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1.发明授权Turbo aero engine provided with a device for heating turbine disks on revving up 失效涡轮增压涡轮发动机配有一个加热涡轮盘的装置
公开(公告)号：US5586860A
公开(公告)日：1996-12-24
申请号：US332101
申请日：1994-10-31
CPC分类号： F01D5/082 , Y02T50/676
摘要： Turbo aero engine including a heating arrangement for the internal portions (12) of turbine disks on revving up so as to reduce the temperature gradient in the disks. Heating gas passes through pipes (11) integral with the stator and reheats the disks by passing through a gasket (13) designed with the tongues (18) and orifices (20 and 22) which allow the gas to circulate towards the zones to be heated when the revving up has firstly heated the portions of the machine close to the pipes (11) and then makes it possible to interrupt the communication when the temperatures even out and the original heat expansions become uniform and offset the orifices (20 and 23).
摘要翻译： 涡轮增压器航空发动机包括用于涡轮盘的内部部分（12）的加热装置，用于减小涡轮盘中的温度梯度。 加热气体通过与定子成一体的管道（11），并通过设置有舌片（18）和孔口（20和22）的垫圈（13）再次加热盘片，该垫圈（13）和孔口（20和22）允许气体朝向待加热区域循环 当加速首先将机器的部分靠近管道（11）加热，然后当温度均匀并且原始热膨胀变得均匀并偏移孔口（20和23）时，可以中断连通。
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公开(公告)号：US07182508B2
公开(公告)日：2007-02-27
申请号：US10915913
申请日：2004-08-11
申请人： Jean-Louis Bertrand , Daniel Fiammingo , Daniel Moille , William Passaquin , Sylvie Ribeyrolles , Yvan Serikoff
发明人： Jean-Louis Bertrand , Daniel Fiammingo , Daniel Moille , William Passaquin , Sylvie Ribeyrolles , Yvan Serikoff
IPC分类号： G04B37/00
CPC分类号： G04B19/283 , G04B19/28
摘要： This device comprises a first axial retention shoulder secured to the case, adjacent to a cylindrical seat, a second, opposite axial retention shoulder formed by one face of an annular groove secured to the rim, an annular retention element made of polymer bearing against each of said shoulders, said first shoulder being adjacent to the base of a conical surface, secured to the case, for the axial introduction of said annular retention element engaged with said annular groove. Said annular retention element forms an endless ring whose section is divided in the radial direction into two portions of which one is, perpendicularly to the plane of said endless ring, substantially thinner than the other, these two portions being intended to interact respectively with said first shoulder and second shoulder.
摘要翻译： 该装置包括固定到壳体上的与圆柱形座相邻的第一轴向保持凸肩，由固定到轮辋的环形槽的一个面形成的第二相对轴向保持肩部，由聚合物制成的环形保持元件， 所述肩部，所述第一肩部邻近锥形表面的基部，固定到所述壳体，用于轴向引入与所述环形槽接合的所述环形保持元件。 所述环形保持元件形成环形环，该环形部分在径向上分成两部分，垂直于所述环形环的平面，其中一部分基本上比另一部分薄，这两部分分别与所述第一 肩和第二肩。
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公开(公告)号：US20050007890A1
公开(公告)日：2005-01-13
申请号：US10915913
申请日：2004-08-11
申请人： Jean-Louis Bertrand , Daniel Fiammingo , Daniel Moille , William Passaquin , Sylvie Ribeyrolles , Yvan Serikoff
发明人： Jean-Louis Bertrand , Daniel Fiammingo , Daniel Moille , William Passaquin , Sylvie Ribeyrolles , Yvan Serikoff
CPC分类号： G04B19/283 , G04B19/28
摘要： This device comprises a first axial retention shoulder secured to the case, adjacent to a cylindrical seat, a second, opposite axial retention shoulder formed by one face of an annular groove secured to the rim, an annular retention element made of polymer bearing against each of said shoulders, said first shoulder being adjacent to the base of a conical surface, secured to the case, for the axial introduction of said annular retention element engaged with said annular groove. Said annular retention element forms an endless ring whose section is divided in the radial direction into two portions of which one is, perpendicularly to the plane of said endless ring, substantially thinner than the other, these two portions being intended to interact respectively with said first shoulder and second shoulder.
摘要翻译： 该装置包括固定到壳体上的与圆柱形座相邻的第一轴向保持凸肩，由固定到轮辋的环形槽的一个面形成的第二相对轴向保持肩部，由聚合物制成的环形保持元件， 所述肩部，所述第一肩部邻近锥形表面的基部，固定到所述壳体，用于轴向引入与所述环形槽接合的所述环形保持元件。 所述环形保持元件形成环形环，该环形部分在径向上分成两部分，垂直于所述环形环的平面，其中一部分基本上比另一部分薄，这两部分分别与所述第一 肩和第二肩。
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4.发明授权公开(公告)号：US06890151B2
公开(公告)日：2005-05-10
申请号：US10283279
申请日：2002-10-30
CPC分类号： F01D25/246 , F01D9/042 , F04D29/542
摘要： A fixed guide vane assembly includes a circular casing composed of at least two parts (11) and supporting sectors (5), each composed of an inner segment (7) and an outer segment (6) connected by vanes (8). The parts of the casing and the sectors of the guide vane assembly are held together by a system forming a slide and a slider. An anti-rotation mechanism (30) is provided to prevent the sectors from rotating with respect to the casing.
摘要翻译： 固定导向叶片组件包括由至少两个部分（11）和支撑扇区（5）组成的圆形壳体，每个部分由内部段（7）和由叶片（8）连接的外部段（6）构成。 壳体的部件和导叶组件的扇区通过形成滑块和滑块的系统保持在一起。 提供防旋转机构（30）以防止扇区相对于壳体旋转。
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公开(公告)号：US4730983A
公开(公告)日：1988-03-15
申请号：US89414
申请日：1987-08-26
申请人： Jacky Naudet , Jean-Louis Bertrand
发明人： Jacky Naudet , Jean-Louis Bertrand
CPC分类号： F01D5/3015 , F01D11/006
摘要： A locking and sealing system is disclosed for attaching a rotor blade to a rotor blade disk in a turbojet engine. The system has a first split ring member which locks the rotor blade foot portion onto the rotor blade disk. A second split ring member is inserted between the first split ring member in a downstream flange of the rotor blade foot portions to provide a positive seal to prevent air leakage between the foot portions and the notches formed in the rotor disk.
摘要翻译： 公开了用于将转子叶片附接到涡轮喷气发动机中的转子叶片盘的锁定和密封系统。 该系统具有第一开口环构件，其将转子叶片脚部分锁定到转子叶片盘上。 第二开口环构件插入在转子叶片脚部的下游凸缘中的第一开口环构件之间，以提供正密封，以防止脚部和形成在转子盘中的凹口之间的空气泄漏。
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公开(公告)号：US07901129B2
公开(公告)日：2011-03-08
申请号：US12164864
申请日：2008-06-30
CPC分类号： G04B37/05 , G04B37/084 , G04B37/22
摘要： This watch case comprises a protective casing surrounded by a middle (5) and a bezel (9). The protective casing includes a glass (3), a side wall (2) and a bottom (1). A planar peripheral surface extending along the entire edge of the inner face of the glass is in contact with a similar bearing surface on the side wall (2), at least part of which forms the width of the cross section of a pressure resistant structure having parallel lateral faces (SR) perpendicular to the bearing surface, and which extends without a gap as far as the bottom (1) of the casing. The components of the casing are secured and sealed with at least one annular seal (4) surrounding the lateral face of the glass (3) and the outer lateral face of the side wall (2) of the casing, and this seal is clamped.
摘要翻译： 该表壳包括由中间（5）和边框（9）包围的保护壳体。 保护壳体包括玻璃（3），侧壁（2）和底部（1）。 沿着玻璃的内表面的整个边缘延伸的平面周边表面与侧壁（2）上的相似的支承表面相接触，其至少一部分形成了耐压结构的横截面的宽度， 垂直于支承表面的平行的侧面（SR），并且在与壳体的底部（1）没有间隙的情况下延伸。 壳体的部件用围绕玻璃（3）的侧面和壳体的侧壁（2）的外侧面的至少一个环形密封件（4）固定和密封，并且该密封件被夹紧。
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7.发明申请Rotation-locking of sectors of rectifier blades by bars in the parting planes of the housing 有权在壳体的分型平面中通过杆旋转锁定整流器叶片公开(公告)号：US20050079047A1
公开(公告)日：2005-04-14
申请号：US10925996
申请日：2004-08-26
申请人： Jean-Louis Bertrand , Jean-Francois Chabot , Leopold De-Verduzan , Francis Dome , Julien Girardot , Stephanie Pariset
发明人： Jean-Louis Bertrand , Jean-Francois Chabot , Leopold De-Verduzan , Francis Dome , Julien Girardot , Stephanie Pariset
CPC分类号： F01D9/042 , F01D25/246
摘要： The invention relates to a rotation-locking device of a sector of rectifier blades (5) mounted in a sector of the turbojet housing. A sector of blades comprises a support base (3). A housing sector comprises two recesses perpendicular to the axis of the housing, each receiving an edge (34-1, 34-2) of the support base. At one and the same axial end of the housing sector, each recess opens out into a seat (30-1, 30-2) defining an axial face (32-1). The device comprises an axial stop (26) adapting itself on each side in the seats (30-1; 30-1) of the two recesses, and once the complementary sector of the housing is installed and during operation of the turbojet, bearing on the axial faces (32-1) under the thrust of the complementary sector of rectifier blades in order to provide rotation locking.
摘要翻译： 本发明涉及一种安装在涡轮喷气发动机壳体的扇形区中的整流叶片（5）的扇形旋转锁定装置。 刀片扇区包括支撑基座（3）。 壳体扇区包括垂直于壳体的轴线的两个凹槽，每个凹部接收支撑基座的边缘（34-1,34-2）。 在壳体扇形体的同一轴向端部处，每个凹部开口形成限定轴向面（32-1）的座（30-1,30-2）。 该装置包括在两个凹部的座（30-1,30-1）中的每一侧自适应的轴向止动件（26），并且一旦壳体的互补部分被安装并且在涡轮喷气发动机运行期间 在整流叶片的互补扇区的推力下的轴向面（32-1）以提供旋转锁定。
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8.发明授权Retaining arrangement for a bearing, in particular for a high pressure compressor shaft 有权用于轴承的保持装置，特别是用于高压压缩机轴公开(公告)号：US06338578B1
公开(公告)日：2002-01-15
申请号：US09554516
申请日：2000-05-17
申请人： Danielle Christiane Roberte Adde , Jean-Louis Bertrand , Gérard Jean Lavigne , Olivier Richard Lefebvre
发明人： Danielle Christiane Roberte Adde , Jean-Louis Bertrand , Gérard Jean Lavigne , Olivier Richard Lefebvre
IPC分类号： F16C3364
CPC分类号： F01D25/162 , F02C7/36 , F05D2230/64 , F05D2230/70 , F05D2260/30 , F16C19/06 , F16C35/073 , F16C2360/23 , Y10S384/906
摘要： A retaining arrangement is provided for retaining a bearing around a stub shaft having a machined cavity and which includes a ring forming a stop for the bearing nut and a locking piece.
摘要翻译： 提供保持装置用于将轴承保持在具有加工空腔的短轴周围，并且包括形成用于轴承螺母和锁定件的止挡件的环。
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公开(公告)号：US20120218393A1
公开(公告)日：2012-08-30
申请号：US13044184
申请日：2011-03-09
IPC分类号： H04N13/04
CPC分类号： G06T7/97 , G02B27/2214 , G06T2207/10021 , G06T2207/20228 , H04N13/111 , H04N13/161 , H04N13/282
摘要： An automatic method for producing 3D multi-view interweaved image(s) from a stereoscopic image pair source to be displayed via an auto-multiscopic display. The technique is optimized to allow its use as part of a real-time 3D video handling system. Preferably, the 3D interweaved image(s) are generated from a stereo pair where partial disparity is calculated between the pixels of the stereo images. The partial disparity information is then used at a sub-pixel level to produce a series of target (intermediary) views for the sub-pixel components at each image position (x, y). Then, these target views are used to generate a desired number of views resulting in glass-free 3D via an auto-multiscopic display.
摘要翻译： 一种用于从立体图像对源产生3D多视角交织图像以通过自动多显示显示来显示的自动方法。 该技术被优化，以允许其作为实时3D视频处理系统的一部分使用。 优选地，3D交织的图像是从在立体图像的像素之间计算部分差异的立体对产生的。 然后在子像素级别处使用部分视差信息以在每个图像位置（x，y）处产生用于子像素分量的一系列目标（中间）视图。 然后，这些目标视图用于产生期望数量的视图，通过自动多显示显示产生无玻璃3D。
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10.发明授权Rotation-locking of sectors of rectifier blades by bars in the parting planes of the housing 有权在壳体的分型平面中通过杆旋转锁定整流器叶片公开(公告)号：US07059832B2
公开(公告)日：2006-06-13
申请号：US10925996
申请日：2004-08-26
申请人： Jean-Louis Bertrand , Jean-Francois Laurent Chabot , Leopold Jean-Marie De-Verduzan , Francis Dome , Julien Girardot , Stephanie Pariset
发明人： Jean-Louis Bertrand , Jean-Francois Laurent Chabot , Leopold Jean-Marie De-Verduzan , Francis Dome , Julien Girardot , Stephanie Pariset
IPC分类号： F01D9/04
CPC分类号： F01D9/042 , F01D25/246
摘要： The invention relates to a rotation-locking device of a sector of rectifier blades (5) mounted in a sector of the turbojet housing. A sector of blades comprises a support base (3). A housing sector comprises two recesses perpendicular to the axis of the housing, each receiving an edge (34-1, 34-2) of the support base. At one and the same axial end of the housing sector, each recess opens out into a seat (30-1, 30-2) defining an axial face (32-1). The device comprises an axial stop (26) adapting itself on each side in the seats (30-1; 30-1) of the two recesses, and once the complementary sector of the housing is installed and during operation of the turbojet, bearing on the axial faces (32-1) under the thrust of the complementary sector of rectifier blades in order to provide rotation locking.
摘要翻译： 本发明涉及一种安装在涡轮喷气发动机壳体的扇形区中的整流叶片（5）的扇形旋转锁定装置。 刀片扇区包括支撑基座（3）。 壳体扇区包括垂直于壳体的轴线的两个凹槽，每个凹部接收支撑基座的边缘（34-1,34-2）。 在壳体扇形体的同一个轴向端处，每个凹部开口形成限定轴向面（32-1）的座（30-1,30-2）。 该装置包括在两个凹部的座（30-1,30-1）中的每一侧自适应的轴向止动件（26），并且一旦外壳的互补部分被安装并且在涡轮喷气发动机运行期间 在整流叶片的互补扇区的推力下面的轴向面（32-1）以提供旋转锁定。
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