公开(公告)号：EP3881006A1

公开(公告)日：2021-09-22

申请号：EP19809549.9

申请日：2019-11-13

申请人： Johnson Matthey Public Limited Company ,  Delta Motorsport Limited

发明人： CARPENTER, Nick ,  CHANDLER, Guy ,  GIDNEY, Jeremy ,  HERRING, Scott ,  MORGAN, Chris ,  O'CONNELL, Timothy ,  WILKSCH, Mark

IPC分类号： F23R3/40 ,  F23R3/00

公开(公告)号：EP3187278B1

公开(公告)日：2019-06-26

申请号：EP16204614.8

申请日：2016-12-16

申请人： General Electric Company

发明人： Simpson, Stanley Frank ,  Hardwicke, Canan Uslu ,  Moroso, Joseph Leonard ,  Moricca, Timothy Michael

IPC分类号： B22C9/10 ,  F23R3/40 ,  B22D19/00

公开(公告)号：EP3009636A1

公开(公告)日：2016-04-20

申请号：EP15179517.6

申请日：2015-08-03

申请人： MITSUBISHI HEAVY INDUSTRIES, LTD.

发明人： Suzuki, Kenji

IPC分类号： F02C3/20 ,  F02C7/22 ,  F23R3/40

CPC分类号： F23R3/40 ,  C01B3/384 ,  F02C3/20 ,  F02C3/205 ,  F02C7/22 ,  F02C7/224 ,  F05D2250/25 ,  F23C2900/03002 ,  F23K5/08 ,  F23K5/20 ,  F23R3/005 ,  F23R3/28 ,  F23R2900/00017 ,  F23R2900/00018 ,  Y02T50/675

摘要： A fuel supply system (1) includes a fuel reformer (30) disposed to contact at least one of a combustion chamber (20) or a wall of the combustion chamber (20). The fuel reformer includes a reformer chamber wall enclosing a fuel reformer chamber (50), and a reforming catalyst support sheet (32) disposed in the fuel reformer chamber.

摘要翻译： 燃料供给系统（1）包括设置成接触燃烧室（20）或燃烧室（20）的壁中的至少一个的燃料重整器（30）。 燃料重整器包括包围燃料重整器室（50）的重整器室壁和设置在燃料重整器室中的重整催化剂支撑片（32）。

公开(公告)号：EP2850365A1

公开(公告)日：2015-03-25

申请号：EP13790273.0

申请日：2013-05-14

申请人： Reformtech Heating Holding AB

发明人： LINDSTRÖM, Bård ,  HAGSTRÖM, Daniel

IPC分类号： F23C13/02 ,  F23R3/40 ,  B60H1/22

CPC分类号： F23C13/02 ,  F23C13/06 ,  F23D11/44 ,  F23D11/446 ,  F23D2900/21002

摘要： The present invention relates to a system for utilizing liquid fuels, such as diesel and gasoline, in a catalytic reactor for producing clean heat from the fuel. In particular it relates to a fuel injection system for a catalytic burner (310, 313). It includes preheating elements (308′, 309, 315; FT) for preheating the catalytic burner (310, 313) and primary fuel supply elements (307) for supplying fuel to the catalytic burner (310, 313). The preheating elements (308′, 309, 315; FT) and the primary fuel supply elements (307) are provided in separate compartments (310, 312), the compartments being connected with each other via a channel (CH).

公开(公告)号：EP2208937A3

公开(公告)日：2014-04-16

申请号：EP10150799.4

申请日：2010-01-14

申请人： General Electric Company

发明人： Kraemer, Gilbert Otto ,  Kraemer, Cristina Colindres

IPC分类号： F23R3/40 ,  F23C13/08 ,  F23C13/06 ,  B01J33/00

CPC分类号： F23C13/08 ,  B01J21/10 ,  B01J23/18 ,  B01J23/58 ,  B01J23/6447 ,  B01J23/78 ,  B01J23/8437 ,  B01J33/00 ,  B01J35/04 ,  B01J37/0215 ,  F23C13/06 ,  F23C2900/13001 ,  F23C2900/13002 ,  F23D2900/00001 ,  F23R3/40

摘要： Methods and apparatuses are provided for protecting a catalyst (56) within a combustor (30). In one embodiment, a catalytic reactor (14) includes a protective coating (58) that may be chemically removed or mechanically removed while the catalytic reactor (14) is disposed in a combustor (30).

公开(公告)号：EP1553345A3

公开(公告)日：2012-12-19

申请号：EP05000267.4

申请日：2005-01-07

申请人： Siemens Energy, Inc.

发明人： Laster, Walter Ray ,  Bandaru, Ramarao V. ,  Baer, Joan Mae

IPC分类号： F23R3/40 ,  F02C9/22 ,  F02C9/18

CPC分类号： F02C9/22 ,  F02C9/18 ,  F05D2260/20 ,  F23R3/40

摘要： A catalytic gas turbine includes a compressor, a catalytic combustor, a turbine, and a flow path conducting a bypass portion of the compressed air around the combustor and turbine. A method of operating the catalytic gas turbine to activate a catalyst in the catalytic combustor includes opening an inlet guide vane upstream of the compressor to a position to produce an increased volume of compressed air. The increased volume exceeds a volume of compressed air needed to support combustion. A bypass portion of the compressed air is extracted and directed around the combustor and turbine. The method may also include extracting a recirculation portion of the compressed air and directing the recirculation portion into the inlet of the compressor.

公开(公告)号：EP2378096A1

公开(公告)日：2011-10-19

申请号：EP09838327.6

申请日：2009-01-14

申请人： Toyota Jidosha Kabushiki Kaisha

发明人： KASUGA, Shunsuke ,  WATANABE, Atushi ,  TANAKA, Shin-ichiro ,  AZEGAMI, Osamu

IPC分类号： F02C3/24 ,  F02C7/143 ,  F02C9/40 ,  F02D19/08 ,  F23R3/40

CPC分类号： F02C3/24 ,  F01N3/2066 ,  F01N2560/026 ,  F01N2610/02 ,  F02C9/40 ,  F02M25/00 ,  F23J15/02 ,  F23J2219/10 ,  F23L2900/00001 ,  F23R3/286 ,  F23R2900/00002 ,  Y02T10/24

摘要： A combuster (2) of a gas turbine engine (1) is fed with liquid ammonia and that liquid ammonia is burned to drive a turbine (3). Inside the exhaust passage of the gas turbine engine (1), an NO x selective reduction catalyst (9) is arranged. Inside the intake air which flows into the compressor (4), liquid ammonia is fed. This liquid ammonia is used to cool the intake air. The NO x which is contained in the exhaust gas is reduced by the unburned ammonia which is exhausted into the exhaust passage by the NO x selective reduction catalyst (9).

摘要翻译： 燃气涡轮发动机（1）的燃烧器（2）被供给液氨，并且燃烧液氨以驱动涡轮（3）。 在燃气涡轮发动机（1）的排气通道内部设置有NO x选择还原催化剂（9）。 在流入压缩机（4）的进气内部，供给液氨。 该液氨用于冷却进气。 废气中含有的NO x被通过NO x选择还原催化剂（9）排出到排气通道中的未燃的氨减少。

公开(公告)号：EP2206968A2

公开(公告)日：2010-07-14

申请号：EP09180590.3

申请日：2009-12-23

申请人： General Electric Company

发明人： Liu, Ke ,  Haynes, Joel Meier ,  Watson, Rick Bruce

IPC分类号： F23R3/40 ,  F02C3/30 ,  F02C3/20

CPC分类号： F02C3/30 ,  F02C3/20 ,  F02C7/22 ,  F05D2220/75 ,  F23C13/06 ,  F23C2900/03002 ,  F23C2900/9901 ,  F23R3/286 ,  F23R3/40 ,  F23R2900/00002 ,  Y02T50/678

摘要： A gas turbine system (10) includes a fuel inlet configured to receive a fuel stream (18); an oxygen inlet configured to introduce a first oxygen-containing gas (32, 130); a fuel reformer system (12) comprising: a pre-mixing zone (34, 110) configured to mix a first portion (30, 121) of the fuel stream and the oxygen-containing gas in a pre-mixing device (200, 300, 402) to form a gaseous pre-mix (138); a diffuser (404) configured to provide a thermal shield between the pre-mixing zone and a catalytic partial oxidation zone; a catalytic partial oxidation zone (40, 114, 420) configured to receive the gaseous pre-mix, wherein the catalytic partial oxidation zone comprises a catalyst composition configured to react the fuel and the oxygen to generate a syngas (42, 126); and a dilution zone (116) configured to mix the syngas into a second portion (124) of the fuel stream to form a fuel mixture (48, 136); a gas turbine pre-mixer (16), configured to mix a second oxygen-containing gas (128) from a gas turbine compressor (14) with the fuel mixture; and a gas turbine combustor (20, 500) configured to combust the fuel mixture.

摘要翻译： 燃气轮机系统（10）包括配置成接收燃料流（18）的燃料入口。 氧气入口，被配置为引入第一含氧气体（32,130）; 燃料重整器系统（12），包括：预混合区（34,110），其构造成将预燃混合装置（200,300）中的燃料流的第一部分（30,121）和含氧气体 ，402）以形成气态预混物（138）; 扩散器（404），其构造成在所述预混合区域和催化部分氧化区域之间提供热屏蔽; 配置成接收气态预混物的催化部分氧化区（40,114,420），其中所述催化部分氧化区包括催化剂组合物，所述催化剂组合物配置为使燃料和氧反应以产生合成气（42,126）; 和配置成将合成气混合到燃料流的第二部分（124）中以形成燃料混合物（48,136）的稀释区（116）; 燃气轮机预混合器（16），其被配置为将来自燃气涡轮压缩机（14）的第二含氧气体（128）与所述燃料混合物混合; 和燃烧燃料混合物的燃气轮机燃烧器（20,500）。

公开(公告)号：EP1205712B1

公开(公告)日：2010-06-09

申请号：EP01309549.2

申请日：2001-11-13

申请人： GENERAL ELECTRIC COMPANY

发明人： Beebe, Kenneth Winston ,  Keeling, Leslie Boyd

IPC分类号： F23R3/18 ,  F23R3/28 ,  F23R3/40 ,  F23R3/54

CPC分类号： F23C13/00 ,  F23C13/02 ,  F23R3/286 ,  F23R3/40

公开(公告)号：EP2071234A2

公开(公告)日：2009-06-17

申请号：EP08171501.3

申请日：2008-12-12

申请人： Precision Combustion, Inc.

发明人： Pfefferle, William C.

IPC分类号： F23C13/06 ,  F23C6/04 ,  F23R3/40

CPC分类号： F23C13/06 ,  F23C6/04 ,  F23C2900/13001 ,  F23C2900/13002 ,  F23R3/40

摘要： A method is provided for low NOx combustion of high hydrogen content and other fuels in gas turbines wherein at least a portion of the fuel is combusted under fuel rich conditions and a portion of resulting reaction heat is transferred to combustion air prior to non-premixed combustion of the fuel.

摘要翻译： 提供了一种用于燃气涡轮机中的高氢含量和其它燃料的低NOx燃烧的方法，其中燃料的至少一部分在富燃料条件下燃烧，并且一部分所得到的反应热在非预混合燃烧之前被转移到燃烧空气中 的燃料。