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    • 22. 发明授权
    • Method and appliance for operating a gas turbine installation combustion
chamber with liquid fuel
    • 用于操作具有液体燃料的燃气轮机安装燃烧室的方法和设备
    • US6067789A
    • 2000-05-30
    • US74312
    • 1998-05-08
    • Klaus DobbelingLothar RehYunhong Wang
    • Klaus DobbelingLothar RehYunhong Wang
    • F02C3/20F02C3/30F02C7/224F23R3/28F23R3/30
    • F02C3/20F02C3/30F02C7/224F23R3/30F23D2204/10Y02T50/671
    • The object of the invention is to produce a method, for operating a gas turbine installation combustion chamber with liquid fuel, by means of which the NO.sub.X figures obtained when liquid fuel is employed are similar to those for gaseous fuels. The size of the burner is then also reduced. It is also an object of the invention to provide a corresponding appliance for carrying out the method.This is achieved in accordance with the invention in that the liquid fuel (38) is evaporated in at least two steps in a separate evaporative reactor (12). In this arrangement, the liquid fuel (38) is first atomized to a fuel vapor/liquid fuel mixture (61) by direct heat exchange with a first heat exchange medium (21) and is instantaneously evaporated in this process. The evaporation of the remaining residue of the liquid fuel (38) then takes place by indirect heat exchange with a second heat exchange medium (51). For this purpose, an evaporative reactor (12) is arranged vertically upstream of the combustion chamber (2) and is connected to it, which evaporative reactor (12) accommodates, at its inlet end, a dual-fluid nozzle (22) connected both to a liquid fuel line (19) and to a supply line (20) for a first heat exchange medium (21).
    • 本发明的目的是产生一种用于操作具有液体燃料的燃气轮机安装燃烧室的方法,通过该方法,当使用液体燃料时获得的NOX数值与用于气体燃料的NOx相似。 然后燃烧器的尺寸也减小。 本发明的另一个目的是提供一种用于执行该方法的相应装置。 这是根据本发明实现的,因为液体燃料(38)在独立的蒸发反应器(12)中以至少两个步骤蒸发。 在这种布置中,液体燃料(38)首先通过与第一热交换介质(21)的直接热交换而雾化到燃料蒸汽/液体燃料混合物(61),并在该过程中瞬间蒸发。 然后通过与第二热交换介质(51)的间接热交换来进行液体燃料(38)的剩余残余物的蒸发。 为此,蒸发反应器(12)被布置在燃烧室(2)的垂直上游并与其连接,该蒸发反应器(12)在其入口端处容纳连接两者的双流体喷嘴(22) 到液体燃料管线(19)和用于第一热交换介质(21)的供应管线(20)。
    • 23. 发明授权
    • Ceramic liner
    • 陶瓷衬里
    • US5957067A
    • 1999-09-28
    • US119585
    • 1998-07-21
    • Klaus DobbelingArmin HegerAndreas Pfeiffer
    • Klaus DobbelingArmin HegerAndreas Pfeiffer
    • F23M5/00F23M5/02F23M5/04F23R3/00E04B2/00F27D1/14
    • F23M5/04F23M5/02F23R3/007F23M2900/05002F23M2900/05004
    • In the case of a ceramic liner for combustion spaces, comprising at least one wall element (3), made of refractory structural ceramic and having at least one through-opening (6), and a fastening element (4), consisting of refractory structural ceramic, per opening (6), the fastening element (4) is resiliently fastened by its foot in a metallic holding device (5) fastened on the metallic supporting wall (1). The head (20) of the fastening element (4) rests in the opening (6) in the wall element (3).The wall element (3) is designed in the form of a box, having a base (25) which runs parallel to the metallic wall (1), having an inside wall (23) which surrounds the opening (6) in an annular manner and is supported directly or indirectly on the metallic supporting wall (1), and having outside walls (24) which extend up to the metallic supporting wall (1) without touching the latter.
    • 在用于燃烧空间的陶瓷衬套的情况下,包括由耐火结构陶瓷制成并具有至少一个通孔(6)的至少一个壁元件(3)和由耐火结构体构成的紧固元件(4) 陶瓷,每个开口(6),紧固元件(4)通过其脚部弹性地固定在紧固在金属支撑壁(1)上的金属保持装置(5)中。 紧固元件(4)的头部(20)位于壁元件(3)的开口(6)中。 壁元件(3)被设计成箱子的形式,具有平行于金属壁(1)延伸的基部(25),具有以环形方式包围开口(6)的内壁(23) 并且直接或间接地支撑在金属支撑壁(1)上,并且具有延伸到金属支撑壁(1)的外壁(24)而不与其接触。
    • 28. 发明授权
    • Mixing ducts for a gas-turbine annular combustion chamber
    • 用于燃气轮机环形燃烧室的混合管道
    • US5839283A
    • 1998-11-24
    • US751721
    • 1996-11-18
    • Klaus Dobbeling
    • Klaus Dobbeling
    • F23R3/16F23R3/04F23R3/10F23R3/20F23R3/28F23R3/32F23R3/34F23R3/42F23R3/46F23R3/50F23R3/12F02C3/00
    • F23R3/10F23R3/045F23R3/286F23R3/50F23R2900/03041
    • In a gas-turbine annular combustion chamber (4) which is arranged downstream of a compressor (1) and is equipped on its front plate with at least one row of premix burners (5) arranged in an annular form, in each case a combustion-air duct (15) designed as a diffuser leads directly downstream of the compressor outlet from the guide vanes (9) of the last compressor row to each burner (5), at the downstream end of which combustion-air duct (15) at least one longitudinal-vortex generator (16) is located, at least one fuel injection means (17) being provided in or downstream of the longitudinal-vortex generator (16). A mixing duct (19) which ends in the combustion chamber (4) and has a constant height (H) and a length (L) which corresponds approximately to twice the value of the hydraulic duct diameter (D) is arranged downstream of the fuel injection means (17). The overall size of the gas turbine in the region of the combustion chamber (4) can thereby be substantially reduced. In addition, the pressure loss between compressor outlet and turbine inlet is reduced.
    • 在燃气轮机环形燃烧室(4)中,该燃气涡轮机环形燃烧室(4)布置在压缩机(1)的下游并且在其前板上装有至少一排以环形形式布置的预混燃烧器(5),在每种情况下燃烧 设计为扩散器的空气管道(15)在压缩机出口的下游从最后的压缩机排的导向叶片(9)直到每个燃烧器(5),其下游端处的燃烧空气管道(15)处于 至少一个纵向涡流发生器(16),至少一个燃料喷射装置(17)设置在纵向涡流发生器(16)的下游。 在燃烧室(4)中终止并具有恒定高度(H)和长度(L)的混合管道(19),其大约等于液压管道直径(D)值的两倍,设置在燃料的下游 注射装置(17)。 因此,燃烧室(4)区域中的燃气轮机的整体尺寸可以大大减小。 此外,压缩机出口和涡轮机入口之间的压力损失减小。
    • 30. 发明授权
    • Process for air-blown gasification of carbon-containing fuels
    • 含碳燃料气吹气化方法
    • US5656043A
    • 1997-08-12
    • US421251
    • 1995-04-13
    • Klaus Dobbeling
    • Klaus Dobbeling
    • C10J3/46C10J3/48C10L3/00
    • C10J3/487C10J2200/152C10J2300/1223C10J2300/1861F23C2900/07002
    • When carrying out a radiant heat exchange between two media, one medium being a hot gas (5) and the other medium being a gasification mixture (11) of fuel and steam, the device consists of a gasification vessel (1) which, for its part, consists of a reaction space (2), an intermediate tube (4) and a flow space (3). In the reaction space (2), the hot gases (5) flow away centrally in the direction of the intermediate tube (4) and the flow space (3). The gasification mixture (11) flows in the opposite direction out of the flow space (3) and the intermediate tube (4). This gasification mixture surrounds the hot gases (5) in such a way that the radiant heat exchange takes place between the two media (5, 11).
    • 当在两个介质之间进行辐射热交换时,一个介质是热气(5),另一个介质是燃料和蒸汽的气化混合物(11),该装置由气化容器(1) 部分由反应空间(2),中间管(4)和流动空间(3)组成。 在反应空间(2)中,热气体(5)沿中间管(4)和流动空间(3)的方向中心流动。 气化混合物(11)沿相反方向流出流动空间(3)和中间管(4)。 这种气化混合物围绕热气体(5),使得辐射热交换发生在两个介质(5,11)之间。