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1. 发明授权

US08931847B2 Passenger seating assemblies and aspects thereof 有权
标题翻译：乘客座椅总成及其方面
公开(公告)号：US08931847B2
公开(公告)日：2015-01-13
申请号：US13066003
申请日：2011-04-04
申请人： Jeremy Cailleteau , David Da Silva
发明人： Jeremy Cailleteau , David Da Silva
IPC分类号： A47C7/54 , B60N2/46 , B64D11/06 , B60N2/02 , B60N2/68 , B60N3/00
CPC分类号： B64D11/0638 , B60N2/0224 , B60N2/682 , B60N2/686 , B60N2/757 , B60N3/004 , B64D11/003 , B64D11/06 , B64D11/0627 , B64D11/0636 , B64D11/064 , B64D11/0643 , B64D11/0644 , B64D11/0646
摘要： Multiple features of seating assemblies are detailed. Innovations in or to tray tables, luggage bars, arm rests, seat backs, and seat frames are included, with features being incorporated into seating assemblies either separately or in any combination. The assemblies are configured principally for passenger aircraft but may be used elsewhere as appropriate or desired.
摘要翻译：详细的座位组合的多个功能。包括托盘，行李箱，扶手，座椅靠背和座椅框架中的创新，其特征是单独地或以任何组合结合到座椅组件中。组件主要用于客机，但可以在其他地方适当或期望地使用。

2. 发明授权

US08133013B2 Stage of a turbine or compressor, particularly for a turbomachine 有权
标题翻译：涡轮或压缩机的阶段，特别是涡轮机
公开(公告)号：US08133013B2
公开(公告)日：2012-03-13
申请号：US12257761
申请日：2008-10-24
申请人： David Audeon , David Da Silva
发明人： David Audeon , David Da Silva
IPC分类号： F01D11/08
CPC分类号： F01D25/246 , F01D11/08 , F04D29/526 , F05D2260/30 , Y02T50/671
摘要： A stage of a turbine or compressor for a turbomachine including at least a vane disk surrounded with a sectorized ring supported by a casing and including a circumferential flange radially clamped on a rail of the casing by substantially C-shaped cross-section locks which are axially engaged on the casing rail and the flange of the ring is disclosed. The inner and outer walls of each lock includes radial bearing surfaces on the flange of the ring and the casing rail, respectively. The bearing surfaces only extend on a part of the width of the lock.
摘要翻译：用于涡轮机的涡轮机或压缩机的级，包括至少一个叶片盘，所述叶片盘被由壳体支撑的扇形环包围，并且包括径向夹在壳体的轨道上的周向凸缘，其基本上为C形的横截面锁定，公开了套筒轨道上的接合和环的凸缘。每个锁的内壁和外壁分别包括在环的凸缘和壳体轨道上的径向支承表面。轴承表面仅在锁的宽度的一部分上延伸。

3. 发明授权

US08277179B2 Turbine or compressor stage for a turbomachine 有权
标题翻译：用于涡轮机的涡轮机或压缩机平台
公开(公告)号：US08277179B2
公开(公告)日：2012-10-02
申请号：US12266929
申请日：2008-11-07
申请人： David Audeon , David Da Silva
发明人： David Audeon , David Da Silva
IPC分类号： F01D25/24 , F04D29/52
CPC分类号： F01D11/08 , F05D2240/11 , F05D2260/30 , Y02T50/671
摘要： A turbine or compressor stage for a turbomachine is disclosed. The stage includes a blade wheel surrounded by a sectorized ring carried by a casing. Each ring sector includes a circumferential rim that is clamped radially a casing rail by two clamps of C-shaped section that are engaged on the circumferential end portions of the rim of the ring sector and on the corresponding portions of the casing rail.
摘要翻译：公开了一种用于涡轮机的涡轮机或压缩机级。舞台包括由壳体承载的扇形环包围的叶轮。每个环形部分包括圆周边缘，该圆周边缘通过两个C形截面的夹具径向地夹紧在壳体轨道上，C形部分接合在环形部分的边缘的周向端部和壳体轨道的相应部分上。

4. 发明授权

US08192149B2 Turbine or compressor stage for a turbojet 有权
标题翻译：用于涡轮喷气发动机的涡轮机或压缩机级
公开(公告)号：US08192149B2
公开(公告)日：2012-06-05
申请号：US12266813
申请日：2008-11-07
申请人： David Audeon , David Da Silva
发明人： David Audeon , David Da Silva
IPC分类号： F01D5/20 , F01D9/00
CPC分类号： F01D11/08 , F05D2240/11 , Y02T50/671 , Y10T24/44744
摘要： A turbojet turbine or compressor stage is disclosed. The stage includes at least one rotor disk mounted inside a sectorized ring supported by a casing and including a circumferential flange radially clamped on an annular rail of the casing by a substantially C-shaped cross-section annular locking device which is axially engaged on the casing rail and on the flange of the ring. A substantially cylindrical heat shielding foil is interposed between the ring and the device. The foil or the device includes at least one extra thickness which respectively bears on the device, or the foil, to radially immobilize this foil.
摘要翻译：公开了一种涡轮喷气涡轮机或压缩机级。所述平台包括安装在由壳体支撑的扇形环内的至少一个转子盘，并且包括通过基本上C形的横截面环形锁定装置径向夹紧在所述壳体的环形轨道上的圆周凸缘，所述环形凸缘轴向地接合在所述壳体轨道和环的法兰上。在环和装置之间插入大致圆筒形的隔热箔。箔片或器件包括至少一个额外的厚度，其分别承载在器件或箔上，以径向地固定该箔。

5. 发明申请

US20090123273A1 TURBINE OR COMPRESSOR STAGE FOR A TURBOJET 有权
标题翻译：涡轮机或压缩机阶段的涡轮机
公开(公告)号：US20090123273A1
公开(公告)日：2009-05-14
申请号：US12266813
申请日：2008-11-07
申请人： David Audeon , David Da Silva
发明人： David Audeon , David Da Silva
IPC分类号： F04D29/58
CPC分类号： F01D11/08 , F05D2240/11 , Y02T50/671 , Y10T24/44744
摘要： A turbojet turbine or compressor stage, comprising at least one rotor disk mounted inside a sectorized ring (120) supported by a casing (116) and comprising a circumferential flange (132) radially clamped on an annular rail (136) of the casing by a substantially C-shaped cross-section annular locking device (138) which is axially engaged on the casing rail and on the flange of the ring, a substantially cylindrical heat shielding foil (146) being interposed between the ring and the device, the foil, or the device, comprising at least one extra thickness (150) which respectively bears on the device, or the foil, to radially immobilize this foil.
摘要翻译：涡轮喷气涡轮机或压缩机级，包括安装在由壳体（116）支撑的扇形环（120）内的至少一个转子盘，并且包括径向地夹在壳体的环形轨道（136）上的周向凸缘（132）基本上为C形的横截面环形锁定装置（138），其轴向地接合在所述壳体轨道和所述环的凸缘上，大致圆柱形的热屏蔽箔（146）插入在所述环和所述装置之间，所述箔，或所述装置包括分别承载在所述装置上的至少一个额外的厚度（150）或所述箔，以径向地固定所述箔。

6. 发明授权

US08167552B2 Asymmetrical member for locking ring sectors to a turbine engine casing 有权
标题翻译：用于将环形部分锁定到涡轮发动机壳体的不对称构件
公开(公告)号：US08167552B2
公开(公告)日：2012-05-01
申请号：US12430542
申请日：2009-04-27
申请人： Serge Louis Antunes , David Da Silva
发明人： Serge Louis Antunes , David Da Silva
IPC分类号： F01D11/00
CPC分类号： F01D25/246 , F01D11/24 , F05D2240/11 , Y02T50/671
摘要： A locking member for a device for fastening ring sectors to an aircraft turbine engine casing is disclosed. The member has first and second clamping branches, which are connected together by curving joining portions, via a connecting branch. The joining portion of center thickness E1 has an inside surface of mean radius Rm1, and the joining portion of center thickness E2 has an inside surface of mean radius Rm2. Thickness E1 is strictly smaller than thickness E2, and mean radius Rm1 is strictly smaller than mean radius Rm2.
摘要翻译：公开了一种用于将环形部分紧固到飞行器涡轮发动机壳体的装置的锁定构件。该构件具有通过连接分支通过弯曲连接部分连接在一起的第一和第二夹持分支。中心厚度E1的接合部分具有平均半径Rm1的内表面，中心厚度E2的接合部分具有平均半径Rm2的内表面。厚度E1严格小于厚度E2，平均半径Rm1严格小于平均半径Rm2。

7. 发明申请

US20120091764A1 Passenger seating assemblies and aspects thereof 有权
标题翻译：乘客座椅总成及其方面
公开(公告)号：US20120091764A1
公开(公告)日：2012-04-19
申请号：US13066003
申请日：2011-04-04
申请人： Jeremy Cailleteau , David Da Silva
发明人： Jeremy Cailleteau , David Da Silva
IPC分类号： A47B83/02 , B60N2/46 , A47C7/54 , B60N2/44 , B64D11/06
CPC分类号： B64D11/0638 , B60N2/0224 , B60N2/682 , B60N2/686 , B60N2/757 , B60N3/004 , B64D11/003 , B64D11/06 , B64D11/0627 , B64D11/0636 , B64D11/064 , B64D11/0643 , B64D11/0644 , B64D11/0646
摘要： Multiple features of seating assemblies are detailed. Innovations in or to tray tables, luggage bars, arm rests, seat backs, and seat frames are included, with features being incorporated into seating assemblies either separately or in any combination. The assemblies are configured principally for passenger aircraft but may be used elsewhere as appropriate or desired.
摘要翻译：详细的座位组合的多个功能。包括托盘，行李箱，扶手，座椅靠背和座椅框架中的创新，其特征是单独地或以任何组合结合到座椅组件中。组件主要用于客机，但可以在其他地方适当或期望地使用。

8. 发明授权

US06717321B2 Electric motor comprising improved means of fixing an end flange to a stator shell 失效
标题翻译：电动马达包括将端部凸缘固定到定子壳体的改进装置
公开(公告)号：US06717321B2
公开(公告)日：2004-04-06
申请号：US09947934
申请日：2001-09-06
申请人： Thierry Mademba-Sy , David Da Silva , Michel Lehir
发明人： Thierry Mademba-Sy , David Da Silva , Michel Lehir
IPC分类号： H02K1300
CPC分类号： H02K5/15 , H02K5/148
摘要： An electric motor comprising a rotor secured to a shaft, a stator comprising a cylindrical shell receiving at one at least of the ends a flange provided with a roller bearing for the rotor shaft, the flange being fixed to the cylindrical shell by a fixing means having a bayonet-type assembly, wherein the assembling of the flange onto the shell being achieved through a relative displacement in an axial translation and a rotary relative motion.
摘要翻译：一种电动机，包括固定在轴上的转子，定子包括一个圆柱形壳体，该圆柱形壳体在至少一端至少接收一个凸缘，所述凸缘设置有用于转子轴的滚子轴承，所述凸缘通过固定装置固定到所述圆柱形壳体，一种卡口式组件，其中凸缘到外壳的组装通过轴向平移和旋转相对运动中的相对位移来实现。

9. 发明授权

US06240755B1 Handle for the door of an automobile vehicle comprising a lock cylinder cap 失效
标题翻译：用于汽车车门的手柄，包括锁芯盖
公开(公告)号：US06240755B1
公开(公告)日：2001-06-05
申请号：US09502319
申请日：2000-02-11
申请人： David Da Silva
发明人： David Da Silva
IPC分类号： E05B1718
CPC分类号： E05B17/186 , E05B77/34 , E05B85/10 , Y10T70/7955 , Y10T70/8649 , Y10T292/57
摘要： The invention proposes a handle for the door of an automobile vehicle, of the type in which the handle comprises an external gripping lever that is designed to be moved by a user from a rest position to an open position to control a lock that is associated with a lock cylinder of the type comprising a stator, one end of which is accessible from the outside so that a key can be inserted in the lock cylinder through a slit that opens out into the end of the cylinder, wherein the gripping lever comprises a protective cap and/or trim covering the lock cylinder that is assembled so that it is free to slide with respect to the gripping lever between a normal assembly position in which the cap conceals at least the slit in the lock cylinder when the gripping lever is in its rest position, and a displaced position enabling access to the key insertion slit.
摘要翻译：本发明提出了一种用于汽车车辆门的手柄，其中手柄包括外部夹持杆，其被设计成由使用者从静止位置移动到打开位置以控制与一种锁芯，其包括定子，其一端可从外部接近，使得钥匙能够通过开口到气缸的端部的狭缝插入到锁芯中，其中夹持杆包括保护帽和/或装饰件，其覆盖锁定缸体，其被组装成使得其在正常组装位置之间相对于抓握杆自由滑动，其中当夹持杆处于其中时，盖子至少隐藏在锁芯中的狭缝静止位置，以及允许进入钥匙插入缝隙的位移位置。

10. 发明申请

US20090285679A1 ASYMMETRICAL MEMBER FOR LOCKING RING SECTORS TO A TURBINE ENGINE CASING 有权
标题翻译：用于锁定环段的非对称构件到涡轮发动机壳体
公开(公告)号：US20090285679A1
公开(公告)日：2009-11-19
申请号：US12430542
申请日：2009-04-27
申请人： Serge Louis Antunes , David Da Silva
发明人： Serge Louis Antunes , David Da Silva
IPC分类号： F01D25/24
CPC分类号： F01D25/246 , F01D11/24 , F05D2240/11 , Y02T50/671
摘要： This invention relates to a locking member (24) for a device for fastening ring sectors to an aircraft turbine engine casing. The member has first and second clamping branches (28, 30), which are connected together by means of curving joining portions (36a, 36b), via a connecting branch (32), the joining portion (36a) of centre thickness E1 having an inside surface (36a′) of mean radius Rm1, and the joining portion (36b) of centre thickness E2 having an inside surface (36b′) of mean radius Rm2. According to the invention, thickness E1 is strictly smaller than thickness E2, and mean radius Rm1 is strictly smaller than mean radius Rm2.
摘要翻译：本发明涉及一种用于将环形部分紧固到飞行器涡轮发动机壳体的装置的锁定构件（24）。该构件具有通过连接分支（32）通过弯曲接合部分（36a，36b）连接在一起的第一和第二夹持分支（28,30），中心厚度E1的接合部分（36a）具有平均半径Rm1的内表面（36a'）和具有平均半径Rm2的内表面（36b'）的中心厚度E2的接合部分（36b）。根据本发明，厚度E1严格小于厚度E2，平均半径Rm1严格小于平均半径Rm2。

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