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1. 发明专利

JP2009097841A gas turbine 有权
标题翻译：燃气轮机
公开(公告)号：JP2009097841A
公开(公告)日：2009-05-07
申请号：JP2007272592
申请日：2007-10-19
申请人： Mitsubishi Heavy Ind Ltd , 三菱重工業株式会社
发明人： MATSUYAMA KEISUKE , MIYAUCHI KOTARO
IPC分类号： F23R3/42 , F02C7/24 , F23R3/16 , F23R3/18
CPC分类号： F02C7/24 , F01D9/023 , F05D2260/96 , F05D2260/963 , F23M20/005 , F23R3/00 , F23R2900/00014
摘要： PROBLEM TO BE SOLVED: To provide a gas turbine, improving the appearance of a combustion vibration reducing device disposed in a tail cylinder of a combustor. SOLUTION: The combustion vibration reducing device 34 is disposed in the tail cylinder of the combustor to form a gas space S, and the gas space L and the interior of the tail cylinder 32 are communicated with each other through a plurality of air holes 343. The combustion vibration reducing device 34 includes: a first member 341 having a substantially U-shaped section formed by pressing and disposed on the outer periphery of the tail cylinder 32 with the opening part of a substantially U-shaped sectional form directed toward the tail 32; and a second member 342 blocking up the opening part of a substantially U-shaped sectional form of the first member 341 to form a gas space S up to the first member 341, and having a plurality of air holes 343. In a radial sectional view of the tail cylinder 32, when the outside diameter of the tail cylinder 32 changes as it goes toward the axial direction of the tail cylinder 32, the distances d1, d2 from the axis L of the tail cylinder 32 to each bent part of the substantially U-shaped sectional form of the first member 341 are set substantially uniform. COPYRIGHT: (C)2009,JPO&INPIT
摘要翻译：要解决的问题：提供一种燃气轮机，改善设置在燃烧器的尾缸中的燃烧减振装置的外观。解决方案：燃烧减振装置34设置在燃烧器的尾筒中以形成气体空间S，并且气体空间L和尾气缸32的内部通过多个空气相互连通燃烧减振装置34包括：第一构件341，其具有通过按压并设置在尾筒32的外周上而形成的大致U形截面，其中大致U形截面形状的开口部分指向尾巴32; 以及第二构件342，其阻挡第一构件341的大致U形截面形状的开口部分，以形成直到第一构件341的气体空间S，并且具有多个气孔343。尾尾筒32的外径当尾巴32的外径朝向尾筒32的轴向方向变化时，从尾筒32的轴线L到基本上与尾筒32的各个弯曲部分的距离d1，d2 第一构件341的U形截面形状基本上均匀地设置。版权所有（C）2009，JPO＆INPIT

2. 发明专利

JP2005195284A Fuel nozzle for gas turbine, combuster for gas turbine and combustion method of combuster for gas turbine 审中-公开
标题翻译：燃气涡轮燃油喷嘴，气体燃烧器燃烧器和燃气轮机燃烧器燃烧方法
公开(公告)号：JP2005195284A
公开(公告)日：2005-07-21
申请号：JP2004003507
申请日：2004-01-08
申请人： Mitsubishi Heavy Ind Ltd , 三菱重工業株式会社
发明人： OOTA MASATOYO , AOYAMA KUNIAKI , NISHIDA KOICHI , MIYAUCHI KOTARO , NAKAMURA SOSUKE , TACHIBANA TERUYA , BANDAI SHIGEMI
IPC分类号： F23R3/28 , F02C3/30 , F02C7/22 , F02C7/228 , F23R3/00 , F23R3/14 , F23R3/36
摘要： PROBLEM TO BE SOLVED: To provide a combuster for a gas turbine, preventing flash-back phenomenon in combustion, and supplying stable combustion in all operation regions extending from a low-load combustion to a high-load combustion, a fuel nozzle thereof, and a combustion method thereof. SOLUTION: This fuel nozzle 30 for the gas turbine includes: a fuel supply pipe 31 disposed along an air current; and a swirler 32 disposed in the periphery of the fuel supply pipe 31 to apply swirl force to the air current. The fuel supply pipe 31 supplies fuel 41, 51 into the air current. The fuel supply pipe 31 includes: an air inlet part 60 for taking some of the air current into the inside of the fuel supply pipe 31; an air release hole 62 formed at the downstream side tip part of the fuel supply pipe 31; and an air pipe 63 connecting the air inlet part 60 and the air release hole 62. The air taken into the inside of the fuel supply pipe 31 from the air inlet part 60 is released from the air release hole 62 through the air pipe 63. The released air 74, 75 prevents stagnation of swirl in the downstream area of the fuel supply pipe 31. COPYRIGHT: (C)2005,JPO&NCIPI
摘要翻译：要解决的问题：为了提供一种用于燃气轮机的燃烧器，防止燃烧中的闪回现象，并且在从低负荷燃烧到高负荷燃烧的所有操作区域中提供稳定的燃烧，燃料喷嘴及其燃烧方法。该燃气轮机的燃料喷嘴30包括：燃料供给管31，沿着气流配置; 以及设置在燃料供给管31的周边的旋流器32，以向气流施加旋转力。燃料供给管31将燃料41,41供给到气流中。燃料供给管31包括：空气入口部60，用于将一些气流进入燃料供给管31的内部; 形成在燃料供给管31的下游侧的前端部的排气孔62; 连接空气入口部分60和空气释放孔62的空气管63.从空气入口部分60吸入燃料供应管31内部的空气通过空气管63从空气释放孔62释放。释放的空气74,75防止燃料供应管31的下游区域中的涡流的停滞。版权所有（C）2005，JPO＆NCIPI

3. 发明专利

JP2015045321A ガスタービン、ガスタービンの制御装置、ガスタービンの起動方法有权
标题翻译：气体涡轮机，气体涡轮机控制装置和气体涡轮机的启动方法
公开(公告)号：JP2015045321A
公开(公告)日：2015-03-12
申请号：JP2014018878
申请日：2014-02-03
申请人：三菱重工業株式会社 , Mitsubishi Heavy Ind Ltd
发明人： TATSUMI NAOYA , MIYAUCHI KOTARO
IPC分类号： F02C7/26 , F01D19/00 , F02C9/00
摘要：【課題】ガスタービン、ガスタービンの制御装置、ガスタービンの起動方法において、再起動時における動翼とケーシングとの接触を防止して適正に再起動可能とする。【解決手段】圧縮機11と燃焼器12とタービン13とを有し、ディスクキャビティ32の雰囲気温度DCTを計測する温度計測部43と、雰囲気温度DCTに基づいてガスタービン10の起動制限時間taを設定する起動制限時間設定部44と、起動制限時間taが経過した後にガスタービン10を起動可能とする制御装置41とを設け、起動制限時間設定部44は、雰囲気温度DCTが高いほど起動制限時間taを長く設定する。【選択図】図1
摘要翻译：要解决的问题：通过在燃气轮机，燃气轮机的控制装置和燃气轮机的激活方法中防止活动叶片和壳体之间的接触来实现适当的再活化。解决方案：气体涡轮10包括：压缩机11; 燃烧器12; 涡轮机13; 测量盘腔32的大气温度DCT的温度测量单元43; 激活极限时间设定部44基于大气温度DCT设定燃气轮机10的起动极限时刻ta; 以及控制单元41，其能够在激活极限时间ta之后激活燃气轮机10。激活极限时间设定部44设定激活限制时间ta，使得激活限制时间ta随着大气温度DCT变高而变长。

4. 发明专利

JP2014159942A Combustor and rotary machine 有权
标题翻译： COMBUSTOR和旋转机
公开(公告)号：JP2014159942A
公开(公告)日：2014-09-04
申请号：JP2014008390
申请日：2014-01-21
申请人： Mitsubishi Heavy Ind Ltd , 三菱重工業株式会社
发明人： YUASA ATSUSHI , SAITO TOSHIHIKO , MIYAUCHI KOTARO , SAITO KEISHIRO , TAKIGUCHI TOMOSHI
IPC分类号： F23R3/30 , F23R3/14 , F23R3/20 , F23R3/28
CPC分类号： F23R3/343 , F23R3/14 , F23R3/60
摘要： PROBLEM TO BE SOLVED: To provide a combustor capable of forming a more uniform premixture.SOLUTION: A combustor comprises: a combustor inner tube 3 surrounding a fuel nozzle from an outer peripheral side, and a plurality of connection members 14 provided at intervals in the circumferential direction to interconnect the rear end of the combustor inner tube 3 and a casing and defining flow passages P for flowing of compressed air to be introduced into the combustor inner tube 3, in which the compressed air flowing in the flow passages P is introduced into the fuel nozzle while being reversed in the flow direction at the rear end of the combustor inner tube 3. Parts or all of the flow passages P blow air obliquely toward the circumferential direction.
摘要翻译：要解决的问题：提供一种能够形成更均匀的预混合物的燃烧器。解决方案：燃烧器包括：燃烧器内管3，其从外周侧围绕燃料喷嘴;以及多个连接构件14，将燃烧器内管3的后端与壳体连接起来，并且限定用于流入被引入燃烧器内管3的压缩空气流动的流路P，其中流入流路P的压缩空气被引入燃料喷嘴在燃烧器内管3的后端沿流动方向反转。部分或全部流路P朝向圆周方向倾斜吹送空气。

5. 发明专利

JP2009203943A Gas turbine control method and device 有权
标题翻译：气体涡轮机控制方法和装置
公开(公告)号：JP2009203943A
公开(公告)日：2009-09-10
申请号：JP2008048835
申请日：2008-02-28
申请人： Mitsubishi Heavy Ind Ltd , 三菱重工業株式会社
发明人： NOMURA MASUMI , MIYAUCHI KOTARO
IPC分类号： F02C9/00 , F01D17/00 , F01D25/00 , F02C7/00 , F02C9/34 , F02C9/52 , F23R3/00 , F23R3/34
CPC分类号： F02C9/52 , F02C9/28 , F02C9/54 , F05D2270/114 , F05D2270/14 , F05D2270/301 , F05D2270/3061 , F05D2270/332 , F05D2270/334
摘要： PROBLEM TO BE SOLVED: To control a gas turbine for maintaining an efficient operation state, by preventing operation from deviating from an operation state in an ideal fuel flow rate and air flow rate supposed in design.
SOLUTION: This gas turbine control device is composed of a frequency analyzing means 13 in a combustor, a state grasping means 12 for grasping a combustion state based on an each frequency band analyzing result, an operation process quantity including the ratio of the air flow rate and pilot fuel and a state signal including an atmospheric state and a load quantity, a combustion characteristic grasping means 14 for grasping a characteristic of combustion vibration, and a control part 3 for driving by correcting an initial design value of the preset air flow rate and the pilot ratio in response to the operation process quantity and the state signal, by calculating at least one correction quantity of the air flow rate and the pilot ratio supplied to the combustor every time when the combustion vibration exceeds a predetermined management value from a combustion vibration characteristic and the combustion state. The control part 3 is operated by the initial design value by resetting a correction of the initial design value in a state where the combustion vibration becomes less than the predetermined management value by a specific time.
COPYRIGHT: (C)2009,JPO&INPIT
摘要翻译：要解决的问题：为了控制燃气轮机以保持有效的运行状态，通过防止操作偏离设计中假设的理想燃料流量和空气流量的运行状态。解决方案：该燃气轮机控制装置由燃烧器中的频率分析装置13，基于每个频带分析结果来掌握燃烧状态的状态把持装置12构成，运转处理量包括空气流量和引导燃料以及包括大气状态和负载量的状态信号，用于掌握燃烧振动特性的燃烧特性把持装置14以及通过校正预设空气的初始设计值进行驱动的控制部3 每当燃烧振动超过预定的管理值时，通过计算提供给燃烧器的空气流量和引燃比的至少一个校正量，从而响应于操作处理量和状态信号的流量和导频比燃烧振动特性和燃烧状态。控制部3通过在燃烧振动变得小于预定管理值一定时间的状态下复位初始设计值的校正，通过初始设计值来操作。版权所有（C）2009，JPO＆INPIT

6. 发明专利

JP2006097983A Gas turbine combustor 审中-公开
标题翻译：气体涡轮搅拌机
公开(公告)号：JP2006097983A
公开(公告)日：2006-04-13
申请号：JP2004285292
申请日：2004-09-29
申请人： Mitsubishi Heavy Ind Ltd , 三菱重工業株式会社
发明人： ISHIGURO TATSUO , TANAKA KATSUNORI , MIYAUCHI KOTARO , OKADA IKUO
IPC分类号： F23R3/06 , F02C7/00 , F23R3/18
摘要： PROBLEM TO BE SOLVED: To provide an inexpensive and strong acoustic liner for a gas turbine combustor.
SOLUTION: At least an acoustic liner portion of the gas turbine combustor is manufactured by casting. A core for forming a housing and a sound absorbing hole of the acoustic liner is formed by manufacturing a number of small cores of the same shape and combining them to be used as the core of the acoustic liner as a whole.
COPYRIGHT: (C)2006,JPO&NCIPI
摘要翻译：要解决的问题：为燃气轮机燃烧器提供便宜且强大的声学衬垫。解决方案：通过铸造制造燃气轮机燃烧器的至少一个声衬套部分。用于形成声衬垫的外壳和吸音孔的芯通过制造相同形状的多个小芯体并将其组合以整体用作声垫的芯体而形成。版权所有（C）2006，JPO＆NCIPI

7. 发明专利

JP2014173794A Fuel spray nozzle 有权
标题翻译：燃油喷雾喷嘴
公开(公告)号：JP2014173794A
公开(公告)日：2014-09-22
申请号：JP2013047523
申请日：2013-03-11
申请人： Mitsubishi Heavy Ind Ltd , 三菱重工業株式会社
发明人： KAJIMURA SHUHEI , SAITO KEISHIRO , INOUE KEI , MIYAUCHI KOTARO
IPC分类号： F23R3/28 , F02C7/232 , F02C9/40
CPC分类号： F23R3/286 , F02C7/22 , F23C2203/30 , F23C2900/07021 , F23D11/383 , F23R3/14
摘要： PROBLEM TO BE SOLVED: To provide a fuel spray nozzle capable of attaining NOx reduction at low costs.SOLUTION: A fuel spray nozzle comprises: a liquid fuel flow passage 15 working as the flow passage of liquid fuel; a liquid fuel injection hole 19 putting the liquid fuel flow passage 15 in communication with the inside of a combustion burner and working as the hole for injecting the liquid fuel into the combustion burner; an additive agent flow passage 14 working as the flow passage of an additive agent; and an additive agent injection hole 18a putting the additive agent flow passage 14 in communication with the inside of the combustion burner and working as the hole for injecting the additive agent into the combustion burner at an angle for collision with the liquid fuel injected from the liquid fuel injection hole 19. As thus constructing, the fuel spray nozzle can be provided, which can attain NOx reduction at low cost.
摘要翻译：要解决的问题：提供能够以低成本实现NOx还原的燃料喷嘴。解决方案：燃料喷嘴包括：液体燃料流动通道15，其作为液体燃料的流动通道; 液体燃料喷射孔19，其将液体燃料流路15与燃烧器的内部连通并作为将液体燃料喷射到燃烧器中的孔; 作为添加剂的流路工作的添加剂流路14; 以及添加剂注入孔18a，其将添加剂流路14与燃烧器的内部连通并作为用于将添加剂以与液体喷射的液体燃料碰撞的角度喷射到燃烧器中的孔燃料喷射孔19.由此构成，可以设置能够以低成本实现NOx还原的燃料喷雾喷嘴。

8. 发明专利

JP2009079789A Cooling structure of gas turbine combustor 有权
标题翻译：燃气轮机组的冷却结构
公开(公告)号：JP2009079789A
公开(公告)日：2009-04-16
申请号：JP2007247224
申请日：2007-09-25
申请人： Mitsubishi Heavy Ind Ltd , 三菱重工業株式会社
发明人： ISHIGURO TATSUO , TANAKA KATSUNORI , MIYAUCHI KOTARO
IPC分类号： F23R3/06 , F01D25/12 , F02C7/18 , F23R3/28 , F23R3/42
CPC分类号： F23R3/283 , F23R3/005 , F23R3/06 , F23R2900/03042 , F23R2900/03044
摘要： PROBLEM TO BE SOLVED: To provide a cooling structure capable of reducing NOx in a gas turbine combustor.
SOLUTION: The gas turbine combustor comprises a heat chamber wall surface having a cooling passage through which the cooling air flows, inside of a double wall structure. The cooling passage is opened at a main cooling air supply opening formed at a side of a combustion region. The cooling air supplied from the main cooling air supply opening is guided in the direction along an inner wall surface by a guide member. As the cooling air flowing in the cooling passage inside of the wall surface is reutilized in cooling a film along an inner wall surface, the cooling air can be saved. Thus the air supplied from the compressor can be utilized more as the air for combustion, and NOx can be reduced.
COPYRIGHT: (C)2009,JPO&INPIT
摘要翻译：要解决的问题：提供能够减少燃气轮机燃烧器中的NOx的冷却结构。解决方案：燃气轮机燃烧器包括具有冷却通道的加热室壁表面，冷却空气通过该冷却通道在双壁结构内部流动。冷却通道在形成在燃烧区域一侧的主冷却空气供给口处打开。从主冷却空气供给口供给的冷却空气通过导向部件沿着内壁面的方向被引导。当在壁面内的冷却通道中流动的冷却空气沿着内壁面冷却膜时被再利用，可以节省冷却空气。因此，从压缩机供给的空气可以更多地用作燃烧空气，并且可以减少NOx。版权所有（C）2009，JPO＆INPIT

9. 发明专利

JP2014185791A Combustor, and gas turbine 有权
标题翻译：燃烧器和燃气轮机
公开(公告)号：JP2014185791A
公开(公告)日：2014-10-02
申请号：JP2013059587
申请日：2013-03-22
申请人： Mitsubishi Heavy Ind Ltd , 三菱重工業株式会社
发明人： ISONO MITSUNORI , SAITO TOSHIHIKO , MIYAUCHI KOTARO
IPC分类号： F23R3/20 , F02C7/22 , F23R3/28
CPC分类号： F02C9/32 , F02C7/222 , F05D2210/12 , F05D2270/333 , F23M20/005 , F23R3/14 , F23R3/286 , F23R3/343 , F23R3/46 , F23R2900/00014
摘要： PROBLEM TO BE SOLVED: To provide a combustor capable of sufficiently reducing combustion vibration by restraining variation of a flow rate of fuel supplied to a combustion region, and a gas turbine.SOLUTION: A combustor 4 comprises plural fuel nozzles 20 that extend in an axial line direction of a combustor body and can inject fuel from an injection hole 24 arranged on a combustion chamber side. The combustor comprises a phase adjusting part 33 for partially varying a flow passage cross section area of at least one fuel nozzle 20 in the axial line direction so that phase of variation of a flow rate of the fuel is not identical between at least two fuel nozzles 20 among plural fuel nozzles 20.
摘要翻译：要解决的问题：提供一种能够通过抑制供给到燃烧区域的燃料和燃气轮机的燃料流量的变化来充分降低燃烧振动的燃烧器。燃烧器4包括多个燃料喷嘴20，其以轴向延伸并且能够从设置在燃烧室侧的喷射孔24喷射燃料。燃烧器包括相位调节部分33，用于在轴线方向上部分地改变至少一个燃料喷嘴20的流路横截面面积，使得至少两个燃料喷嘴之间的燃料流量的变化相位不相同 20个在多个燃料喷嘴20中。

10. 发明专利

JP2010127242A Gas turbine control device 有权
标题翻译：气体涡轮控制装置
公开(公告)号：JP2010127242A
公开(公告)日：2010-06-10
申请号：JP2008304991
申请日：2008-11-28
申请人： Mitsubishi Heavy Ind Ltd , 三菱重工業株式会社
发明人： NOMURA MASUMI , TOYAMA KOZO , KAWAKAMI TOMO , MIYAUCHI KOTARO , FUJIBAYASHI KUNIHARU
IPC分类号： F02C9/28 , F02C9/00 , F02C9/34 , F02C9/52
CPC分类号： F02C9/18 , F01D17/04 , F01D17/085 , F02C9/22 , F02C9/28 , F02C9/52 , F02C9/54 , F05D2270/053 , F05D2270/082 , F05D2270/14 , F05D2270/303 , F23N1/022 , F23N5/022 , F23N2021/10 , F23N2023/42 , F23N2025/13 , F23N2037/20 , F23N2041/20 , F23R2900/00013
摘要： PROBLEM TO BE SOLVED: To improve combustion stability, and to prevent generation of combustion vibration, by improving a degree of freedom of setting an air flow rate and a fuel flow rate in response to a target load, in a gas turbine plant. SOLUTION: This gas turbine control device includes a first function generator 62 for setting the fuel flow rate or the air flow rate supplied to a combustor 32 in response to the target load, an intake temperature detector 22 for detecting the intake temperature of a compressor inlet, a second function generator 69 for setting a correction quantity for correcting a preset value of the fuel flow rate or the air flow rate based on a detection value of the intake temperature detector, a third function generator 66 for setting a correction quantity of correcting the correction quantity by adding the target load, a first computing element 68 for arithmetically operating the correction quantity set by the second function generator 69 and a corrected correction quantity from the correction quantity corrected by the third function generator 66, and a second computing element 64 for calculating the fuel flow rate or the air flow rate supplied to the combustor 32 by adding the corrected correction quantity to the preset value of the fuel flow rate or the air flow rate set by the first function generator. COPYRIGHT: (C)2010,JPO&INPIT
摘要翻译：要解决的问题：为了提高燃烧稳定性和防止燃烧振动的产生，通过提高在目标负荷下设定空气流量和燃料流量的自由度，在燃气轮机厂。解决方案：该燃气轮机控制装置包括用于响应于目标负载设定供给到燃烧器32的燃料流量或空气流量的第一功能发生器62，用于检测进气温度的进气温度检测器22 压缩机入口，第二函数发生器69，用于根据进气温度检测器的检测值设定用于校正燃料流量或空气流量的预设值的校正量;第三函数发生器66，用于设定校正量通过添加目标负载来校正校正量的第一计算元件68，用于算术地操作由第二函数发生器69设置的校正量的第一计算元件68和来自由第三函数发生器66校正的校正量的校正校正量，以及第二计算元件64，用于计算通过相加校正的相应值供给到燃烧器32的燃料流量或空气流量指示数量为由第一功能发生器设定的燃料流量或空气流量的预设值。版权所有（C）2010，JPO＆INPIT

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