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41. 发明专利

JP4326317B2 Gas turbine control device 有权
公开(公告)号：JP4326317B2
公开(公告)日：2009-09-02
申请号：JP2003412870
申请日：2003-12-11
申请人：三菱重工業株式会社
发明人：文倫藤井
IPC分类号： F01D17/00 , F01D15/10 , F01D17/02 , F02C7/042 , F02C7/057 , F02C9/28
CPC分类号： F01D15/10 , F02C9/28 , F05D2220/76 , F05D2270/061 , F05D2270/081 , F05D2270/304 , Y02T50/677

42. 发明专利

JP2011043136A Fuel control device at starting of gas turbine engine 审中-公开
标题翻译：燃油涡轮发动机启动燃油控制装置
公开(公告)号：JP2011043136A
公开(公告)日：2011-03-03
申请号：JP2009192934
申请日：2009-08-24
申请人： Honda Motor Co Ltd , 本田技研工業株式会社
发明人： SASAKI TORU , KASAI NORIO
IPC分类号： F02C7/26 , F02C9/00 , F02C9/28
CPC分类号： F02C9/28 , F05D2260/85 , F05D2270/081 , F05D2270/3013 , F05D2270/303 , F05D2270/304 , Y02T50/677
摘要： PROBLEM TO BE SOLVED: To provide a fuel control device during a starting period of a gas turbine engine, which hardly generates white smoke caused by reduction of spraying performance at the starting of the engine even in an unstable zone with low exhaust gas temperature.
SOLUTION: In the fuel control device, a first fuel flow rate Wf_P3 is calculated on the basis of detected output pressure P3 of a compressor, a second fuel flow rate Wf_St at the starting of the engine is calculated at the starting of the engine on the basis of a detected temperature T1 of an inflow air, a temperature EGT of an exhaust gas, the number of rotation N2 of the compressor, and pressure P1 of the inflow air, either of the first fuel flow rate Wf_P3 and the second fuel flow rate Wf_St is selected on the basis of the detected temperature EGT of the exhaust gas, and opening and closing of a fuel adjustment valve 32 is controlled on the basis of the selected fuel flow rate.
COPYRIGHT: (C)2011,JPO&INPIT
摘要翻译：要解决的问题：为了在燃气轮机的起动期间提供燃料控制装置，即使在低排气的不稳定区域中，由于在发动机起动时喷射性能降低也难以产生白烟温度。解决方案：在燃料控制装置中，基于压缩机的检测输出压力P3计算第一燃料流量Wf_P3，在起动时计算发动机起动时的第二燃料流量Wf_St 基于流入空气的检测温度T1，排气的温度EGT，压缩机的旋转数N2和流入空气的压力P1，第一燃料流量Wf_P3和第二燃料流量Wf 基于排气的检测温度EGT选择燃料流量Wf_St，并且基于所选择的燃料流量来控制燃料调节阀32的打开和关闭。版权所有（C）2011，JPO＆INPIT

43. 发明专利

JP2007016640A Gas turbine facilities using humid air 有权
标题翻译：使用湿气的气体涡轮机设备
公开(公告)号：JP2007016640A
公开(公告)日：2007-01-25
申请号：JP2005197088
申请日：2005-07-06
申请人： Hitachi Ltd , 株式会社日立製作所
发明人： SASAKI KENJI , ARAKI HIDEFUMI , KATAGIRI YUKINORI , TSUKAMOTO MORIAKI , HOIZUMI SHINICHI
IPC分类号： F02C3/30 , F02C7/08 , F02C7/143
CPC分类号： F01D25/30 , F01D25/32 , F02C3/30 , F02C3/305 , F02C6/18 , F02C7/08 , F02C7/141 , F05D2270/081 , F05D2270/0831 , F05D2270/16
摘要： PROBLEM TO BE SOLVED: To provide gas turbine facilities using humid air capable of preventing generation of white smoke all year around and inhibiting a drop of thermal efficiency by inhibiting surplus heat discharge.
SOLUTION: In the gas turbine facilities using humid air including a humidifying device 6 humidifying compressed air for combustion, a heat collection device collecting waste heat from the gas turbine or the compressed air and raising temperature of humidifying water of the humidifying device, a regeneration heat exchanger 7 collecting waste heat from the gas turbine 1 and raising temperature of compressed air for combustion, a dehumidifying device 10 dehumidifying and collecting moisture in exhaust gas passing through the regeneration heat exchanger, and an exhaust gas reheating device 11 reheating exhaust gas after dehumidified, a temperature measuring means 27 measuring temperature of exhaust gas passing through the exhaust gas reheating device 11 and a heating temperature adjusting means raising temperature of heating temperature of the exhaust gas reheating device when exhaust gas temperature measured by the temperature measuring means is equal to or less than a predetermined value are provided.
COPYRIGHT: (C)2007,JPO&INPIT
摘要翻译：要解决的问题：提供使用能够防止全年白烟产生的潮湿空气的燃气轮机设备，并通过抑制多余的放热来抑制热效率的降低。解决方案：在使用潮湿空气的燃气轮机设备中，包括加湿装置6，加湿用于燃烧的压缩空气，收集装置，其收集来自燃气轮机或压缩空气的废热以及加湿装置的加湿水的升温，收集来自燃气轮机1的废热和用于燃烧的压缩空气的升高温度的再生用热交换器7，对通过再生用热交换器的排气中的湿气进行除湿收集的除湿装置10以及排气再加热装置11 除湿后的温度测量装置27测量通过排气再加热装置11的废气的温度和当由温度测量装置测量的排气温度相等时升高废气再加热装置的加热温度的加热温度调节装置达到或小于预定的va 提供lue。版权所有（C）2007，JPO＆INPIT

44. 发明专利

JP2005171873A Device for computing turbine mechanical output and device for controlling gas turbine provided with the same 有权
标题翻译：用于计算涡轮机械输出的装置和用于控制其提供的气体涡轮的装置
公开(公告)号：JP2005171873A
公开(公告)日：2005-06-30
申请号：JP2003412870
申请日：2003-12-11
申请人： Mitsubishi Heavy Ind Ltd , 三菱重工業株式会社
发明人： FUJII FUMITOMO
IPC分类号： F01D17/00 , F01D15/10 , F01D17/02 , F02C7/042 , F02C7/057 , F02C9/28
CPC分类号： F01D15/10 , F02C9/28 , F05D2220/76 , F05D2270/061 , F05D2270/081 , F05D2270/304 , Y02T50/677
摘要： PROBLEM TO BE SOLVED: To provide a device for computing turbine mechanical output, capable of accurately determining gas turbine mechanical output and maintaining air fuel ratio in an appropriate range even under transient state in which generator output changes and gas turbine speed changes, and a device for controlling a gas turbine provided with the same.
SOLUTION: The device for computing gas turbine mechanical output 22 computes gas turbine mechanical output P by a formula (a) based on generator effective electric power Pe measured by a generator effective power meter 12, turbine revolution speed N measured by a gas turbine revolution speed meter 11, inertia moment J of the gas turbine and gravitational acceleration g. A combustion air quantity control device 26 controls combustion air quantity based on the gas turbine mechanical output P.
COPYRIGHT: (C)2005,JPO&NCIPI
摘要翻译：要解决的问题：为了提供一种用于计算涡轮机械输出的装置，即使在发电机输出变化和燃气轮机速度变化的瞬态下，能够精确地确定燃气轮机械输出并将空燃比维持在适当的范围内，以及用于控制设有该燃气轮机的燃气轮机的装置。解决方案：用于计算燃气涡轮机械输出22的装置基于由发电机有效功率计12测量的发电机有效电力Pe，通过公式（a）计算燃气轮机械输出P，由气体测量的涡轮转速N 涡轮转速表11，燃气轮机的惯性矩J和重力加速度g。燃烧空气量控制装置26基于燃气轮机械输出P控制燃烧空气量。（C）2005，JPO＆NCIPI

45. 发明授权

KR101136228B1 가스 터빈 시스템에서 연료 성분의 변화를 보상하기 위한방법 및 장치 有权
标题翻译：用于补充燃气组合物在气体涡轮机系统中的变化的方法和装置
公开(公告)号：KR101136228B1
公开(公告)日：2012-04-17
申请号：KR1020067007616
申请日：2004-10-11
申请人： 지멘스 악티엔게젤샤프트
发明人： 베렌브링크,페터 , 블로메이어,말테
IPC分类号： F02C9/34 , F02C9/26
CPC分类号： F02C9/34 , F05D2270/08 , F05D2270/081
摘要： 본 발명은 병렬식으로 작동되는 두 개 이상의 버너 스테이지로 구성되는 가스 터빈 시스템에서의 연료 성분의 변화를 보상하기 위한 방법에 관한 것으로, 두 개 이상의 버너 스테이지로의 연료의 공급은 연료 성분의 변화에 반응하여 조절되며, 버너 스테이지들 사이의 연료 스플리트, 즉 버너 스테이지들로 공급되는 연료의 속도의 상대적인 증가,가 목표 값으로 조절되거나 연료 공급의 조절 동안 목표 값을 일정하게 유지한다. 목표 값은, 예를 들면, 일정하거나 하나의 변수 또는 다수의 변수의 함수일 수 있다. 더욱 상세하게는, 가스 터빈 시스템은 파일럿 버너 스테이지 및 주 버너 스테이지를 포함할 수 있다. 연료의 공급이 조절되면, 파일럿 버너와 주 버너 스테이지 사이의 연료 스플리트는 목표 값으로 조절되거나 목표 값으로 일정하게 유지된다.

46. 发明公开

KR1020060096435A 가스 터빈 시스템에서 연료 성분의 변화를 보상하기 위한방법 및 장치 有权
标题翻译：用于补充燃气组合物在气体涡轮机系统中的变化的方法和装置
公开(公告)号：KR1020060096435A
公开(公告)日：2006-09-11
申请号：KR1020067007616
申请日：2004-10-11
申请人： 지멘스 악티엔게젤샤프트
发明人： 베렌브링크,페터 , 블로메이어,말테
IPC分类号： F02C9/34 , F02C9/26
CPC分类号： F02C9/34 , F05D2270/08 , F05D2270/081
摘要： The invention relates to a method for compensating variations in fuel composition in a gas turbine system consisting of at least two parallel-operated burner stages, wherein the fuel supply to at least two of the burner stages is adjusted in response to variations in fuel composition, wherein the fuel split between the burner stages, i.e. the relative increase in speed of the fuel supplied to the burner stages, is adjusted to a target value or maintained at a target value during adjustment of the fuel supply. The target value can, for example, be a constant or a function of one or several variables. More particularly, the gas turbine system can comprise a pilot burner stage and a main burner stage. When the fuel supply is adjusted, the fuel split between the pilot burner stage and the main burner stage is adjusted to a target value or maintained at a target value.
摘要翻译：本发明涉及一种用于补偿由至少两个平行操作的燃烧器级构成的燃气轮机系统中的燃料组成变化的方法，其中至少两个燃烧器级的燃料供应是根据燃料组成的变化进行调整的，其中在燃料级之间分配的燃料，即供应到燃烧器级的燃料的速度的相对增加在调节燃料供应期间被调整到目标值或维持在目标值。例如，目标值可以是常数或一个或多个变量的函数。更具体地，燃气轮机系统可以包括引燃燃烧器级和主燃烧器级。当调节燃料供应时，将引燃燃烧器级和主燃烧器级之间的燃料分配调节到目标值或维持在目标值。

47. 发明授权

EP2873836B1 Engine fuel delivery system 审中-实审转让
公开(公告)号：EP2873836B1
公开(公告)日：2018-08-29
申请号：EP14190784.0
申请日：2014-10-29
申请人： Rolls-Royce plc
发明人： Swann, Peter
IPC分类号： F02C3/20 , F02C7/236 , F02C9/40
CPC分类号： B64D45/00 , B64D37/30 , F02C3/20 , F02C7/236 , F02C9/40 , F05D2270/07 , F05D2270/081 , Y02T50/671 , Y02T50/677 , Y02T50/678
摘要： This invention concerns a fuel delivery system for an aircraft engine, comprising a fuel delivery regulator arranged to receive fuel from a plurality of fuel sources for supply to the engine. An engine operating condition sensor reading is received by a control unit arranged to control operation of the regulator. The control unit actuates the regulator based on a received signal from the engine operating condition sensor in order to vary the volume of fuels from the plurality of fuel sources supplied to the engine during at least a portion of the landing/take-off (LTO) cycle relative to a further portion of the aircraft flight. The different fuels may comprise kerosene and an alternative fuel, such as a biofuel.

48. 发明公开

EP2685280A3 Fuel system 有权转让
公开(公告)号：EP2685280A3
公开(公告)日：2018-01-24
申请号：EP13168164.5
申请日：2013-05-17
申请人： Rolls-Royce plc
发明人： Swann, Peter
IPC分类号： F02C3/30 , F02C9/40
CPC分类号： G01N33/0004 , F02C3/30 , F02C9/00 , F02C9/28 , F02C9/40 , F05D2270/08 , F05D2270/081 , F05D2270/0831 , F05D2270/804 , Y02T50/671 , Y02T50/677
摘要： A fuel system (12) comprising a vapour trail detection sensor (20) configured to generate a first signal (28) which indicates the optical depth of a vapour trail (35). A control unit (40) is provided responsive to the first signal (28) and configured to generate a second signal (80) in dependence upon the first signal (28). The second signal (80) defines a percentage of at least one of a first fuel composition and second fuel composition required to produce a resultant fuel composition. At least one regulator (42) is provided configured to receive and be responsive to the second signal (80) and regulate the percentage of first and second fuel composition required to produce the resultant fuel composition.

49. 发明授权

EP2860374B1 Fuel delivery system 有权转让
标题翻译：燃油输送系统
公开(公告)号：EP2860374B1
公开(公告)日：2017-06-14
申请号：EP14184757.4
申请日：2014-09-15
申请人： Rolls-Royce plc
发明人： Swann, Peter
IPC分类号： F02C3/20 , F02C7/22 , F02C9/40 , G01S17/88
CPC分类号： F02C9/28 , F02C3/20 , F02C7/22 , F02C9/40 , F05D2270/081 , F05D2270/082 , G01N21/538 , Y02T50/671 , Y02T50/677

50. 发明公开

EP2873836A1 Engine fuel delivery system 审中-实审转让
标题翻译： Motorkraftstoffabgabesystem
公开(公告)号：EP2873836A1
公开(公告)日：2015-05-20
申请号：EP14190784.0
申请日：2014-10-29
申请人： Rolls-Royce plc
发明人： Swann, Peter
IPC分类号： F02C3/20 , F02C7/236 , F02C9/40
CPC分类号： B64D45/00 , B64D37/30 , F02C3/20 , F02C7/236 , F02C9/40 , F05D2270/07 , F05D2270/081 , Y02T50/671 , Y02T50/677 , Y02T50/678
摘要： This invention concerns a fuel delivery system for an aircraft engine, comprising a fuel delivery regulator arranged to receive fuel from a plurality of fuel sources for supply to the engine. An engine operating condition sensor reading is received by a control unit arranged to control operation of the regulator. The control unit actuates the regulator based on a received signal from the engine operating condition sensor in order to vary the volume of fuels from the plurality of fuel sources supplied to the engine during at least a portion of the landing/take-off (LTO) cycle relative to a further portion of the aircraft flight. The different fuels may comprise kerosene and an alternative fuel, such as a biofuel.
摘要翻译：本发明涉及一种用于飞行器发动机的燃料输送系统，其包括燃料输送调节器，燃料输送调节器布置成从多个燃料源接收燃料以供给发动机。发动机工况条件传感器读数被设置成控制调节器运行的控制单元接收。控制单元基于来自发动机操作状态传感器的接收信号来致动调节器，以便在至少一部分着陆/起飞（LTO）期间改变从提供给发动机的多个燃料源中的燃料的体积，相对于飞机飞行的另一部分。不同的燃料可以包括煤油和替代燃料，例如生物燃料。

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