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公开(公告)号：US20120063914A1
公开(公告)日：2012-03-15
申请号：US13322027
申请日：2010-05-21
IPC分类号： F01D5/02
CPC分类号： F01D5/066 , F05D2250/712 , Y02T50/671
摘要： A low-pressure turbine for a turbomachine including turbine disks with festooned annular flanges for fastening to a festooned annular flange of a drive cone connecting the turbine disks to a turbine shaft, solid portions of the festooned annular flanges of the turbine disks and of the drive cone being connected to peripheries of the turbine disks and of the drive cone, respectively, via concave filets that are asymmetrical.
摘要翻译： 一种用于涡轮机的低压涡轮机，包括具有带有环形凸缘的涡轮盘，其具有用于紧固到将涡轮盘连接到涡轮轴的驱动锥的花键环形凸缘，涡轮盘的花式环形凸缘和驱动器的实心部分 锥体分别通过不对称的凹形盘连接到涡轮盘和驱动锥的周边。
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32.发明申请公开(公告)号：US20110274541A1
公开(公告)日：2011-11-10
申请号：US13127836
申请日：2009-09-29
IPC分类号： F01D25/28
CPC分类号： F01D5/066 , F01D25/243 , F01D25/246 , F05D2260/30 , F05D2260/31 , Y02T50/671
摘要： A radial annular flange including in inner or outer periphery alternating solid portions including orifices for passing fastener bolts, and hollow portions having bottoms that are substantially flat. The bottom of at least one keying hollow portion is situated radially inside, or outside, respectively, a circle centered on the axis of the flange and externally, or respectively internally, tangential to the orifices. Two hollow portions are situated on either side of the keying hollow portion having bottoms of concave curved shapes situated radially on the outside, or respectively on the inside, relative to the flat bottoms of the other hollow portions.
摘要翻译： 径向环形凸缘，其包括在内部或外部周边，交替的实心部分包括用于通过紧固件螺栓的孔口，以及具有基本上平坦的底部的中空部分。 至少一个键合中空部分的底部分别径向地位于或位于围绕凸缘的轴线的中心的圆周上，或者分别位于与孔口相切的内部。 两个中空部分位于键合中空部分的任一侧，具有相对于另一个中空部分的平坦底部径向位于外侧或分别在内侧的凹形弯曲形状的底部。
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公开(公告)号：US20080273980A1
公开(公告)日：2008-11-06
申请号：US12038864
申请日：2008-02-28
IPC分类号： F01D5/30
CPC分类号： F01D5/22 , F01D5/3023 , F01D5/3053 , F01D11/008 , F01D21/045 , F05B2260/301 , F16B43/00 , F16B2043/008
摘要： A turbomachine fan (10) comprising blades (12) and inter-blade platforms (18) having radial flanges (20) fastened to flanges (22) of a rotor disk (16) by means of threaded rods inserted into bushes (26) mounted in orifices in the flanges of the platforms (18), wherein each bush (26) comprises at least one deformable part (30) interposed transversely between the threaded rod (24) and an edge of the orifice in which the bush (26) is mounted, this deformable part (30) being intended to allow the platform (18) to pivot in the event of an impact of a blade (12) against the platform (18) and to absorb some of the energy of the impact.
摘要翻译： 包括叶片（12）和叶片间平台（18）的涡轮机风扇（10），其具有通过插入到衬套（26）中的螺杆固定到转子盘（16）的凸缘（22）的径向凸缘（20） 在平台（18）的凸缘中的孔中，其中每个衬套（26）包括至少一个可变形部分（30），所述可变形部分横向插入在所述螺杆（24）和所述孔的边缘之间，所述衬套（26） 该可变形部分（30）旨在允许平台（18）在叶片（12）碰撞平台（18）的情况下枢转并且吸收冲击的一些能量。
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公开(公告)号：US09039351B2
公开(公告)日：2015-05-26
申请号：US12994972
申请日：2009-04-27
CPC分类号： F01D5/026 , F01D5/06 , F01D25/243 , Y02T50/671
摘要： A radial annular flange of a rotor or stator element of a turbomachine including, at an inner/outer periphery, alternating solid portions and hollow portions, the solid portions including orifices for passing fastener bolts. The flange in the bottom of at least one hollow portion has a radius relative to the axis of the turbomachine that is less/greater than the radius of a circle that is tangential to the outsides/insides of the orifices for passing bolts through the solid portions.
摘要翻译： 涡轮机的转子或定子元件的径向环形凸缘在内/外周边包括交替的实心部分和中空部分，固体部分包括用于通过紧固件螺栓的孔口。 至少一个中空部分的底部中的凸缘具有相对于涡轮机的轴线的半径，该半径小于/大于与用于使螺栓穿过固体部分的孔口的外部/内部相切的圆的半径 。
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35.发明授权公开(公告)号：US08757980B2
公开(公告)日：2014-06-24
申请号：US13077033
申请日：2011-03-31
IPC分类号： F01D5/30
摘要： A one-piece rotor spool for a gas turbine engine extending along the axis of the engine is disclosed. The spool includes an upstream portion and a downstream portion that are radially offset relative to one another. The radially outer downstream portion includes a plurality of housings for rotor blades formed in the outer surface of the radially outer downstream portion. The radially inner upstream portion includes an attachment mechanism designed to interact with a rotor ring in order to prevent a tangential movement of the rotor ring relative to the radially inner upstream portion.
摘要翻译： 公开了一种用于沿发动机轴线延伸的燃气涡轮发动机的整体转子线轴。 卷轴包括相对于彼此径向偏移的上游部分和下游部分。 径向外部的下游部分包括形成在径向外部下游部分的外表面中的转子叶片的多个壳体。 径向内部上游部分包括设计成与转子环相互作用的附接机构，以便防止转子环相对于径向内部上游部分的切向运动。
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公开(公告)号：US20140072405A1
公开(公告)日：2014-03-13
申请号：US14118092
申请日：2012-05-15
IPC分类号： F01D25/02
CPC分类号： F01D25/02 , F02C7/047 , F05D2260/30
摘要： A turbomachine separator including a device for de-icing the turbomachine separator, and a distribution element, wherein the separator is formed by an inner ferrule and an outer ferrule, wherein the inner ferrule is fitted with a first mounting flange and a second mounting flange, the de-icing device including an internal air supply duct, able to inject air into the separator, wherein the internal supply duct is connected to an air inlet, wherein the air inlet forms a projection external to the de-icing device, allowing a flexible connection with a tube of the distribution element for conveying hot air, a first fastener constructed and arranged to be attached to the first mounting flange; and a second fastener constructed and arranged to be attached to the second mounting flange.
摘要翻译： 一种涡轮机分离器，包括用于使涡轮机分离器除冰的装置和分配元件，其中所述分离器由内套圈和外套圈形成，其中所述内套圈装配有第一安装凸缘和第二安装凸缘， 除冰装置包括能够将空气注入分离器的内部空气供应管道，其中内部供应管道连接到空气入口，其中空气入口形成除冰装置外部的突出部，允许柔性 与用于输送热空气的分配元件的管连接，构造和布置成附接到第一安装凸缘的第一紧固件; 以及构造和布置成附接到第二安装凸缘的第二紧固件。
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公开(公告)号：US20130064619A1
公开(公告)日：2013-03-14
申请号：US13699684
申请日：2011-05-12
CPC分类号： B23C3/30 , B23C7/00 , B23C2220/366 , Y10T409/303808 , Y10T409/30952
摘要： A machining method for machining peripheral slots in a disk of a turbine of a turbine engine, such as an airplane turboprop or turbojet, the method including: machining the slots by reaming using a substantially cylindrical reamer of length greater than an axial thickness of the disk, and extending substantially parallel to the axis of the disk, outlines of the slots being machined by moving the reamer perpendicularly to its axis along the profile of each slot.
摘要翻译： 一种加工方法，用于加工诸如飞机涡旋螺旋桨或涡轮喷气发动机之类的涡轮发动机的涡轮机的圆周槽中的周边槽，该方法包括：利用长度大于盘的轴向厚度的大致圆柱形的铰刀来扩孔来加工槽 并且基本上平行于盘的轴线延伸，通过沿着每个槽的轮廓垂直于其轴线移动铰刀来加工槽的轮廓。
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公开(公告)号：US20120244001A1
公开(公告)日：2012-09-27
申请号：US13513227
申请日：2010-12-06
IPC分类号： F01D5/30
CPC分类号： F01D5/3015 , F01D5/326 , F05D2260/30
摘要： A retaining ring assembly for at least one blade of a rotor disk of a turbine engine and a supporting flange for the ring. The flange and the ring are rotating parts having an axis X, the flange including an attachment edge configured to be connected to the rotor disk and a free edge configured to bear against the retaining ring; and the flange bears against the ring such that the bearing force of the flange on the ring has an axial component and a radial component relative to the axis of revolution X.
摘要翻译： 一种用于涡轮发动机的转子盘的至少一个叶片和用于环的支撑凸缘的保持环组件。 凸缘和环是具有轴线X的旋转部件，凸缘包括构造成连接到转子盘的附接边缘和被配置为承受保持环的自由边缘; 并且凸缘抵靠环，使得环上的凸缘的支承力具有相对于旋转轴线X的轴向分量和径向分量。
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公开(公告)号：US08257023B2
公开(公告)日：2012-09-04
申请号：US12055615
申请日：2008-03-26
IPC分类号： F01D5/04
CPC分类号： F04D19/022 , F01D5/146 , F01D5/147 , F05D2220/326 , F05D2220/327 , Y02T50/671 , Y02T50/673
摘要： The present invention relates to the field of blades, particularly fan blades, intended for turbojets, particularly of the aeronautical type. Its objective is to provide a fan blade the features of which will enable the number of fan blades to be reduced while at the same time providing satisfactory performance. According to the invention, the fan blade comprises a plurality of aerodynamic parts which are superposed in a radial direction Z and the number of aerodynamic profiles varies from one aerodynamic part to the other.
摘要翻译： 本发明涉及用于涡轮喷气发动机，特别是航空类型的叶片领域，特别是风扇叶片领域。 其目的是提供一种风扇叶片，其特征在于能够减少风扇叶片的数量，同时提供令人满意的性能。 根据本发明，风扇叶片包括多个空气动力部件，它们沿径向Z重叠，并且空气动力学轮廓的数量从一个空气动力部分变化到另一个。
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公开(公告)号：US20110097206A1
公开(公告)日：2011-04-28
申请号：US12994972
申请日：2009-04-27
IPC分类号： F01D9/00
CPC分类号： F01D5/026 , F01D5/06 , F01D25/243 , Y02T50/671
摘要： A radial annular flange of a rotor or stator element of a turbomachine including, at an inner/outer periphery, alternating solid portions and hollow portions, the solid portions including orifices for passing fastener bolts. The flange in the bottom of at least one hollow portion has a radius relative to the axis of the turbomachine that is less/greater than the radius of a circle that is tangential to the outsides/insides of the orifices for passing bolts through the solid portions.
摘要翻译： 涡轮机的转子或定子元件的径向环形凸缘在内/外周边包括交替的实心部分和中空部分，固体部分包括用于通过紧固件螺栓的孔口。 至少一个中空部分的底部中的凸缘具有相对于涡轮机的轴线的半径，该半径小于/大于与用于使螺栓穿过固体部分的孔口的外部/内部相切的圆的半径 。
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