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51. 发明公开

EP2623729A3 Gas turbine engine with a fan and booster joint and corresponding method 有权
标题翻译： Gasturbinentriebwerk mit einemGebläseund Booster-AnschlussstückundzugehörigesVerfahren
公开(公告)号：EP2623729A3
公开(公告)日：2015-07-08
申请号：EP13153474.5
申请日：2013-01-31
申请人： Pratt & Whitney Canada Corp.
发明人： Ivakitch, Richard , Eleftheriou, Andreas , Bonniere, Philippe
IPC分类号： F01D21/04 , F01D25/16 , F01D5/06 , F01D5/02
CPC分类号： F01D21/04 , F01D5/066 , F01D21/045 , F05D2220/36 , F05D2250/75 , Y10T29/49318
摘要： A gas turbine engine having at least one spool assembly, the at least one spool assembly including a fan rotor (14), a compressor (16) disposed downstream of the fan rotor (14), a turbine (18) and a shaft (12) connecting the fan rotor (14), compressor (16) and turbine (18), a joint (32) affixed to an upstream end (36) of the shaft (12), and including a first link (40) connecting the fan rotor (14) to the shaft (12) and a second link (42) connecting the compressor (16) to the shaft (12), the second link (42) being less rigid then the first link (40). A corresponding method of disassociating a fan rotor deflection from a compressor deflection is also provided.
摘要翻译：一种具有至少一个阀芯组件的燃气涡轮发动机，所述至少一个阀芯组件包括风扇转子（14），设置在所述风扇转子（14）下游的压缩机（16），涡轮机（18）和轴（12 ，连接风扇转子（14），压缩机（16）和涡轮机（18），固定在轴（12）的上游端（36）的接头（32），并且包括连接风扇转子（14）连接到轴（12）和将压缩机（16）连接到轴（12）的第二连杆（42），第二连杆（42）刚好比第一连杆（40）刚刚。还提供了将风扇转子偏转与压缩机偏转分离的相应方法。

52. 发明公开

EP2846005A3 Vorrichtung zur Energieabsorption, Strömungsmaschine und Verfahren zur Energieabsorption 有权
标题翻译：一种用于能量流机的吸收和用于能量吸收设备的方法
公开(公告)号：EP2846005A3
公开(公告)日：2015-07-01
申请号：EP14179664.9
申请日：2014-08-04
申请人： MTU Aero Engines AG
发明人： Sasse, Stefan , Schinko, Norbert
IPC分类号： F01D21/04 , F01D25/24 , F01D17/02 , F02C7/05
CPC分类号： F01D21/045 , F01D17/02 , F01D21/04 , F01D25/24 , F02C7/05 , F05D2260/311 , Y02T50/671
摘要： Offenbart ist eine Vorrichtung (1) zur Absorption einer auf ein Element (2) wirkenden Einschlagenergie zumindest eines Schaufelfragments, wobei das Element in eine Öffnung (10) einer Strömungsmaschine eingesetzt ist, die einen Gehäuseabschnitt (6) im Bereich einer Laufschaufelreihe radial durchsetzt, wobei die Vorrichtung eine Halterung (18) zum Halten des Elements in einer Soll-Position aufweist, die ab einer voreingestellten Maximalbelastung das Element freigibt, und einen rückwärtigen Käfig (22) zum Sichern des Elements bei einer radial nach außen gerichteten Verschiebung hat, eine Strömungsmaschine mit einer derartigen Vorrichtung, sowie ein Verfahren zur mehrstufigen Energieabsorption.

53. 发明公开

EP2848776A2 Compressor blade monitoring system 审中-公开
标题翻译： Verdichterschaufelüberwachungssystem
公开(公告)号：EP2848776A2
公开(公告)日：2015-03-18
申请号：EP14184199.9
申请日：2014-09-10
申请人： General Electric Company
发明人： Yu, Lijie , Ansari, Adil , Badami, Vivek Venugopal , Bliss, John Thomas , Chadha, Rahul , Gupta, Rajan
IPC分类号： F01D21/00 , F01D21/14
CPC分类号： F04D27/001 , F01D21/00 , F01D21/003 , F01D21/04 , F01D21/10 , F01D21/14 , F02C9/00 , F03D17/00 , F04D29/324 , F05D2260/80 , F05D2260/81 , G01B7/14 , G01B11/14 , G01B21/16 , G01D21/00 , G06F17/40 , G06F19/00
摘要： A system 2 including: at least one computing device 120 configured to monitor a compressor blade 10 in a turbomachine 5 by: extracting time of arrival (TOA) data about the compressor blade 10 at a defined interval; correlating turbomachine operating conditions with the TOA data; extracting resonance data about the compressor blade 10 during startup or shutdown of the turbomachine 5, and extracting static deflection and tip clearance data about the compressor blade 10 during steady state operation of the turbomachine 5; creating a baseline compressor blade comparison level based upon the extracted resonance data, extracted static deflection and tip clearance data, and correlation between the turbomachine operating conditions and the TOA data; and iteratively extracting updated TOA data and performing the correlating, the extracting of the resonance data, static deflection and tip clearance data using the updated TOA data at the defined interval to create an updated baseline compressor blade comparison level.
Corresponding computer program product with a program code executed by such a computing device.
摘要翻译：系统2包括：至少一个计算设备120，被配置为通过以下定义的间隔提取关于压缩机叶片10的到达时间（TOA）数据来监测涡轮机5中的压缩机叶片10. 将涡轮机操作条件与TOA数据相关联; 在涡轮机5的启动或关闭期间提取关于压缩机叶片10的共振数据，以及在涡轮机5的稳态操作期间提取关于压缩机叶片10的静态偏转和叶尖间隙数据; 基于提取的共振数据，提取的静态偏转和尖端间隙数据以及涡轮机操作条件和TOA数据之间的相关性来创建基准压缩机叶片比较水平; 并且迭代地提取更新的TOA数据并且以所定义的间隔执行关联，提取共振数据，静态偏转和提前间隙数据，以创建更新的基线压缩机叶片比较水平。具有由这种计算设备执行的程序代码的相应的计算机程序产品。

54. 发明公开

EP2846005A2 Vorrichtung zur Energieabsorption, Strömungsmaschine und Verfahren zur Energieabsorption 有权
标题翻译：一种用于能量流机的吸收和用于能量吸收设备的方法
公开(公告)号：EP2846005A2
公开(公告)日：2015-03-11
申请号：EP14179664.9
申请日：2014-08-04
申请人： MTU Aero Engines AG
发明人： Sasse, Stefan , Schinko, Norbert
IPC分类号： F01D21/04 , F01D25/24
CPC分类号： F01D21/045 , F01D17/02 , F01D21/04 , F01D25/24 , F02C7/05 , F05D2260/311 , Y02T50/671
摘要： Offenbart ist eine Vorrichtung (1) zur Absorption einer auf ein Element (2) wirkenden Einschlagenergie zumindest eines Schaufelfragments, wobei das Element in eine Öffnung (10) einer Strömungsmaschine eingesetzt ist, die einen Gehäuseabschnitt (6) im Bereich einer Laufschaufelreihe radial durchsetzt, wobei die Vorrichtung eine Halterung (18) zum Halten des Elements in einer Soll-Position aufweist, die ab einer voreingestellten Maximalbelastung das Element freigibt, und einen rückwärtigen Käfig (22) zum Sichern des Elements bei einer radial nach außen gerichteten Verschiebung hat, eine Strömungsmaschine mit einer derartigen Vorrichtung, sowie ein Verfahren zur mehrstufigen Energieabsorption.
摘要翻译：公开了一种用于一个元件（2）的至少一个叶片片段的作用的冲击能量，其中，在开口（10）的元件被插入的涡轮机，其中通过在转子叶片排的区域中的壳体部分（6）穿过的径向的吸收的装置（1），该装置包括用于保持所述构件在期望的位置，从而释放由预设的最大负荷的元件的保持器（18），和后罩（22），用于在径向向外的位移固定构件，具有流机这样的装置，以及用于多级的能量吸收的方法。

55. 发明公开

EP2746541A2 A method of detecting and localizing partial rotor-stator rubbing during the operation of a turbine 有权
标题翻译：涡轮机的操作期间检测和局部转子Statorreibung的位置的方法
公开(公告)号：EP2746541A2
公开(公告)日：2014-06-25
申请号：EP13196683.0
申请日：2013-12-11
申请人： Doosan Skoda Power S.r.o. , Západoceská Univerzita V Plzni
发明人： Cerný, Václav, Ing. , Liska, Jindrich
IPC分类号： F01D25/04 , F01D25/16 , F01D19/00 , F01D21/00 , F01D21/04 , F01D11/20 , F02C9/28
CPC分类号： G01M13/045 , F01D11/20 , F01D19/00 , F01D21/003 , F01D21/04 , F01D25/04 , F01D25/164 , F02C9/28 , G01H1/006 , G01M15/14
摘要： The invention relates to a method of detecting and localizing partial rotor-stator rubbing during the operation of a turbine, in which the rotor (1) of the turbine is monitored by means of at least one pair of sensors (3, 30, 4, 40) of the rotor vibrations arranged in one plane of measuring (330, 440) perpendicular to the axis of the rotor (1) and by at least one pair of sensors of the absolute vibrations of the bearings (2, 20). When using this method of processing, synchronically digitalized signals of the sensors (3, 30, 4, 40) of rotor vibrations, first the arithmetic mean of the individual harmonic bands in full spectrum in the frequency domain is calculated, by which means the information about the subharmonic components and their multiples in the full spectrum of these signals is transfered into the frequency band -1 X to 1 X (where X indicates the rotational frequency of the rotor (1)), at the same time is by the calculation of the median estimated the level of the signal noise, with which individual frequency bands of the full spectrum are encumbered, and which is subtracted from the amplitudes in the individual frequency bands of full spectrum of the signals of the sensors. Thus normalized accumulated full spectrum of the signals of the sensors of rotor vibrations is created, in which, subsequently, the amplitude of the predetermined subharmonic component/components of the signals of rotor vibrations is compared with the amplitudes of the frequency components in its proximity determined by the Fourier transform or by approximation with the Fourier series. Simultaneously, the presence of the monitored subharmonic component of the signals of the rotor vibrations in the spectrum of these signals is deduced, on the basis of which subsequently the occurrence of rotor-stator rubbing is deduced. In case of the rubbing occurrence the place/places of the turbine where it takes place is further localized.
摘要翻译：本发明的涡轮，其中，所述转子（1）的涡轮机的，借助于监视的至少一对传感器（3，30，4的的手术过程中涉及检测的方法和定位部分转子 - 定子研磨，在一个平面内垂直于所述转子（1）的轴线和由至少一对轴承（2,20）的绝对值的振动传感器的测量（330，440）的转子振动的40）。当使用处理的方法中，所述传感器的转子振动的synchronically数字化信号（3，30，4，40）中，首先在频域全谱的单个谐波频带计算的算术平均值，通过该装置中的信息关于分谐波成分及其在合成信号的全谱的倍数被转移到频带 - 1 X 1到X（其中X表示转子的旋转频率（1）），在同一时间是通过计算中值估计的信号的噪声的电平，与该全光谱的各个频带被担保，并且所有这一切都被从幅度在所述传感器的信号的全谱的各个频带中减去。转子振动的传感器的信号。因此归一化累积的全谱被创建，其中，随后，转子振动的信号的预定谐波分量/分量的振幅与频率分量的在其附近的幅度确定性开采相比由傅立叶变换或用傅立叶级数近似。同时，在合成信号的频谱中的转子振动的信号的监测次谐波成分的存在推导出，在此基础上的转子 - 定子研磨的随后发生推导上。在发生摩擦的地方的情况下，/它发生在涡轮机的地方进一步本地化。

56. 发明公开

EP2734710A1 VERFAHREN ZUR HERSTELLUNG EINES EINLAUFBELAGS, EINLAUFSYSTEM, STRÖMUNGSMASCHINE SOWIE LEITSCHAUFEL 失效转让
标题翻译：用于生产LINING跑，冒系统及涡轮机轮叶
公开(公告)号：EP2734710A1
公开(公告)日：2014-05-28
申请号：EP12759627.8
申请日：2012-07-18
申请人： MTU Aero Engines GmbH
发明人： BAYER, Erwin , HESS, Thomas , HILLER, Sven-J. , GEIGER, Peter
IPC分类号： F01D21/00 , F01D21/04
CPC分类号： F01D5/288 , F01D21/006 , F01D21/04 , Y10T29/49316
摘要： The invention relates to a method for producing an inlet lining for a turbomachine for slowing down a rotor in the event of a shaft fracture, wherein the inlet lining is formed as an integral generative blade section when a blade is produced generatively. The invention further relates to an inlet system, comprising an inlet ring that is arranged circumferentially on a series of blades and has a chamber-like material structure, to a turbomachine having such an inlet system, and to a guide blade having such an inlet lining.

57. 发明公开

EP2715070A1 WEAR PIN GAP CLOSURE DETECTION SYSTEM FOR GAS TURBINE ENGINE 有权
标题翻译：检测系统的VERSCHLEISSSTIFTLÜCKENSVERSCHLUSS燃气涡轮发动机
公开(公告)号：EP2715070A1
公开(公告)日：2014-04-09
申请号：EP12722647.0
申请日：2012-05-15
申请人： Siemens Energy, Inc.
发明人： SINGH, Ram Bahadur , WASDELL, David, L. , MILLER, Keith, A.
IPC分类号： F01D11/00 , F01D21/04 , F04D27/02
CPC分类号： F01D11/001 , F01D21/04 , F04D27/008 , F04D27/0292 , F05D2240/55 , F05D2250/32 , F05D2260/30 , F05D2260/36 , F05D2260/80
摘要： A wear indication system for use in turbine engines to measure the rate of gap closure between a seal holder and a rotor disk in a compressor blade assembly is disclosed. The wear indication system may include a support system capable of supporting a wear indicator formed from a relatively soft wear material without enabling the wear indicator to shift position or to fall out. One or more wear pins may be releasably attached to a compression plate with a seal holder. The seal holder may restrain the wear pin in position in an interference fit. During turbine engine operation, the wear pin is used to determine the rate of gap closing between a rotor disk and a seal holder precisely so that gas turbine engine repair can be scheduled and proper actions be taken to prevent rubbing between rotating and stationary parts of a compressor.

58. 发明公开

EP2661565A1 DISPOSITIF ET PROCEDE DE PROTECTION MECANIQUE. 有权转让
标题翻译：机械保护方法及其设备
公开(公告)号：EP2661565A1
公开(公告)日：2013-11-13
申请号：EP12702572.4
申请日：2012-01-03
申请人： Turbomeca
发明人： BATLLE, Frédéric, Ferdinand, Jacques
IPC分类号： F16D9/04 , F01D21/02
CPC分类号： F16D9/00 , F01D21/02 , F01D21/04 , F16D9/04
摘要： The invention relates to the field of mechanical protection methods and devices, and in particular relates to a mechanical protection device comprising a transmission shaft (1) with a resonant frequency in bending that corresponds to a predetermined overspeed in the rotation of the transmission shaft (1) that is not damped enough to avoid breakage of the transmission shaft (1) as a result of said bending resonance, and to a mechanical protection method involving the breakage of the transmission shaft (1) as a result of this bending resonance.

59. 发明公开

EP2602434A2 Dynamic load reduction system 有权
标题翻译：系统还原动态负载
公开(公告)号：EP2602434A2
公开(公告)日：2013-06-12
申请号：EP12194798.0
申请日：2012-11-29
申请人： General Electric Company
发明人： Wallace, Thomas Tracy , Simpson, William Joseph , List, John Howard , Tao, Jason Jianxin , Steen, Tod Robert
IPC分类号： F01D5/02 , F01D21/04 , F01D25/04
CPC分类号： F01D5/026 , F01D21/04 , F01D21/045 , F01D25/04 , F05D2260/31 , Y10T403/645
摘要： Bolted together first and second flanges (146, 147) include bolts (160) disposed through first bolt holes (158) in the first flange (146). The bolts extend at least partially through second holes (168) in the second flange (147). Bolt (160) include bolt heads (170), threads (174), and shanks (172) therebetween. Crushable spacers (182) disposed around the shanks (172) of a first plurality (180) of the bolts (160) and contacting and axially extending between the bolt heads (170) and the first flange (146). Bushings (192) disposed around a second plurality (194) of the bolts (160) and contacting and axially extending between the bolt heads (170) and the second flange (147). A shank outer diameter (SD) may be smaller than a thread diameter (TD) and heat shrink tubing (185) may be disposed around the bolt shanks (172) of at least some of the spacers (182). First bolt holes (158) may extend into an open annular slot (154) on first flange (146) and second holes (168) may extend partially through a forward extending annular rail (152) of second flange (147) with rail (152) received within slot (154).

60. 发明公开

EP2540974A2 Fan blade with sheath 有权转让
标题翻译： LüfterschaufelmitUmhüllung
公开(公告)号：EP2540974A2
公开(公告)日：2013-01-02
申请号：EP12172593.1
申请日：2012-06-19
申请人： United Technologies Corporation
发明人： Schwarz, Frederick M. , Weisse, Michael A. , Graves, William R.
IPC分类号： F01D5/28 , F02K3/06
CPC分类号： F01D5/28 , F01D5/14 , F01D5/141 , F01D5/147 , F01D21/04 , F02K3/06 , F04D29/324 , F05D2240/303 , Y02T50/672 , Y02T50/673
摘要： A fan blade includes an airfoil with a leading edge and a trailing edge in a chordwise direction, a root and a tip in a spanwise direction; and a sheath (52) with a solid portion (68) to cover the leading edge (56) and first and second flanks (70,70) extending in the chordwise direction to bond to the pressure and suction sides of the airfoil, respectively. The dimensions of the sheath are varied with respect to the spanwise direction of the blade.
摘要翻译：风扇叶片包括具有前缘的翼型和沿翼弦方向的后缘，沿翼展方向的根部和尖端; 以及具有实心部分（68）以覆盖前缘（56）的护套（52）和沿弦向方向延伸的第一和第二侧翼（70,70），以分别结合到翼型的压力和吸力侧。鞘的尺寸相对于叶片的翼展方向变化。

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