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公开(公告)号：US20100109208A1
公开(公告)日：2010-05-06
申请号：US12263915
申请日：2008-11-03
IPC分类号： B29C70/44
CPC分类号： B29C70/446 , B29C33/48 , B29C70/54 , B29L2031/3076 , Y10S425/06 , Y10T29/49895 , Y10T29/49904
摘要： A multi-segment tool and tooling system for vacuum forming a composite part. A tool can include a first tool having first and second surfaces. A second tool can have an opening positioned on a first tool in a location other than the first surface or the second surface. The first tool and second tool can receive at least a portion of a preform composite. The first tool can have a vacuum barrier attached to the first surface and to the second surface encapsulating the preform composite and the second tool. A tooling system can include a first tool having a core and a base with a core extending upwards from the base. A second tool can be positioned upon the core where the core extends above the second tool. A vacuum barrier sealed to the base and the core can include a composite, the first tool and the second tool.
摘要翻译： 用于真空成型复合部件的多段工具和加工系统。 工具可以包括具有第一和第二表面的第一工具。 第二工具可以具有位于除了第一表面或第二表面之外的位置处的第一工具上的开口。 第一工具和第二工具可以容纳预制件复合材料的至少一部分。 第一工具可以具有附接到第一表面的真空阻挡层和封装预型件复合材料和第二工具的第二表面。 工具系统可以包括具有芯的第一工具和具有从基部向上延伸的芯的基部。 第二工具可以定位在芯部上，其中芯部在第二工具上方延伸。 密封到基部和芯部的真空屏障可以包括复合材料，第一工具和第二工具。
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公开(公告)号：US08394315B2
公开(公告)日：2013-03-12
申请号：US13217709
申请日：2011-08-25
IPC分类号： B29C70/44
CPC分类号： B29C70/446 , B29C33/48 , B29C70/54 , B29L2031/3076 , Y10S425/06 , Y10T29/49895 , Y10T29/49904
摘要： A multi-segment tool and tooling system for vacuum forming a composite part. A tool can include a first tool having first and second surfaces. A second tool can have an opening positioned on a first tool in a location other than the first surface or the second surface. The first tool and second tool can receive at least a portion of a preform composite. The first tool can have a vacuum barrier attached to the first surface and to the second surface encapsulating the preform composite and the second tool. A tooling system can include a first tool having a core and a base with a core extending upwards from the base. A second tool can be positioned upon the core where the core extends above the second tool. A vacuum barrier sealed to the base and the core can include a composite, the first tool and the second tool.
摘要翻译： 用于真空成型复合部件的多段工具和加工系统。 工具可以包括具有第一和第二表面的第一工具。 第二工具可以具有位于除了第一表面或第二表面之外的位置处的第一工具上的开口。 第一工具和第二工具可以容纳预制件复合材料的至少一部分。 第一工具可以具有附接到第一表面的真空阻挡层和封装预型件复合材料和第二工具的第二表面。 工具系统可以包括具有芯的第一工具和具有从基部向上延伸的芯的基部。 第二工具可以定位在芯部上，其中芯部在第二工具上方延伸。 密封到基部和芯部的真空屏障可以包括复合材料，第一工具和第二工具。
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公开(公告)号：US20140034414A1
公开(公告)日：2014-02-06
申请号：US13585533
申请日：2012-08-14
申请人： Brian Bobby Burkett , Galdermir Cezar Botura , Claude Marc Hubert , David Bert Sweet , Joseph Christopher Zecca , Timothy Robert Olson
发明人： Brian Bobby Burkett , Galdermir Cezar Botura , Claude Marc Hubert , David Bert Sweet , Joseph Christopher Zecca , Timothy Robert Olson
CPC分类号： H01C17/02 , B64D15/12 , B64D33/02 , B64D2033/0206 , B64D2033/0233 , Y10T29/49083
摘要： An electric heater (40) for integration into an acoustic panel (20) having sound-penetrating pores (30) communicating with a sound-canceling medium. The heater (40) includes an electrically conductive layer (53) with resistance-setting apertures (63) filled with sealant (73). Openings (83), which contribute to the sound-penetrating pores (30), extend through the sealant-filled apertures (63). The acoustic panel (20) can be assimilated into an aircraft component, such as a nacelle inlet lip, which requires both noise-reducing and ice-protecting features.
摘要翻译： 一种用于集成到具有与声音消除介质通信的声音穿透孔（30）的声学面板（20）的电加热器（40）。 加热器（40）包括具有填充有密封剂（73）的电阻设定孔（63）的导电层（53）。 有助于声音穿透孔（30）的开口（83）延伸穿过密封剂填充的孔（63）。 声学面板（20）可以被吸收到飞机部件中，例如机舱入口唇缘，其需要降噪和防冰特征。
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公开(公告)号：US08919494B2
公开(公告)日：2014-12-30
申请号：US13585533
申请日：2012-08-14
申请人： Brian Bobby Burkett , Galdemir Cezar Botura , Claude Marc Hubert , David Bert Sweet , Joseph Christopher Zecca , Timothy Robert Olson
发明人： Brian Bobby Burkett , Galdemir Cezar Botura , Claude Marc Hubert , David Bert Sweet , Joseph Christopher Zecca , Timothy Robert Olson
IPC分类号： E04B1/86
CPC分类号： H01C17/02 , B64D15/12 , B64D33/02 , B64D2033/0206 , B64D2033/0233 , Y10T29/49083
摘要： An electric heater (40) for integration into an acoustic panel (20) having sound-penetrating pores (30) communicating with a sound-canceling medium. The heater (40) includes an electrically conductive layer (53) with resistance-setting apertures (63) filled with sealant (73). Openings (83), which contribute to the sound-penetrating pores (30), extend through the sealant-filled apertures (63). The acoustic panel (20) can be assimilated into an aircraft component, such as a nacelle inlet lip, which requires both noise-reducing and ice-protecting features.
摘要翻译： 一种用于集成到具有与声音消除介质通信的声音穿透孔（30）的声学面板（20）的电加热器（40）。 加热器（40）包括具有填充有密封剂（73）的电阻设定孔（63）的导电层（53）。 有助于声音穿透孔（30）的开口（83）延伸穿过密封剂填充的孔（63）。 声学面板（20）可以被吸收到飞机部件中，例如机舱入口唇缘，其需要降噪和防冰特征。
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公开(公告)号：US20110308723A1
公开(公告)日：2011-12-22
申请号：US13217709
申请日：2011-08-25
CPC分类号： B29C70/446 , B29C33/48 , B29C70/54 , B29L2031/3076 , Y10S425/06 , Y10T29/49895 , Y10T29/49904
摘要： A multi-segment tool and tooling system for vacuum forming a composite part. A tool can include a first tool having first and second surfaces. A second tool can have an opening positioned on a first tool in a location other than the first surface or the second surface. The first tool and second tool can receive at least a portion of a preform composite. The first tool can have a vacuum barrier attached to the first surface and to the second surface encapsulating the preform composite and the second tool. A tooling system can include a first tool having a core and a base with a core extending upwards from the base. A second tool can be positioned upon the core where the core extends above the second tool. A vacuum barrier sealed to the base and the core can include a composite, the first tool and the second tool.
摘要翻译： 用于真空成型复合部件的多段工具和加工系统。 工具可以包括具有第一和第二表面的第一工具。 第二工具可以具有位于除了第一表面或第二表面之外的位置处的第一工具上的开口。 第一工具和第二工具可以容纳预制件复合材料的至少一部分。 第一工具可以具有附接到第一表面的真空阻挡层和封装预型件复合材料和第二工具的第二表面。 工具系统可以包括具有芯的第一工具和具有从基部向上延伸的芯的基部。 第二工具可以定位在芯部上，其中芯部在第二工具上方延伸。 密封到基部和芯部的真空屏障可以包括复合材料，第一工具和第二工具。
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公开(公告)号：US08025499B2
公开(公告)日：2011-09-27
申请号：US12263915
申请日：2008-11-03
CPC分类号： B29C70/446 , B29C33/48 , B29C70/54 , B29L2031/3076 , Y10S425/06 , Y10T29/49895 , Y10T29/49904
摘要： A multi-segment tool and tooling system for vacuum forming a composite part. A tool can include a first tool having first and second surfaces. A second tool can have an opening positioned on a first tool in a location other than the first surface or the second surface. The first tool and second tool can receive at least a portion of a preform composite. The first tool can have a vacuum barrier attached to the first surface and to the second surface encapsulating the preform composite and the second tool. A tooling system can include a first tool having a core and a base with a core extending upwards from the base. A second tool can be positioned upon the core where the core extends above the second tool. A vacuum barrier sealed to the base and the core can include a composite, the first tool and the second tool.
摘要翻译： 用于真空成型复合部件的多段工具和加工系统。 工具可以包括具有第一和第二表面的第一工具。 第二工具可以具有位于除了第一表面或第二表面之外的位置处的第一工具上的开口。 第一工具和第二工具可以容纳预制件复合材料的至少一部分。 第一工具可以具有附接到第一表面的真空阻挡层和封装预型件复合材料和第二工具的第二表面。 工具系统可以包括具有芯的第一工具和具有从基部向上延伸的芯的基部。 第二工具可以定位在芯部上，其中芯部在第二工具上方延伸。 密封到基部和芯部的真空屏障可以包括复合材料，第一工具和第二工具。
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7.发明授权Acoustic nacelle inlet lip having composite construction and an integral electric ice protection heater disposed therein 有权具有复合结构的声学舱入口唇缘和设置在其中的整体式电冰保护加热器公开(公告)号：US07923668B2
公开(公告)日：2011-04-12
申请号：US11733628
申请日：2007-04-10
CPC分类号： B64D15/12 , B64D33/02 , B64D2033/0206 , B64D2033/0233 , B64D2033/0286 , H05B3/28
摘要： An engine nacelle inlet lip includes both acoustic treatment and electric heating for ice protection. The inlet lip has a composite outer skin and a composite inner skin, with the composite outer skin having at least one integrated heater element embedded in the composite material. An acoustic cellular core positioned between the outer and inner skin acts to attenuate fan noise from the engine. Covering the outer skin and overlying the acoustic core is a perforated erosion shield having a first set of openings that pass entirely thorough its thickness. The composite outer skin includes a second set of openings such that sound waves can pass from an inner barrel portion of the inlet lip through the erosion shield, outer skin, and heater element to the underlying acoustic cellular core.
摘要翻译： 发动机舱入口唇缘包括用于防冰的声学处理和电加热。 入口唇缘具有复合外皮和复合内皮，其中复合外皮具有嵌入复合材料中的至少一个集成加热元件。 定位在外皮和内皮之间的声音芯体用于衰减来自发动机的风扇噪音。 覆盖外皮并覆盖声芯是穿孔侵蚀屏蔽，其具有完全穿过其厚度的第一组开口。 复合外皮包括第二组开口，使得声波可以从入口唇缘的内筒部分通过侵蚀屏蔽件，外皮和加热器元件传递到下面的声波细胞芯。
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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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