公开(公告)号：US09481054B2

公开(公告)日：2016-11-01

申请号：US13958246

申请日：2013-08-02

Applicant: AIRCELLE

Inventor： Bertrand Desjoyeaux ,  Olivier Hubier

IPC: B64D33/00 ,  B23P15/00 ,  B29C70/84 ,  B64D33/02 ,  B29C70/44 ,  B29C70/48

CPC classification number: B23P15/008 ,  B29C70/44 ,  B29C70/48 ,  B29C70/84 ,  B64D33/02 ,  B64D2033/0286 ,  Y10T29/49346

Abstract: A method for manufacturing an air-intake structure for a turbojet-engine nacelle includes two component parts, i.e. one air-intake lip structure and one outer cowl for the air-intake structure. In particular, the method includes the following steps: separately manufacturing the component parts such that each integrates one overlapping portion with a part to which is to be attached. The overlapping portion is configured such that an outer surface of the outer overlapping portion provides continuity with an outer surface of the outer cowl associated with the inner overlapping portion. To secure the overlapping portions, glue or a fastener may be used.

Abstract translation: 用于制造涡轮喷气发动机机舱的进气结构的方法包括两个部件，即一个进气口结构和一个用于进气结构的外罩。 特别地，该方法包括以下步骤：分开制造组成部件，使得每个部件将一个重叠部分与要附接的部分集成。 重叠部分构造成使得外部重叠部分的外表面与外部整流罩的与内部重叠部分相关联的外表面提供连续性。 为了固定重叠部分，可以使用胶水或紧固件。

公开(公告)号：US09476383B2

公开(公告)日：2016-10-25

申请号：US13944187

申请日：2013-07-17

Applicant: AIRCELLE

Inventor： Pierre Caruel

IPC: F02K1/54 ,  B64D33/04 ,  F02K1/72 ,  F02K1/76

CPC classification number: F02K1/54 ,  B64D33/04 ,  F02K1/72 ,  F02K1/766 ,  Y02T50/671

Abstract: A thrust reverser with grids includes a jet engine pylon, a one piece cowl either directly or indirectly slidably mounted on the jet engine pylon between a direct jet position and a reverse jet position, and a system for locking this cowl on a beam. The system has a single tertiary lock, which is positioned on one side of the jet engine pylon being capable of locking a corresponding upper edge of the cowl. In addition, the tertiary lock includes a locker to lock the cowl, a blocker for blocking the locker, and a position detector in order to detect the position of the locker. The system further includes another detector to detect proper closing of the other upper edge of the cowl.

Abstract translation: 具有网格的推力反向器包括喷气式发动机塔架，直接或间接可滑动地安装在喷气发动机塔架上的直接喷射位置和反向喷射位置之间的一个整流罩，以及用于将该罩盖锁定在梁上的系统。 该系统具有单个三级锁，其位于喷气发动机塔的一侧，能够锁定整流罩的相应上边缘。 此外，三级锁包括用于锁定整流罩的储物柜，用于阻挡储物柜的阻塞器和用于检测储物柜位置的位置检测器。 该系统还包括用于检测整流罩的另一个上边缘的适当关闭的另一检测器。

公开(公告)号：US20160305913A1

公开(公告)日：2016-10-20

申请号：US15193157

申请日：2016-06-27

Applicant: AIRCELLE

Inventor： Andre BAILLARD

IPC: G01N29/22

CPC classification number: G01N29/223 ,  G01N29/04 ,  G01N29/043 ,  G01N29/225 ,  G01N29/265 ,  G01N29/28 ,  G01N2291/0231 ,  G01N2291/048

Abstract: The disclosure relates to a device for non-destructive testing of a composite part that includes at least two magnetic bodies, at least one of said at least two magnetic bodies being adapted such as to exercise a force of attraction such as to allow mutual restraint, or restraint of one by the other, of the magnetic bodies on either side of said part, said magnetic bodies being intended to be positioned directly on at least one wall of the part to be tested; and at least one transmitting ultrasound probe positioned on one of said magnetic bodies, and at least one receiving ultrasound probe positioned on the other one of said magnetic bodies.

Abstract translation: 本公开涉及一种用于对包括至少两个磁体的复合部件的非破坏性测试的装置，所述至少两个磁体中的至少一个适于运动吸引力以允许相互制约， 或约束一个由另一个的磁体在所述部分的任一侧上，所述磁体旨在直接定位在待测试部件的至少一个壁上; 以及定位在所述磁体之一上的至少一个发射超声探头和位于所述磁体中另一个上的至少一个接收超声探头。

公开(公告)号：US20160263845A1

公开(公告)日：2016-09-15

申请号：US15164913

申请日：2016-05-26

Applicant: AIRCELLE

Inventor： Arnaud DELEHOUZE ,  Jean-Philippe MUCHERIE

IPC: B29C73/04 ,  B29C73/06 ,  F01D25/24 ,  B64D27/16 ,  B64D29/08 ,  B29C67/00 ,  B28B1/00

CPC classification number: B29C73/04 ,  B28B1/001 ,  B29C64/00 ,  B29C64/135 ,  B29C73/06 ,  B29L2031/3076 ,  B29L2031/749 ,  B33Y10/00 ,  B33Y80/00 ,  B64D27/16 ,  B64D29/08 ,  F01D25/24 ,  F05D2220/323 ,  F05D2230/31 ,  F05D2230/60 ,  F05D2230/80

Abstract: A method for repairing sandwich panels made of composite materials following impact that has damaged the core of the panel is provided. The method involves acquisition of a numerical model of the shape of the damaged zone then use of a stereolithography method based on the numerical model to create a replacement core or a mould in which this replacement core will be moulded, followed by creation of replacement component comprising this core, then the instillation of this component which is fitted into an opening cut in the sandwich panel around the damage, and finally attachment of the replacement component to the panel.

Abstract translation: 本发明提供了一种修复由冲击造成的复合材料制成的夹芯板的方法。 该方法包括获取受损区域的形状的数值模型，然后使用基于数值模型的立体光刻方法来创建替换芯或模具，其中该替换芯将被模制，随后创建替换部件，其包括 然后将该组件滴入装配在夹层板周围的开口处的损伤周围，最后将更换部件附接到面板上。

公开(公告)号：US09410485B2

公开(公告)日：2016-08-09

申请号：US14272884

申请日：2014-05-08

Applicant: AIRCELLE

Inventor： Franck Laurant ,  Francois Bellet ,  Jean-Philippe Joret

IPC: B32B3/24 ,  B64D33/02 ,  B64D29/00 ,  B64C7/02 ,  B64C1/00 ,  F02C7/20 ,  B64D33/08 ,  F02C7/04 ,  F01D25/24 ,  B29L31/00 ,  B29L31/30 ,  B32B3/26 ,  F02C6/08

CPC classification number: F02C7/20 ,  B29L2031/3076 ,  B29L2031/7504 ,  B32B3/266 ,  B32B2250/03 ,  B32B2250/40 ,  B32B2605/18 ,  B64C7/02 ,  B64D29/00 ,  B64D33/08 ,  B64D2241/00 ,  F01D25/24 ,  F02C6/08 ,  F02C7/04 ,  F05D2240/14 ,  F05D2270/09 ,  F05D2300/603 ,  Y02T50/672 ,  Y10T428/24182 ,  Y10T428/24281 ,  Y10T428/24322 ,  Y10T428/24612

Abstract: A composite panel includes an inner skin and an outer skin and has an opening for receiving a sampling scoop, which forms a channel and the sampling opening of which is in communication with the outer skin. In particular, the outer skin is shaped such that, at the opening, same forms at least a portion of a flow surface of the sampling scoop.

Abstract translation: 复合面板包括内皮和外皮，并且具有用于接收采样勺的开口，其形成通道，并且其采样开口与外皮连通。 特别地，外皮成形为使得在开口处相同形成采样勺的流动表面的至少一部分。

公开(公告)号：US09382814B2

公开(公告)日：2016-07-05

申请号：US13860726

申请日：2013-04-11

Applicant: AIRCELLE

Inventor： Serge Bunel ,  Vincent Peyron ,  Hazem Kioua ,  Jerome Lescure

IPC: F02K1/80 ,  B64D29/06 ,  F16L37/113 ,  F01D25/24 ,  F01D25/28 ,  F02K1/56 ,  F02K1/76 ,  F16B2/14 ,  F16L23/036 ,  F16L37/10

CPC classification number: F01D25/28 ,  F01D25/243 ,  F02K1/56 ,  F02K1/766 ,  F02K1/80 ,  F05B2240/911 ,  F05D2230/60 ,  F05D2250/411 ,  F05D2260/30 ,  F05D2260/50 ,  F16B2/14 ,  F16L23/036 ,  F16L37/101 ,  Y02T50/671

Abstract: A device for connecting a thrust reverser front frame to a fan casing includes a crenulated flange secured to the front frame, an annular component to accept this flange secured to the fan casing, and a crenulated annulus of a shape that complements the flange and pivot-mounted on the annular component. The crenulated flange, the annular component and the crenulated annulus are designed in such a way that a rotation of the annulus with respect to the annular component has the effect of locking this flange against this annular component through the collaboration between the respective crenulations of the flange and of the annulus.

Abstract translation: 用于将推力反向器前框架连接到风扇壳体的装置包括固定到前框架的螺旋形凸缘，用于接收固定到风扇壳体上的该凸缘的环形部件，以及与凸缘和枢轴连接部分互补的形状的圆环， 安装在环形部件上。 齿形凸缘，环形部件和棘轮环形空间被设计成使得环形件相对于环形部件的旋转具有通过凸缘的相应齿形部之间的协作将该凸缘锁定在该环形部件上的作用 和环带。

公开(公告)号：US09274002B2

公开(公告)日：2016-03-01

申请号：US14245816

申请日：2014-04-04

Applicant: AIRCELLE

Inventor： Lionel Gay ,  Thibaud Chopard ,  Odile Lefeu ,  Frédéric Joubert

IPC: G01N21/35 ,  G01N21/3563 ,  G01J3/45 ,  G01N21/95 ,  G01N29/04 ,  G01N29/12 ,  G01N21/84

CPC classification number: G01J3/45 ,  G01N21/3563 ,  G01N21/95 ,  G01N29/041 ,  G01N29/12 ,  G01N2021/3595 ,  G01N2021/8472 ,  G01N2201/0221 ,  G01N2291/0231 ,  G01N2291/2694

Abstract: A method for the non-destructive inspection of a part made from an organic-matrix composite material (CMO) includes the steps of: a) carrying out a surface inspection of the part by Fourier transform infrared spectroscopy (FTIS), b) if step a) reveals a defect, carrying out in-depth inspections of the organic-matrix composite material according to two complementary ultrasound techniques.

Abstract translation: 一种用于对由有机基质复合材料（CMO）制成的部件进行非破坏性检查的方法包括以下步骤：a）通过傅立叶变换红外光谱法（FTIS）对部件进行表面检查，b）如果步骤 a）显示缺陷，根据两种互补超声技术对有机基质复合材料进行深入检查。

公开(公告)号：US09272309B2

公开(公告)日：2016-03-01

申请号：US14100249

申请日：2013-12-09

Applicant: AIRCELLE

Inventor： Patrick Gaffie ,  Romain Artinian

IPC: B05D7/00 ,  B44C3/02 ,  B05D7/14 ,  B05D7/16 ,  B05D5/00 ,  G09F21/08

CPC classification number: B05D7/57 ,  B05D5/00 ,  B05D7/00 ,  B05D7/14 ,  B05D7/16 ,  B05D7/50 ,  B05D7/56 ,  B05D2202/00 ,  B05D2503/00 ,  B44C3/02 ,  G09F21/08 ,  Y10T428/24802

Abstract: A method for applying a pattern, such as a logo, onto the outer skin of an aircraft element includes the following steps: a) applying a coat of paint onto the aircraft element; b) applying a top coat (base coat) onto the coat of paint; c) applying a first coat of transparent varnish (clear coat) onto the base coat; d) applying the pattern onto the first coat of transparent varnish; and e) applying a second coat of transparent varnish (clear coat) onto the pattern.

Abstract translation: 用于将诸如标志的图案应用于飞机元件的外皮上的方法包括以下步骤：a）将涂层涂在飞行器元件上; b）将涂层（底漆）涂于油漆涂层上; c）将第一层透明清漆（透明涂层）涂于底漆上; d）将图案涂于第一层透明清漆上; 和e）将第二层透明清漆（透明涂层）涂覆到图案上。

公开(公告)号：US20160042675A1

公开(公告)日：2016-02-11

申请号：US14922361

申请日：2015-10-26

Applicant: AIRCELLE

Inventor： Christophe MARCHETTI ,  Jerome REBIERE-DESVEAUX ,  Serge RIERE

IPC: G09F21/10 ,  B64D47/02

CPC classification number: G09F21/10 ,  B64D47/02 ,  B64D2203/00 ,  G09F9/33

Abstract: A device for displaying an luminous message on the fairing of an aircraft includes: an electroluminescent sheet plated against the fairing; a means for attaching the electroluminescent sheet onto the fairing; a means for supplying the electroluminescent sheet with electricity; a means for electrically connecting the electroluminescent sheet to the means for supplying electricity; and a means for controlling the electroluminescent sheet in an powered-on state, in which the electroluminescent sheet is supplied with electricity and emits light, or in a powered-off state, in which the electroluminescent sheet is inoperative.

Abstract translation: 用于在飞行器的整流罩上显示发光信息的装置包括：电镀发光板， 用于将电致发光片附着到整流罩上的装置; 用于向所述电致发光片供电的装置; 用于将电致发光片电连接到用于供电的装置的装置; 以及用于在电致电状态下控制电致发光片的装置，其中电致发光片被供电并发光，或者在电致发光片不起作用的关闭状态下。

公开(公告)号：US20160039528A1

公开(公告)日：2016-02-11

申请号：US14885422

申请日：2015-10-16

Applicant: AIRCELLE

Inventor： Pierre CARUEL

IPC: B64D29/06 ,  F01D25/24 ,  B64D33/02

CPC classification number: B64D29/06 ,  B64D33/02 ,  B64D2033/0206 ,  B64D2033/0273 ,  F01D25/24 ,  F02C3/04 ,  F02C7/04 ,  F02K1/64 ,  F02K3/06 ,  F05D2220/323 ,  F05D2220/327 ,  F05D2260/96 ,  Y02T50/672

Abstract: A nacelle for an aircraft turbojet engine includes: a substantially cylindrical internal envelope, a substantially cylindrical external envelope, a downstream partition wall and an upstream partition wall secured to the cylindrical internal envelope and a front lip disposed forward of the upstream partition wall. The cylindrical internal envelope includes an upstream portion including an acoustic shroud connected, by an attachment flange, to a downstream portion including a fan casing. In particular, the front lip is extended and disposed over the upstream partition wall by presenting a downstream edge between the upstream and downstream partition walls in order to be secured to a homologous edge of the cylindrical external envelope so as to arrange a maintenance access to the attachment flange

Abstract translation: 用于飞行器涡轮喷气发动机的机舱包括：基本上圆柱形的内部封套，基本上圆柱形的外部封套，下游分隔壁和固定到圆柱形内部封套的上游分隔壁和设置在上游分隔壁前方的前唇缘。 圆柱形内封套包括上游部分，其包括通过附接凸缘连接到包括风扇壳体的下游部分的声罩。 特别地，前唇通过在上游和下游隔壁之间呈现下游边缘而延伸并设置在上游分隔壁上方，以便固定到圆柱形外壳的同源边缘，以便安排对 附件法兰