公开(公告)号：US08177933B2

公开(公告)日：2012-05-15

申请号：US12856081

申请日：2010-08-13

Applicant: Alain Foucault ,  Etienne Juchauld ,  David Marsal ,  Stéphane Otin

Inventor： Alain Foucault ,  Etienne Juchauld ,  David Marsal ,  Stéphane Otin

IPC: B29C53/56 ,  B65H81/00 ,  F04D29/32

CPC classification number: B29C70/68 ,  B29L2031/08 ,  F01D5/282 ,  F01D5/34 ,  F05D2300/44 ,  F05D2300/603 ,  F05D2300/614 ,  Y02T50/672

Abstract: A first insert (15) forming a ring is placed inside and in contact with a core (10) in degradable material. On the outer face of the core a plurality of inserts (20) is arranged each comprising a platform (21) applied against the outer face of the core and at least one blade (22) extending substantially radially outwards. A fibrous structure (56) is wound around the core passing over the platforms (21) and over the inner surface of the ring-shaped insert (15). Molding of the fibrous structure, impregnated with a composition containing a resin, is performed before polymerization of the resin and removal of the core.

Abstract translation: 形成环的第一插入件（15）放置在可降解材料的内部并与芯（10）接触。 在芯的外表面上，布置有多个插入件（20），每个插入件包括施加在芯的外表面上的平台（21）和基本上径向向外延伸的至少一个叶片（22）。 纤维结构（56）缠绕在穿过平台（21）并且在环形插入件（15）的内表面上的芯上。 在树脂聚合并除去芯之前进行用含有树脂的组合物浸渍的纤维结构的成型。

公开(公告)号：US20110073717A1

公开(公告)日：2011-03-31

申请号：US12994808

申请日：2009-05-14

Applicant: Alain Foucault ,  Etienne Juchauld ,  Arnaud Pierrot ,  Stephane Rousselin

Inventor： Alain Foucault ,  Etienne Juchauld ,  Arnaud Pierrot ,  Stephane Rousselin

IPC: B64D27/24 ,  B64D27/04 ,  B64D27/02

CPC classification number: B64D27/24 ,  B64C2201/042 ,  B64D2027/026 ,  B64D2041/005 ,  B64D2211/00 ,  Y02T50/55 ,  Y02T50/64 ,  Y02T90/36 ,  Y02T90/44

Abstract: An aircraft with a hybrid power supply, the aircraft comprising: an external structure (12 to 20); electrical equipment (34); internal combustion propulsion means (40); and means for feeding energy to the propulsion means; the aircraft being characterized in that it further comprises: a plurality of converters for directly converting light energy into electrical energy (24), which converters are disposed on at least a fraction of the outside surface of the external structure; means (32) for comparing the electrical energy produced by said converters with the instantaneous consumption of said electrical equipment (34); means (36) for recovering the excess electrical energy, if any; and means (38) for delivering to said propulsion means (40) additional energy taken from said excess electrical energy, if any.

Abstract translation: 一种具有混合动力供应的飞机，该飞机包括：外部结构（12至20）; 电气设备（34）; 内燃推进装置（40）; 以及用于将能量供给推进装置的装置; 该飞机的特征在于它还包括：多个转换器，用于将光能直接转换成电能（24），这些转换器设置在外部结构的外表面的至少一部分上; 用于将由所述转换器产生的电能与所述电气设备（34）的瞬时消耗进行比较的装置（32）; 用于恢复过剩电能的装置（36）（如果有的话） 以及用于向所述推进装置（40）输送从所述多余电能（如果有的话）获取的额外能量的装置（38）。

公开(公告)号：US07685828B2

公开(公告)日：2010-03-30

申请号：US12200266

申请日：2008-08-28

Applicant: Alain Auguste Jacques Foucault ,  Etienne Juchauld ,  Arnaud Jean-Marie Pierrot ,  Stephane Rousselin

Inventor： Alain Auguste Jacques Foucault ,  Etienne Juchauld ,  Arnaud Jean-Marie Pierrot ,  Stephane Rousselin

IPC: F02C6/00

CPC classification number: F02C7/32 ,  F02C6/18 ,  Y02E20/14 ,  Y02T50/671

Abstract: A turbomachine comprising at least one Stirling cycle thermal engine which is mounted at the end of a radial arm of the exhaust casing and comprises a working chamber located outside the primary and secondary flows, a displacing piston associated with a moving element of an energy generation system, and two exchangers, heating and cooling, formed in parts of the radial arm respectively intercepting the primary flow and the secondary flow, these two exchangers communicating with each other and with the working chamber for the circulation of a working fluid.

Abstract translation: 一种涡轮机，包括至少一个斯特林循环热力发动机，其安装在排气壳体的径向臂的端部并且包括位于主流和次流之外的工作室，与能量产生系统的移动元件相关联的位移活塞 和两个交换器，加热和冷却，形成在径向臂的部分中，分别拦截一次流和二次流，这两个交换器彼此连通并与工作室连通，用于工作流体的循环。

公开(公告)号：US20090058089A1

公开(公告)日：2009-03-05

申请号：US12200266

申请日：2008-08-28

Applicant: Alain Auguste Jacques FOUCAULT ,  Etienne JUCHAULD ,  Arnaud Jean-Marie PIERROT ,  Stephane ROUSSELIN

Inventor： Alain Auguste Jacques FOUCAULT ,  Etienne JUCHAULD ,  Arnaud Jean-Marie PIERROT ,  Stephane ROUSSELIN

IPC: F02C6/00 ,  F02G1/043 ,  F01B29/10

CPC classification number: F02C7/32 ,  F02C6/18 ,  Y02E20/14 ,  Y02T50/671

Abstract: A turbomachine comprising at least one Stirling cycle thermal engine which is mounted at the end of a radial arm (36) of the exhaust casing (24) and comprises a working chamber (40) located outside the primary (B) and secondary (A) flows, a displacing piston (42) associated with a moving element (44) of an energy generation system, and two exchangers, heating (58) and cooling (62), formed in parts of the radial arm respectively intercepting the primary flow (B) and the secondary flow (A), these two exchangers (58, 62) communicating with each other and with the working chamber (40) for the circulation of a working fluid.

Abstract translation: 一种涡轮机，包括至少一个斯特林循环热力发动机，其安装在排气壳体（24）的径向臂（36）的端部，并且包括位于主要（B）和次要（A）外部的工作室（40） 与能量产生系统的移动元件（44）相关联的位移活塞（42）和形成在径向臂的部分中的两个交换器（58）和冷却（62），分别拦截主流（B） ）和二次流（A），这两个交换器（58,62）彼此连通并与工作室（40）连通，用于工作流体的循环。

公开(公告)号：US09464575B2

公开(公告)日：2016-10-11

申请号：US14240889

申请日：2012-08-22

Applicant: Etienne Juchauld ,  Jean-Pierre Badinier ,  Jean Pierre Roberdeau ,  Marc Serrau

Inventor： Etienne Juchauld ,  Jean-Pierre Badinier ,  Jean Pierre Roberdeau ,  Marc Serrau

IPC: F02C7/264 ,  F23Q3/00 ,  F02C7/266

CPC classification number: F02C7/264 ,  F02C7/266 ,  F23Q3/002 ,  F23Q3/008 ,  F23R2900/00

Abstract: A method and device for igniting a turbomachine combustion chamber including alternately: an intake phase of a fluid into a chamber through an intake port, during which a piston compresses an elastic mechanism under pressure of the fluid such that the elastic mechanism applies onto a piezoelectric element a force sufficient for the piezoelectric element to induce between the electrodes an electric voltage enabling an electric arc to be generated, until the piston reaches a predetermined position for closing a valve for sealing the intake port; and an exhaust phase of the fluid, during which the elastic mechanism pushes back the piston to induce a fluid ejection out of the chamber through an exhaust port, and the valve is open.

Abstract translation: 一种用于点燃涡轮机燃烧室的方法和装置，其包括：通过进气口将流体进入腔室的进气相，在该进气口期间，活塞在压力下压缩弹性机构，使得弹性机构施加到压电元件 足以使压电元件在电极之间产生能够产生电弧的电压，直到活塞到达用于封闭用于密封进气口的阀的预定位置; 以及流体的排气相，在此期间弹性机构推回活塞以通过排气口将流体喷射出室，并且阀打开。

公开(公告)号：US20140216052A1

公开(公告)日：2014-08-07

申请号：US14240889

申请日：2012-08-22

Applicant: Etienne Juchauld ,  Jean-Pierre Badinier ,  Jean Pierre Roberdeau ,  Marc Serrau

Inventor： Etienne Juchauld ,  Jean-Pierre Badinier ,  Jean Pierre Roberdeau ,  Marc Serrau

IPC: F02C7/264

CPC classification number: F02C7/264 ,  F02C7/266 ,  F23Q3/002 ,  F23Q3/008 ,  F23R2900/00

Abstract: A method and device for igniting a turbomachine combustion chamber including alternately: an intake phase of a fluid into a chamber through an intake port, during which a piston compresses an elastic mechanism under pressure of the fluid such that the elastic mechanism applies onto a piezoelectric element a force sufficient for the piezoelectric element to induce between the electrodes an electric voltage enabling an electric arc to be generated, until the piston reaches a predetermined position for closing a valve for sealing the intake port; and an exhaust phase of the fluid, during which the elastic mechanism pushes back the piston to induce a fluid ejection out of the chamber through an exhaust port, and the valve is open.

Abstract translation: 一种用于点燃涡轮机燃烧室的方法和装置，其包括：通过进气口将流体进入腔室的进气相，在该进气口期间，活塞在压力下压缩弹性机构，使得弹性机构施加到压电元件 足以使压电元件在电极之间产生能够产生电弧的电压，直到活塞到达用于封闭用于密封进气口的阀的预定位置; 以及流体的排气相，在此期间弹性机构推回活塞以通过排气口将流体喷射出室，并且阀打开。

公开(公告)号：US20110048620A1

公开(公告)日：2011-03-03

申请号：US12856081

申请日：2010-08-13

Applicant: Alain FOUCAULT ,  Etienne Juchauld ,  David Marsal ,  Stéphane Otin

Inventor： Alain FOUCAULT ,  Etienne Juchauld ,  David Marsal ,  Stéphane Otin

IPC: B29C53/60

CPC classification number: B29C70/68 ,  B29L2031/08 ,  F01D5/282 ,  F01D5/34 ,  F05D2300/44 ,  F05D2300/603 ,  F05D2300/614 ,  Y02T50/672

Abstract: A first insert (15) forming a ring is placed inside and in contact with a core (10) in degradable material. On the outer face of the core a plurality of inserts (20) is arranged each comprising a platform (21) applied against the outer face of the core and at least one blade (22) extending substantially radially outwards. A fibrous structure (56) is wound around the core passing over the platforms (21) and over the inner surface of the ring-shaped insert (15). Moulding of the fibrous structure, impregnated with a composition containing a resin, is performed before polymerization of the resin and removal of the core.

Abstract translation: 形成环的第一插入件（15）放置在可降解材料的内部并与芯（10）接触。 在芯的外表面上，布置有多个插入件（20），每个插入件包括施加在芯的外表面上的平台（21）和基本上径向向外延伸的至少一个叶片（22）。 纤维结构（56）缠绕在穿过平台（21）并且在环形插入件（15）的内表面上的芯上。 在树脂聚合并除去芯之前进行用含有树脂的组合物浸渍的纤维结构的成型。