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1. 发明公开

KR1020140052883A 재열 버너 장치 有权
标题翻译： REHEAT燃烧器装置
公开(公告)号：KR1020140052883A
公开(公告)日：2014-05-07
申请号：KR1020130126875
申请日：2013-10-24
申请人： 제네럴 일렉트릭 테크놀러지 게엠베하
发明人： 시아니안드레아 , 우드존필립 , 펜넬더글라스안토니 , 프라이탁에발트 , 토이어안드레
IPC分类号： F23R3/42 , F02C7/00 , F23R3/16
CPC分类号： F23R3/20 , F02C6/003 , F02C6/02 , F05D2250/12 , F05D2250/13 , F23R3/12 , F23R3/16 , F23R3/18 , F23R3/34 , F23R3/346 , F23R2900/03341 , F23R3/42 , F02C7/00
摘要： A rehear burner device includes: a central body; a ring-shaped duct having a cross-sectional zone; and a middle fuel injection plane connected to the cross-sectional zone of the ring-shaped duct along the central body. The central body is arranged on the upstream portion of a combustion chamber, and a structure body of the reheat burner device is limited by various parameters. The structure body of the reheat burner is limited by various dependence factors.
摘要翻译：重画炉装置包括：中心体; 具有横截面区域的环形导管; 以及沿着中心体与环形管道的横截面区域连接的中间燃料喷射平面。中心体设置在燃烧室的上游部分，并且再热燃烧器装置的结构体受到各种参数的限制。再热燃烧器的结构体受各种依赖因素的限制。

2. 发明公开

KR1020140034079A 연소기용 음향 감쇠기 장치 有权
标题翻译：用于燃烧器的呼吸阻尼器装置
公开(公告)号：KR1020140034079A
公开(公告)日：2014-03-19
申请号：KR1020130107807
申请日：2013-09-09
申请人： 제네럴 일렉트릭 테크놀러지 게엠베하
发明人： 보틴미르코루벤 , 조겐센스티븐더블유 , 펜넬더글라스안토니
IPC分类号： F02C7/24 , F02C7/00
CPC分类号： F02C7/24 , F23M20/005 , F23R3/08 , F23R2900/00014
摘要： Disclosed is an acoustic attenuator for a combustor including an inner liner constructed to be used in the first temperature during operation and an outer liner constructed to be operated in the second temperature which is lower than the first temperature during the operation. The acoustic attenuator comprises a plurality of flexibility sheets and at least one midair bodies fixed in one of the flexibility sheets and including an inner volume. The acoustic attenuator is fixed at the inner liner and the outer liner to communicate the inner volume of the midair bodies with a chamber formed by the inner liner. The flexibility sheets accommodates the contraction and expansion of the inner liner for the outer liner.
摘要翻译：公开了一种用于燃烧器的声衰减器，其包括构造成在操作期间在第一温度中使用的内衬层和构造成在操作期间以低于第一温度的第二温度操作的外衬套。声衰减器包括多个柔性片和至少一个固定在一个柔性片中并包括内容积的空中体。声衰减器固定在内衬和外衬里，以将空中体的内体与内衬形成的室连通。柔性片容纳用于外衬套的内衬的收缩和膨胀。

3. 发明授权

KR101663495B1 재열 버너 장치 有权
标题翻译： REHEAT燃烧器装置
公开(公告)号：KR101663495B1
公开(公告)日：2016-10-07
申请号：KR1020130126875
申请日：2013-10-24
申请人： 제네럴 일렉트릭 테크놀러지 게엠베하
发明人： 시아니안드레아 , 우드존필립 , 펜넬더글라스안토니 , 프라이탁에발트 , 토이어안드레
IPC分类号： F23R3/42 , F02C7/00 , F23R3/16
CPC分类号： F23R3/20 , F02C6/003 , F02C6/02 , F05D2250/12 , F05D2250/13 , F23R3/12 , F23R3/16 , F23R3/18 , F23R3/34 , F23R3/346 , F23R2900/03341
摘要： 재열버너장치는중심몸체, 단면영역을갖는환형덕트, 중심몸체를따라배치되어환형덕트의단면영역에활성적으로연결되어있는중간연료분사평면을포함하고, 상기중심몸체는연소실의상류에배치되고, 재열버너장치의구조체는다양한파라미터들에의해한정되고, 재열버너장치의구조물은다양한의 존도에의해한정된다.

4. 发明授权

KR101619201B1 캔형 연소기용 버너 有权
标题翻译：燃烧器为燃烧器
公开(公告)号：KR101619201B1
公开(公告)日：2016-05-10
申请号：KR1020130125805
申请日：2013-10-22
申请人： 제네럴 일렉트릭 테크놀러지 게엠베하
发明人： 시아니안드레아 , 우드존필립 , 펜넬더글라스안토니 , 프라이탁에발트 , 벤즈우르스 , 토이어안드레
IPC分类号： F23R3/02 , F23R3/16 , F23R3/28
CPC分类号： F23R3/16 , F05B2260/222 , F23R3/20 , F23R3/286 , F23R3/34 , F23R3/346 , F23R3/36 , F23R3/46 , F23R2900/03341
摘要： 본발명은혼합및 분사장치를구비한가스터빈의연소실용버너에관한것으로서, 상기혼합및 분사장치는가스-유동채널을구성하는제한벽 및각각상기가스-유동채널내로제 1 가로방향으로연장하는적어도 2개의유선형몸체들(22)을포함한다. 각각의유선형몸체(22)는상기주-유동방향(14)과근본적으로평행하게배열되는 2개의측면들을가지며, 상기측면들은상기몸체의선단에지를형성하기위해상류측에서서로결합되고또한상기몸체(22)의후미에지를형성하기위해하류측에서결합된다. 각각의유선형몸체(22)는유선형프로파일로서형성되는상기제 1 가로방향(49)과수직인단면을갖는다. 상기유선형몸체들(22) 중적어도하나에는혼합구조체, 및상기유동채널내로상기주-유동방향(14)과근본적으로평행하게적어도하나의연료를도입시키기위해그 후미에지에위치된적어도하나의연료노즐이구비되며, 상기유선형몸체들(22) 중적어도 2개는캔형연소기를위해사용될수 있도록상기제 1 가로방향을따라다른길이를갖는다. 본발명은또한가스터빈에서상기버너를사용하기위한방법에관한것이다.

5. 发明授权

KR101555500B1 연속 연소에 의한 가스터빈 작동방법 및 상기 방법을 실시하는 가스터빈 有权
标题翻译：使用具有顺序燃烧器和气体涡轮机的气体涡轮机进行操作的方法
公开(公告)号：KR101555500B1
公开(公告)日：2015-10-06
申请号：KR1020130125213
申请日：2013-10-21
申请人： 제네럴 일렉트릭 테크놀러지 게엠베하
发明人： 시아니안드레아 , 에로그루아드난 , 펜넬더글라스안토니 , 뜨란니꼴라스 , 프라이타크에발트
IPC分类号： F02C9/26 , F02C5/00 , F23R3/00
CPC分类号： F02C7/12 , F02C7/141 , F02C7/228 , F02C9/28 , F05D2270/08 , Y02E20/16
摘要： 본발명은연속연소(14, 15, 17, 19)에의한가스터빈(10) 작동방법을개시하며, 상기가스터빈(10)은압축기(13), 상기압축기(13)로부터압축공기를수용하며제1 연소실(14)과제1 버너(17)들을갖는제1 연소기(14, 17), 예정된제2 연소기입구온도를가지며상기제1 연소기(14, 17)로부터고온가스를수용하며제2 연소실(15)과제2 버너(19)들을갖는제2 연소기(15, 19), 및제2 연소기(15, 19)로부터고온가스를수용하는터빈(16)을포함한다. 부분-부하작동을위한 CO 방출물은가스터빈(10)의기저-부하작동을위한제2 연소기입구온도를감소시키고, 그리고가스터빈부하(RL)를기저-부하에서부분-부하로감소시킬때 제2 연소기입구온도를증가시킴으로써감소된다.

6. 发明授权

KR101551673B1 연소기용 음향 감쇠기 장치 有权
标题翻译：用于燃烧器的呼吸阻尼器装置
公开(公告)号：KR101551673B1
公开(公告)日：2015-09-09
申请号：KR1020130107807
申请日：2013-09-09
申请人： 제네럴 일렉트릭 테크놀러지 게엠베하
发明人： 보틴미르코루벤 , 조겐센스티븐더블유 , 펜넬더글라스안토니
IPC分类号： F02C7/24 , F02C7/00
CPC分类号： F02C7/24 , F23M20/005 , F23R3/08 , F23R2900/00014
摘要： 작동중에제 1 온도에서사용하도록구성된내부라이너및 작동중에상기제 1 온도보다낮은제 2 온도에서작동하도록구성된외부라이너를구비하는연소기용음향감쇠기장치가개시되고, 상기음향감쇠기장치는복수의가요성시트들; 및내부체적을갖는적어도하나의중공몸체로서, 상기복수의가요성시트들중 하나에각각고정되는상기적어도하나의중공몸체를포함하고, 상기음향감쇠기장치는상기적어도하나의중공몸체의내부체적이상기내부라이너에의해서형성된챔버와교통하도록상기내부라이너및 상기외부라이너모두에고정되도록구성되고, 상기복수의가요성시트들은상기외부라이너에대한상기내부라이너의팽창및 수축을수용한다.

7. 发明公开

KR1020140051793A 캔형 연소기용 버너 有权
标题翻译：燃烧器为燃烧器
公开(公告)号：KR1020140051793A
公开(公告)日：2014-05-02
申请号：KR1020130125805
申请日：2013-10-22
申请人： 제네럴 일렉트릭 테크놀러지 게엠베하
发明人： 시아니안드레아 , 우드존필립 , 펜넬더글라스안토니 , 프라이탁에발트 , 벤즈우르스 , 토이어안드레
IPC分类号： F23R3/02 , F23R3/16 , F23R3/28
CPC分类号： F23R3/16 , F05B2260/222 , F23R3/20 , F23R3/286 , F23R3/34 , F23R3/346 , F23R3/36 , F23R3/46 , F23R2900/03341 , F23R3/02 , F23R3/28
摘要： The present invention relates to a burner for a combustion chamber of a gas turbine with a mixing and injection device, wherein the mixing and injection device includes a limiting wall that defines a gas-flow channel and at least two streamlined bodies (22). Each streamlined body extends in a first transverse direction into the gas-flow channel. Each streamlined body (22) has two lateral surfaces that are arranged essentially parallel to a main-flow direction (14). The lateral surfaces are joined to one another at their upstream side to form a leading edge of the body and joined at their downstream side to form a trailing edge of the body (22). Each streamlined body (22) has a cross-section perpendicular to the first transverse direction (49) that is shaped as a streamlined profile. At least one of the streamlined bodies (22) is provided with a mixing structure and with at least one fuel nozzle located at its trailing edge for introducing at least one fuel essentially parallel to the main-flow direction (14) into the flow channel, wherein at least two of the streamlined bodies (22) have different lengths along the first transverse direction such that the at least two may be used for a can combustor. The present invention also relates to a method for using the burner in a gas turbine.
摘要翻译：本发明涉及一种具有混合和注入装置的燃气轮机的燃烧室的燃烧器，其中混合和喷射装置包括限定气流通道的限制壁和至少两个流线型主体（22）。每个流线型主体在第一横向方向上延伸到气体流动通道中。每个流线型主体（22）具有基本上平行于主流动方向（14）布置的两个侧表面。侧表面在其上游侧彼此接合以形成主体的前缘并在其下游侧接合以形成主体（22）的后缘。每个流线型本体（22）具有垂直于第一横向方向（49）的横截面，其被形成为流线型轮廓。至少一个流线型本体（22）设置有混合结构，并具有至少一个位于其后缘处的燃料喷嘴，用于将基本上平行于主流动方向（14）的至少一个燃料引入流动通道，其中所述流线型主体（22）中的至少两个沿着所述第一横向方向具有不同的长度，使得所述至少两个可以用于罐式燃烧器。本发明还涉及一种在燃气轮机中使用燃烧器的方法。

8. 发明公开

KR1020140051089A 연속 연소에 의한 가스터빈 작동방법 및 상기 방법을 실시하는 가스터빈 有权
标题翻译：使用具有顺序燃烧器和气体涡轮机的气体涡轮机进行操作的方法
公开(公告)号：KR1020140051089A
公开(公告)日：2014-04-30
申请号：KR1020130125213
申请日：2013-10-21
申请人： 제네럴 일렉트릭 테크놀러지 게엠베하
发明人： 시아니안드레아 , 에로그루아드난 , 펜넬더글라스안토니 , 뜨란니꼴라스 , 프라이타크에발트
IPC分类号： F02C9/26 , F02C5/00 , F23R3/00
CPC分类号： F02C7/12 , F02C7/141 , F02C7/228 , F02C9/28 , F05D2270/08 , Y02E20/16
摘要： In the present invention, disclosed is a method for operating a gas turbine (10) with sequential combustion (14, 15, 17, and 19). The gas turbine (10) comprises a compressor (13); a first combustor (14 and 17) which receives compressed air from the compressor (13) and has a first combustion chamber (14) and first burners (17); a second combustor (15 and 19) which has a scheduled second combustor inlet temperature, receives overheated gas from the first combustor (14 and 17), and has a second combustion chamber (15) and second burners (19); and a turbine (16) which receives the overheated gas from the second combustor (15 and 19). The CO emission for partial load operation is decreased by increasing the second combustor inlet temperature when the second combustor inlet temperature for the base load operation of the gas turbine (10) is decreased and the gas turbine load (RLGT) is decreased from the base load to the partial load.
摘要翻译：在本发明中，公开了一种用于操作具有顺序燃烧（14,15,17和19）的燃气轮机（10）的方法。燃气轮机（10）包括压缩机（13）; 第一燃烧器（14和17），其从压缩机（13）接收压缩空气并具有第一燃烧室（14）和第一燃烧器（17）; 具有预定的第二燃烧器入口温度的第二燃烧器（15和19）接收来自第一燃烧器（14和17）的过热气体，并具有第二燃烧室（15）和第二燃烧器（19）; 以及从第二燃烧器（15和19）接收过热气体的涡轮机（16）。当用于燃气轮机（10）的基本负载操作的第二燃烧器入口温度降低并且燃气轮机负荷（RLGT）从基本负载减小时，通过增加第二燃烧器入口温度来降低部分负荷运行的CO排放到部分负载。

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