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    CROSS ENGINE COORDINATION DURING GAS TURBINE ENGINE MOTORING
    3.
    发明公开
    CROSS ENGINE COORDINATION DURING GAS TURBINE ENGINE MOTORING 审中-公开
    燃气轮机发动机运转时的交叉发动机协调

    公开(公告)号：EP3296522A1

    公开(公告)日：2018-03-21

    申请号：EP17182126.7

    申请日：2017-07-19

    Applicant: United Technologies Corporation

    Inventor： GELWAN, David ,  CLAUSON, Jesse W. ,  BERRY, James K.

    IPC: F01D13/00 ,  F02C6/00

    CPC classification number: B64D31/12 ,  B64D41/00 ,  B64F1/34 ,  F01D13/00 ,  F01D19/00 ,  F01D21/003 ,  F02C6/00 ,  F02C6/20 ,  F02C7/277 ,  F05D2220/323 ,  F05D2270/13 ,  F05D2270/304 ,  F05D2270/312 ,  F05D2270/54

    Abstract: A system is provided for cross engine coordination during gas turbine engine motoring. The system includes a first gas turbine engine (10A) of a first engine system (100A), a first air turbine starter (120A) of the first engine system (100A), a first starter air valve (116A) of the first engine system (100A), and a controller (102A). The controller (102A) is operable to command the first starter air valve (116A) to control delivery of compressed air to the first air turbine starter (120A) during motoring of the first gas turbine engine (10A), monitor cross engine data of a second gas turbine engine (10B) of a second engine system (100B) to detect a present condition or a commanded action that modifies an aspect of the compressed air received at the first starter air valve (116A), and command an adjustment to the first engine system (100A) to compensate for the modified aspect of the compressed air based on the cross engine data.

    Abstract translation: 在燃气轮机发动机驱动期间提供用于交叉引擎协调的系统。 该系统包括第一发动机系统（100A）的第一燃气涡轮发动机（10A），第一发动机系统（100A）的第一空气涡轮起动器（120A），第一发动机系统（100A）的第一起动器空气阀（116A） （100A）和控制器（102A）。 控制器（102A）可操作以命令第一启动器空气阀（116A）在第一燃气涡轮发动机（10A）的驱动期间控制压缩空气向第一空气涡轮启动器（120A）的输送，监测第一燃气涡轮发动机 第二发动机系统（100B）的第二燃气涡轮发动机（10B），以检测修改在第一启动器空气阀（116A）接收的压缩空气的一个方面的当前状况或命令动作，并且命令对第一启动器空气阀 发动机系统（100A）基于交叉引擎数据补偿压缩空气的修改方面。

    RANGE EXTENDER VEHICLE
    4.
    发明公开
    RANGE EXTENDER VEHICLE 审中-公开
    范围扩展车辆

    公开(公告)号：EP3275718A1

    公开(公告)日：2018-01-31

    申请号：EP16767615.4

    申请日：2016-01-13

    Applicant: Technologies' Xanadu of Resonatory-Solar- Systemed Co., Ltd

    Inventor： JIN, Pu

    IPC: B60L11/12

    CPC classification number: B60L11/123 ,  B60K6/24 ,  B60K6/46 ,  B60L11/12 ,  B60L2220/10 ,  B60W10/06 ,  B60W10/08 ,  B60W10/26 ,  B60W20/10 ,  B60W20/13 ,  B60W30/18054 ,  B60W2510/244 ,  B60W2510/246 ,  B60Y2400/431 ,  F01D15/10 ,  F02C6/20 ,  F02C7/06 ,  F02C7/08 ,  F02C9/18 ,  F05D2220/76 ,  Y02T10/6217 ,  Y02T10/6286 ,  Y02T10/6295 ,  Y02T10/7258

    Abstract: A range extender vehicle comprises: a turboshaft engine (1) arranged on a vehicle frame (12) chassis, a turboshaft engine controller (2), a generator (3), a battery pack (4), a battery controller (5), a driving motor (6), a battery heat radiator (7), and a gas storage tank (9). A signal end of the turboshaft engine (1) is connected to the turboshaft engine controller (2). A transmission shaft (1-6) is connected to a rotatory shaft of the generator (3). The generator (3) outputs an electric energy to the battery pack (4) and the driving motor (6) respectively. The battery pack (4) and the driving motor (6) are connected together and are connected to the battery controller (5) at the signal end. The transmission shaft of the driving motor (6) is connected to wheels (11). A cold air channel of the battery heat radiator (7) leads to the battery pack (4). A gas pipeline of the gas storage tank (9) is connected to a gas inlet pipeline of the turboshaft engine (1). The present invention forms a highly efficient, stable, and environmental friendly system, and has advantages of a high power to weight ratio, a low power consumption, a low emission, a low noise and vibration, eliminating the need for an exhaust gas treatment system and being easy to maintain, and having a long serving life.

    Abstract translation: 一种增程器车辆包括：布置在车架（12）底盘上的涡轮轴发动机（1），涡轮轴发动机控制器（2），发电机（3），电池组（4），电池控制器（5） 驱动马达（6），电池散热器（7）和储气罐（9）。 涡轮轴发动机（1）的信号端连接到涡轮轴发动机控制器（2）。 传动轴（1-6）连接到发电机（3）的旋转轴。 发电机（3）分别向电池组（4）和驱动电机（6）输出电能。 电池组（4）和驱动电机（6）连接在一起并在信号端连接到电池控制器（5）。 驱动马达（6）的传动轴连接到轮子（11）。 电池散热器（7）的冷空气通道通向电池组（4）。 储气罐（9）的气体管路连接涡轮轴发动机（1）的进气管路。 本发明形成了一种高效，稳定，环保的系统，具有重量比高，功耗低，排放少，噪音低，振动小的优点，不需要废气处理系统 易于维护，使用寿命长。

    Electrical power generator for a gas turbine engine
    6.
    发明公开
    Electrical power generator for a gas turbine engine 有权
    电流发生器用于燃气涡轮发动机

    公开(公告)号：EP2910739A1

    公开(公告)日：2015-08-26

    申请号：EP15152873.4

    申请日：2015-01-28

    Applicant: Rolls-Royce plc

    Inventor： Edwards, Huw Llewelyn

    IPC: F01D15/10 ,  F02C9/28 ,  H02P9/04 ,  H02P9/48

    CPC classification number: H02P9/04 ,  F01D15/10 ,  F02C6/20 ,  F02C9/00 ,  F02C9/28 ,  F05D2220/323 ,  F05D2220/764 ,  F05D2220/7642 ,  F05D2220/7646 ,  F05D2270/01 ,  F05D2270/02 ,  F05D2270/061 ,  F05D2270/071 ,  F05D2270/304 ,  F05D2270/309 ,  F05D2270/332 ,  F05D2270/335 ,  H02P9/007 ,  H02P9/48

    Abstract: An electrical power generation system (100) for an aircraft gas turbine engine (10). The system comprises an alternating current electrical generator (110) having a rotor (114) comprising a plurality of electromagnetic rotor windings (118) and a stator (124) comprising a plurality of electrical stator windings (126). The rotor (114) is mechanically coupled to a shaft (36) of the gas turbine engine (10) by a transmission system (129). The electrical generator (110) further includes an electrical output frequency controller (130), a torque sensor arrangement configured to determine a torque imposed on the transmission system (129) by the generator (110) and a controller (112) configured to operate the electrical power generation system in first mode and second modes. In the first mode, the frequency of the electrical power output of the electrical generator (110) is controlled by the electrical output frequency controller (130) to lie within predetermined limits, and a reduced idle signal is provided to a gas turbine engine controller (132). In the second mode, the frequency of the electrical power output of the electrical generator (132) is not controlled by the electrical output frequency controller (130) and an increased idle signal is provided to the gas turbine engine controller (132). The electrical generator controller (112) is configured to operate the electrical power generation system (100) in the first mode when the torque is below a predetermined limit, and in the second mode when the torque is above a predetermined limit.

    Gasturbine
    7.
    发明公开
    Gasturbine 审中-公开
    燃气轮机

    公开(公告)号：EP2894315A1

    公开(公告)日：2015-07-15

    申请号：EP14151119.6

    申请日：2014-01-14

    Applicant: Siemens Aktiengesellschaft

    Inventor： Savilius, Nicolas ,  Link, Marco

    IPC: F02C3/10 ,  F02C3/113 ,  F02C6/20 ,  F02C7/36

    CPC classification number: F02C3/10 ,  F02C3/113 ,  F02C6/20 ,  F02C7/36 ,  F05D2260/406

    Abstract: Eine zweiwellige Gasturbine (10) umfasst einen Verdichter (13), eine Hochdruckturbine (14), eine Niederdruckturbine (15), eine in dem Verdichter (13) und der Hochdruckturbine (14) angeordnete erste Welle (28) sowie eine in der Niederdruckturbine (15) angeordnete zweite Welle (29). Die Gasturbine umfasst eine Kupplung (16, 30), mit der die erste Welle (28) und die zweite Welle (29) miteinander zumindest in eine Drehrichtung drehmomentübertragend verbindbar sind.

    Abstract translation: 的两轴的燃气涡轮（10）包括压缩机（13），高压涡轮（14），一个低压涡轮机（15），一个在所述压缩机（13）和所述高压涡轮（14）布置的第一轴（28）和一个（在低压涡轮机 15）布置的第二轴（29）。 该燃气涡轮机包括一个离合器（16，30），与该第一轴（28）和第二轴（29）彼此连接以传递转矩，在一个旋转方向上的至少。

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