公开(公告)号：US20240175400A1

公开(公告)日：2024-05-30

申请号：US18351735

申请日：2023-07-13

申请人： General Electric Company

发明人： Darek Tomasz Zatorski ,  Kurt David Murrow ,  Paul Robert Gemin ,  Philip M. Cioffi ,  John Russell Yagielski

IPC分类号： F02C9/56 ,  F01D15/10 ,  F01D15/12 ,  F02C7/32

CPC分类号： F02C9/56 ,  F01D15/12 ,  F02C7/32 ,  F01D15/10 ,  F05D2220/323 ,  F05D2240/40 ,  F05D2270/052 ,  F05D2270/07 ,  F05D2270/335 ,  F05D2270/44 ,  F05D2270/62

摘要： A propulsion assembly includes a first torque source coupled with a first shaft and a second torque source coupled with a second shaft. A coupler selectively couples the first and second torque sources. When the first and second torque sources are coupled via the coupler, in response to a command to decouple the first torque source, an unloading operation is performed to decrease the torque output provided by the first torque source to a threshold, and when reached, the first shaft is decoupled from the coupler. When the first torque source is coupled with the coupler but the second torque source is not, in response to a command to couple the second torque source, a speed matching operation is performed to increase the speed of the second shaft to match a speed of the first shaft, and when the speeds are matched, the second shaft is coupled to the coupler.

公开(公告)号：US20180370620A1

公开(公告)日：2018-12-27

申请号：US16007473

申请日：2018-06-13

申请人： AIRBUS HELICOPTERS

发明人： Anthony LEONARD

IPC分类号： B64C27/00 ,  B64D31/06 ,  B64D35/02 ,  F02C9/28

CPC分类号： B64C27/001 ,  B64D31/06 ,  B64D35/02 ,  F02C9/00 ,  F02C9/28 ,  F02C9/56 ,  F05D2220/329 ,  F05D2260/96 ,  F05D2270/304 ,  F05D2270/334 ,  F05D2270/807

摘要： A regulation system for controlling the vibratory behavior in twisting and/or the twisting stability of a drivetrain of a rotorcraft, the regulation system comprising two regulation loops that are interleaved one in the other, the two regulation loops being arranged “in cascade” relative to each other to regulate firstly a first speed of rotation NG of a gas generator of at least one turboshaft engine driving said drivetrain in rotation, and secondly a second speed of rotation NTL of a free turbine of the engine(s).

公开(公告)号：US09771876B2

公开(公告)日：2017-09-26

申请号：US14546491

申请日：2014-11-18

申请人： General Electric Company

发明人： Lewis Berkley Davis, Jr. ,  Scott Arthur Day ,  Harold Lamar Jordan, Jr. ,  Rex Allen Morgan

IPC分类号： F02C9/42 ,  F02C9/56 ,  F02C9/28

CPC分类号： F02C9/56 ,  F02C9/28 ,  F02C9/42 ,  F05D2270/0831

摘要： Various embodiments include a system having: at least one computing device configured to tune a set of gas turbines (GTs) by performing actions including: commanding each GT in the set of GTs to a base load level, based upon a measured ambient condition for each GT; commanding each GT in the set of GTs to adjust a respective output to match a nominal mega-watt power output value, and subsequently measuring an actual emissions value for each GT; adjusting an operating condition of each GT in the set of GTs based upon a difference between the respective measured actual emissions value and a nominal emissions value at the ambient condition; and further adjusting an operating condition of each GT in the set of GTs based upon a determined emissions measurement error.

公开(公告)号：US09429077B2

公开(公告)日：2016-08-30

申请号：US13312232

申请日：2011-12-06

申请人： Keith Morgan

发明人： Keith Morgan

IPC分类号： F02C1/00 ,  F02C7/36 ,  F02C9/00 ,  F02C9/42 ,  F02C6/02

CPC分类号： F02C6/02 ,  F01D15/10 ,  F01D25/36 ,  F02C3/10 ,  F02C3/113 ,  F02C7/36 ,  F02C9/00 ,  F02C9/42 ,  F02C9/56 ,  F05B2220/309 ,  F05D2220/329 ,  F05D2270/053

摘要： Electric power from the low spool of a turboshaft engine is transferred to drive the compressor of an other turboshaft engine. This is used to assist in maintaining the other turboshaft idling while a single engine provides flight power or to increase acceleration for instance.

摘要翻译： 来自涡轮轴发动机的低阀芯的电力被传送以驱动另一涡轮轴发动机的压缩机。 这用于在单个发动机提供飞行动力或增加加速度的情况下帮助维持另一个涡轮轴空转。

公开(公告)号：US20140260295A1

公开(公告)日：2014-09-18

申请号：US13804799

申请日：2013-03-14

申请人： PRATT & WHITNEY CANADA CORP.

发明人： Richard ULLYOTT ,  Lazar MITROVIC ,  Jean DUBREUIL ,  Stephen Christopher KENNY ,  Guy BOUCHARD ,  Ilya B. MEDVEDEV ,  Keith MORGAN ,  Daris Jehangir KARANJIA ,  Nashed Azer YOUSSEF

IPC分类号： F02C3/113

CPC分类号： F02C3/113 ,  F02C3/107 ,  F02C7/36 ,  F02C9/56 ,  F05D2260/4031

摘要： A method of adjusting a rotational speed of the low pressure compressor rotor(s) of a gas turbine engine, including rotating the high pressure compressor rotor(s) with the high pressure turbine rotor(s) through the high pressure spool, rotating the low pressure turbine rotor(s) with a flow of exhaust gases from the high pressure turbine, rotating the low pressure spool with the low pressure turbine rotor(s), rotating a load of the engine with the low pressure spool, driving a rotation of the low pressure compressor rotor(s) with the low pressure spool through a variable transmission defining a variable transmission ratio between rotational speeds of the compressor rotor(s) and the low pressure spool, and adjusting the transmission ratio to obtain a desired rotational speed for the low pressure compressor rotor(s). A method of adjusting rotational speeds of a gas turbine engine and a gas turbine engine are also described.

摘要翻译： 一种调节燃气涡轮发动机的低压压缩机转子的转速的方法，包括通过高压阀芯与高压涡轮转子一起旋转高压压缩机转子，使低压 来自高压涡轮机的废气流的高压涡轮机转子，用低压涡轮转子旋转低压阀芯，用低压阀芯旋转发动机的负载，驱动 通过限定压缩机转子和低压阀芯的转速之间的可变传动比的可变传动装置与低压阀芯连接的低压压缩机转子，并且调整传动比以获得所需的转速 低压压缩机转子。 还描述了一种调节燃气涡轮发动机和燃气涡轮发动机的转速的方法。

公开(公告)号：US20140216047A1

公开(公告)日：2014-08-07

申请号：US14155813

申请日：2014-01-15

申请人： Hitachi, Ltd.

发明人： Tetsuro MORISAKI ,  Naohiro KUSUMI ,  Noriaki HINO ,  Tomomichi ITO ,  Kazuo TAKAHASHI

IPC分类号： F02C9/56

CPC分类号： F02C9/56 ,  F01D5/06 ,  F01D13/003 ,  F02C3/113 ,  F02C7/268 ,  F02C7/275 ,  F02C7/32 ,  F02C7/36 ,  F02C9/28 ,  F02C9/32 ,  F02C9/34 ,  F02C9/48 ,  F02C9/50 ,  F02C9/54 ,  F03D15/00 ,  F23R3/34 ,  F23R3/343 ,  F23R3/346 ,  Y02E10/72

摘要： A two-shaft gas turbine having high operability is provided. The two-shaft gas turbine includes: a gas generator having a compressor, a combustor and a high pressure turbine; a power turbine having a low pressure turbine; a load connected to the power turbine; a motor/generator capable of rotatably driving the gas generator and capable of extracting power from the gas generator; electric equipment controlling the rotational driving and the power extraction by delivering electric power between the electric equipment and the motor/generator; and a control device controlling the electric equipment, wherein the combustor has a plurality of combustion regions to which a fuel is supplied through fuel adjustment means which are independent from each other, and the control device controls a delivery amount of the electric power delivered by the electric equipment corresponding to the number of combustion regions to which the fuel is supplied.

摘要翻译： 提供了具有高可操作性的双轴燃气轮机。 双轴燃气轮机包括：具有压缩机，燃烧器和高压汽轮机的气体发生器; 具有低压涡轮机的动力涡轮机; 连接到动力涡轮机的负载; 能够旋转地驱动气体发生器并且能够从气体发生器提取动力的电动机/发电机; 电气设备通过在电气设备和电动机/发电机之间传递电力来控制旋转驱动和功率提取; 以及控制所述电气设备的控制装置，其特征在于，所述燃烧器具有多个燃烧区域，所述多个燃烧区域通过彼此独立的燃料调节装置供给燃料，并且所述控制装置控制由所述燃料调节装置输送的电力的输送量 对应于供给燃料的燃烧区域的数量的电气设备。

公开(公告)号：US08275500B2

公开(公告)日：2012-09-25

申请号：US12046245

申请日：2008-03-11

申请人： Guerry Buehman

发明人： Guerry Buehman

IPC分类号： G05D1/00

CPC分类号： F02C9/56 ,  F05D2220/329

摘要： A system and method of controlling a gas turbine engine controller in a rotorwing aircraft includes determining when a fixed collective takeoff (FCTO) of the rotorwing aircraft is being conducted. A control loop gain of the gas turbine engine controller is at least selectively varied when the FCTO is being conducted.

摘要翻译： 控制转子飞行器中的燃气涡轮发动机控制器的系统和方法包括确定何时正在进行转子飞行器的固定集体起飞（FCTO）。 当正在进行FCTO时，至少选择性地改变燃气涡轮发动机控制器的控制回路增益。

公开(公告)号：US07884491B2

公开(公告)日：2011-02-08

申请号：US12830404

申请日：2010-07-05

申请人： David G. Halsey ,  Charles J. Romenesko

发明人： David G. Halsey ,  Charles J. Romenesko

IPC分类号： H02P9/04 ,  F02C6/00

CPC分类号： F02C9/56 ,  F01D15/10 ,  F01D21/14 ,  F02C3/10 ,  F02C6/00 ,  F02C9/26 ,  F02C9/28 ,  F05D2220/76 ,  F05D2270/052 ,  F05D2270/304 ,  F05D2270/309 ,  F05D2270/44

摘要： A power turbine speed control system for a turbo-shaft type gas turbine engine that has a gas generator compressor spool and a power turbine spool and drives an electrical generator that powers at least one electrical load by way of at least one electrical bus, comprises a power turbine controller that senses the rotary speed of the power turbine spool and generates at least one signal that changes the torque of the electrical generator in response to the sensed change in the rotary speed of the power turbine spool.

摘要翻译： 一种用于涡轮轴式燃气涡轮发动机的动力涡轮机速度控制系统，其具有气体发生器压缩机线轴和动力涡轮机线轴，并驱动通过至少一个电气总线对至少一个电力负载供电的发电机，包括： 动力涡轮机控制器，其感测动力涡轮阀芯的旋转速度并产生响应于感测到的动力涡轮阀芯的转速的变化而改变发电机的扭矩的至少一个信号。

公开(公告)号：US07777358B2

公开(公告)日：2010-08-17

申请号：US12568439

申请日：2009-09-28

申请人： David G. Halsey ,  Charles J. Romenesko

发明人： David G. Halsey ,  Charles J. Romenesko

IPC分类号： H02P9/04 ,  F02C3/22

CPC分类号： F02C9/56 ,  F01D15/10 ,  F01D21/14 ,  F02C3/10 ,  F02C6/00 ,  F02C9/26 ,  F02C9/28 ,  F05D2220/76 ,  F05D2270/052 ,  F05D2270/304 ,  F05D2270/309 ,  F05D2270/44

摘要： A power turbine speed control system for a turbo-shaft type gas turbine engine that has a gas generator compressor spool and a power turbine spool and drives an electrical generator that powers at least one electrical load by way of at least one electrical bus, comprises a power turbine controller that senses the rotary speed of the power turbine spool and generates at least one signal that changes the torque of the electrical generator in response to the sensed change in the rotary speed of the power turbine spool.

摘要翻译： 一种用于涡轮轴式燃气涡轮发动机的动力涡轮机速度控制系统，其具有气体发生器压缩机线轴和动力涡轮机线轴，并驱动通过至少一个电气总线对至少一个电力负载供电的发电机，包括： 动力涡轮机控制器，其感测动力涡轮阀芯的旋转速度并产生响应于感测到的动力涡轮阀芯的转速的变化而改变发电机的扭矩的至少一个信号。

公开(公告)号：US07643928B2

公开(公告)日：2010-01-05

申请号：US10750836

申请日：2004-01-05

申请人： Richard Soucy

发明人： Richard Soucy

IPC分类号： G06F19/00 ,  G06G7/70

CPC分类号： F02C9/56 ,  F05D2270/021 ,  F05D2270/053 ,  F05D2270/06 ,  F05D2270/304

摘要： A system and method for controlling the speed of a turbine engine, the turbine engine being operative to provide power to a primary load. When a decrease in the power requirement of the primary load is detected, at least a portion of the power generated by the turbine engine is redirected to a secondary load, thereby maintaining the speed of the turbine engine below a rated maximum speed. In the example of a turbine-powered train in which the turbine engine provides power to electric traction motors driving the wheels of the train, when a wheel spin is detected, at least a portion of the power generated by the turbine engine is diverted from the respective electric traction motor to rheostats for conversion to heat.

摘要翻译： 一种用于控制涡轮发动机的速度的系统和方法，所述涡轮发动机可操作以向主负载提供动力。 当检测到初级负载的功率要求的下降时，由涡轮发动机产生的功率的至少一部分被重定向到次级负载，从而将涡轮发动机的速度保持在额定最大速度以下。 在涡轮机动力列车的示例中，其中涡轮发动机为驱动列车的车轮的电力牵引马达提供动力，当检测到车轮旋转时，由涡轮发动机产生的功率的至少一部分从 相应的电动牵引电机变阻器转换为热量。