater element (223) having a second edge proximate to the second end, wherein the second end is joined to the first end such that the first external surface and the second external surface combine to form at least a portion of a substantially continuous leading edge surface; a first bus bar connected to the first edge of the first heater element; and a second bus bar connected to the second edge of the second heater element; wherein the first and second bus bars (230) are disposed between the first end and the second end when the first end is joined to the second end.
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公开(公告)号：EP3333081B1
公开(公告)日：2019-07-17
申请号：EP18151771.5
申请日：2008-12-17
申请人： Goodrich Corporation , Rohr, Inc.
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公开(公告)号：EP2219947A2
公开(公告)日：2010-08-25
申请号：EP08867872.7
申请日：2008-12-17
申请人： Goodrich Corporation , Rohr, Inc.
发明人： ZECCA, Joseph Christopher , BOTURA, Galdemir Cezar , BURKETT, Brian Bobby , HUBERT, Claude Marc , LAYLAND, Michael John , OLSON, Timothy Robert , ROMAN, James Michael
CPC分类号： B64D15/12 , B64D33/02 , B64D2033/0206 , B64D2033/0233 , F02C7/045 , F02C7/047 , F05D2250/132 , H05B3/06 , Y02T50/672 , Y10T29/49826
摘要： An aircraft component (200) includes a first segment (110) having a first leading edge surface that extends to a first end (222) of the first segment. The aircraft component also includes a second segment (112) having a second leading edge surface that extends to a second end of the second segment. The second end (226) is substantially adjacent to the first end of the first segment, and is connected to the first end. The first leading edge surface includes electrical resistance heating (223) that extends to the first end of the first segment. In addition, the second leading edge surface includes electrical resistance heating (227) that extends to the second end of the second segment. The electrical resistance heating is capable of providing ice protection heating immediately on either side of a juncture (211) between the connected first and second ends.
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