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1.发明公开Methods and apparatus for operating gas turbine engines 有权Methode und Apparat zum Betreiben von Gasturbinen
公开(公告)号：EP1429016A1
公开(公告)日：2004-06-16
申请号：EP03257760.3
申请日：2003-12-10
发明人： Kraft, Robert Eugene
CPC分类号： F23C15/00 , F02C5/02 , F02K3/08 , F02K7/02 , F02K7/075 , F05D2270/11 , F23R7/00 , Y02T50/671
摘要： A method for operating a pulse detonation system (50). The method includes providing a pulse detonation chamber (62) including a plurality of detonation tubes (58) extending therein, and detonating a mixture of fuel and air within each detonation tube such that at least a first tube is detonated at a different time than at least a second detonation tube.
摘要翻译： 一种用于操作脉冲爆震系统（50）的方法。 该方法包括提供包括在其中延伸的多个引爆管（58）的脉冲爆炸室（62），并且在每个引爆管内引爆燃料和空气的混合物，使得至少第一管在不同于第 至少一个第二个爆管。
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公开(公告)号：EP1429016B1
公开(公告)日：2006-03-08
申请号：EP03257760.3
申请日：2003-12-10
发明人： Kraft, Robert Eugene
CPC分类号： F23C15/00 , F02C5/02 , F02K3/08 , F02K7/02 , F02K7/075 , F05D2270/11 , F23R7/00 , Y02T50/671
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公开(公告)号：EP0712114A2
公开(公告)日：1996-05-15
申请号：EP95307857.3
申请日：1995-11-03
IPC分类号： G10K11/178 , B06B1/06
CPC分类号： F02C7/045 , F05D2220/327 , F05D2260/962 , G10K11/178 , G10K2210/121 , G10K2210/1281 , G10K2210/3032 , G10K2210/3217 , G10K2210/32271 , G10K2210/32291 , Y02T50/671
摘要： An active liner for attenuating noise includes a rigid backplate (26) supporting a piezoelectric panel (28). A pressure transducer (30) is disposed in the panel (28) for sensing acoustic pressure of noise being propagated against a face surface of the panel. A controller (36) includes a predetermined schedule of acoustic impedance for controlling a displacement driver (32) joined to the panel (28) to effect a displacement velocity of the panel face surface (28b) for obtaining a predetermined acoustic impedance at the sensed acoustic pressure for attenuating noise.
摘要翻译： 活性衬里包括刚性背板，压电板具有固定地连接到背板的后表面，以及用于直接面对噪声的相对表面。 压力传感器设置在面板中，用于感测抵靠面板表面传播的噪声的声压。 电子设备电驱动面板以在垂直于面板表面的方向上实现其压电位移。 装置可操作地连接到压力传感器和驱动装置，用于控制面板表面的位移。 控制装置包括预定的声阻抗调度表，用于控制驱动装置，以实现用于声压的面板表面的速度，以获得预定的声阻抗以衰减噪声。
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4.发明公开Apparatus and method for suppressing dynamic pressure instability in bleed duct 审中-公开用于抑制排气管道中的动态压力不稳定的装置和方法
公开(公告)号：EP2031213A3
公开(公告)日：2017-06-21
申请号：EP08162307.6
申请日：2008-08-13
CPC分类号： F02C6/08 , F02K3/06 , F05D2250/51 , F05D2260/213 , Y02T50/675
摘要： An apparatus and method for suppressing dynamic instability in a bleed duct (42) of a gas turbine engine (10) includes a fan bypass duct (32) configured to permit a flow of air (28) through the gas turbine engine (10). The fan bypass duct (42) defines a fan duct surface (31), and the bleed duct (42) has an inlet (41) in fluid communication with the fan bypass duct (32) and a flow control valve (44) having an opened position and a closed position. A flow diverter (50) is positioned on the fan duct surface (31) proximate the inlet (41) of the bleed duct (42) and diverts the flow of air (28) from the inlet (41) when the flow control valve (44) is closed, while permitting a portion (57) of the flow of air (28) to enter the inlet (41) when the flow control valve (44) is opened.
摘要翻译： 一种用于抑制燃气涡轮发动机（10）的排气管道（42）中的动态不稳定性的设备和方法包括被配置为允许空气（28）流过燃气涡轮发动机（10）的风扇旁路管道（32）。 风扇旁路管道42限定风扇管道表面31，并且排气管道42具有与风扇旁路管道32流体连通的入口41和流量控制阀44， 打开位置和关闭位置。 分流器（50）位于排气管道（42）的入口（41）附近的风扇管道表面（31）上，并且当流量控制阀门（41）从入口（41）转向空气（28） 44）关闭，同时在流量控制阀（44）打开时允许空气（28）流动的一部分（57）进入入口（41）。
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5.发明公开Apparatus and method for suppressing dynamic pressure instability in bleed duct 审中-公开装置和方法用于在排出管路抑制动态压力不稳定
公开(公告)号：EP2031213A2
公开(公告)日：2009-03-04
申请号：EP08162307.6
申请日：2008-08-13
CPC分类号： F02C6/08 , F02K3/06 , F05D2250/51 , F05D2260/213 , Y02T50/675
摘要： An apparatus and method for suppressing dynamic instability in a bleed duct (42) of a gas turbine engine (10) includes a fan bypass duct (32) configured to permit a flow of air (28) through the gas turbine engine (10). The fan bypass duct (42) defines a fan duct surface (31), and the bleed duct (42) has an inlet (41) in fluid communication with the fan bypass duct (32) and a flow control valve (44) having an opened position and a closed position. A flow diverter (50) is positioned on the fan duct surface (31) proximate the inlet (41) of the bleed duct (42) and diverts the flow of air (28) from the inlet (41) when the flow control valve (44) is closed, while permitting a portion (57) of the flow of air (28) to enter the inlet (41) when the flow control valve (44) is opened.
摘要翻译： 一种用于在燃气涡轮发动机（10）的泄放管道（42）抑制动态不稳定性的装置和方法包括：配置为通过所述燃气涡轮发动机（10），以允许空气（28）的流动的风扇旁通管道（32）。 风扇旁通管道（42）定义一风扇管道表面（31）和具有在泄放管道（42）具有在与风扇旁通管道（32）流体连通的入口（41）和流量控制阀（44） 打开位置和关闭位置。 流动转向器（50）被定位在所述风扇管道表面（31）邻近所述泄放管道（42）的入口（41）上，并且从所述入口（41）当流量控制阀转向空气（28）的流动（ 44）被关闭，同时允许空气（28的流的一部分（57）），进入当流量控制阀（44）被打开的入口（41）。
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6.发明授权
公开(公告)号：EP1336739B1
公开(公告)日：2011-05-04
申请号：EP03250788.1
申请日：2003-02-07
CPC分类号： F02C7/045 , F01D21/045 , F05D2250/191 , F05D2250/283
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7.发明公开
公开(公告)号：EP1336739A3
公开(公告)日：2005-03-16
申请号：EP03250788.1
申请日：2003-02-07
CPC分类号： F02C7/045 , F01D21/045 , F05D2250/191 , F05D2250/283
摘要： A fan casing (10) for a gas turbine engine is provided which combines the functions of blade containment and noise suppression. The fan casing has an annular metallic inner shell (14) with a plurality of holes (17) are formed therethrough. An acoustic absorber (39), such as a cellular resonator, is disposed around the inner shell (14).
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8.发明公开Gas turbine fan casing with containment and noise suppression functions 有权Durchschlagsicheres undgeräuschdämpfendesBläsergehäusefürein Mantelstromtriebwerk
公开(公告)号：EP1336739A2
公开(公告)日：2003-08-20
申请号：EP03250788.1
申请日：2003-02-07
CPC分类号： F02C7/045 , F01D21/045 , F05D2250/191 , F05D2250/283
摘要： A fan casing (10) for a gas turbine engine is provided which combines the functions of blade containment and noise suppression. The fan casing has an annular metallic inner shell (14) with a plurality of holes (17) are formed therethrough. An acoustic absorber (39), such as a cellular resonator, is disposed around the inner shell (14).
摘要翻译： 提供了一种用于燃气涡轮发动机的风扇壳体（10），其结合了叶片容纳和噪声抑制的功能。 风扇壳体具有环形金属内壳（14），其中形成有多个孔（17）。 诸如蜂窝谐振器的吸声器（39）围绕内壳（14）设置。
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公开(公告)号：EP0712114B1
公开(公告)日：2002-10-09
申请号：EP95307857.3
申请日：1995-11-03
IPC分类号： G10K11/178 , B06B1/06 , G10K11/20
CPC分类号： F02C7/045 , F05D2220/327 , F05D2260/962 , G10K11/178 , G10K2210/121 , G10K2210/1281 , G10K2210/3032 , G10K2210/3217 , G10K2210/32271 , G10K2210/32291 , Y02T50/671
摘要： The active liner comprises the rigid backplate, the piezoelectric panel having a back surface fixedly joined to the backplate, and an opposite face surface for directly facing the noise. The pressure transducer is disposed in the panel for sensing acoustic pressure of the noise being propagated against the panel face surface. A device electrically drives the panel to effect piezoelectric displacement of it in a direction normal to the panel face surface. A device is operatively joined to the pressure transducer and the driving device for controlling displacement of the panel face surface. The control device includes a predetermined schedule of acoustic impedance for controlling the driving device to effect a velocity of the panel face surface for the acoustic pressure for obtaining the predetermined acoustic impedance to attenuate the noise.
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公开(公告)号：EP0712114A3
公开(公告)日：1998-01-07
申请号：EP95307857.3
申请日：1995-11-03
IPC分类号： G10K11/178 , B06B1/06
CPC分类号： F02C7/045 , F05D2220/327 , F05D2260/962 , G10K11/178 , G10K2210/121 , G10K2210/1281 , G10K2210/3032 , G10K2210/3217 , G10K2210/32271 , G10K2210/32291 , Y02T50/671
摘要： An active liner for attenuating noise includes a rigid backplate (26) supporting a piezoelectric panel (28). A pressure transducer (30) is disposed in the panel (28) for sensing acoustic pressure of noise being propagated against a face surface of the panel. A controller (36) includes a predetermined schedule of acoustic impedance for controlling a displacement driver (32) joined to the panel (28) to effect a displacement velocity of the panel face surface (28b) for obtaining a predetermined acoustic impedance at the sensed acoustic pressure for attenuating noise.
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