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公开(公告)号：US09880527B2
公开(公告)日：2018-01-30
申请号：US14750330
申请日：2015-06-25
Applicant: General Electric Company
Inventor： Guoxin Li , R. Sheldon Carpenter
CPC classification number: G05B13/026 , F01D17/06 , F01D17/085 , F02C9/28 , F05D2220/32 , F05D2240/24 , F05D2260/80 , F05D2270/03 , F05D2270/301 , F05D2270/44
Abstract: A method of tracking variable states of a gas turbine engine in transient conditions includes obtaining input data representative of rotor velocity and pressure ratio; calculating a reference transient scheduled trajectory based on the input data; calculating a speed reference transient scheduled trajectory based on the input data; calculating a feedforward variable based on the reference transient scheduled trajectory; obtaining a feedback control variable; and determining a control variable based on a combination of the feedforward variable and the feedback control variable.
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公开(公告)号：US20160369702A1
公开(公告)日：2016-12-22
申请号：US14902034
申请日：2014-07-03
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： John R. Otto , James B. Coffin
IPC: F02C7/36 , F16H3/72 , F02K3/06 , F04D25/02 , F04D29/053
CPC classification number: F02C7/36 , F02C3/113 , F02K3/06 , F04D25/028 , F04D29/053 , F05D2220/36 , F05D2250/411 , F05D2260/40311 , F05D2270/03 , F16H3/72 , F16H3/724
Abstract: A fan drive gear system for a turbofan engine includes a geared architecture and a gear controller supporting the geared architecture and controlling rotation of the geared architecture relative a static structure.
Abstract translation: 用于涡轮风扇发动机的风扇驱动齿轮系统包括齿轮架构和支撑齿轮架构的齿轮控制器，并且相对于静态结构控制齿轮架构的旋转。
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3.发明申请ENGINE DRIVEN-SHAFT DRIVEN COMPRESSOR UTILIZING INFINITELY VARIABLE TRANSMISSION 有权使用无限可变传动的发动机驱动压缩机公开(公告)号：US20160167790A1
公开(公告)日：2016-06-16
申请号：US14549213
申请日：2014-11-20
Applicant: Hamilton Sundstrand Corporation
Inventor： Harold W. Hipsky , Gregory L. DeFrancesco
CPC classification number: B64D13/06 , B64D13/02 , B64D2013/0618 , F02C6/08 , F02C7/32 , F02C7/36 , F02K3/00 , F05D2260/40 , F05D2270/03
Abstract: An air compressing system is provided that includes a compressor configured to compressor air. An engine is operatively connected to the compressor. Further, an infinitely variable transmission is operatively connected between the engine and the compressor. A first shaft operatively connects the engine to the infinitely variable transmission and is configured to rotate at a first speed and a second shaft operatively connects the infinitely variable transmission to the compressor and is configured to rotate at a second speed.
Abstract translation: 提供一种空气压缩系统，其包括被构造成压缩空气的压缩机。 发动机可操作地连接到压缩机。 此外，无级变速器可操作地连接在发动机和压缩机之间。 第一轴将发动机可操作地连接到无级变速器，并且构造成以第一速度旋转，并且第二轴将无级变速器可操作地连接到压缩机并且构造成以第二速度旋转。
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公开(公告)号：US08899008B2
公开(公告)日：2014-12-02
申请号：US13471926
申请日：2012-05-15
Applicant: Douglas Alan Jones , Gerardo Plata Contreras , Robert Allen Baten , Victor Gerardo Cabal Velarde , Jingmei Zhang , Jesus Elios Almendarez Mendez , Richard Michael Watkins
Inventor： Douglas Alan Jones , Gerardo Plata Contreras , Robert Allen Baten , Victor Gerardo Cabal Velarde , Jingmei Zhang , Jesus Elios Almendarez Mendez , Richard Michael Watkins
CPC classification number: F02C7/047 , F01D25/02 , F02C7/057 , F02C7/08 , F05D2260/213 , F05D2260/95 , F05D2270/03 , F05D2270/11 , F05D2270/303
Abstract: A system includes an anti-icing heat recovery system, which includes a first heat exchanger, a second heat exchanger, and a variable speed fan. The first heat exchanger is configured to receive a working fluid from an exhaust section of a gas turbine engine and to transfer heat from the working fluid to a cooled intermediate heat transfer medium to generate a heated intermediate heat transfer medium. The second heat exchanger is configured to receive the heated intermediate heat transfer medium from the first heat exchanger and to transfer heat from the heated intermediate heat transfer medium to air entering the gas turbine engine. The variable speed fan is configured to urge the working fluid from the exhaust section of the gas turbine engine through the first heat exchanger.
Abstract translation: 一种系统包括防冰热回收系统，其包括第一热交换器，第二热交换器和变速风扇。 第一热交换器被配置为从燃气涡轮发动机的排气部分接收工作流体并将热量从工作流体传递到冷却的中间传热介质以产生加热的中间传热介质。 第二热交换器构造成从第一热交换器接收加热的中间传热介质，并将热量从加热的中间传热介质传递到进入燃气涡轮发动机的空气。 变速风扇构造成通过第一热交换器促使来自燃气涡轮发动机的排气部的工作流体。
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5.发明申请公开(公告)号：US20160356280A1
公开(公告)日：2016-12-08
申请号：US14731047
申请日：2015-06-04
Applicant: United Technologies Corporation
Inventor： Victor Pascu , Anthony C. Jones
CPC classification number: F04D27/004 , F02C9/16 , F02C9/28 , F04D17/10 , F05D2220/50 , F05D2270/03 , F05D2270/061 , F05D2270/07 , F05D2270/112 , F05D2270/20 , F05D2270/303 , F05D2270/304 , F05D2270/313
Abstract: Systems and methods for controlling an auxiliary power unit (APU) are provided. The systems and methods may comprise detecting an operating condition of the APU, determining an optimal APU frequency in response to the operating condition, and setting an angular velocity of the APU to the optimal APU frequency.
Abstract translation: 提供了用于控制辅助电源单元（APU）的系统和方法。 系统和方法可以包括检测APU的操作状态，响应于操作条件确定最佳APU频率，并将APU的角速度设置为最佳APU频率。
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Patent Agency Ranking
公开(公告)号：US20160201564A1
公开(公告)日：2016-07-14
申请号：US15073768
申请日：2016-03-18
Applicant: IHI Corporation
Inventor： Daisuke OBA
CPC classification number: F02C9/30 , F02C7/236 , F05D2260/40 , F05D2270/03 , F05D2270/3015 , F05D2270/304 , F23K5/04
Abstract: A fuel system includes: a constant-volume pump and a centrifugal pump increasing the pressure of fuel to be supplied to an engine for aviation and discharging the fuel; an operation controller configured to select in accordance with the operation state of the engine, one of a constant-volume pump-using mode of increasing the pressure of fuel using the constant-volume pump and a centrifugal pump-using mode of increasing it using the centrifugal pump; and a speed changer connecting the engine and the centrifugal pump, changing the rotational speed of rotational power output from the engine and transmitting the rotational power to the centrifugal pump, and being capable of adjusting the speed-changing ratio of the rotational speed.
Abstract translation: 燃料系统包括：恒定容积泵和离心泵，其增加供应给发动机的燃料的压力，用于航空和排放燃料; 操作控制器，被配置为根据发动机的操作状态来选择使用恒定体积泵增加燃料的压力的恒定体积的泵使用模式和使用恒定容积泵的离心泵使用模式， 离心泵; 以及连接发动机和离心泵的变速器，改变从发动机输出的旋转动力的转速并将旋转动力传递到离心泵，并且能够调节转速的变速比。
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公开(公告)号：US20150378327A1
公开(公告)日：2015-12-31
申请号：US14750330
申请日：2015-06-25
Applicant: General Electric Company
Inventor： Guoxin Li , R. Sheldon Carpenter
CPC classification number: G05B13/026 , F01D17/06 , F01D17/085 , F02C9/28 , F05D2220/32 , F05D2240/24 , F05D2260/80 , F05D2270/03 , F05D2270/301 , F05D2270/44
Abstract: A method of tracking variable states of a gas turbine engine in transient conditions includes obtaining input data representative of rotor velocity and pressure ratio; calculating a reference transient scheduled trajectory based on the input data; calculating a speed reference transient scheduled trajectory based on the input data; calculating a feedforward variable based on the reference transient scheduled trajectory; obtaining a feedback control variable; and determining a control variable based on a combination of the feedforward variable and the feedback control variable.
Abstract translation: 在瞬态条件下跟踪燃气涡轮发动机的可变状态的方法包括获得代表转子速度和压力比的输入数据; 基于输入数据计算参考瞬态调度轨迹; 基于输入数据计算速度参考瞬态调度轨迹; 基于参考瞬态调度轨迹计算前馈变量; 获得反馈控制变量; 以及基于所述前馈变量和所述反馈控制变量的组合来确定控制变量。
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公开(公告)号：US20150192075A1
公开(公告)日：2015-07-09
申请号：US14528562
申请日：2014-10-30
Inventor： Michael GRIFFITHS
CPC classification number: F02C9/30 , F01D19/00 , F02C7/236 , F02C7/26 , F02C9/28 , F02C9/32 , F05D2220/323 , F05D2260/85 , F05D2270/03 , F05D2270/07 , F05D2270/304 , F05D2270/56 , F05D2270/64 , F05D2270/66 , Y02T50/671
Abstract: An engine fuel control system includes a fuel metering valve that controls the flow of fuel between supply and delivery lines which delivers fuel to engine burners. The fuel control system includes a fixed displacement main pump which receives fuel from a low pressure source and delivers the fuel at a first high pressure to the supply line, an augmenter pump which receives fuel from the low pressure source and delivers the fuel at a second high pressure to one or more fuel-pressure operated auxiliary engine devices, and a start valve which is actuated at low engine speeds to open a flow path which diverts fuel delivered by the augmenter pump away from the auxiliary engine devices to the supply line to augment the fuel delivered thereto by the main pump, the start valve being actuated at higher engine speeds to shut the flow path.
Abstract translation: 发动机燃料控制系统包括燃料计量阀，其控制在将燃料输送到发动机燃烧器的供应和输送管线之间的燃料流动。 燃料控制系统包括固定排量主泵，其从低压源接收燃料并将燃料以第一高压输送到供应管线;增压泵，其从低压源接收燃料并在第二高压源处输送燃料 一个或多个燃料压力操作的辅助发动机装置的高压，以及以低发动机转速致动的起动阀，以打开将由增压泵输送的燃料从辅助发动机装置转移到供应管线以增加的流动路径 由主泵输送的燃料，起动阀以更高的发动机转速被致动以关闭流路。
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公开(公告)号：US20190061969A1
公开(公告)日：2019-02-28
申请号：US16110699
申请日：2018-08-23
Applicant: PRATT & WHITNEY CANADA CORP.
Inventor： Philippe Beauchesne-Martel
CPC classification number: B64D31/06 , F01D17/105 , F01D17/16 , F02C9/20 , F02C9/54 , F04D27/0246 , F05D2220/323 , F05D2270/03 , F05D2270/053 , F05D2270/061 , F05D2270/304 , F05D2270/309 , F05D2270/54
Abstract: Herein provided are methods and systems for controlling an engine having a variable geometry mechanism. A power level difference between a requested engine power level and a current engine power level is determined at a computing device. The power level difference is compared to a predetermined power threshold at the computing device. When the power level difference exceeds the predetermined power threshold, a position control signal for changing a position of the variable geometry mechanism is generated and output at the computing device, the position control signal generated based on a requisite bias level, the requisite bias level being based on the power level difference.
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公开(公告)号：US09970447B2
公开(公告)日：2018-05-15
申请号：US14934711
申请日：2015-11-06
Applicant: TOYOTA JIDOSHA KABUSHIKI KAISHA
Inventor： Kohei Oda , Kenji Umayahara
IPC: F04D27/02 , B60L1/00 , B60L11/18 , H01M8/04694 , H01M8/04746
CPC classification number: F04D27/0261 , B60L1/003 , B60L11/1883 , F05B2260/821 , F05B2270/101 , F05B2270/1032 , F05B2270/335 , F05B2270/404 , F05D2260/821 , F05D2270/03 , F05D2270/304 , F05D2270/335 , F05D2270/44 , H01M8/04694 , H01M8/04753 , H01M2250/20 , Y02T90/32 , Y02T90/34
Abstract: A fuel cell system includes an air compressor that supplies oxidant gas to a fuel cell installed in a fuel cell vehicle, a measured rotational speed acquirer that acquires a measured value of rotational speed of the air compressor, and a controller that calculates a rotational speed command value of the air compressor based on required generated power of the fuel cell, calculates a torque command value of the air compressor based on the calculated rotational speed command value and current rotational speed of the air compressor, and controls rotational speed of the air compressor based on the calculated torque command value. The controller estimates the current rotational speed of the air compressor baaed on the measured value of the rotational speed acquired by the measured rotational speed acquirer and a history of the calculated torque command value, and calculates the torque command value by using the estimated rotational speed.
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