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公开(公告)号：US09341142B2
公开(公告)日：2016-05-17
申请号：US13770653
申请日：2013-02-19
Applicant: AIRCELLE
Inventor： Alexandre Bellanger , Florent Bouillon , Laurent Dubois
CPC classification number: F02K1/72 , B64D29/06 , F02K1/80 , F05D2300/44 , F05D2300/603 , F05D2300/612 , F05D2300/614 , Y02T50/672
Abstract: The present disclosure relates to a beam, in particular for a cascade thrust reverser, including a skin made of a composite material and defining a closed section, wherein said beam is filled with a core material.
Abstract translation: 本公开涉及一种梁，特别是用于级联推力反向器的梁，包括由复合材料制成并限定封闭部分的表皮，其中所述梁填充有芯材料。
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公开(公告)号：US09109509B2
公开(公告)日：2015-08-18
申请号：US13671233
申请日：2012-11-07
Applicant: AIRCELLE
Inventor： Christophe Thorel , Bertrand Desjoyeaux , Florent Bouillon , John Moutier , Stéphane Bardin
CPC classification number: F02C7/04 , B64D29/06 , F02C7/045 , F02K1/80 , F02K1/827 , Y02T50/672 , Y10T29/49826 , Y10T403/45
Abstract: A unit for an aircraft thruster is provided that includes a first ferrule configured to be attached to a second ferrule and a first connection flange configured to be secured to a second corresponding connection flange secured to the second ferrule. The connection flange includes a portion forming a plane extending along a radial direction with respect to the first ferrule. A link between the first ferrule and the corresponding connection flange is offset to a distance from said plane corresponding to a length for damping a shear-generating flexural moment, generated by fluxes of forces passing through the first ferrule.
Abstract translation: 提供了一种用于飞机推进器的单元，其包括构造成附接到第二套圈的第一套圈和构造成固定到固定到第二套圈的第二对应连接凸缘的第一连接凸缘。 连接凸缘包括形成相对于第一套圈沿径向方向延伸的平面的部分。 第一套圈和对应的连接凸缘之间的连接偏移到与所述平面相对应的距离，该长度与用于阻尼通过第一套圈的力的通量产生的剪切产生弯曲力矩的长度相对应。
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公开(公告)号：US09010681B2
公开(公告)日：2015-04-21
申请号：US13662905
申请日：2012-10-29
Applicant: Aircelle
Inventor： Alexandre Bellanger , Florent Bouillon , Laurent Dubois
IPC: B64D29/06
CPC classification number: B64D29/06
Abstract: A supporting half-structure for an aircraft engine nacelle is provided that includes at least one longitudinal beam and a front half-frame, the beam and the half-frame being formed of composite materials. The half frame has an open section, and the half-structure defines a structure selected from the group consisting of: the beam and the front half-frame form a one-piece part; the beam has an extension with an open section, the shape of which matches that of the front half-frame, the extension being attached to the half frame; and the front half-frame has an extension with an open shape, the shape of which matches the beam, wherein the extension is attached to the beam.
Abstract translation: 提供了一种用于飞机发动机机舱的支撑半结构，其包括至少一个纵向梁和前半框架，梁和半框架由复合材料形成。 半框架具有开口部分，并且半结构限定了从由以下组成的组中选择的结构：梁和前半框架形成一体式部件; 梁具有开口部分的延伸部分，其形状与前半框架的形状相匹配，延伸部分附接到半框架; 并且前半框架具有开口形状的延伸部，其形状与梁的形状相匹配，其中延伸部附接到梁上。
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Patent Agency Ranking
公开(公告)号：US20130315657A1
公开(公告)日：2013-11-28
申请号：US13671233
申请日：2012-11-07
Applicant: AIRCELLE
Inventor： Christophe Thorel , Bertrand Desjoyeaux , Florent Bouillon , John Moutier , Stéphane Bardin
IPC: F02C7/04
CPC classification number: F02C7/04 , B64D29/06 , F02C7/045 , F02K1/80 , F02K1/827 , Y02T50/672 , Y10T29/49826 , Y10T403/45
Abstract: A unit for an aircraft thruster is provided that includes a first ferrule configured to be attached to a second ferrule and a first connection flange configured to be secured to a second corresponding connection flange secured to the second ferrule. The connection flange includes a portion forming a plane extending along a radial direction with respect to the first ferrule. A link between the first ferrule and the corresponding connection flange is offset to a distance from said plane corresponding to a length for damping a shear-generating flexural moment, generated by fluxes of forces passing through the first ferrule.
Abstract translation: 提供了一种用于飞机推进器的单元，其包括构造成附接到第二套圈的第一套圈和构造成固定到固定到第二套圈的第二对应连接凸缘的第一连接凸缘。 连接凸缘包括形成相对于第一套圈沿径向方向延伸的平面的部分。 第一套圈和对应的连接凸缘之间的连接偏移到与所述平面相对应的距离，该长度与用于阻尼通过第一套圈的力的通量产生的剪切产生弯曲力矩的长度相对应。
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公开(公告)号：US20130062462A1
公开(公告)日：2013-03-14
申请号：US13662905
申请日：2012-10-29
Applicant: AIRCELLE
Inventor： Alexandre Bellanger , Florent Bouillon , Laurent Dubois
CPC classification number: B64D29/06
Abstract: A supporting half-structure for an aircraft engine nacelle is provided that includes at least one longitudinal beam and a front half-frame, the beam and the half-frame being formed of composite materials. The half frame has an open section, and the half-structure defines a structure selected from the group consisting of: the beam and the front half-frame form a one-piece part; the beam has an extension with an open section, the shape of which matches that of the front half-frame, the extension being attached to the half frame; and the front half-frame has an extension with an open shape, the shape of which matches the beam, wherein the extension is attached to the beam.
Abstract translation: 提供了一种用于飞机发动机机舱的支撑半结构，其包括至少一个纵向梁和前半框架，梁和半框架由复合材料形成。 半框架具有开口部分，并且半结构限定了从由以下组成的组中选择的结构：梁和前半框架形成一体式部件; 梁具有开口部分的延伸部分，其形状与前半框架的形状相匹配，延伸部分附接到半框架; 并且前半框架具有开口形状的延伸部，其形状与梁的形状相匹配，其中延伸部附接到梁上。
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6.发明申请LEADING EDGE STRUCTURE, IN PARTICULAR FOR AN AIR INLET OF AN AIRCRAFT ENGINE NACELLE 审中-公开引擎边缘结构，特别是飞机发动机空气入口公开(公告)号：US20130230390A1
公开(公告)日：2013-09-05
申请号：US13872325
申请日：2013-04-29
Applicant: AIRCELLE
Inventor： Florent Bouillon , Caroline Coat
IPC: F01D25/02
CPC classification number: F01D25/02 , B29C70/24 , B29C70/88 , B29K2995/0013 , B64D33/02 , B64D2033/0233 , B64D2033/0286 , Y02T50/43
Abstract: A leading edge structure for an air inlet of an aircraft nacelle includes a leading edge and an inner partition defining a longitudinal compartment that is located inside the leading edge and accommodates a de-icing and/or anti-icing mat. The leading edge structure includes a multi-axial composite structure placed on top of a heating element for anti-icing and/or de-icing.
Abstract translation: 用于飞机机舱的空气入口的前缘结构包括前缘和内部分隔板，其限定位于前缘内部并容纳除冰和/或防冰垫的纵向隔室。 前缘结构包括放置在用于防冰和/或除冰的加热元件顶部的多轴复合结构。
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公开(公告)号：US20130161415A1
公开(公告)日：2013-06-27
申请号：US13770653
申请日：2013-02-19
Applicant: AIRCELLE
Inventor： Alexandre Bellanger , Florent Bouillon , Laurent Dubois
IPC: B64D29/06
CPC classification number: F02K1/72 , B64D29/06 , F02K1/80 , F05D2300/44 , F05D2300/603 , F05D2300/612 , F05D2300/614 , Y02T50/672
Abstract: The present disclosure relates to a beam, in particular for a cascade thrust reverser, including a skin made of a composite material and defining a closed section, wherein said beam is filled with a core material.
Abstract translation: 本公开涉及一种梁，特别是用于级联推力反向器的梁，包括由复合材料制成并限定封闭部分的表皮，其中所述梁填充有芯材料。
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公开(公告)号：US20130062461A1
公开(公告)日：2013-03-14
申请号：US13662886
申请日：2012-10-29
Applicant: Aircelle
Inventor： Alexandre BELLANGER , Florent Bouillon , Laurent Dubois , Emmanuel Anfray
CPC classification number: B64D29/06
Abstract: A supporting half-structure for an aircraft engine nacelle is provided that includes at least one longitudinal beam and a front half-frame connected to each other and formed at least partly in composite materials. The half-structure includes a connecting hinge positioned in a junction area of the longitudinal beam and of the half-frame, the hinge being formed by composite materials laid out so that fibres of the composite materials are positioned in alignment with fibres of composite materials forming said front half-frame.
Abstract translation: 提供了一种用于飞机发动机机舱的支撑半结构，其包括至少一个纵向梁和彼此连接并且至少部分地形成复合材料的前半框架。 半结构包括位于纵向梁和半框架的接合区域中的连接铰链，铰链由复合材料形成，复合材料布置成使得复合材料的纤维与复合材料的纤维成对准 前半帧说
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