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    • 1. 发明申请
    • REHEAT COMBUSTOR FOR A GAS TURBINE ENGINE
    • 燃气轮机发动机用燃气轮机
    • US20120260665A1
    • 2012-10-18
    • US13474422
    • 2012-05-17
    • Adnan EROGLUThiemo MEEUWISSENPeter FLOHR
    • Adnan EROGLUThiemo MEEUWISSENPeter FLOHR
    • F02C3/14F02C7/12F02C3/06
    • F23R3/286F23R3/34F23R2900/03042F23R2900/03341F23R2900/03342
    • A reheat combustor for a gas turbine engine includes a fuel/gas mixer for mixing fuel, air and combustion gases produced by a primary combustor and expanded through a high pressure turbine. Fuel injectors inject fuel into the mixer together with spent cooling air previously used for convectively cooling the reheat combustor. The fuel mixture is burnt in an annular reheat combustion chamber prior to expansion through low pressure turbine inlet guide vanes. The fuel/gas mixer and optionally the combustion chamber define cooling paths through which cooling air flows to convectively cool their walls. The fuel injectors are also convectively cooled by the cooling air after it has passed through the fuel/gas mixer cooling paths. The low pressure turbine inlet guide vanes may also define convective cooling paths in series with the combustion chamber cooling paths.
    • 用于燃气涡轮发动机的再热燃烧器包括燃料/气体混合器,用于混合由主燃烧器产生并通过高压涡轮机膨胀的燃料,空气和燃烧气体。 燃料喷射器将燃料与先前用于对流冷却再热燃烧器的废冷却空气一起注入混合器。 燃料混合物在通过低压涡轮机入口导向叶片膨胀之前在环形再热燃烧室中燃烧。 燃料/气体混合器和可选的燃烧室限定冷却空气流过的冷却路径,以对流地冷却其壁。 燃料喷射器在通过燃料/气体混合器冷却路径之后也被冷却空气对流地冷却。 低压涡轮机入口导向叶片还可以限定与燃烧室冷却路径串联的对流冷却路径。
    • 3. 发明申请
    • METHOD FOR OPERATING A GAS TURBINE
    • 操作气体涡轮的方法
    • US20090260368A1
    • 2009-10-22
    • US12471665
    • 2009-05-26
    • Eribert BenzPeter FlohrAdnan ErogluFelix GuetheJaan Hellat
    • Eribert BenzPeter FlohrAdnan ErogluFelix GuetheJaan Hellat
    • F02C7/22
    • F02C6/003C10J3/00C10J2300/093C10J2300/0959C10J2300/1606C10J2300/165C10J2300/1671C10J2300/1675C10J2300/1678C10J2300/1892F02C3/28F25J3/04545F25J3/04575Y02E20/16Y02E20/18
    • A method for operating a gas turbine (11), which is used especially in a combined-cycle power plant (30), includes inducting and compressing air by the gas turbine (11), the compressed air is fed to a combustor (18, 19) for the combustion of a syngas which is produced from coal, and the hot gases which result during the combustion are expanded in a subsequent turbine (16, 17), performing work, wherein some of the compressed air is separated into oxygen and nitrogen, and the oxygen is used in a coal gasification plant (34) for producing the syngas. With such a method, a reduction of the NOx emission is achieved without noticeable loss of output and flexibility of operation by a gas turbine (11) with reheating being used, which includes two combustors (18, 19) and two turbines (16, 17), wherein in the first combustor (18) syngas is combusted, using the compressed air, and the resulting hot gases are expanded in the first turbine (16), and wherein in the second combustor syngas is combusted, using the gases which issue from the first turbine (16), and the resulting hot gases are expanded in the second turbine (17), the two combustors (18, 19) are operated with undiluted syngas, and the flame temperature (TF) in the first combustor (18) of the gas turbine (11) is lowered compared with the operation with natural gas (TNG), while the second combustor (19) is operated largely in the normal operation (TNG) which is designed for natural gas.
    • 用于特别在联合循环发电厂(30)中使用的燃气轮机(11)的方法包括:通过燃气轮机(11)对空气进行吸入和压缩,将压缩空气供给至燃烧器(18), 19),用于燃烧由煤产生的合成气,并且在燃烧期间产生的热气体在随后的涡轮机(16,17)中膨胀,进行工作,其中一些压缩空气被分离成氧和氮 ,并且在用于生产合成气的煤气化设备(34)中使用氧气。 通过这样的方法,可以实现NOx排放的减少,而不会出现明显的输出损失和使用具有再加热的燃气轮机(11)的操作灵活性,其包括两个燃烧器(18,19)和两个涡轮机(16,17) ),其中在所述第一燃烧器(18)中,使用所述压缩空气燃烧合成气,并且所得热气体在所述第一涡轮机(16)中膨胀,并且其中在所述第二燃烧器中合成气被燃烧,使用从 第一涡轮机(16),并且所产生的热气体在第二涡轮机(17)中膨胀,两个燃烧器(18,19)用未稀释的合成气进行操作,并且第一燃烧器(18)中的火焰温度(TF) 与天然气(TNG)的运转相比,燃气轮机(11)的运转下降,而第二燃烧器(19)在为天然气设计的正常运行(TNG)中运行较大。
    • 4. 发明授权
    • Method for operating a gas turbine and a gas turbine for implementing the method
    • 用于操作燃气轮机和用于实施该方法的燃气轮机的方法
    • US07574855B2
    • 2009-08-18
    • US11275477
    • 2006-01-09
    • Eribert BenzPeter FlohrJaan HellatGraham Webb
    • Eribert BenzPeter FlohrJaan HellatGraham Webb
    • F02C1/06
    • F02C6/10F02C3/205Y02E20/16
    • In a method for operating a gas turbine (11) in a combined cycle power plant (40), air is drawn in and compressed though the gas turbine (11), the compressed air is led to a combustor (18, 19) to burn a syngas recovered from a fossil fuel, especially coal, and the gases that result in the course of the combustion are expanded in a downstream turbine (16, 17). In such a method, an improved degree of efficiency is achieved by virtue of the fact that a gas turbine (11) with reheating is used, which includes two combustors (18, 19) and two turbines (16, 17); in the first combustor (18), syngas is burned with the compressed air, and the resultant hot gases, e.g., flue gases, are expanded in the first turbine (16), and in the second combustor syngas is burned by the gases coming from the first turbine (16), and the resultant hot gases are expanded in the second turbine (17).
    • 在组合循环发电厂(40)中操作燃气轮机(11)的方法中,空气被吸入并通过燃气轮机(11)压缩,压缩空气被引导到燃烧器(18,19)以燃烧 从化石燃料,特别是煤回收的合成气,并且导致燃烧过程的气体在下游涡轮机(16,17)中膨胀。 在这种方法中,通过使用具有再加热的燃气轮机(11),其包括两个燃烧器(18,19)和两个涡轮机(16,17),实现了提高的效率。 在第一燃烧器(18)中,合成气用压缩空气燃烧,并且所产生的热气体,例如烟道气体在第一涡轮机(16)中膨胀,并且在第二燃烧器中,合成气被来自 第一涡轮机(16),并且所产生的热气体在第二涡轮机(17)中膨胀。
    • 6. 发明申请
    • BURNER FOR THE OPERATION OF A HEAT GENERATOR
    • 燃烧器用于发电机的运行
    • US20090081599A1
    • 2009-03-26
    • US12238792
    • 2008-09-26
    • Stefano BerneroPeter FlohrGijsbertis OomensMartin Zajadatz
    • Stefano BerneroPeter FlohrGijsbertis OomensMartin Zajadatz
    • F23D11/00
    • F23D17/002F23C7/008F23C2900/07002F23R3/343
    • A burner (23) for operating a heat generator includes a swirler (2) for a combustion air flow (9), and also devices (7, 12) for injecting at least one fuel into the combustion air flow (9), wherein a mixing path (3) is arranged downstream of the swirler (2), and wherein at least one nozzle (20) for feeding liquid pilot fuel is arranged in the region radially outside the discharge opening of the mixing path (3) of the burner. With such a burner, an operating mode which is as pollutant-free and overheating-free as possible can be enabled even at low load and under transient conditions if the at least one nozzle (20) is arranged in a burner front plate (32), wherein at least one discharge opening (15), through which the pilot fuel discharges into the combustion chamber (16), is provided in a front face (34) of the burner front plate (32), which is arranged essentially parallel to a combustion chamber rear wall (28).
    • 用于操作发热器的燃烧器(23)包括用于燃烧空气流(9)的旋流器(2),以及用于将至少一种燃料喷射到燃烧空气流(9)中的装置(7,12),其中 混合路径(3)布置在旋流器(2)的下游,并且其中用于供给液体引燃燃料的至少一个喷嘴(20)布置在燃烧器的混合路径(3)的排出口径向外侧的区域中。 通过这样的燃烧器,即使在低负载和瞬态条件下,如果至少一个喷嘴(20)布置在燃烧器前板(32)中,也可以实现尽可能无污染和过热的操作模式, 其特征在于,在所述燃烧器前板(32)的前表面(34)上设置有至少一个排气口(15),其中所述先导燃料排出到所述燃烧室(16)中,所述排放口基本上平行于 燃烧室后壁(28)。
    • 10. 发明授权
    • Device for rapid attachment of serially-mounted electrical apparatus
    • 用于快速连接串联电气设备的装置
    • US5297002A
    • 1994-03-22
    • US859730
    • 1992-06-08
    • Peter Flohr
    • Peter Flohr
    • H01H9/02H02B1/04H02B1/052H02B1/20
    • H02B1/052
    • In order to secure a series built-in unit on the section of a fitting rail (4) and to be able to detach it again therefrom and from the electric collector busbar (2, 5), in the region of a recess (13) on both side of the housing wall of the device is pivotably fitted a U-bracket-shaped coupling component (3) of elastic material which is divided by a slot (7) extending into the two U-arms of the frame-like widened connecting web into a supporting end (8) for the engagement of the fitting rail (4) and an actuating end (9) spring-loaded on the casing (1) lockable and unlockable by swinging in relation to the bearing position (6).
    • PCT No.PCT / DE91 / 00634 Sec。 371日期:1992年6月8日 102(e)日期1992年6月8日PCT 1991年8月5日PCT PCT。 出版物WO92 / 08264 日期为1992年5月14日。为了将一系列内置装置固定在装配轨道(4)的部分上,并能够从该集电箱母线(2,5)再次从该区域中分离, 在装置的壳体壁的两侧上的凹部(13)可枢转地装配有弹性材料的U形托架形联接部件(3),该联接部件(3)被延伸到两个U形臂中的槽(7) 所述框架状加宽的连接卷材成为用于嵌合轨道(4)的接合的支撑端(8)和弹簧加载在所述壳体(1)上的致动端(9),所述致动端可通过相对于所述轴承 位置(6)。