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公开(公告)号:US07837150B2
公开(公告)日:2010-11-23
申请号:US11963014
申请日:2007-12-21
申请人: Joseph Christopher Zecca , Galdemir Cezar Botura , Brian Bobby Burkett , Claude Marc Hubert , Michael John Layland , Timothy Robert Olson , James Michael Roman
发明人: Joseph Christopher Zecca , Galdemir Cezar Botura , Brian Bobby Burkett , Claude Marc Hubert , Michael John Layland , Timothy Robert Olson , James Michael Roman
IPC分类号: B64D15/12
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 includes a first segment having a first leading edge surface that extends to a first end of the first segment. The aircraft component also includes a second segment having a second leading edge surface that extends to a second end of the second segment. The second end 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 that extends to the first end of the first segment. In addition, the second leading edge surface includes electrical resistance heating 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 between the connected first and second ends.
摘要翻译: 飞行器部件包括具有延伸到第一段的第一端的第一前缘表面的第一段。 飞行器部件还包括具有延伸到第二段的第二端的第二前缘表面的第二段。 第二端基本上与第一段的第一端相邻,并且连接到第一端。 第一前缘表面包括延伸到第一段的第一端的电阻加热。 此外,第二前缘表面包括延伸到第二段的第二端的电阻加热。 电阻加热能够在连接的第一和第二端之间的接合部的任一侧立即提供加冰保护加热。
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公开(公告)号:US20100038475A1
公开(公告)日:2010-02-18
申请号:US11963014
申请日:2007-12-21
申请人: Joseph Christopher Zecca , Galdemir Cezar Botura , Brian Bobby Burkett , Claude Marc Hubert , Michael John Layland , Timothy Robert Olson , James Michael Roman
发明人: Joseph Christopher Zecca , Galdemir Cezar Botura , Brian Bobby Burkett , Claude Marc Hubert , Michael John Layland , Timothy Robert Olson , James Michael Roman
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 includes a first segment having a first leading edge surface that extends to a first end of the first segment. The aircraft component also includes a second segment having a second leading edge surface that extends to a second end of the second segment. The second end 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 that extends to the first end of the first segment. In addition, the second leading edge surface includes electrical resistance heating 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 between the connected first and second ends.
摘要翻译: 飞行器部件包括具有延伸到第一段的第一端的第一前缘表面的第一段。 飞行器部件还包括具有延伸到第二段的第二端的第二前缘表面的第二段。 第二端基本上与第一段的第一端相邻,并且连接到第一端。 第一前缘表面包括延伸到第一段的第一端的电阻加热。 此外,第二前缘表面包括延伸到第二段的第二端的电阻加热。 电阻加热能够在连接的第一和第二端之间的接合部的任一侧立即提供加冰保护加热。
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