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1. 发明申请

US20150007573A1 ANNULAR-COMBUSTION-CHAMBER BYPASS 审中-公开
标题翻译：环形燃烧室旁路
公开(公告)号：US20150007573A1
公开(公告)日：2015-01-08
申请号：US14382918
申请日：2013-03-15
申请人： SIEMENS AKTIENGESELLSCHAFT
发明人： Francois Benkler , Thomas Brandenburg , Olga Deiss , Thomas Grieb , Marco Link , Nicolas Savilius , Daniel Vogtmann , Jan Wilkes
IPC分类号： F23R3/26 , F23R3/08
CPC分类号： F23R3/26 , F23R3/04 , F23R3/08
摘要： An annular combustion chamber (1) for a gas turbine, the chamber having an outer shell (12) which has at least one inlet opening (4) for a burner (3) and an outlet (7) which opens into a turbine chamber (8), wherein ducts (14) which can be closed, which are oriented substantially parallel to the symmetry axis (2) of the annular combustion chamber (1), and through which final compressor air is guided into the annular combustion chamber (1) are provided in the outer shell (12) in the region of the outlet (7). Ring segments around the outer shell have projections selectively movable to at least partially block and open the ducts. A gas turbine is also disclosed.
摘要翻译：一种用于燃气轮机的环形燃烧室（1），所述腔室具有外壳（12），所述外壳具有用于燃烧器（3）的至少一个入口（4）和通向涡轮室（7）的出口（7） 8），其中可以关闭的导管（14）基本上平行于环形燃烧室（1）的对称轴线（2）定向，并且最终的压缩机空气通过该导管引导到环形燃烧室（1）中，在出口（7）的区域中设置在外壳（12）中。围绕外壳的环形段具有选择性地可移动以至少部分地阻挡和打开导管的突起。还公开了一种燃气轮机。

2. 发明授权

US10088163B2 Jet burner with cooling duct in the base plate 有权
公开(公告)号：US10088163B2
公开(公告)日：2018-10-02
申请号：US14773345
申请日：2014-02-07
申请人： Siemens Aktiengesellschaft
发明人： Christian Beck , Simon Bez , Bjorn Buchholz , Thomas Grieb , Matthias Hase , Werner Krebs , Berthold Kostlin , Stefan Reich , Marc Tertilt , Jan Wilkes
IPC分类号： F23R3/10 , F23R3/00 , F23R3/28 , F23R3/34 , F23R3/04
摘要： A jet burner has a hot-gas side, which faces toward a combustion chamber during operation, and a cold-gas side, which faces away from a combustion chamber, including a base plate on which there are arranged multiple jet nozzles, wherein the base plate has at least one cooling duct, wherein the at least one cooling duct issues into a burner stage which comprises a pilot burner arranged on the base plate.

3. 发明申请

US20160018109A1 JET BURNER WITH COOLING DUCT IN THE BASE PLATE 审中-公开
标题翻译：喷气式燃烧器在基板中具有冷却导管
公开(公告)号：US20160018109A1
公开(公告)日：2016-01-21
申请号：US14773345
申请日：2014-02-07
申请人： SIEMENS AKTIENGESELLSCHAFT
发明人： Christian Beck , Simon Bez , Bjorn Buchholz , Thomas Grieb , Matthias Hase , Werner Krebs , Berthold Kostlin , Stefan Reich , Marc Tertilt , Jan Wilkes
IPC分类号： F23R3/00 , F23R3/34 , F23R3/04
CPC分类号： F23R3/005 , F23R3/002 , F23R3/04 , F23R3/10 , F23R3/286 , F23R3/343 , F23R2900/03043 , F23R2900/03045 , F23R2900/03282
摘要： A jet burner has a hot-gas side, which faces toward a combustion chamber during operation, and a cold-gas side, which faces away from a combustion chamber, including a base plate on which there are arranged multiple jet nozzles, wherein the base plate has at least one cooling duct, wherein the at least one cooling duct issues into a burner stage which comprises a pilot burner arranged on the base plate.
摘要翻译：喷气燃烧器具有在操作期间朝向燃烧室的热气侧和面向远离燃烧室的冷气侧，所述冷气侧包括其上布置有多个喷嘴的基板，其中所述基座板具有至少一个冷却管道，其中所述至少一个冷却管道发射到燃烧器台，所述燃烧器台包括布置在所述基板上的引燃燃烧器。

4. 发明申请

US20150027128A1 HEAT-SHIELD ELEMENT FOR A COMPRESSOR-AIR BYPASS AROUND THE COMBUSTION CHAMBER 审中-公开
标题翻译：用于燃烧室周围的压缩空气旁路的加热元件
公开(公告)号：US20150027128A1
公开(公告)日：2015-01-29
申请号：US14384257
申请日：2013-03-12
申请人： SIEMENS AKTIENGESELLSCHAFT
发明人： Francois Benkler , Thomas Brandenburg , Olga Deiss , Thomas Grieb , Marco Link , Nicolas Savilius , Daniel Vogtmann , Jan Wilkes
IPC分类号： F23R3/08 , F23R3/50
CPC分类号： F23R3/08 , F23R3/005 , F23R3/007 , F23R3/50 , F23R3/60 , F23R2900/03042
摘要： A heat-shield element (14), for lining a combustion-chamber wall (13), the chamber wall has a first wall (17) with a hot side (18) which can be loaded with a hot medium, a cold side (19) which lies opposite the hot side (18), and a circumferential edge (24) which extends on a first (20), a second (21) and a third narrow side (22) of the first wall (17) to a first height (25) beyond the cold side (19), the circumferential edge (24) extends on a fourth narrow side (23) to a second shorter height (26), substantially at the second height (26), a second wall (27) lies opposite the cold side (19) and extends over the width of the fourth narrow side (23) from the fourth narrow side (23) and over a part of the length of the narrow sides (20, 22), which adjoin the fourth narrow side; (23), the second wall (27) has an edge (29) at the end (28) thereof which faces away from the fourth narrow side (23), which edge (29) extends to the first height (25). Furthermore, a combustion chamber and a gas turbine are disclosed.
摘要翻译：一种用于衬里燃烧室壁（13）的隔热元件（14），所述室壁具有第一壁（17），所述第一壁具有热侧（18），所述第一壁可以装载有热介质，冷侧 19），以及在第一壁（17）的第一（20），第二（21）和第三窄边（22）上延伸到第一壁（17）的周向边缘（24）第一高度（25）超过冷侧（19），圆周边缘（24）在第四窄边（23）延伸到第二较短高度（26），基本上在第二高度（26），第二壁 27）与冷侧（19）相对并且从第四窄边（23）延伸到第四窄边（23）的宽度上并且在窄边（20,22）的一部分长度上延伸，其邻接第四窄边（23）中，第二壁（27）在其端部（28）处具有远离第四窄边（23）的边缘（29），该边缘（29）延伸到第一高度（25）。此外，公开了燃烧室和燃气轮机。

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