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1. 发明授权

US07938224B2 Coating for acoustic treatment integrating the function of frost treatment with hot air 有权
标题翻译：用于结合霜冻处理与热空气功能的声学处理涂层
公开(公告)号：US07938224B2
公开(公告)日：2011-05-10
申请号：US12528007
申请日：2008-02-14
申请人： Valerie Frustie , Bernard Duprieu , Fabrice Gantie
发明人： Valerie Frustie , Bernard Duprieu , Fabrice Gantie
IPC分类号： B64D33/02
CPC分类号： B64D33/02 , B64D2033/0206 , B64D2033/0286 , F02C7/045 , F02C7/047 , F05D2250/283 , F05D2260/96
摘要： A coating for acoustic treatment relative to an aircraft's surface, in particular a leading edge such as an air intake of an aircraft nacelle, includes an acoustically resistive layer, at least one alveolar structure (30), and a reflective layer. The alveolar structure (30) includes a number of tubes that empty out, on the one hand, at a first imaginary surface (34), and, on the other hand, at a second imaginary surface (36). The alveolar structure (30) includes cut-outs or openings (38) made at the side walls of certain tubes that make it possible to link adjacent tubes so as to create a network of communicating tubes that isolate at least one tube or a group of non-communicating tubes, whereby at least one of the communicating tubes is connected to at least one hot gas intake (40).
摘要翻译：用于相对于飞行器表面，特别是诸如飞机机舱的进气口的前缘的声学处理的涂层包括声阻层，至少一个肺泡结构（30）和反射层。肺泡结构（30）包括多个管，一方面在第一假想表面（34）处，另一方面在第二假想表面（36）处排空。肺泡结构（30）包括在某些管的侧壁处制成的切口或开口（38），使得可以连接相邻的管，以便形成连通管的网络，其隔离至少一个管或一组非连通管，其中至少一个连通管连接到至少一个热气体进口（40）。

2. 发明授权

US07971684B2 Acoustic panel 有权
标题翻译：声学面板
公开(公告)号：US07971684B2
公开(公告)日：2011-07-05
申请号：US12528017
申请日：2008-02-19
申请人： Fabrice Gantie , Bernard Duprieu , Valerie Frustie , Alain Porte , Thomas Gilles , Jacques Lalane
发明人： Fabrice Gantie , Bernard Duprieu , Valerie Frustie , Alain Porte , Thomas Gilles , Jacques Lalane
IPC分类号： E04B1/82
CPC分类号： G10K11/172 , F02C7/24 , F02K1/827 , G10K11/168
摘要： A panel for acoustic treatment connected to a surface of an aircraft, includes—from the outside to the inside—an acoustically resistive porous layer, at least one alveolar structure, and a reflective or impermeable layer, whereby the acoustically resistive porous layer includes—at the outside surface that can be in contact with the aerodynamic flows—one sheet or piece of sheet metal including open zones (14) that allow sound waves to pass and filled zones (16) that do not allow sound waves to pass, characterized in that the sheet or piece of sheet metal of the acoustically resistive layer includes sets of microperforations (18), whereby each set of microperforations forms an open zone (14), the sets of microperforations being separated from one another by at least one series of bands separated by filled zones (16).
摘要翻译：连接到飞行器表面的用于声学处理的面板包括从外部到内部的声阻多孔层，至少一个肺泡结构以及反射或不可渗透层，其中所述声阻多孔层包括可以与气动流动接触的外表面 - 包括允许声波通过并且不允许声波通过的区域（16）的开放区域（14）的一片或片状金属片，其特征在于，阻声层的片状物或片状物包括一组微穿孔（18），由此每组微穿孔形成开放区域（14），所述微穿孔组彼此分开至少一系列带分离通过填充区（16）。

3. 发明授权

US08065899B2 Advanced feed device for a superplastic press forming system 有权
标题翻译：用于超塑性压制成型系统的先进进料装置
公开(公告)号：US08065899B2
公开(公告)日：2011-11-29
申请号：US12419673
申请日：2009-04-07
申请人： Valerie Frustie
发明人： Valerie Frustie
IPC分类号： B21B45/02 , B21D37/16
CPC分类号： B21D37/14 , B21D26/055 , Y10S72/709
摘要： A feed device for a superplastic press-forming press has a slide that moves vertically and a base between which is held a tool having a cover and a bottom die enclosing a forming tool, which includes at least one heating shuttle to transport the bottom die, equipped with the forming tool and a cover, with the heating shuttle adapted to complete the press and constitute the base of the press during a hot-press forming operation.
摘要翻译：用于超塑性压制成型压力机的进料装置具有垂直移动的滑动件和保持具有盖的工具的底座和封闭成形工具的底模，该成型工具包括至少一个用于输送底模的加热梭，装有成形工具和盖子，加热梭适于在热压成形操作期间完成压机并构成压机的基座。

4. 发明申请

US20100096213A1 COATING FOR ACOUSTIC TREATMENT HAVING A HOT AIR ICING PROCESSING FUNCTION OF FROST TREATMENT WITH HOT AIR 有权
标题翻译：用于具有热空气的热处理功能的热疗处理功能的涂层
公开(公告)号：US20100096213A1
公开(公告)日：2010-04-22
申请号：US12528007
申请日：2008-02-14
申请人： Valerie Frustie , Bemard Duprieu , Fabrice Gantie
发明人： Valerie Frustie , Bemard Duprieu , Fabrice Gantie
IPC分类号： B64D33/02
CPC分类号： B64D33/02 , B64D2033/0206 , B64D2033/0286 , F02C7/045 , F02C7/047 , F05D2250/283 , F05D2260/96
摘要： A coating for acoustic treatment relative to an aircraft's surface, in particular a leading edge such as an air intake of an aircraft nacelle, includes an acoustically resistive layer, at least one alveolar structure (30), and a reflective layer. The alveolar structure (30) includes a number of tubes that empty out, on the one hand, at a first imaginary surface (34), and, on the other hand, at a second imaginary surface (36). The alveolar structure (30) includes cut-outs or openings (38) made at the side walls of certain tubes that make it possible to link adjacent tubes so as to create a network of communicating tubes that isolate at least one tube or a group of non-communicating tubes, whereby at least one of the communicating tubes is connected to at least one hot gas intake (40).
摘要翻译：用于相对于飞行器表面，特别是诸如飞机机舱的进气口的前缘的声学处理的涂层包括声阻层，至少一个肺泡结构（30）和反射层。肺泡结构（30）包括多个管，一方面在第一假想表面（34）处，另一方面在第二假想表面（36）处排空。肺泡结构（30）包括在某些管的侧壁处制成的切口或开口（38），使得可以连接相邻的管，以便形成连通管的网络，其隔离至少一个管或一组非连通管，其中至少一个连通管连接到至少一个热气体进口（40）。

5. 发明申请

US20100116587A1 ACOUSTIC PANEL 有权
标题翻译：声学面板
公开(公告)号：US20100116587A1
公开(公告)日：2010-05-13
申请号：US12528017
申请日：2008-02-19
申请人： Fabrice Gantie , Bernard Duprieu , Valerie Frustie , Alain Porte , Thomas Gilles , Jacques Lalane
发明人： Fabrice Gantie , Bernard Duprieu , Valerie Frustie , Alain Porte , Thomas Gilles , Jacques Lalane
IPC分类号： E04B1/82
CPC分类号： G10K11/172 , F02C7/24 , F02K1/827 , G10K11/168
摘要： The invention relates to a panel for an acoustic treatment at the surface of an aircraft, that comprises from the outside to the inside an acoustically resistive porous layer, at least one cellular structure and a reflective or non-permissive layer, wherein the acoustically resistive porous layer includes, at the outer surface that may contact the aerodynamic flows of a sheet or foil, open areas (14) permissive to sound waves and solid area (6) not permissive to sound waves, characterised in that the sheet or foil of the acoustically resistive layer includes sets of microperforations (18), each set of microperforations defining an open area (14), the set of microperforations being separated by at least one series of spaced bands of solid areas (16).
摘要翻译：本发明涉及一种用于在飞行器表面处进行声学处理的面板，其包括从外部到内部的声阻多孔层，至少一个蜂窝结构和反射或非允许层，其中所述声阻多孔在可能接触片材或箔片的空气动力学流动的外表面处包括允许声波的开放区域（14）和不允许声波的固体区域（6），其特征在于，声学的片材或箔片电阻层包括一组微穿孔（18），每套微穿孔限定开放区域（14），所述一组微穿孔由至少一系列间隔的固体区域（16）分隔开。

6. 发明申请

US20100089690A1 METHOD FOR MAKING AN ACOUSTIC TREATMENT COATING AND COATING THUS OBTAINED 审中-公开
标题翻译：用于制造声学处理涂层和涂层的方法
公开(公告)号：US20100089690A1
公开(公告)日：2010-04-15
申请号：US12527984
申请日：2008-02-14
申请人： Fabrice Gantie , Bernard Duprieu , Valerie Frustie , Alain Porte , Thomas Gilles , Jacques Lalane
发明人： Fabrice Gantie , Bernard Duprieu , Valerie Frustie , Alain Porte , Thomas Gilles , Jacques Lalane
IPC分类号： E04B1/82 , G06F17/50
CPC分类号： F02C7/045 , B64D2033/0206 , F02C7/047 , F05D2230/60 , F05D2250/282 , F05D2250/283 , F05D2250/32 , F05D2250/60 , F05D2250/71 , G10K11/172 , Y02T50/672
摘要： A process for the producing a coating for acoustic treatment relative to a leading edge such as an air intake of an aircraft nacelle, the coating including a reflective layer, an alveolar structure, and an acoustically resistive layer, includes:Digitizing the shape of the alveolar structure that it will have when it will be installed at the surface to be treated,Positioning in a virtual manner—so as to define their geometries—two series of bands so as to delimit a tube between, two adjacent bands of a first series, and two second adjacent bands of a second series,Cutting out each band according to their geometries defined above,Producing cut-outs in each band to allow the assembly of the bands,Assembling the bands so as to obtain an alveolar structure that has shapes that are suited to the surface to be treated.
摘要翻译：一种用于制造用于声学处理的涂层的方法，所述涂层相对于诸如飞机机舱的进气口的前缘，所述涂层包括反射层，肺泡结构和声阻层，包括：数字化肺泡的形状当它将被安装在待处理的表面时将具有的结构 - 以虚拟的方式定位 - 以便限定它们的几何 - 两个系列的带，以便在第一系列的两个相邻带之间界定管，和第二系列的两个第二相邻带，根据其上述的几何形状切割每个带，在每个带中产生切口以允许带的组装，组装条带以获得具有形状的肺泡结构适合于待处理的表面。

7. 发明申请

US20090282889A1 Advanced feed device for a superplastic press forming system 有权
标题翻译：用于超塑性压制成型系统的先进进料装置
公开(公告)号：US20090282889A1
公开(公告)日：2009-11-19
申请号：US12419673
申请日：2009-04-07
申请人： Valerie Frustie
发明人： Valerie Frustie
IPC分类号： B21D37/16
CPC分类号： B21D37/14 , B21D26/055 , Y10S72/709
摘要： A feed device for a superplastic press-forming press has a slide that moves vertically and a base between which is held a tool having a cover and a bottom die enclosing a forming tool, which includes at least one heating shuttle to transport the bottom die, equipped with the forming tool and a cover, with the heating shuttle adapted to complete the press and constitute the base of the press during a hot-press forming operation.
摘要翻译：用于超塑性压制成型压力机的进料装置具有垂直移动的滑动件和保持具有盖的工具的底座和封闭成形工具的底模，该成型工具包括至少一个用于输送底模的加热梭，装有成形工具和盖子，加热梭适于在热压成形操作期间完成压机并构成压机的基座。

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