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1. 发明公开

EP2902708A1 MULTI-FUEL-SUPPORTING GAS-TURBINE COMBUSTOR 有权
标题翻译：多燃料支持的燃气轮机燃烧器
公开(公告)号：EP2902708A1
公开(公告)日：2015-08-05
申请号：EP14844741.0
申请日：2014-06-12
申请人： Kawasaki Jukogyo Kabushiki Kaisha
发明人： OGATA, Masahiro , ODA, Takeo , KINOSHITA, Yasuhiro
IPC分类号： F23R3/34 , F02C7/22 , F23R3/30 , F23R3/36
CPC分类号： F23R3/286 , F02C3/22 , F02C7/222 , F02C7/232 , F02C9/40 , F23C2900/9901 , F23D2900/00015 , F23R3/34 , F23R3/343 , F23R3/346 , F23R3/36 , F23R3/46 , F23R2900/00002
摘要： To provide a multifuel gas turbine combustor capable of combusting gases containing hydrogen in a high concentration with a low NOx while maintaining a low emission performance brought about by the pre-mixture combustion in the main burner, the gas turbine combustor includes a main burner (12) for supplying to and combusting a premixed gas (M), containing a first fuel (F1), within a first combustion region (S1) of a combustion chamber (10), and a supplemental burner (20) for supplying to and combusting a second fuel (F2) of a composition different from that of the first fuel (F1) within a second combustion region (S2) defined downstream of the first combustion region (S1) within the combustion chamber (10). The first fuel (F1) is of a hydrocarbon system and the second fuel (F2) is a gas containing hydrogen in a concentration exceeding the stable combustion limiting concentration of the hydrogen.
摘要翻译：本发明提供一种多燃料气体燃气轮机燃烧器，该燃料燃气轮机燃烧器能够在保持主燃烧器中的预混合燃烧所带来的低排放性能的同时以低NOx燃烧含有高浓度氢的气体，并且包括主燃烧器（12 ），用于在燃烧室（10）的第一燃烧区域（S1）内供应并燃烧包含第一燃料（F1）的预混合气体（M）;以及辅助燃烧器（20），用于供应并燃烧在所述燃烧室（10）内限定在所述第一燃烧区域（S1）下游的第二燃烧区域（S2）内具有不同于所述第一燃料（F1）的组成的第二燃料（F2）。第一燃料（F1）是烃系统，第二燃料（F2）是含有浓度超过氢的稳定燃烧极限浓度的氢的气体。

2. 发明授权

EP1555407B1 METHOD AND SYSTEM FOR CONTROLLING GAS TURBINE ENGINE 有权
标题翻译：方法和系统，以控制燃气涡轮发动机
公开(公告)号：EP1555407B1
公开(公告)日：2013-04-10
申请号：EP03756645.2
申请日：2003-10-16
申请人： KAWASAKI JUKOGYO KABUSHIKI KAISHA
发明人： BAINO, Makoto , KOUNO, Yukinobu , SASAE, Keisuke , KIMURA, Hideo , KINOSHITA, Yasuhiro , KOBAYASHI, Masayoshi , YOSHIMURA, Takanobu
IPC分类号： F23R3/34 , F02C9/28 , F02C9/26 , F02C9/34
CPC分类号： F23R3/343 , F02C9/26 , F02C9/28 , F02C9/34 , F05D2270/082 , F05D2270/10 , F23N2041/20 , Y02T50/677

3. 发明授权

EP2955445B1 MULTIFUEL GAS TURBINE COMBUSTOR 有权
公开(公告)号：EP2955445B1
公开(公告)日：2019-11-27
申请号：EP15168221.8
申请日：2014-06-12
申请人： KAWASAKI JUKOGYO KABUSHIKI KAISHA
发明人： OGATA, Masahiro , ODA, Takeo , KINOSHITA, Yasuhiro
IPC分类号： F23R3/28 , F23R3/46 , F02C7/232 , F02C9/40 , F23R3/34 , F23R3/36 , F02C7/22

4. 发明公开

EP1555407A1 METHOD AND SYSTEM FOR CONTROLLING GAS TURBINE ENGINE 有权
标题翻译： VERFAHREN UND SYSTEM ZUR STEUERUNG EINES GASTURBINENMOTORS
公开(公告)号：EP1555407A1
公开(公告)日：2005-07-20
申请号：EP03756645.2
申请日：2003-10-16
申请人： Kawasaki Jukogyo Kabushiki Kaisha
发明人： BAINO, Makoto , KOUNO, Yukinobu , SASAE, Keisuke , KIMURA, Hideo , KINOSHITA, Yasuhiro , KOBAYASHI, Masayoshi , YOSHIMURA, Takanobu
IPC分类号： F02C9/34 , F02C9/28
CPC分类号： F23R3/343 , F02C9/26 , F02C9/28 , F02C9/34 , F05D2270/082 , F05D2270/10 , F23N2041/20 , Y02T50/677
摘要： In a control method of a gas turbine engine, an engine controller 4 outputs a combustor power command FD based on an engine condition from an engine condition detector 3. Then, a combustion controller 6 determines each fuel flow rate based on the combustion power command FD. The combustor controller 6 overrides each fuel flow rate for a certain period, to realize smooth stage-process.
摘要翻译：在燃气轮机的控制方法中，发动机控制器4根据发动机状况从发动机状况检测器3输出燃烧器动力指令FD。然后，燃烧控制器6根据燃烧功率指令FD 。燃烧器控制器6在一定时间内超过每个燃料流量，以实现平稳的阶段过程。

5. 发明公开

EP3217097A1 BURNER, COMBUSTOR, AND GAS TURBINE 有权
标题翻译：燃烧器，燃烧器和燃气轮机
公开(公告)号：EP3217097A1
公开(公告)日：2017-09-13
申请号：EP15857808.8
申请日：2015-11-04
申请人： Kawasaki Jukogyo Kabushiki Kaisha
发明人： OGATA, Masahiro , ODA, Takeo , KINOSHITA, Yasuhiro , HIRANO, Kohshi , UTO, Takahiro
IPC分类号： F23R3/28 , F02C7/22 , F23R3/30 , F23R3/34 , F23R3/36
CPC分类号： F02C7/228 , F02C3/04 , F02C7/22 , F02C7/222 , F05D2220/32 , F05D2240/35 , F23R3/28 , F23R3/286 , F23R3/30 , F23R3/34 , F23R3/346 , F23R3/36 , F23R3/44
摘要： A burner (6) injects a mixture of fuel and air from a base end side far from a combustion chamber (48) toward a distal end side close to the combustion chamber(48). The burner (6) has a fuel passage (76, 78, 80) having a turn-back part (80) turning back and channeling the fuel between the base end side and the distal end side. The burner (6) has a premixed gas passage (82) formed to surround the fuel passage (76, 78, 80). The burner (6) has a fuel introduction part (84) introducing the fuel channeled through the fuel passage (76, 78, 80) into the premixed gas passage (82) from the base end side to the distal end side. The burner (6) has an air supply part (62) supplying the premixed gas passage (82) with air on the base end side. Therefore, the burner (6) is capable of preventing a flashback with a simple structure.
摘要翻译：燃烧器（6）从远离燃烧室（48）的基端侧向靠近燃烧室（48）的前端侧喷射燃料和空气的混合物。燃烧器（6）具有燃料通路（76,78,80），该燃料通路（76,78,80）具有在基端侧与前端侧之间使燃料回流并引导的折回部（80）。燃烧器（6）具有形成为包围燃料通路（76,78,80）的预混合气体通路（82）。燃烧器6具有燃料导入部84，该燃料导入部84将从燃料通路76,78,80导出的燃料从基端侧向前端侧导入预混合气体通路82。燃烧器（6）具有在基端侧向预混合气体通路（82）供给空气的空气供给部（62）。因此，燃烧器（6）能够以简单的结构防止回火。

6. 发明授权

EP2902708B1 MULTI-FUEL-SUPPORTING GAS-TURBINE COMBUSTOR 有权
标题翻译：燃气轮机燃烧室多种燃料
公开(公告)号：EP2902708B1
公开(公告)日：2017-02-01
申请号：EP14844741.0
申请日：2014-06-12
申请人： Kawasaki Jukogyo Kabushiki Kaisha
发明人： OGATA, Masahiro , ODA, Takeo , KINOSHITA, Yasuhiro
IPC分类号： F23R3/34 , F02C7/22 , F23R3/30 , F23R3/36
CPC分类号： F23R3/286 , F02C3/22 , F02C7/222 , F02C7/232 , F02C9/40 , F23C2900/9901 , F23D2900/00015 , F23R3/34 , F23R3/343 , F23R3/346 , F23R3/36 , F23R3/46 , F23R2900/00002

7. 发明公开

EP2955445A1 MULTIFUEL GAS TURBINE COMBUSTOR 有权
标题翻译： MEHRSTOFFBRENNKAMMERFÜREINE GASTURBINE
公开(公告)号：EP2955445A1
公开(公告)日：2015-12-16
申请号：EP15168221.8
申请日：2014-06-12
申请人： KAWASAKI JUKOGYO KABUSHIKI KAISHA
发明人： OGATA, Masahiro , ODA, Takeo , KINOSHITA, Yasuhiro
IPC分类号： F23R3/34 , F02C7/22 , F23R3/30 , F23R3/36
CPC分类号： F23R3/286 , F02C3/22 , F02C7/222 , F02C7/232 , F02C9/40 , F23C2900/9901 , F23D2900/00015 , F23R3/34 , F23R3/343 , F23R3/346 , F23R3/36 , F23R3/46 , F23R2900/00002
摘要： To provide a multifuel gas turbine combustor capable of combusting gases containing hydrogen in a high concentration with a low NOx while maintaining a low emission performance brought about by the pre-mixture combustion in the main burner, the gas turbine combustor includes a main burner (12) for supplying to and combusting a premixed gas (M), containing a first fuel (F1), within a first combustion region (S1) of a combustion chamber (10), and a supplemental burner (20) for supplying to and combusting a second fuel (F2) of a composition different from that of the first fuel (F1) within a second combustion region (S2) defined downstream of the first combustion region (S1) within the combustion chamber (10). The first fuel (F1) is of a hydrocarbon system and the second fuel (F2) is a gas containing hydrogen in a concentration exceeding the stable combustion limiting concentration of the hydrogen.
摘要翻译：为了提供一种能够在保持由主燃烧器中的预混合燃烧引起的低排放性能的同时以低NOx燃烧高浓度的氢气的多燃气涡轮燃烧器，燃气轮机燃烧器包括主燃烧器（12）），用于在燃烧室（10）的第一燃烧区域（S1）内供给和燃烧含有第一燃料（F1）的预混合气体（M）和用于供给和燃烧燃料的辅助燃烧器（20）在第一燃烧区域（S1）的下游的第二燃烧区域（S2）内具有不同于第一燃料（F1）的组成的第二燃料（F2）。第一燃料（F1）是烃系统，第二燃料（F2）是含有浓度超过氢的稳定的燃烧极限浓度的氢的气体。

8. 发明公开

EP2933561A1 MULTI-FUEL-CAPABLE GAS TURBINE COMBUSTOR 审中-公开
标题翻译： MULTIKRAFTSTOFFFÄHIGEGASTURBINENBRENNKAMMER
公开(公告)号：EP2933561A1
公开(公告)日：2015-10-21
申请号：EP13862678.3
申请日：2013-12-13
申请人： Kawasaki Jukogyo Kabushiki Kaisha
发明人： OGATA, Masahiro , ODA, Takeo , KINOSHITA, Yasuhiro
IPC分类号： F23R3/36 , F02C3/22 , F02C3/24 , F02C7/22 , F02C7/228 , F23R3/28 , F23R3/34
CPC分类号： F02C3/22 , F02C3/24 , F02C7/228 , F02C9/40 , F23C2900/9901 , F23R3/286 , F23R3/346 , F23R3/36
摘要： A multi-fuel-capable gas turbine combustor is provided which is able to sufficiently utilize various fuels having a characteristic deviating from a premixing characteristic range suitable for generating a premixed gas, even while maintaining favorable low-emission performance by premixed combustion. The gas turbine combustor includes: a main burner configured to supply a premixed gas containing a first fuel for premixing, to a first combustion region within a combustion chamber to cause premixed combustion; and a supplemental burner configured to supply a second fuel for reheating having a different composition from that of the first fuel, to a second combustion region at a location downstream of the first combustion region within the combustion chamber, to cause diffusion combustion. The first fuel has a premixing characteristic range suitable for generating a premixed gas. The second fuel has a characteristic deviating from the premixing characteristic range.
摘要翻译：提供一种多燃料燃气轮机燃烧器，其能够充分利用具有偏离适合于产生预混合气体的预混合特性范围的特性的各种燃料，即使在通过预混燃烧保持有利的低排放性能的同时也是如此。燃气轮机燃烧器包括：主燃烧器，其构造成将包含用于预混合的第一燃料的预混合气体供应到燃烧室内的第一燃烧区域以引起预混燃烧; 以及补充燃烧器，其构造成将具有与第一燃料的组成不同的组成的再加热用的第二燃料供给到燃烧室内的第一燃烧区域下游的第二燃烧区域，以引起扩散燃烧。第一种燃料具有适于产生预混合气体的预混合特性范围。第二燃料具有偏离预混合特性范围的特性。

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