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41. 发明授权

US07428815B2 Method of operating a compressor near the compressor pumping limit and compressor 失效
标题翻译：在压缩机泵送极限和压缩机附近操作压缩机的方法
公开(公告)号：US07428815B2
公开(公告)日：2008-09-30
申请号：US11110965
申请日：2005-04-20
申请人： Peter Fledersbacher , Gernot Hertweck , Steffen Schiedt , Guido Vent , Jürgen Willand
发明人： Peter Fledersbacher , Gernot Hertweck , Steffen Schiedt , Guido Vent , Jürgen Willand
IPC分类号： F02B33/44
CPC分类号： F02B37/12 , F01D17/06 , F01D17/16 , F02B37/24 , F02C7/042 , F02C7/057 , F04D25/04 , F04D27/02 , F05D2220/40 , F05D2270/101 , Y02T10/144
摘要： In a method of operating a compressor near the compressor pumping limit wherein the compressor includes a control arrangement for adjusting the momentary operating state of the compressor, the flow velocity of a mass flow through the compressor in the boundary layer along the wall of the flow passage is determined for detecting operation of the compressor close to the pumping limit from a reversal of the direction of the mass flow vector in the boundary layer and the control arrangement is actuated so as to prevent the compressor from transgressing the pumping limit.
摘要翻译：在压缩机泵送极限附近操作压缩机的方法中，其中压缩机包括用于调节压缩机的瞬时操作状态的控制装置，沿着流动通道的壁在边界层中通过压缩机的质量流的流速被确定为从边界层中的质量流矢量的方向反转来检测靠近泵送极限的压缩机的操作，并且控制装置被致动以防止压缩机超过泵送极限。

42. 发明授权

US07118322B2 Device for injecting cooling air into a turbine rotor 有权
标题翻译：将冷却空气注入涡轮转子的装置
公开(公告)号：US07118322B2
公开(公告)日：2006-10-10
申请号：US10801599
申请日：2004-03-17
申请人： Didier Mortgat
发明人： Didier Mortgat
IPC分类号： F01D17/14
CPC分类号： F01D5/148 , F01D5/085 , F01D9/02 , F01D9/065 , F01D17/16 , F05D2300/50212 , Y02T50/671 , Y02T50/673 , Y02T50/676
摘要： A device for injecting cooling air into a turbo-machine turbine rotor includes a plurality of injectors distributed regularly around a longitudinal axis of the turbomachine and mounted between an inner shroud and an outer shroud. Each injector has a bimetallic structure with a first metal material forming a major portion of the structure of the injector and having a first coefficient of thermal expansion, and a second metal material forming a complementary portion of the structure in the vicinity of the suction side wall meeting the trailing edge of the injector, and having a second coefficient of thermal expansion that is smaller than the first.
摘要翻译：用于将冷却空气注入涡轮机涡轮机转子的装置包括多个喷射器，其定期围绕涡轮机的纵向轴线分布并且安装在内护罩和外护罩之间。每个喷射器具有双金属结构，其具有形成喷射器结构的主要部分并具有第一热膨胀系数的第一金属材料，以及在吸力侧壁附近形成该结构的互补部分的第二金属材料满足喷射器的后缘，并且具有小于第一热膨胀系数的第二热膨胀系数。

43. 发明申请

US20060018761A1 Adaptable fluid flow device 审中-公开
标题翻译：适应流体流动装置
公开(公告)号：US20060018761A1
公开(公告)日：2006-01-26
申请号：US11146187
申请日：2005-06-07
申请人： John Webster , Caetano Peng
发明人： John Webster , Caetano Peng
IPC分类号： B64C11/24
CPC分类号： F01D5/148 , F01D7/00 , F01D17/16 , F05D2300/505 , Y02T50/673
摘要： An adaptable fluid-foil comprising at least two panels, the panels are joined at opposing edges, in use, a fluid passes over at least part of one of the panels characterized in that a panel comprises a shape memory element, the shape memory element is arranged to change the shape of the fluid-foil between a first shape and a second shape, so that in use, the first shape is optimal for a first fluid flow condition and the second shape is optimal for a second fluid flow condition.
摘要翻译：包括至少两个面板的适应性流体薄片，所述面板在使用中在相对边缘处连接，流体通过其中一个面板的至少一部分，其特征在于，面板包括形状记忆元件，所述形状记忆元件是被布置成在第一形状和第二形状之间改变流体箔的形状，使得在使用中，第一形状对于第一流体流动状态是最佳的，并且第二形状对于第二流体流动状态是最佳的。

44. 发明申请

US20050008489A1 Antiwear device for a variable pitch system for a turbomachine vane 审中-公开
标题翻译：用于涡轮机叶片的变桨距系统的抗磨装置
公开(公告)号：US20050008489A1
公开(公告)日：2005-01-13
申请号：US10756259
申请日：2004-01-14
申请人： Philippe Perruchaut , Christian Piekosz
发明人： Philippe Perruchaut , Christian Piekosz
IPC分类号： F02C1/00 , F01D17/16 , F04D29/02 , F04D29/56 , F03D1/00
CPC分类号： F04D29/563 , F01D17/16 , F01D17/162 , F01D17/165 , F04D29/023 , F05D2230/64 , F05D2300/17 , F05D2300/2112 , Y02T50/672
摘要： A flexible link is hinged at a first end to a control ring and is fixed at a second end to a pivot for a vane that is to be controlled that is capable of turning in a smooth bearing passing through a portion of the body of a turbomachine. An insert ring constituted by a nickel- or cobalt-based metal material is interference fitted on the vane pivot, and the smooth bearing is made of a ceramic material.
摘要翻译：柔性连杆在第一端铰接到控制环，并且在第二端处固定到用于待控制的叶片的枢轴，该叶片能够以平滑的轴承转动，该平滑轴承穿过涡轮机主体的一部分。由镍基或钴基金属材料构成的插入环被干涉地装配在叶片枢轴上，并且平滑轴承由陶瓷材料制成。

45. 发明申请

US20040187495A1 Nozzle vane driving control apparatus of variable nozzle turbocharger 有权
标题翻译：可变喷嘴涡轮增压器喷嘴叶片驱动控制装置
公开(公告)号：US20040187495A1
公开(公告)日：2004-09-30
申请号：US10780910
申请日：2004-02-19
申请人： Jidosha Denki Kogyo Co., Ltd.
发明人： Yoshiyuki Ando , Takumi Arao , Takaaki Sekine , Haruo Saito
IPC分类号： F02D023/00
CPC分类号： H02K7/116 , F01D17/16 , F01D17/165 , F02B37/24 , F05D2220/40 , H02K5/225 , H02K11/00 , Y02T10/144
摘要： In a nozzle vane driving control apparatus of a variable nozzle turbocharger including an actuator for carrying out a driving operation for opening and closing a nozzle vane of a variable nozzle and an ECU for controlling the opening degree of the nozzle vane which is obtained by the actuator, an actuator cover for covering a pinion and reduction gears by interposing a base provided integrally with a motor case portion therebetween, a unit body accommodating each of control boards, a position sensor for detecting the rotating position of an output shaft and a connector having a terminal connecting a motor and each of the control boards, and a unit cover for covering the unit body are removably fastened and fixed with a bolt and are thus integrated with each other.
摘要翻译：一种可变喷嘴涡轮增压器的喷嘴叶片驱动控制装置，包括用于执行用于打开和关闭可变喷嘴的喷嘴叶片的驱动操作的致动器和用于控制由致动器获得的喷嘴叶片的开度的ECU ，用于通过将与其间的电动机壳体部分整体设置的基座相互覆盖小齿轮和减速齿轮的致动器盖，容纳每个控制板的单元体，用于检测输出轴的旋转位置的位置传感器和具有连接电动机和每个控制板的端子和用于覆盖单元主体的单元盖可拆卸地用螺栓紧固和固定，并因此彼此一体化。

46. 发明授权

US06699010B2 Nozzle adjustment mechanism for variable-capacity turbine 有权
标题翻译：可变容量涡轮喷嘴调节机构
公开(公告)号：US06699010B2
公开(公告)日：2004-03-02
申请号：US09853679
申请日：2001-05-14
申请人： Yasuaki Jinnai
发明人： Yasuaki Jinnai
IPC分类号： F04D1716
CPC分类号： F16D1/06 , F01D17/16 , F01D17/165 , Y10T29/49323
摘要： A nozzle adjustment mechanism for a variable-capacity turbine has a connection between a connecting lever, for connecting a nozzle drive component driven by a actuator to a nozzle vane, and an edge of a nozzle shaft on the nozzle vane. The connection has a high degree of strength and does not experience deformation. A connecting hole of the connecting lever has a stopper surface which is flat or curved. The connecting edge of the nozzle shaft also has a stopper surface which corresponds to the stopper surface of the connecting hole. When the connecting edge of the nozzle shaft goes into the connecting hole of the connecting lever, the stopper surface of the connecting edge is brought into contact with the stopper surface of the connecting hole. After contact is made, a fixing process is applied to the connecting edge. The connector lever and the connecting edge of the nozzle shaft are thus effectively locked together in such a way that neither can rotate with respect to the other. The end of the nozzle shaft, in other words, prevents the shaft's rotation.
摘要翻译：用于可变容量涡轮机的喷嘴调节机构具有用于将由致动器驱动的喷嘴驱动部件连接到喷嘴叶片的连接杆与喷嘴叶片上的喷嘴轴的边缘之间的连接。连接强度高，不会发生变形。连接杆的连接孔具有平坦或弯曲的止动表面。喷嘴轴的连接边缘也具有与连接孔的止动面相对应的止动面。当喷嘴轴的连接边缘进入连接杆的连接孔时，连接边缘的止动面与连接孔的止动面接触。接触后，对连接边缘进行定影处理。因此，连接器杆和喷嘴轴的连接边缘以相对于另一个旋转的方式被有效地锁定在一起。换句话说，喷嘴轴的端部防止轴旋转。

47. 发明申请

US20030011199A1 Method and operational strategy for controlling variable stator vanes of a gas turbine power generator compressor component during under-frequency events 有权
标题翻译：在低频事件期间控制燃气轮机发电机压缩机部件的可变定子叶片的方法和操作策略
公开(公告)号：US20030011199A1
公开(公告)日：2003-01-16
申请号：US09893608
申请日：2001-06-29
发明人： Thomas Edward Wickert , Bryan Edward Sweet
IPC分类号： H02P009/04 , H02K007/18 , F02C006/00 , F01D015/10
CPC分类号： F04D27/0246 , F01D15/10 , F01D17/14 , F01D17/16 , F02C9/20 , F05D2270/061 , F05D2270/304
摘要： A method is provided for controlling variable inlet and stator vanes of a heavy-duty gas turbine electrical power generator compressor component upon occurrence of power grid under-frequency events. Variable inlet guide vanes and the front four variable stator vanes of the compressor are ganged together by means of a common actuation mechanism. Altering the angle of the ganged vanes changes the overall airflow consumption of the compressor and affects the amount of turbine output power produced. Predetermined operational schedules for varying the angular position of the stator vanes in accordance with compressor speed are defined for both nominal and under-frequency operating conditions to ensure optimum compressor efficiency without violating minimum safe compressor surge margin criteria. During a power grid under-frequency event, the variable stator vanes of the compressor are operated in a manner that provides a smooth transition from the predetermined nominal operational schedule to the predetermined under-frequency operational schedule.
摘要翻译：提供一种用于在发生电力网频率事件时控制重型燃气轮机发电机压缩机部件的可变入口和定子叶片的方法。压缩机的可变入口引导叶片和前四个可变定子叶片通过公共致动机构联接在一起。改变组合叶片的角度会改变压缩机的总体气流消耗并影响所产生的涡轮机输出功率。根据压缩机转速来定义用于改变定子叶片的角位置的预定操作计划，用于额定和低频操作条件，以确保最佳压缩机效率，而不会违反最小安全压缩机喘振裕度标准。在电网欠频事件期间，压缩机的可变定子叶片以提供从预定的标称操作时间表到预定的低频操作时间表的平滑过渡的方式操作。

48. 发明申请

US20020146316A1 METHODS AND APPARATUS FOR ADJUSTING GAS TURBINE ENGINE VARIABLE VANES 有权
标题翻译：调整气体涡轮发动机可变气门的方法和装置
公开(公告)号：US20020146316A1
公开(公告)日：2002-10-10
申请号：US09826107
申请日：2001-04-04
发明人： Mark Jeffery Bouyer
IPC分类号： F01D017/16
CPC分类号： F01D17/16 , F01D17/162
摘要： A gas turbine engine including a variable geometry system that includes a mounting system to facilitate extending a useful life of a variable geometry system is described. The engine includes a high pressure compressor including a plurality of variable vanes and rotating vanes. The variable geometry system is coupled to an actuator and includes a master lever, an aft mount, and a slot and groove joint. The master lever is coupled to the aft mount with the slot and groove joint, and adjusts a position of the variable vanes without inducing angular displacement on the aft mount.
摘要翻译：描述了包括可变几何系统的燃气涡轮发动机，其包括用于延长可变几何系统的使用寿命的安装系统。发动机包括具有多个可变叶片和旋转叶片的高压压缩机。可变几何系统耦合到致动器，并且包括主杆，后座和槽槽接头。主杆通过槽和槽接头联接到船尾安装件，并调整可变叶片的位置，而不会在后座上引起角位移。

49. 发明授权

US5730580A Turbomachines having rogue vanes 失效
标题翻译：涡轮机有流氓叶片
公开(公告)号：US5730580A
公开(公告)日：1998-03-24
申请号：US409437
申请日：1995-03-24
申请人： David Japikse
发明人： David Japikse
IPC分类号： F01D17/16 , F04D27/02 , F04D29/44 , F04D29/46 , F04D29/56
CPC分类号： F04D29/462 , F01D17/16 , F04D27/00 , F04D27/02 , F04D29/448 , F04D29/563 , F05D2220/40
摘要： A turbomachine has a set of vanes in the airfoil cascade of its diffuser system. A first portion of the vanes are "rogue" vanes. A second portion of the vanes are "remaining" vanes. For a given flow through the vane set, the angle of incidence of the rogue vanes differs from the angle of incidence of the remaining normal vanes. The remaining vanes may be free-floating or positionable. The rogue vanes can be fixed or scheduled to dominate flow through the diffuser system, thereby improving efficiency of operation. Optionally, additional "intermediate" vanes can be disposed between the "rogue" vanes and the "remaining" vanes. In a centrifugal pump or compressor, the "rogue" vanes are positioned such that a preponderance of the flow will proceed through the impeller, subsequently through the rogue vanes, and then smoothly into the volute so that flow will pass smoothly through the system with minimum frictional effects and maximum pressure recovery. For centrifugal or axial turbomachines, the use of one or more sets of rogue vanes creates a "channelizing" effect of the flow throughout the entire turbomachine.
摘要翻译：涡轮机在其扩散器系统的翼型级联中具有一组叶片。叶片的第一部分是“流氓”叶片。叶片的第二部分是“剩余”叶片。对于通过叶片组的给定流量，流氓叶片的入射角与剩余的普通叶片的入射角不同。剩余的叶片可以是自由浮动的或可定位的。流氓叶片可以固定或调度，以支配通过扩散系统的流动，从而提高操作效率。任选地，附加的“中间”叶片可以设置在“流氓”叶片和“剩余”叶片之间。在离心泵或压缩机中，“流氓”叶片被定位成使得流动的优势将通过叶轮进行，随后通过流氓叶片，然后平滑地进入蜗壳，使得流动将以最小的速度顺利地通过系统摩擦效应和最大压力恢复。对于离心式或轴向涡轮机，使用一套或多组流氓叶片会在整个涡轮机上产生流动的“通道化”效应。

50. 发明授权

US3326522A Reversible, inward flow, independent power turbine 失效
标题翻译：可逆，向内流动，独立动力涡轮机
公开(公告)号：US3326522A
公开(公告)日：1967-06-20
申请号：US46041465
申请日：1965-06-01
申请人： BRISTOL SIDDELEY ENGINES LTD
发明人： WILLIAM PICKERING ALBERT
IPC分类号： F01D1/08 , F01D1/30 , F01D3/02 , F01D9/04 , F01D17/16
CPC分类号： F01D9/045 , F01D1/08 , F01D1/30 , F01D3/025 , F01D17/16

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