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公开(公告)号：US08152460B2
公开(公告)日：2012-04-10
申请号：US12332685
申请日：2008-12-11
CPC分类号： F04D29/545 , F04D27/0215
摘要： A turbomachine compressor, including an air bleed device including a duct having a suction end opening out into an outer casing of the compressor level with a rotor wheel and a stator stage of the compressor is disclosed. A screen sheet of annular shape is mounted radially inside the casing facing a portion of the suction end of the duct so as to make the bleeding of air uniform over 360° around the axis of the compressor.
摘要翻译： 公开了一种涡轮机压缩机，其包括排气装置，其包括具有吸入端的管道，所述管道具有与压缩机级别的外壳体一起转动的转子轮和压缩机的定子级。 环形屏幕片径向安装在壳体内部，面向管道的吸入端的一部分，以使空气的渗出在压缩机的轴线周围均匀地超过360°。
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公开(公告)号：US08777558B2
公开(公告)日：2014-07-15
申请号：US12935132
申请日：2009-03-25
申请人： Antoine Robert Alain Brunet , Olivier Stephane Domercq , Laurent Jablonski , Vincent Paul Gabriel Perrot
发明人： Antoine Robert Alain Brunet , Olivier Stephane Domercq , Laurent Jablonski , Vincent Paul Gabriel Perrot
CPC分类号： F04D29/526 , F04D29/164 , F04D29/685
摘要： A casing for a turbomachine rotor wheel includes a plurality of circumferential grooves, each of substantially constant section, with the section areas of the circumferential grooves decreasing from upstream to downstream on going from the first groove to the last groove. By treating the casing in this way, the efficiency of the rotor wheel is optimized and its surge margin is improved.
摘要翻译： 用于涡轮机转子轮的壳体包括多个周向槽，每个周向槽基本上恒定的部分，周向槽的截面从第一槽到最后槽从上游到下游减小。 通过这种方式处理外壳，优化了转子轮的效率，提高了转速轮缘的效率。
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公开(公告)号：US20110085896A1
公开(公告)日：2011-04-14
申请号：US12935132
申请日：2009-03-25
申请人： Antoine Robert Alain Brunet , Olivier Stephane Domercq , Laurent Jablonski , Vincent Paul Gabriel Perrot
发明人： Antoine Robert Alain Brunet , Olivier Stephane Domercq , Laurent Jablonski , Vincent Paul Gabriel Perrot
IPC分类号： F01D25/24
CPC分类号： F04D29/526 , F04D29/164 , F04D29/685
摘要： A casing for a turbomachine rotor wheel includes a plurality of circumferential grooves, each of substantially constant section, with the section areas of the circumferential grooves decreasing from upstream to downstream on going from the first groove to the last groove. By treating the casing in this way, the efficiency of the rotor wheel is optimized and its surge margin is improved.
摘要翻译： 用于涡轮机转子轮的壳体包括多个周向槽，每个周向槽基本上恒定的部分，周向槽的截面从第一槽到最后槽从上游到下游减小。 通过这种方式处理外壳，优化了转子轮的效率，提高了转速轮缘的效率。
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公开(公告)号：US08967969B2
公开(公告)日：2015-03-03
申请号：US13388317
申请日：2010-07-23
CPC分类号： F16F1/324 , F16C25/083 , F16C2360/00 , F16F3/02
摘要： A prestressing device extending about an axis between a first plane that is substantially perpendicular to the axis and a second plane that is substantially parallel to the first plane and axially offset relative to the latter. The device includes a first annular body extending in the first plane, and a first series of at least three tabs, each of which is connected to the first body and extending in an essentially radial direction, each of the tabs of the first series including a planar surface extending in the second plane. This arrangement ensures surface contact between the parts of the elements to be subjected to prestressing. The device can be used for example for a rotor, and for example for a rotor of an unducted propeller for a turbine engine.
摘要翻译： 预应力装置，其围绕基本上垂直于所述轴线的第一平面之间的轴线延伸，以及基本上平行于所述第一平面并相对于所述第一平面轴向偏移的第二平面。 该装置包括在第一平面中延伸的第一环形体和至少三个突出部的第一系列，每个突片连接到第一主体并沿基本上径向方向延伸，第一系列的每个突片包括一个 平面在第二平面中延伸。 这种布置确保要进行预应力的元件的部分之间的表面接触。 该装置可以例如用于转子，并且例如用于涡轮发动机的未被驱动的螺旋桨的转子。
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公开(公告)号：US08827653B2
公开(公告)日：2014-09-09
申请号：US13258481
申请日：2010-02-23
CPC分类号： B64C11/06 , B64C11/48 , B64D2027/026 , F16C19/163 , F16C23/06 , F16C35/073 , F16C2326/43 , F16C2360/23 , Y02T50/66
摘要： A non-streamlined propeller including blades with a variable setting for a turbine engine, the blades of the propeller being rotatably mounted about the axes thereof in radial recesses of a rotor element, and each blade being supported by a plate held in a recess by a sectored ring, and including an inner portion mounted, by interlocking, in a groove of the plate, the ring sectors being inserted into the recess from the inside and locked by a nut screwed onto the plate.
摘要翻译： 一种非流线型螺旋桨，包括具有用于涡轮发动机的可变设置的叶片，螺旋桨的叶片围绕其轴线可旋转地安装在转子元件的径向凹部中，并且每个叶片由保持在凹部中的板支撑 并且包括通过互锁地安装在所述板的槽中的内部部分，所述环形部分从内部插入到所述凹部中并且被螺纹拧入所述板上的螺母锁定。
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6.发明申请ASSEMBLY HAVING A CONTROL DEVICE WITH RACKS FOR CONTROLLING THE ANGULAR POSITION OF PIVOTALLY-MOUNTED BLADES IN A TURBINE ENGINE 有权具有用于控制涡轮发动机中的倾斜叶片的角度位置的控制装置的组装公开(公告)号：US20130011261A1
公开(公告)日：2013-01-10
申请号：US13578765
申请日：2011-02-07
IPC分类号： F01D7/00
CPC分类号： F04D29/362 , B63H3/002 , B64C11/32 , B64C11/48 , B64D2027/026 , F03D7/0224 , F04D29/36 , F05D2260/74
摘要： An assembly in a turbine engine for controlling plural toothed pivotally-mounted blades arranged in azimuth around the axis of the turbine engine and including an actuator ring controlling a position of the blades. Racks mounted on the ring present corresponding sets of teeth meshing with the set of teeth of a respective one of the blades to place it in a selected angular position, and they are held in the radial direction by radial positioning mechanism fastened to the blade. Each rack is mounted on the ring by plural guides spaced apart circumferentially around the ring, that connect together movements of the rack and of the ring in the circumferential direction, and that are configured to slide relative to the ring, for each guide in its own radial direction, and relative to the rack in a direction of movement that is substantially radial and specific to the rack.
摘要翻译： 涡轮发动机中的组件，其用于控制围绕涡轮发动机的轴线方位布置的多个带齿的可枢转地安装的叶片，并且包括控制叶片位置的致动器环。 安装在环上的机架呈现出与相应一个叶片的齿组啮合的相应组齿，以将其置于选定的角度位置，并且通过紧固到叶片的径向定位机构将其保持在径向方向。 每个机架通过围绕环周向间隔开的多个引导件安装在环上，所述引导件在圆周方向上将齿条和环的运动连接在一起，并且被配置为相对于环滑动，对于每个引导件在其自身中 径向方向，并且相对于齿条在基本上径向并且特定于齿条的运动方向上。
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公开(公告)号：US20120128490A1
公开(公告)日：2012-05-24
申请号：US13388461
申请日：2010-07-23
CPC分类号： F16F1/328 , B64D2027/005 , F01D25/164 , F02C6/206 , F05D2220/36 , F05D2250/182 , F05D2250/184 , F05D2300/501 , F16C25/083 , F16C2360/00 , F16F1/027 , Y02T50/66
摘要： A prestressing device extending about an axis between a first plane and a second plane, the first plane being located at a predetermined distance from the second plane, each plane being perpendicular to the axis. The device includes at least three deformation areas. The deformation areas extend in the first plane. The device further includes, between each deformation area, a planar contact surface extending in the second plane.
摘要翻译： 一个在第一平面和第二平面之间围绕轴线延伸的预应力装置，第一平面位于与第二平面预定距离处，每个平面垂直于轴线。 该装置包括至少三个变形区域。 变形区域在第一平面内延伸。 该装置还在每个变形区域之间包括在第二平面中延伸的平面接触表面。
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公开(公告)号：US20050022535A1
公开(公告)日：2005-02-03
申请号：US10900111
申请日：2004-07-28
CPC分类号： F02C7/185 , F01D25/12 , F04D29/584 , F05D2260/213 , Y02T50/676
摘要： The invention relates to a method of supplying cooling air to the hot portions of a turbojet that comprises, from upstream to downstream: a compressor; a diffuser; a combustion chamber; a distributor; and a turbine driving said compressor, in which method a flow of air is bled from the flow of air delivered by the compressor, the bled-off flow is cooled in a heat exchanger situated radially outside the combustion chamber, and is then directed radially inwards via the stationary blades of the distributor and used for cooling the moving wheel of the turbine, the method wherein the flow of cooling air is bled from the zone of the end of the combustion chamber that surrounds the diffuser, and wherein the stationary blades of the distributor are also cooled by a second flow of air bled from the diffuser.
摘要翻译： 本发明涉及向涡轮喷气发动机的热部分供应冷却空气的方法，所述方法包括从上游到下游：压缩机; 扩散器 燃烧室; 经销商 以及驱动所述压缩机的涡轮机，在该方法中，空气流从压缩机输送的空气流中排出，该排出流在位于燃烧室径向外侧的热交换器中冷却，然后径向向内 通过分配器的固定叶片并用于冷却涡轮机的移动轮，其中冷却空气的流动从围绕扩散器的燃烧室的端部的区域排出，并且其中固定叶片 分配器也通过从扩散器排出的第二次空气流冷却。
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9.发明授权Assembly having a control device with racks for controlling the angular position of pivotally-mounted blades in a turbine engine 有权具有控制装置的组件具有用于控制涡轮发动机中枢转安装的叶片的角位置的齿条公开(公告)号：US09068574B2
公开(公告)日：2015-06-30
申请号：US13578765
申请日：2011-02-07
CPC分类号： F04D29/362 , B63H3/002 , B64C11/32 , B64C11/48 , B64D2027/026 , F03D7/0224 , F04D29/36 , F05D2260/74
摘要： An assembly in a turbine engine for controlling plural toothed pivotally-mounted blades arranged in azimuth around the axis of the turbine engine and including an actuator ring controlling a position of the blades. Racks mounted on the ring present corresponding sets of teeth meshing with the set of teeth of a respective one of the blades to place it in a selected angular position, and they are held in the radial direction by radial positioning mechanism fastened to the blade. Each rack is mounted on the ring by plural guides spaced apart circumferentially around the ring, that connect together movements of the rack and of the ring in the circumferential direction, and that are configured to slide relative to the ring, for each guide in its own radial direction, and relative to the rack in a direction of movement that is substantially radial and specific to the rack.
摘要翻译： 涡轮发动机中的组件，其用于控制围绕涡轮发动机的轴线方位布置的多个带齿的可枢转地安装的叶片，并且包括控制叶片位置的致动器环。 安装在环上的机架呈现出与相应一个叶片的齿组啮合的相应组齿，以将其置于选定的角度位置，并且通过紧固到叶片的径向定位机构将其保持在径向方向。 每个机架通过围绕环周向间隔开的多个引导件安装在环上，所述引导件在圆周方向上将齿条和环的运动连接在一起，并且被配置为相对于环滑动，对于每个引导件在其自身中 径向方向，并且相对于齿条在基本上径向并且特定于齿条的运动方向上。
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公开(公告)号：US20130315744A1
公开(公告)日：2013-11-28
申请号：US13983241
申请日：2012-02-20
IPC分类号： F01D5/30
CPC分类号： F01D5/3069 , F01D5/3015 , F04D29/321 , F04D29/322 , F05D2220/36
摘要： A fan rotor including a disk carrying blades including roots engaged in slots in the disk, a frustoconical cap mounted on the disk upstream from the blades, and a retaining mechanism axially retaining the blades on the disk and including a ring mounted in an annular groove of the disk and forming an abutment for the roots of the blades, the ring being festooned or crenellated and co-operating with a festooned radial annular bead of the annular groove of the disk, and a mechanism preventing the ring from moving in rotation, which includes an annulus carrying at least one axial tooth inserted in hollow portions of the bead of the disk and of the ring, the annulus being fastened by bolts on an upstream radial face of the disk.
摘要翻译： 一种风扇转子，包括一个带有叶片的盘片，叶片包括啮合在盘中的槽中的根部，一个安装在叶片上方的盘上的截头圆锥形盖，以及一个将叶片轴向保持在盘上的保持机构， 并且形成用于叶片根部的邻接件，该环被挂饰或锯齿，并且与盘的环形槽的花式径向环形凸缘配合，以及防止环旋转运动的机构，其包括 一个带有至少一个轴向齿的环形空间，该轴向齿插入盘和环的胎圈的中空部分中，环通过螺栓紧固在盘的上游径向面上。
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