公开(公告)号：US09193453B2

公开(公告)日：2015-11-24

申请号：US14140647

申请日：2013-12-26

申请人： AIRBUS HELICOPTERS

发明人： Jean-Baptiste Vallart ,  Hilario Vieira

IPC分类号： B64C19/00 ,  B64C27/32 ,  B64C27/57 ,  B64C27/12 ,  B64D31/00 ,  B64D31/06 ,  F02C9/00 ,  B64C27/04

CPC分类号： B64D31/06 ,  B64C27/04 ,  B64C27/12 ,  B64C27/57 ,  B64D31/00 ,  F02C9/00 ,  F05D2220/329 ,  F05D2270/335 ,  F05D2270/44 ,  Y02T50/671

摘要： A method of driving a rotorcraft rotor (1, 2) at variable controlled speeds. Starting from a required speed (Nr), a setpoint for total power (Pt) is calculated while taking account of an anticipated power (Pf) to be delivered by the power plant (3) for driving the main rotor (1) at the required speed (Nr), and while taking account of a power surplus (S) relating to progressive power needs to be delivered from a current power (Pc) for driving the main rotor (1) at a current speed (V) of rotation to an anticipated power (Pf) for driving the main rotor (1) at the required speed (Nr). By way of example, account may be taken at least of the acceleration or conversely of the deceleration of the main rotor (1) between the current speed (V) and the required speed (Nr), or indeed account may be taken of the flight circumstance of the rotorcraft determining the calculated required speed (Nr).

摘要翻译： 以可变的受控速度驱动旋翼航空器转子（1,2）的方法。 从所需速度（Nr）开始，计算用于总功率（Pt）的设定点，同时考虑由用于驱动主转子（1）的所需发电厂（3）提供的预期功率（Pf） 速度（Nr），并且考虑到与逐行动力有关的功率剩余（S）需要从用于驱动主转子（1）的当前功率（Pc）以当前旋转速度（V）传递到 用于以所需速度（Nr）驱动主转子（1）的预期功率（Pf）。 作为示例，可以至少考虑到当前速度（V）和所需速度（Nr）之间的主转子（1）的减速度的加速度或相反，或者实际上可以考虑飞行 旋翼航空器确定计算所需速度（Nr）的情况。

公开(公告)号：US09188021B2

公开(公告)日：2015-11-17

申请号：US14077571

申请日：2013-11-12

申请人： Edward David Thompson ,  Michael Twerdochlib

发明人： Edward David Thompson ,  Michael Twerdochlib

IPC分类号： F01K13/02 ,  F01K7/06 ,  F01D21/14 ,  F01D25/04 ,  F01D25/06 ,  F01K7/04 ,  F01K7/14 ,  F01K7/24

CPC分类号： F01D21/14 ,  F01D5/26 ,  F01D25/04 ,  F01D25/06 ,  F01K7/04 ,  F01K7/14 ,  F01K7/22 ,  F01K7/24 ,  F01K13/02 ,  F02C9/00 ,  F05D2220/31 ,  F05D2260/80 ,  F05D2270/334 ,  F05D2270/803

摘要： A blade vibration monitor backpressure limiting system (BVMBLS), that in addition to direct blade vibration and condenser backpressure monitoring utilizes other plural types of other parallel, real time monitored power plant operation state (OS) information that influences blade vibration. The system references previously stored information in an information storage device that associates respective types of monitored OS information with blade vibration. The BVMBLS determines in real time a likelihood of whether any of the monitored operation states, alone or in combination with other types of monitored operation states, is indicative of a turbine blade vibration safe operation (SO). The BVMBLS determination is utilized to increase or reduce power generation load incrementally so that power efficiency and maximum load is enhanced while turbine blade vibration is maintained in a safe operation state. The previously stored information is updated to new association information.

摘要翻译： 叶片振动监测器背压限制系统（BVMBLS）除了直接叶片振动和冷凝器背压监测之外，还利用影响叶片振动的其他多种类型的其他并行实时监测的发电厂运行状态（OS）信息。 该系统将先前存储的信息引用到信息存​​储设备中，该信息存储设备将各种监视的OS信息与刀片振动相关联。 BVMBLS实时确定是否单独或与其他类型的监视操作状态组合的任何监视的操作状态是否表示涡轮叶片振动安全操作（SO）的可能性。 BVMBLS确定用于增加或减少发电负载，从而提高功率效率和最大负载，同时涡轮叶片振动保持在安全运行状态。 先前存储的信息被更新为新的关联信息。

公开(公告)号：US20150256051A1

公开(公告)日：2015-09-10

申请号：US14634942

申请日：2015-03-02

申请人： EcoMotors, Inc.

发明人： Will Robert Nielsen Hippen ,  Christopher Meszaros ,  Tyler Garrard ,  Diana Brehob

IPC分类号： H02K9/00 ,  F02C6/12 ,  F02C9/00 ,  H02K5/20

CPC分类号： H02K9/00 ,  F01D25/145 ,  F02C6/12 ,  F02C7/24 ,  F02C9/00 ,  F05D2220/40 ,  F05D2240/14 ,  H02K5/20 ,  H02K7/14 ,  H02K9/19 ,  H02K2205/09

摘要： It is common in electric machines to use the housing as a heat sink to remove energy from the electric machine. In some applications, however, the housing receives energy from a hot element. For example, in an electronically controlled turbocharger, the very hot turbine housing radiates and conducts energy to the electric machine housing exacerbating the heating within the electric machine. To reduce the heat transfer into the electric machine, a gap is provided between the stator and the housing outside the stator. In one alternative, the gap is filled with an insulating material. In another embodiment, the gap is an air gap with the stator located within the housing by circumferential rings or axial rods in corresponding grooves. In yet another embodiment, coolant is provided to the gap at the top and drained away at the bottom under the action of gravity.

摘要翻译： 在电机中通常使用外壳作为散热器来从电机中去除能量。 然而，在一些应用中，壳体从热元件接收能量。 例如，在电子控制的涡轮增压器中，非常热的涡轮机壳体辐射并向电机壳体传导能量，从而加剧电机内的加热。 为了减少传递到电机中的热量，在定子和定子外部的壳体之间设置间隙。 在一个替代方案中，间隙填充有绝缘材料。 在另一个实施例中，间隙是与相应凹槽中的周向环或轴向杆定位在壳体内的定子的气隙。 在另一个实施例中，在顶部的间隙处提供冷却剂并在重力作用下在底部排出。

公开(公告)号：US09091616B2

公开(公告)日：2015-07-28

申请号：US13911779

申请日：2013-06-06

申请人： HONEYWELL INTERNATIONAL INC.

发明人： Kevin Moeckly ,  Richard Ling

IPC分类号： G01M15/05 ,  F02C9/00 ,  G05B17/02

CPC分类号： G01M15/05 ,  F02C9/00 ,  F05D2260/80 ,  F05D2260/81 ,  F05D2270/44 ,  G05B17/02

摘要： An operations support system is provided for an engine receiving fuel. The system includes a diagnostic engine model unit configured to receive engine data from the engine and to generate diagnostics data based on the engine data, the diagnostics data including scalars. The system further includes an engine-specific model unit coupled to the diagnostic engine model unit and configured to receive the scalars and the engine data. The engine-specific model unit includes a fuel flow calculation module configured to determine a current fuel flow for the engine and a set point module configured to generate set point information for the engine using a thermodynamic model that reduces the current fuel flow to the engine, the thermodynamic model being based on component maps associated with the engine. The system further includes a data storage unit coupled to the engine-specific model unit and configured to store the set point information.

摘要翻译： 为接收燃料的发动机提供操作支撑系统。 该系统包括诊断引擎模型单元，其被配置为从引擎接收引擎数据，并且基于引擎数据生成诊断数据，诊断数据包括标量。 该系统还包括耦合到诊断引擎模型单元并被配置为接收标量和引擎数据的引擎特定模型单元。 发动机特定的模型单元包括燃料流量计算模块，其被配置为确定用于发动机的当前燃料流量;以及设定点模块，其被配置为使用减少当前对发动机的燃料流的热力学模型来生成发动机的设定点信息， 热力学模型基于与发动机相关联的分量图。 该系统还包括耦合到引擎特定模型单元并被配置为存储设定点信息的数据存储单元。

公开(公告)号：US20150173254A1

公开(公告)日：2015-06-18

申请号：US14546255

申请日：2014-11-18

申请人： Rolls-Royce Corporation

发明人： Rigoberto J. Rodriguez ,  William L. Siegel ,  Eric D. Schneider ,  Paul Rancuret

IPC分类号： H05K7/20 ,  F02C9/00

CPC分类号： H05K7/20927 ,  F02C9/00 ,  H02J1/102 ,  H02J3/46 ,  H02J4/00

摘要： A turbine engine may include a modular power electronics distribution system having a plurality of modules connectable to a pluggable interface. The pluggable interface may be configured to receive and distribute power to the plurality of modules. Each module may include at least one fault isolation switch and a coolant system including an inlet and return line, as well as a metering valve. At least one power bus may be configured to provide electrical power to at least one of a load or a source via a functional segment. The functional segment may be operable to supply electrical power to the load in a desired form. The modular power electronics distribution system may include a controller in communication with the plurality of modules, the controller configured to control at least one fault isolation switch and metering valve.

摘要翻译： 涡轮发动机可以包括具有可连接到可插拔接口的多个模块的模块化电力电子分配系统。 可插拔接口可以被配置为接收并分配给多个模块的电力。 每个模块可以包括至少一个故障隔离开关和包括入口和回流管线以及计量阀的冷却剂系统。 至少一个电源总线可以被配置为经由功能段向至少一个负载或源提供电力。 功能段可以可操作以以期望的形式向负载提供电力。 模块化电力电子分配系统可以包括与多个模块通信的控制器，所述控制器被配置为控制至少一个故障隔离开关和计量阀。

公开(公告)号：US20150096359A1

公开(公告)日：2015-04-09

申请号：US14265573

申请日：2014-04-30

申请人： GE Aviation Systems Limited

发明人： Christopher Joseph Catt

IPC分类号： G01M15/14

CPC分类号： G07C5/0808 ,  B64D41/00 ,  B64D2045/0085 ,  F01D17/02 ,  F01D17/20 ,  F01D21/003 ,  F02C9/00 ,  F05D2220/50 ,  F05D2260/80 ,  F05D2270/3032 ,  F05D2270/304 ,  F05D2270/44 ,  G07C5/008

摘要： A method of predicting an auxiliary power unit fault in an aircraft having an auxiliary power unit and multiple sensors related to the auxiliary power unit, components thereof, and systems related thereto, including receiving a sensor signal from at least one of the multiple sensors to define a sensor output, comparing the sensor output to a reference value and predicting a fault in the auxiliary power unit based on the comparison.

摘要翻译： 一种在具有辅助动力单元的飞行器中预测辅助动力单元故障的方法，以及与辅助动力单元，其部件及其相关的系统相关的多个传感器，包括从多个传感器中的至少一个接收传感器信号以定义 传感器输出，将传感器输出与参考值进行比较，并根据比较预测辅助动力单元中的故障。

公开(公告)号：US20150040640A1

公开(公告)日：2015-02-12

申请号：US13960091

申请日：2013-08-06

申请人： General Electric Company

发明人： Yuhui Chen

IPC分类号： G01L25/00

CPC分类号： G01L25/00 ,  F01D15/10 ,  F01K5/02 ,  F02C6/18 ,  F02C9/00 ,  F05D2220/64 ,  F05D2220/72 ,  F05D2220/76 ,  F05D2260/4023 ,  F05D2260/821 ,  F05D2270/312 ,  F05D2270/313 ,  F05D2270/331 ,  F05D2270/335 ,  Y02E20/16

摘要： Systems and methods for estimating a base load in a combined cycle power plant with a steam turbine clutch are provided. According to one embodiment of the disclosure, a system may include a controller and a processor communicatively coupled to the controller. The processor may be configured to receive operating parameters associated with a combined cycle power plant. The combined cycle power plant may comprise a gas turbine permanently coupled to a generator and a steam turbine selectively coupled to the generator via a clutch. The processor may be further configured to receive an engagement status associated with the clutch and receive first data and second data. Based on the engagement status, the processor may select the first data or the second data and use that to estimate a base load. The base load estimation may be calibrated based on the operating parameters.

摘要翻译： 提供了一种用于估计具有蒸汽轮机离合器的联合循环发电厂中的基本负载的系统和方法。 根据本公开的一个实施例，系统可以包括通信地耦合到控制器的控制器和处理器。 处理器可以被配置为接收与组合循环发电厂相关联的操作参数。 联合循环发电厂可以包括永久地联接到发电机的燃气轮机和经由离合器选择性地联接到发电机的蒸汽轮机。 处理器可以被进一步配置成接收与离合器相关联的接合状态并接收第一数据和第二数据。 基于参与状态，处理器可以选择第一数据或第二数据，并使用它来估计基本负载。 可以基于操作参数来校准基本负载估计。

公开(公告)号：US20150019104A1

公开(公告)日：2015-01-15

申请号：US13938838

申请日：2013-07-10

申请人： General Electric Company

发明人： Olgu Tanriverdi

IPC分类号： F02C9/00

CPC分类号： F02C9/00 ,  G05B17/02

摘要： A feedback control system is provided and includes a controller to control an operation of a motive element in accordance with current and previous measured states. The controller includes a servo, a processor and an event trigger controller. The event trigger controller is configured to cause the processor to command the servo to perform model based control (MBC) executions in an event a difference between the current and previous measured states exceeds a threshold based on the previous measured state or the current measured state exceeds a limit, and skip the MBC executions in an event the difference does not exceed the threshold and the current measured state does not exceed the limit.

摘要翻译： 提供反馈控制系统，并且包括控制器，以根据当前和之前的测量状态来控制运动元件的操作。 控制器包括伺服器，处理器和事件触发控制器。 事件触发控制器被配置为使得处理器在伺服执行基于模型的控制（MBC）执行的情况下，基于先前的测量状态超过阈值，当前测量状态和先前测量状态之间的差异超过 限制，并且如果差异不超过阈值并且当前测量状态不超过限制，则跳过MBC执行。

公开(公告)号：US20150000297A1

公开(公告)日：2015-01-01

申请号：US14491172

申请日：2014-09-19

申请人： ALSTOM Technology Ltd.

发明人： Manuel ARIAS CHAO ,  Anton NEMET ,  Ulrich Robert STEIGER ,  Darrel Shayne LILLEY

IPC分类号： F02C9/28 ,  F02C7/12

CPC分类号： F02C9/28 ,  F02C7/12 ,  F02C7/18 ,  F02C9/00 ,  F05D2270/303

摘要： The invention relates to a method for determining at least one firing temperature for controlling a gas turbine that comprises at least one compressor, at least one combustion chamber and at least one turbine, compressed air being drawn off at the compressor in order to cool the turbine and being fed to the turbine via at least one external cooling duct and via a control valve arranged in the cooling duct, in which method a plurality of temperatures and pressures of the working medium being measured in various positions of the gas turbine and the at least one firing temperature being derived from the measured temperatures and pressures. A more flexible and more accurate control is achieved additionally by determining the cooling air mass flow via the external cooling duct and by taking said flow into account when deriving the at least one firing temperature.

摘要翻译： 本发明涉及一种用于确定至少一个用于控制燃气涡轮机的燃烧温度的方法，所述燃烧涡轮机包括至少一个压缩机，至少一个燃烧室和至少一个涡轮机，在压缩机处抽出压缩空气以冷却涡轮机 并且经由至少一个外部冷却管道并且经由布置在冷却管道中的控制阀供给到涡轮机，在该方法中，在燃气轮机的各个位置测量工作介质的多个温度和压力，并且至少 一个焙烧温度来自测量的温度和压力。 另外通过确定通过外部冷却管道的冷却空气质量流动并且在得到至少一个焙烧温度时考虑所述流动来实现更灵活和更准确的控制。

公开(公告)号：US20150000294A1

公开(公告)日：2015-01-01

申请号：US14312665

申请日：2014-06-23

申请人： General Electric Company ,  ExxonMobil Upstream Research Company

发明人： Karl Dean Minto ,  Douglas Frank Beadie

IPC分类号： F02C3/34 ,  F02C3/20 ,  F02C9/00

CPC分类号： F02C3/34 ,  F01D17/02 ,  F02C3/20 ,  F02C9/00 ,  F02C9/28 ,  F05D2260/80 ,  F05D2270/0831 ,  F05D2270/80 ,  Y02E20/16 ,  Y02T50/677

摘要： A system includes a plurality of extraction passages configured to passively extract a portion of a gas flow from a downstream region of a gas flow path. The system includes a plurality of sensors respectively coupled to the plurality of extraction passages, wherein the plurality of sensors is configured to measure one or more parameters of the portion of the gas flow traversing the plurality of extraction passages. The system also includes a manifold coupled to the plurality of extraction passages, wherein the manifold is configured to receive the portion of the gas flow from the plurality of extraction passages. The system further includes a return passage coupled to the manifold, wherein the return passage is configured to passively provide the portion of the gas flow to an upstream region of the gas flow path.

摘要翻译： 一种系统包括多个提取通道，其被配置为被动地从气体流路的下游区域提取一部分气流。 该系统包括分别联接到多个提取通道的多个传感器，其中多个传感器被配置成测量穿过多个提取通道的气流的一部分的一个或多个参数。 该系统还包括联接到多个提取通道的歧管，其中歧管被配置为接收来自多个提取通道的气流的一部分。 该系统还包括联接到歧管的返回通道，其中返回通道构造成被动地将气流的一部分提供给气体流动路径的上游区域。