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1. 发明申请

US20110133025A1 ACOUSTIC ATTENUATION PANEL FOR AIRCRAFT FOR ENGINE NACELLE 有权
标题翻译：用于发动机空调的航空器衰减面板
公开(公告)号：US20110133025A1
公开(公告)日：2011-06-09
申请号：US13056822
申请日：2009-07-28
申请人： Guy Bernard Vauchel , Guillaume Ruckert
发明人： Guy Bernard Vauchel , Guillaume Ruckert
IPC分类号： B64C1/40 , B64D33/02 , B64D15/16
CPC分类号： F02C7/045 , B64D33/02 , B64D2033/0206 , B64D2033/0233 , B64D2033/0286 , F02C7/047 , F02C7/24 , F02K1/827 , F05D2300/224 , F05D2300/612 , Y02T50/672
摘要： This acoustic attenuation panel for an aircraft engine nacelle comprises a structuring skin (1) and, by way of acoustic absorption material, a porous material (5) attached to this skin (1).
摘要翻译：用于飞机发动机机舱的声衰减面板包括结构化皮肤（1），并且通过吸声材料，附着到该皮肤（1）上的多孔材料（5）。

2. 发明授权

US08899512B2 Acoustic attenuation panel for aircraft for engine nacelle 有权
标题翻译：用于发动机舱的飞机的声衰减面板
公开(公告)号：US08899512B2
公开(公告)日：2014-12-02
申请号：US13056822
申请日：2009-07-28
申请人： Guy Bernard Vauchel , Guillaume Ruckert
发明人： Guy Bernard Vauchel , Guillaume Ruckert
IPC分类号： B64C1/40 , B64D15/00 , F02K1/82 , F02C7/045 , F02C7/24 , F02C7/047 , B64D33/02
CPC分类号： F02C7/045 , B64D33/02 , B64D2033/0206 , B64D2033/0233 , B64D2033/0286 , F02C7/047 , F02C7/24 , F02K1/827 , F05D2300/224 , F05D2300/612 , Y02T50/672
摘要： An aircraft turbojet engine air intake structure includes an air intake lip provided with a first acoustic attenuation panel which contains a structuring skin and, as an acoustic absorption material, a porous material fastened on the skin. The air intake structure also includes a pneumatic de-icing compartment defined by the lip and by an inner partition. The first acoustic attenuation panel is of the type including an open-cell porous material which is capable of resisting a temperature of up to 200° C. and having high heat conductivity.
摘要翻译：飞机涡轮喷气发动机进气结构包括设置有第一声衰减板的进气口，该第一声衰减板包含结构化皮肤，以及作为吸声材料，紧固在皮肤上的多孔材料。进气结构还包括由唇缘和内隔板限定的气动除冰室。第一声衰减板是包括能够耐受高达200℃的温度并具有高导热性的开孔多孔材料的类型。

3. 发明授权

US08840059B2 Assembly of components connected by a device that maintains the integrity of the surface of one of the components 有权
标题翻译：通过维持组件之一的表面的完整性的装置连接的组件的组装
公开(公告)号：US08840059B2
公开(公告)日：2014-09-23
申请号：US13056727
申请日：2009-07-28
申请人： Guy Bernard Vauchel , Guillaume Ruckert
发明人： Guy Bernard Vauchel , Guillaume Ruckert
IPC分类号： F02B27/00 , F02C7/20 , B64D33/02 , F02C7/047 , B64D15/04 , F02C7/045
CPC分类号： B64D33/02 , B64D15/04 , B64D2033/0206 , B64D2033/0233 , B64D2033/0286 , F02C7/045 , F02C7/047 , F05D2260/96 , Y02T50/672 , Y10T137/0536 , Y10T428/12479 , Y10T428/24149 , Y10T428/24322 , Y10T428/249953 , Y10T428/24997 , Y10T428/249976 , Y10T428/249982 , Y10T442/59
摘要： This assembly comprises a first component (9), a second component (3), and a connecting device (19) for connecting these two components together, this device (19) being of the type that maintains the integrity of the surface of said second component (3), and the assembly being noteworthy in that said connecting device (19) comprises a structural skin (21) fixed to said first component (9) and a porous material (23) attached to this structural skin and fixed by contact to said second component (3).
摘要翻译：该组件包括第一部件（9），第二部件（3）和用于将这两个部件连接在一起的连接装置（19），该装置（19）是保持所述第二部件组件（3），并且组件是值得注意的，因为所述连接装置（19）包括固定到所述第一部件（9）的结构皮肤（21）和附接到该结构皮肤上的多孔材料（23），并通过接触固定所述第二组分（3）。

4. 发明申请

US20110131945A1 ASSEMBLY OF COMPONENTS CONNECTED BY A DEVICE THAT MAINTAINS THE INTEGRITY OF THE SURFACE OF ONE OF THE COMPONENTS 有权
标题翻译：组装与保持组成部分之一的完整性的设备连接的组件
公开(公告)号：US20110131945A1
公开(公告)日：2011-06-09
申请号：US13056727
申请日：2009-07-28
申请人： Guy Bernard Vauchel , Guillaume Ruckert
发明人： Guy Bernard Vauchel , Guillaume Ruckert
IPC分类号： F02G3/00 , B32B3/26 , B32B5/02 , B32B5/24 , B32B5/18 , B32B3/10 , B32B7/12 , B32B3/12
CPC分类号： B64D33/02 , B64D15/04 , B64D2033/0206 , B64D2033/0233 , B64D2033/0286 , F02C7/045 , F02C7/047 , F05D2260/96 , Y02T50/672 , Y10T137/0536 , Y10T428/12479 , Y10T428/24149 , Y10T428/24322 , Y10T428/249953 , Y10T428/24997 , Y10T428/249976 , Y10T428/249982 , Y10T442/59
摘要： This assembly comprises a first component (9), a second component (3), and a connecting device (19) for connecting these two components together, this device (19) being of the type that maintains the integrity of the surface of said second component (3), and the assembly being noteworthy in that said connecting device (19) comprises a structural skin (21) fixed to said first component (9) and a porous material (23) attached to this structural skin and fixed by contact to said second component (3).
摘要翻译：该组件包括第一部件（9），第二部件（3）和用于将这两个部件连接在一起的连接装置（19），该装置（19）是保持所述第二部件组件（3），并且组件是值得注意的，因为所述连接装置（19）包括固定到所述第一部件（9）的结构皮肤（21）和附接到该结构皮肤上的多孔材料（23），并通过接触固定所述第二组分（3）。

5. 发明申请

US20110254196A1 METHOD FOR MAKING AN ACOUSTIC ATTENTUATION PANEL, IN PARTICULAR FOR AERONAUTICS 审中-公开
标题翻译：用于制造声学特性面板的方法，特别是用于气象
公开(公告)号：US20110254196A1
公开(公告)日：2011-10-20
申请号：US13141333
申请日：2009-08-26
申请人： Guy Bernard Vauchel , Guillaume Ruckert
发明人： Guy Bernard Vauchel , Guillaume Ruckert
IPC分类号： B29C71/02
CPC分类号： B29C70/443 , B29C70/086 , B29C70/34 , B29C70/545 , B29D99/0021 , B29K2105/043 , G10K11/168
摘要： The invention relates to a method for making an acoustic attenuation panel, comprising using at least one foam block (1), coating at least the acoustic surface of said foam block (1) with a fresh composite material (9), and making perforations (27; 27a, 27b, 27c, 27d, 27e) in the resulting coating.
摘要翻译：本发明涉及一种制造声衰减面板的方法，包括使用至少一个泡沫块（1），至少用所述泡沫块（1）的声表面涂覆新鲜的复合材料（9），并使穿孔（ 27; 27a，27b，27c，27d，27e）。

6. 发明授权

US08640825B2 Acoustic panel for an ejector nozzle 有权
标题翻译：用于喷射器喷嘴的声学面板
公开(公告)号：US08640825B2
公开(公告)日：2014-02-04
申请号：US13000720
申请日：2009-05-14
申请人： Guy Bernard Vauchel , Emmanuel Drevon , Patrick Gonidec , Guillaume Ruckert , Eric Conete , Renaud Barreteau
发明人： Guy Bernard Vauchel , Emmanuel Drevon , Patrick Gonidec , Guillaume Ruckert , Eric Conete , Renaud Barreteau
IPC分类号： E04B1/84
CPC分类号： G10K11/172 , B64D33/06 , F02K1/827 , F02K3/06 , F05D2300/501 , Y02T50/672
摘要： The invention relates to an acoustic panel (20) for an ejector nozzle (10) comprising the following main components: an external skin (22) containing acoustic holes (29); an internal skin (23); an acoustic structure (21) comprising alveolar-core cells (27) between the internal skin (23) and the external skin (22). At least one main component selected from the external skin (22), the internal skin (23) and the acoustic structure (21) is formed by a composite material and the acoustic structure (21) is held in contact with either or both of the internal (23) and external (22) skins by compression by elastic means and/or by fixing by mechanical fixing means (24). The invention also relates to an injector nozzle (10) and a nacelle (1) comprising such an acoustic panel (20).
摘要翻译：本发明涉及一种用于喷射器喷嘴（10）的声学面板（20），其包括以下主要部件：包含声孔（29）的外部皮肤（22）; 内部皮肤（23）; 在所述内部皮肤（23）和所述外部皮肤（22）之间包括肺泡细胞（27）的声学结构（21）。从外部皮肤（22），内部皮肤（23）和声音结构（21）中选择的至少一个主要部件由复合材料形成，声学结构（21）保持与内部（23）和外部（22）表面通过弹性装置压缩和/或通过机械固定装置（24）固定。本发明还涉及一种喷射器喷嘴（10）和包括这种声学面板（20）的机舱（1）。

7. 发明申请

US20110108357A1 ACOUSTIC PANEL FOR AN EJECTOR NOZZLE 有权
标题翻译：用于喷嘴喷嘴的声学面板
公开(公告)号：US20110108357A1
公开(公告)日：2011-05-12
申请号：US13000720
申请日：2009-05-14
申请人： Guy Bernard Vauchel , Emmanuel Drevon , Patrick Gonidec , Guillaume Ruckert , Eric Conete , Renaud Barreteau
发明人： Guy Bernard Vauchel , Emmanuel Drevon , Patrick Gonidec , Guillaume Ruckert , Eric Conete , Renaud Barreteau
IPC分类号： F02K1/82 , F01N1/24
CPC分类号： G10K11/172 , B64D33/06 , F02K1/827 , F02K3/06 , F05D2300/501 , Y02T50/672
摘要： The invention relates to an acoustic panel (20) for an ejector nozzle (10) comprising the following main components: an external skin (22) containing acoustic holes (29); an internal skin (23); an acoustic structure (21) comprising alveolar-core cells (27) between the internal skin (23) and the external skin (22). At least one main component selected from the external skin (22), the internal skin (23) and the acoustic structure (21) is formed by a composite material and the acoustic structure (21) is held in contact with either or both of the internal (23) and external (22) skins by compression by elastic means and/or by fixing by mechanical fixing means (24). The invention also relates to an injector nozzle (10) and a nacelle (1) comprising such an acoustic panel (20).
摘要翻译：本发明涉及一种用于喷射器喷嘴（10）的声学面板（20），其包括以下主要部件：包含声孔（29）的外部皮肤（22）; 内部皮肤（23）; 在所述内部皮肤（23）和所述外部皮肤（22）之间包括肺泡细胞（27）的声学结构（21）。从外部皮肤（22），内部皮肤（23）和声音结构（21）中选择的至少一个主要部件由复合材料形成，声学结构（21）保持与内部（23）和外部（22）表面通过弹性装置压缩和/或通过机械固定装置（24）固定。本发明还涉及一种喷射器喷嘴（10）和包括这种声学面板（20）的机舱（1）。

8. 发明授权

US09206765B2 Thrust reversing device including variable nozzle section having first position for variation of the nozzle section and a second position for blocking a cold flow jet 有权
标题翻译：推力换向装置包括具有用于改变喷嘴部分的第一位置的可变喷嘴部分和用于阻挡冷流喷射的第二位置
公开(公告)号：US09206765B2
公开(公告)日：2015-12-08
申请号：US13321831
申请日：2010-05-18
申请人： Guy Bernard Vauchel
发明人： Guy Bernard Vauchel
IPC分类号： F02K1/72 , F02K1/76
CPC分类号： F02K1/72 , F02K1/763 , F05D2270/66 , Y10T74/18576
摘要： The invention relates to a thrust reversing device (20) that includes at least one mobile cowling (30) mounted in translation in a direction substantially parallel to a longitudinal axis of a nacelle, capable of moving alternatively from a closing position on which it enables the aerodynamic continuity of the nacelle into an opening position in which it opens a passage in the nacelle for the bypassed flow, wherein said mobile cowling (30) also includes as an extension at least one variable nozzle section (40) including at least one panel (41) mounted so as to be capable of rotation, the panel (41) being adapted for pivoting towards at least one position entailing a variation in the nozzle section (40) on the one hand, and pivoting towards a position in which it blocks a cold flow jet (13) formed between a fixed structure of a turbojet fairing (12 and the nacelle on the other hand, wherein the mobile cowling (30) and the panel (41) are associated with actuation means (50) capable of activating the respective translation and rotation movements thereof, characterized in that said actuation means (50) are connected to an upstream end of the panel (41) by a driving connection rod (61) capable of moving about anchoring points respectively on the corresponding panel (41) and the associated actuation means (50).
摘要翻译：本发明涉及一种推力反向装置（20），其包括至少一个可移动的整流罩（30），该移动整流罩（30）在基本上平行于机舱的纵向轴线的方向上平移地安装，能够从关闭位置交替移动，空气动力学连续性的机舱进入打开位置，在打开位置中，其打开用于旁路流的机舱中的通道，其中所述可移动整流罩（30）还包括作为延伸部的至少一个可变喷嘴部分（40），其包括至少一个面板 41）被安装成能够旋转，所述面板（41）适于朝着至少一个位置枢转，所述至少一个位置一方面导致喷嘴部分（40）的变化，并且朝向其阻挡一个位置的位置枢转形成在涡轮喷气整流装置（12和机舱之间）的固定结构之间的冷流射流（13），其中可移动罩（30）和面板（41）与能够作用的致动装置其特征在于，所述致动装置（50）通过驱动连接杆（61）连接到所述面板（41）的上游端，所述驱动连接杆能够分别在相应的面板上 41）和相关联的致动装置（50）。

9. 发明授权

US09169805B2 Thrust inverter with translatable cascade vanes having detachable front frame 有权
标题翻译：具有可拆卸叶片的推力变频器具有可拆卸的前框架
公开(公告)号：US09169805B2
公开(公告)日：2015-10-27
申请号：US13510352
申请日：2010-10-26
申请人： Guy Bernard Vauchel , Pierre Caruel , Andre Baillard , Peter Sagat
发明人： Guy Bernard Vauchel , Pierre Caruel , Andre Baillard , Peter Sagat
IPC分类号： F01D25/28 , B64D29/08 , F02K1/72 , F02K1/68 , F02K1/54 , F01D25/24 , F02K1/64 , F02C7/20 , B64D29/06
CPC分类号： F02K1/72 , B64D29/06 , B64D29/08 , F01D25/24 , F01D25/243 , F01D25/28 , F02C7/20 , F02K1/54 , F02K1/64 , F02K1/68 , F05D2250/34
摘要： A thrust inverter for a turbojet engine nacelle includes an outer movable cowl and a front frame. The outer movable cowl translates between a closed position and a thrust inversion position and also moves to a supporting position in which the outer movable cowl is hinged and guided by a guiding member located on a pylon. In particular, the front frame holding cascade vanes is mounted downstream from an air blower housing, and part of the front frame is detachably connected to the air blower housing. The front frame is translatable along the guiding member once the front frame is detached from the air blower housing.
摘要翻译：用于涡轮喷气发动机机舱的推力逆变器包括外部可移动整流罩和前部框架。外部可移动整流罩在关闭位置和推力反转位置之间平移，并且还移动到支撑位置，在该支撑位置，外部可移动整流罩由位于塔架上的引导构件铰接并引导。具体地说，前端框架保持级联叶片安装在鼓风机壳体的下游，并且前框架的一部分可拆卸地连接到鼓风机壳体。一旦前框架与鼓风机壳体分离，前框架可沿引导构件平移。

10. 发明授权

US08919693B2 Lockable guiding system for a mobile part of a nacelle 有权
标题翻译：机舱移动部件的可锁定导向系统
公开(公告)号：US08919693B2
公开(公告)日：2014-12-30
申请号：US12531526
申请日：2008-03-07
申请人： Guy Bernard Vauchel
发明人： Guy Bernard Vauchel
IPC分类号： B64D29/00 , B64D33/02 , F02C7/04 , B64D29/06 , B64D29/08 , E05F5/00
CPC分类号： F02C7/04 , B64D29/00 , B64D29/06 , B64D29/08 , E05F5/003 , E05Y2900/502 , F05D2240/14 , F05D2260/52
摘要： The invention relates to a guiding device (100) for part of a jet engine nacelle that can move in translation, comprising: (i) a rail (101) fixedly mounted on part of the nacelle, and (ii) a slide (102) which is connected to the mobile part and which can slide along the rail. The invention is characterized in that the guiding device is provided with a built-in retractable system for preventing the translational movement of the slide, for which purpose the device includes: (i) at least one blocking means (104) mounted such that it can move on the rail and occupy alternatively an engaged position in which it forms a translational abutment for the slide and a released position in which it is moved away from the slide and enables the relative translational movement of the slide beyond the locking system, and (ii) at least one means (130) for controlling the blocking means.
摘要翻译：本发明涉及一种可移动平移的部分喷气发动机机舱的引导装置（100），包括：（i）固定地安装在机舱的一部分上的导轨（101），和（ii）滑块（102）其连接到移动部件并且可以沿着轨道滑动。本发明的特征在于，引导装置设置有内置的可伸缩系统，用于防止滑块的平移运动，为此目的，该装置包括：（i）安装至少一个阻挡装置（104），使得其可在轨道上移动并且占据可选择的接合位置，在该位置中，其形成用于滑动件的平移邻接件和释放位置，其中滑动件移动远离滑动件，并且使得滑块相对于平移运动超过锁定系统，并且（ii ）至少一个用于控制阻挡装置的装置（130）。

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