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1. 发明申请

WO2009133271A8 DEVICE FOR REDUCING NOISE GENERATED BY AN AIRCRAFT JET ENGINE WITH CURVE DUCTS 审中-公开
标题翻译：用于降低飞机喷气发动机产生的噪音的装置
公开(公告)号：WO2009133271A8
公开(公告)日：2010-10-28
申请号：PCT/FR2009000374
申请日：2009-03-31
申请人： AIRBUS OPERATIONS SAS , CENTRE NAT RECH SCIENT , UNIV POITIERS , HUBER JEROME , BONNET JEAN-PAUL , DELVILLE JOEL , JORDAN PETER , STREKOWSKI FRANCOIS
发明人： HUBER JEROME , BONNET JEAN-PAUL , DELVILLE JOEL , JORDAN PETER , STREKOWSKI FRANCOIS
IPC分类号： F02K1/34 , F02K1/46
CPC分类号： F02K1/46 , F02K1/34 , F05D2240/40
摘要： Jet engine, comprising a wall (30) surrounding a first gas flow which is ejected from a downstream end (30a) of the wall along a longitudinal axis (XX'), a second flow of gas running outside the wall in the direction of ejection of the first gas flow, at least one duct (80) being arranged on the periphery of the downstream end of the wall which is desired to eject a gas flow for interacting with the and/or the other gas flow, said at least one duct (80) comprising a terminal section (82) provided at the free end thereof with an outlet opening (84) through which the fluid is ejected, characterised in that the terminal section successively comprises a first section (86) of straight duct aligned along an axis called the median axis and a second duct section (88) forming a curve relative to the straight section, the second portion having a free end provided with the outlet opening and sufficiently close the the median axis (ai) of the fist section such as to give the terminal section a reduced restriction in the direction of formation of the curve.
摘要翻译：喷气发动机包括围绕从纵向轴线（XX'）的壁的下游端（30a）排出的第一气流的壁（30），沿喷射方向在壁外延伸的第二气体流所述第一气流的至少一个管道（80）布置在所述壁的下游端的周边上，所述下游端部期望喷射与所述和/或另一个气流相互作用的气流，所述至少一个管道（80），包括在其自由端处设置有流体喷出的出口（84）的端子部分（82），其特征在于，所述端子部分依次包括沿着沿着所述第一部分轴线称为中轴线，第二管道部分（88）形成相对于直线部分的曲线，第二部分具有设置有出口开口的自由端，并且足够靠近第一部分的中轴（ai），例如给终端部分一个红色在曲线形成方向上的限制。

2. 发明申请

WO2009133273A3 DEVICE WITH SECONDARY JETS REDUCING THE NOISE GENERATED BY AN AIRCRAFT JET ENGINE 审中-公开
标题翻译：二次喷射装置降低飞机喷射发动机产生的噪音
公开(公告)号：WO2009133273A3
公开(公告)日：2009-12-23
申请号：PCT/FR2009000376
申请日：2009-03-31
申请人： AIRBUS OPERATIONS SAS , CENTRE NAT RECH SCIENT , UNIV POITIERS , BONNET JEAN-PAUL , DELVILLE JOEL , JORDAN PETER , STREKOWSKI FRANCOIS
发明人： BONNET JEAN-PAUL , DELVILLE JOEL , JORDAN PETER , STREKOWSKI FRANCOIS
IPC分类号： F02K1/34
CPC分类号： F02K1/34 , F02K1/46 , F05D2240/40 , F05D2250/11
摘要： The invention relates to an aircraft jet engine comprising a wall (30) centred about a longitudinal axis (XX') and surrounding a stream of gas ejected at a downstream end of the wall in the direction of the axis, several pairs of ducts known as primary ducts (30, 32, 34, 36, 38, 40, 42, 44, 46) distributed at the periphery of the downstream end of the wall being able on command each to eject a jet of primary fluid intended to interact with the ejected stream of gas, the primary ducts (32a, 32b) of each pair converging towards one another near the downstream end of the wall so that the primary jets ejected form the two sides of a triangle which meet at the vertex thereof in a view projected onto a plane perpendicular to a transverse plane, characterized in that at least one so-called secondary duct (32c) is associated with each pair of primary ducts and is able on command to eject a jet of secondary fluid directed into the triangle formed by the primary jets.
摘要翻译：本发明涉及一种飞机喷气发动机，其包括以纵向轴线（XX'）为中心且围绕沿轴线方向在壁的下游端处喷射的气体流的壁（30），多对称为分布在壁下游端周边的主管道（30,32,34,36,38,40,42,44,46）能够根据指令分别喷射旨在与喷射相互作用的主要流体射流气流，每对主要导管（32a，32b）在壁的下游端附近彼此会聚，使得主射流喷射形成三角形的两侧，该三角形在投射到视图上的顶点处相遇垂直于横向平面的平面，其特征在于，至少一个所谓的副管道（32c）与每对主管道相关联，并且能够命令喷射引导到由主管道形成的三角形中的二次流体射流飞机。

3. 发明申请

WO2009133273A2 DISPOSITIF À JETS SECONDAIRES DE RÉDUCTION DU BRUIT GÉNÉRÉ PAR UN RÉACTEUR D'AÉRONEF 审中-公开
标题翻译：具有次级喷气机的设备减少飞机喷气发动机产生的噪音
公开(公告)号：WO2009133273A2
公开(公告)日：2009-11-05
申请号：PCT/FR2009/000376
申请日：2009-03-31
申请人： AIRBUS FRANCE , CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE (CNRS) , UNIVERSITE DE POITIERS , BONNET, Jean-Paul , DELVILLE, Joël , JORDAN, Peter , STREKOWSKI, François
发明人： BONNET, Jean-Paul , DELVILLE, Joël , JORDAN, Peter , STREKOWSKI, François
IPC分类号： F02K1/34 , F02K1/46
CPC分类号： F02K1/34 , F02K1/46 , F05D2240/40 , F05D2250/11
摘要： L'invention concerne un réacteur d'aéronef, comprenant une paroi (30) centrée autour d'un axe longitudinal (XX') et entourant un flux de gaz qui est éjecté à une extrémité aval de la paroi dans la direction de l'axe, plusieurs paires de conduits dits primaires (30, 32, 34, 36, 38, 40, 42, 44, 46) répartis à la périphérie de l'extrémité aval de la paroi étant aptes à éjecter sur commande chacun un jet de fluide primaire destiné à interagir avec le flux de gaz éjecté, les conduits primaires (32a, 32b) de chaque paire convergeant l'un vers l'autre à proximité de l'extrémité aval de la paroi de manière à ce que les jets primaires éjectés forment les deux côtés d'un triangle qui se rejoignent au sommet de ce dernier suivant une vue en projection dans un plan perpendiculaire à un plan transversal, caractérisé en ce qu'au moins un conduit dit secondaire (32c) est associé à chaque paire de conduits primaires et est apte à éjecter sur commande un jet de fluide secondaire dirigé dans le triangle formé par les jets primaires.
摘要翻译：本发明涉及一种飞机喷气式发动机，其包括以纵向轴线（XX'）为中心的壁（30），并且围绕在轴的方向上在壁的下游端喷射的气体流，被称为分布在壁的下游端的周边处的主管道（30,32,34,36,38,40,42,44,46）能够按照每个喷射喷射主要流体的射流来与弹出的相互作用每一对气流中，每一对的主要管道（32a，32b）在壁的下游端彼此会聚，使得主喷嘴形成三角形的两侧，三角形的两侧在投影到垂直于横向平面的平面，其特征在于，至少一个所谓的副管道（32c）与每对主要管道相关联，并且能够命令喷射引导到由主要管道形成的三角形形成的三角形的二次流体的射流飞机。

4. 发明申请

WO2008003544A1 STAUBABSAUGADAPTERVORRICHTUNG 审中-公开
公开(公告)号：WO2008003544A1
公开(公告)日：2008-01-10
申请号：PCT/EP2007/054447
申请日：2007-05-08
申请人： ROBERT BOSCH GMBH , JORDAN, Peter , BAUMANN, Otto , DAMMERTZ, Ralph , RENZ, Werner , BERNHARDT, Thomas , SCHMID, Hardy , DI NICOLANTONIO, Aldo , HOSSMANN, Daniela , LENNARTZ, Juergen
发明人： JORDAN, Peter , BAUMANN, Otto , DAMMERTZ, Ralph , RENZ, Werner , BERNHARDT, Thomas , SCHMID, Hardy , DI NICOLANTONIO, Aldo , HOSSMANN, Daniela , LENNARTZ, Juergen
IPC分类号： B23Q11/00
CPC分类号： B23Q11/0046
摘要： Die Erfindung geht aus von einer Staubabsaugadaptervorrichtung mit einer Grundkörpereinheit (12), die eine Koppelstelle (14) zur Ankopplung an eine Handwerkzeugmaschine (16) und wenigstens einen Absaugkanal (18) aufweist, und einer an der Grundkörpereinheit (12) beweglichen Saugkopfeinheit (20). Es wird vorgeschlagen, dass die Staubabsaugadaptervorrichtung wenigstens eine Schnittstelle (22) für eine externe Saugeinheit (24) aufweist.
摘要翻译：从Staubabsaugadaptervorrichtung本发明继续进行基础单元（12），其具有用于连接到的手持式工具（16）和至少一个抽吸通道（18）的连接点（14），和一个在基座单元（12）可动吸头（20），本发明提出，包括用于外部抽吸单元（24）的Staubabsaugadaptervorrichtung至少一个接口（22）。

5. 发明申请

WO2009133273A8 DEVICE WITH SECONDARY JETS REDUCING THE NOISE GENERATED BY AN AIRCRAFT JET ENGINE 审中-公开
标题翻译：具有次级喷气机的设备减少飞机喷气发动机产生的噪音
公开(公告)号：WO2009133273A8
公开(公告)日：2010-10-14
申请号：PCT/FR2009000376
申请日：2009-03-31
申请人： AIRBUS OPERATIONS SAS , CENTRE NAT RECH SCIENT , UNIV POITIERS , HUBER JEROME , BONNET JEAN-PAUL , DELVILLE JOEL , JORDAN PETER , STREKOWSKI FRANCOIS
发明人： HUBER JEROME , BONNET JEAN-PAUL , DELVILLE JOEL , JORDAN PETER , STREKOWSKI FRANCOIS
IPC分类号： F02K1/34
CPC分类号： F02K1/34 , F02K1/46 , F05D2240/40 , F05D2250/11
摘要： The invention relates to an aircraft jet engine comprising a wall (30) centred about a longitudinal axis (XX') and surrounding a stream of gas ejected at a downstream end of the wall in the direction of the axis, several pairs of ducts known as primary ducts (30, 32, 34, 36, 38, 40, 42, 44, 46) distributed at the periphery of the downstream end of the wall being able on command each to eject a jet of primary fluid intended to interact with the ejected stream of gas, the primary ducts (32a, 32b) of each pair converging towards one another near the downstream end of the wall so that the primary jets ejected form the two sides of a triangle which meet at the vertex thereof in a view projected onto a plane perpendicular to a transverse plane, characterized in that at least one so-called secondary duct (32c) is associated with each pair of primary ducts and is able on command to eject a jet of secondary fluid directed into the triangle formed by the primary jets.
摘要翻译：本发明涉及一种飞机喷气式发动机，其包括以纵向轴线（XX'）为中心的壁（30），并且围绕在轴的方向上在壁的下游端喷射的气体流，被称为分布在壁的下游端的周边处的主管道（30,32,34,36,38,40,42,44,46）能够按照每个喷射喷射主要流体的射流来与弹出的相互作用每一对气流中，每一对的主要管道（32a，32b）在壁的下游端彼此会聚，使得主喷嘴形成三角形的两侧，三角形的两侧在投影到垂直于横向平面的平面，其特征在于，至少一个所谓的副管道（32c）与每对主要管道相关联，并且能够命令喷射引导到由主要管道形成的三角形形成的三角形的二次流体的射流飞机。

6. 发明申请

WO2007020389A1 ELECTRICAL CONNECTING DEVICE 审中-公开
标题翻译：电气连接装置
公开(公告)号：WO2007020389A1
公开(公告)日：2007-02-22
申请号：PCT/GB2006/002991
申请日：2006-08-10
申请人： ITT MANUFACTURING ENTERPRISES, INC. , JORDAN, Peter , VILLAIN, Jean Christophe
发明人： JORDAN, Peter , VILLAIN, Jean Christophe
IPC分类号： H01R13/24 , H01R12/22 , H01R12/16
CPC分类号： H01R13/2407 , H01R12/52 , H01R12/7076 , H01R12/714
摘要： An electrical connecting device for two electrical components which, when assembled, have electrical contact areas facing each other. The electrical connecting device comprises: a plurality of metallic connecting elements, each connecting element having first and second contact portions resiliently compressible against each other; and a flexible dielectric carrier sheet for the connecting elements, a portion of each connecting element being attached to the carrier sheet. Each connecting element comprises a strip of material having a bend at an intermediate portion. In the device, the connecting elements are resiliently compressible against each other, independent of any supporting structure. A rigid supporting structure is accordingly not required.
摘要翻译：一种用于两个电气部件的电连接装置，其组装时具有彼此面对的电接触区域。电连接装置包括：多个金属连接元件，每个连接元件具有彼此弹性压缩的第一和第二接触部分; 以及用于所述连接元件的柔性介电载体片，每个连接元件的一部分附接到所述载体片。每个连接元件包括在中间部分具有弯曲的材料条。在该装置中，连接元件可独立于任何支撑结构而彼此弹性压缩。因此，不需要刚性支撑结构。

7. 发明申请

WO1994019637A1 APPARATUS FOR LAYING AND/OR RETRIEVING ELONGATE FLEXIBLE ELEMENTS 审中-公开
标题翻译：用于布置和/或检索最终柔性元件的装置
公开(公告)号：WO1994019637A1
公开(公告)日：1994-09-01
申请号：PCT/GB1994000362
申请日：1994-02-23
申请人： NORTHERN OCEAN SERVICES LIMITED , JORDAN, Peter, Arthur
发明人： NORTHERN OCEAN SERVICES LIMITED
IPC分类号： F16L01/12
CPC分类号： F16L1/225
摘要： Apparatus for laying and/or retrieving elongate flexible elements, such as pipes and cables having accessories at spaced intervals, is mounted on a floating vessel such as a barge (12) and comprises two self powered conveyors (2, 3) pivotally connected together through a hinge (19) but which may be locked relative to one another for use. A trolley (4) runs on wheels (8) on rails (5) on either side of the conveyor system and has an upper surface consisting of a further powered conveyor (6). The sides of conveyor (3) extend to form a chute (7) at the outboard end. In normal operation the trolley (4) is stored and the pipe or cable is carried by the conveyors (2, 3) to the chute (7) which guides it into the water. The shape of the chute (7) permits the pipe/cable to leave the barge at up to 45 DEG either side of the fore and aft axis of the conveyor. When an accessory on the pipe/cable approaches the trolley (4) is raised to support the pipe/cable behind the accessory carrying the pipe with the accessory above and out of contact with the conveyors (2, 3) until the accessory has entered the water. The trolley (4) is then retrieved.
摘要翻译：用于铺设和/或回收细长柔性元件（例如具有间隔间隔的附件的管道和电缆）的装置安装在诸如驳船（12）的浮动容器上，并且包括两个自供电输送机（2,3），其通过铰链（19），但是可以相对于彼此锁定以供使用。手推车（4）在输送机系统的任一侧的轨道（5）上的轮子（8）上运行，并且具有由进一步动力输送机（6）组成的上表面。输送机（3）的侧面在外侧延伸以形成滑槽（7）。在正常操作中，存放手推车（4），管道或电缆由输送机（2,3）运送到将其引导到水中的斜槽（7）。滑槽（7）的形状允许管道/电缆在输送机的前后轴线的任一侧高达45°的离开驳船。当管道/电缆上的附件接近台车（4）时，将附件上的管道/电缆支撑在附件的附件上方，并将附件放在与传送带（2,3）相接触的位置，直到配件进入水。然后取出手推车（4）。

8. 发明申请

WO1987005577A2 SYSTEM FOR OFFSHORE OPERATIONS 审中-公开
标题翻译：海上作业系统
公开(公告)号：WO1987005577A2
公开(公告)日：1987-09-24
申请号：PCT/GB1987000174
申请日：1987-03-13
申请人： THE FLOATING TECHNOLOGY COMPANY LIMITED , JORDAN, Peter, A.
发明人： THE FLOATING TECHNOLOGY COMPANY LIMITED
IPC分类号： B63B35/44
CPC分类号： B63B35/4406
摘要： A system for offshore operations includes a column (1) extending above sea level from the seabed, which is connected by a bridge (2) to a semisubmersible offshore oil production platform (3). The connection of the bridge (2) to the platform (3) is achieved by an improved joint arrangement which permits relative rotation about both substantially vertical and horizontal axes to reduce loads transmitted to the column. The column (1) is connected by a universal joint arrangement (4) to a base on the seabed. The joint (4) has radially outwardly distributed joint surfaces which provides an axial passageway through the joint for risers. The joint arrangement includes a first main joint and a second normally unloaded ball joint which takes up the column loaded in the event of failure of the first joint.
摘要翻译：一种用于海上作业的系统包括从海底延伸到海底的塔（1），其通过桥（2）连接到半潜式海上石油生产平台（3）。桥（2）与平台（3）的连接通过改进的接头装置实现，其允许围绕基本垂直和水平轴线的相对旋转以减少传输到塔的载荷。柱（1）通过万向接头装置（4）连接到海床上的基座。接头（4）具有径向向外分布的接合表面，其提供穿过用于立管的接头的轴向通道。接头装置包括第一主接头和第二通常无负载的球接头，其接收在第一接头失效的情况下装载的列。

9. 发明申请

WO2009133272A8 DEVICE FOR REDUCING THE NOISE GENERATED BY AN AIRCRAFT JET ENGINE WITH FLUID JETS OF THE SAME ORIENTATION 审中-公开
标题翻译：用于减少飞机喷气式发动机产生的噪音的装置与其同一方向的流体喷嘴
公开(公告)号：WO2009133272A8
公开(公告)日：2010-10-28
申请号：PCT/FR2009000375
申请日：2009-03-31
申请人： AIRBUS OPERATIONS SAS , CENTRE NAT RECH SCIENT , UNIV POITIERS , HUBER JEROME , BONNET JEAN-PAUL , DELVILLE JOEL , JORDAN PETER , STREKOWSKI FRANCOIS
发明人： HUBER JEROME , BONNET JEAN-PAUL , DELVILLE JOEL , JORDAN PETER , STREKOWSKI FRANCOIS
IPC分类号： F02K1/34 , F02K1/46
CPC分类号： F02K1/34 , F02K1/46 , F05D2240/40
摘要： Aircraft jet engine with a longitudinal axis (XX'), comprising a wall (30) enclosing a gas flow which is ejected from a downstream end of the wall in the longitudinal axis, several ducts (32, 34, 36, 38, 40, 42, 44, 46) being distributed around the periphery of the downstream end (30a) of the wall each comprising a terminal section, provided with an outlet opening. Each duct can eject a fluid jet through the outlet opening thereof, characterised in that the ducts are designed to eject the fluid jets essentially parallel to each other, each fluid jet ejected through the corresponding outlet opening (32b) forming a lateral angle (d) with the longitudinal axis (XX') in a projection view in a plane with the longitudinal axis.
摘要翻译：具有纵向轴线（XX'）的飞机喷气式发动机包括围绕从纵向轴线的壁的下游端喷射的气流的壁（30），多个管道（32,34,36,38,40,40） 42,44,46）分布在每个包括端子部分的壁的下游端（30a）的周边周围，所述端子部分设置有出口开口。每个管道可以通过其出口开口喷射流体射流，其特征在于，所述管道被设计成基本上相互平行地喷射流体射流，每个通过对应的出口开口（32b）喷射的流体射流形成横向角度（d）纵轴（XX'）处于与纵向轴线平面的投影视图中。

10. 发明申请

WO2009133271A3 DEVICE FOR REDUCING NOISE GENERATED BY AN AIRCRAFT JET ENGINE WITH CURVE DUCTS 审中-公开
标题翻译：用于降低由具有曲线管的飞机喷射发动机产生的噪音的装置
公开(公告)号：WO2009133271A3
公开(公告)日：2010-10-07
申请号：PCT/FR2009000374
申请日：2009-03-31
申请人： AIRBUS OPERATIONS SAS , CENTRE NAT RECH SCIENT , UNIV POITIERS , HUBER JEROME , BONNET JEAN-PAUL , DELVILLE JOEL , JORDAN PETER , STREKOWSKI FRANCOIS
发明人： HUBER JEROME , BONNET JEAN-PAUL , DELVILLE JOEL , JORDAN PETER , STREKOWSKI FRANCOIS
IPC分类号： F02K1/34 , F02K1/46
CPC分类号： F02K1/46 , F02K1/34 , F05D2240/40
摘要： Jet engine, comprising a wall (30) surrounding a first gas flow which is ejected from a downstream end (30a) of the wall along a longitudinal axis (XX'), a second flow of gas running outside the wall in the direction of ejection of the first gas flow, at least one duct (80) being arranged on the periphery of the downstream end of the wall which is desired to eject a gas flow for interacting with the and/or the other gas flow, said at least one duct (80) comprising a terminal section (82) provided at the free end thereof with an outlet opening (84) through which the fluid is ejected, characterised in that the terminal section successively comprises a first section (86) of straight duct aligned along an axis called the median axis and a second duct section (88) forming a curve relative to the straight section, the second portion having a free end provided with the outlet opening and sufficiently close the the median axis (ai) of the fist section such as to give the terminal section a reduced restriction in the direction of formation of the curve.
摘要翻译：喷气发动机，其包括围绕第一气流的壁（30），所述第一气流沿纵向轴线（XX'）从所述壁的下游端（30a）喷射，第二气流在所述壁的喷射方向，第一气流的至少一个管道（80）布置在希望喷出气流用于与所述和/或另一气流相互作用的所述壁的所述下游端的周边上，所述至少一个管道（80）包括在其自由端处设置有排出口（84）的末端部分（82），所述流体通过所述排出口（84）被排出，其特征在于，所述末端部分连续地包括直管道的第一部分（86）称为中轴线的轴线和相对于直线部分形成弯曲的第二管道部分（88），第二部分具有设置有出口开口的自由端并且充分地闭合第一部分的中轴线（a 1），例如给终端部分一个红色在曲线形成的方向上受到限制。

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