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1. 发明申请

US20120240595A1 COMBUSTION CHAMBER HEAD WITH HOLDING MEANS FOR SEALS ON BURNERS IN GAS TURBINES 有权
标题翻译：燃气灶头，燃气灶具燃烧器上的密封
公开(公告)号：US20120240595A1
公开(公告)日：2012-09-27
申请号：US13428633
申请日：2012-03-23
申请人： Miklos GERENDAS
发明人： Miklos GERENDAS
IPC分类号： F23R3/28
CPC分类号： F23R3/283 , F23R3/002 , F23R2900/00012
摘要： A combustion chamber head of a gas turbine has a base plate 113 provided with a centric recess 121 in which at least one burner 106 is arranged, with the base plate 113 being connected to walls of the combustion chamber 108 and to a burner seal 116 sealing the burner 106 towards the rim of the recess 121. The burner seal 116 is arranged upstream of the base plate 113 and can be brought into contact with a collar 118 provided on the base plate 113 and forming the rim of the centric recess 121. A holding element 117 of the burner seal 116 is formed as a ring and arranged upstream of the burner seal 116 and engages with at least one projection 114 of the base plate 113 in a tension-free state.
摘要翻译：燃气轮机的燃烧室头具有设置有中心凹部121的基板113，其中布置有至少一个燃烧器106，其中底板113连接到燃烧室108的壁和燃烧器密封件116的密封燃烧器106朝向凹部121的边缘。燃烧器密封件116布置在基板113的上游，并且可以与设置在基板113上的轴环118接触并形成中心凹部121的边缘。燃烧器密封件116的保持元件117形成为环并且布置在燃烧器密封件116的上游，并且以无张力状态与基板113的至少一个突起114接合。

2. 发明申请

US20120240583A1 SEGMENTED COMBUSTION CHAMBER HEAD 有权
标题翻译： SEGMENTED燃烧室头
公开(公告)号：US20120240583A1
公开(公告)日：2012-09-27
申请号：US13426070
申请日：2012-03-21
申请人： Stefan PENZ , Miklos GERENDAS , Sermed SADIG
发明人： Stefan PENZ , Miklos GERENDAS , Sermed SADIG
IPC分类号： F23R3/00
CPC分类号： F23R3/60 , F23R3/002 , F23R3/10 , F23R3/283 , F23R2900/00012 , F23R2900/00014
摘要： A combustion chamber head for a gas turbine, with the gas turbine having a substantially annular outer combustion chamber wall, at least one substantially annular inner combustion chamber wall, and several burners 106 distributed around a circumference of the gas turbine. Several segment-like head segments are arranged over the circumference in equal number to the number of burners and extend in the radial direction between the inner combustion chamber wall and the outer combustion chamber wall and in the circumferential direction between radial planes formed by the burner axes.
摘要翻译：一种用于燃气轮机的燃烧室头部，其中燃气轮机具有基本上环形的外部燃烧室壁，至少一个基本上环形的内部燃烧室壁和分布在燃气轮机周围的多个燃烧器106。在圆周上布置几个段状的头部段，其数量与燃烧器的数量相等，并且在径向方向上在内燃机室壁和外部燃烧室壁之间以及在由燃烧器轴形成的径向平面之间的圆周方向上延伸。

3. 发明申请

US20120117973A1 GAS-TURBINE COMBUSTION CHAMBER WITH A COOLING-AIR SUPPLY DEVICE 有权
标题翻译：具有冷却空气供应装置的气体涡轮搅拌室
公开(公告)号：US20120117973A1
公开(公告)日：2012-05-17
申请号：US13275805
申请日：2011-10-18
申请人： Miklos GERENDAS
发明人： Miklos GERENDAS
IPC分类号： F23R3/42
CPC分类号： F23R3/06 , F23R2900/03041 , F23R2900/03042 , Y02T50/675
摘要： A gas-turbine combustion chamber has a cooling-air supply device delivering cooling air to a combustion chamber wall 6 to be cooled. The cooling-air supply device includes at least one air-supply duct 8 which, in respect of its flow axis, is arranged vertically to the combustion chamber wall 6, with the air-supply duct 8 being flow-connected to at least one cooling duct 9. The air-supply duct 8 forms a throttle and has a smaller diameter than the cooling duct 9. The cooling duct 9 issues at a shallow angle, relative to its flow axis, to the surface of the combustion chamber wall 6 in a recess 10 of the combustion chamber wall 6, with the cooling duct 9 being designed to impart a swirl to the air flowing through it.
摘要翻译：燃气轮机燃烧室具有向要冷却的燃烧室壁6输送冷却空气的冷却空气供给装置。冷却空气供应装置包括至少一个空气供应管道8，空气供应管道8在其流动轴线上垂直于燃烧室壁6布置，供气管道8与至少一个冷却供气管道8形成节气门并且具有比冷却管道9更小的直径。冷却管道9相对于其流动轴线以相对于燃烧室壁6的表面的浅角度发出燃烧室壁6的凹部10，其中冷却管道9被设计成使流过其的空气产生漩涡。

4. 发明申请

US20110011093A1 GAS-TURBINE COMBUSTION CHAMBER WITH STARTER FILM FOR COOLING THE COMBUSTION CHAMBER WALL 有权
标题翻译：用于冷却燃烧室壁的起动电磁阀的气动涡轮搅拌室
公开(公告)号：US20110011093A1
公开(公告)日：2011-01-20
申请号：US12815829
申请日：2010-06-15
申请人： Miklos GERENDAS , Sermed SADIG
发明人： Miklos GERENDAS , Sermed SADIG
IPC分类号： F02C3/14
CPC分类号： F23R3/06 , F23R3/10 , F23R2900/03042
摘要： A gas turbine combustion chamber has a starter film for cooling the combustion chamber wall, and a combustion chamber head, into which cooling air can be introduced and which is confined to the combustion chamber by a heat shield (5). A base plate (2) is arranged at a certain distance from the heat shield (5) and the base plate (2) is provided with several openings (6) in its rim area for passing the cooling air. Center axes (17) of the openings (6) are inclined at a shallow angle (α) relative to the combustion chamber wall (4).
摘要翻译：燃气轮机燃烧室具有用于冷却燃烧室壁的起动膜和燃烧室头部，其中可以通过隔热罩（5）将冷却空气引入其中并被限制在燃烧室中。基板（2）与隔热板（5）隔开一定距离，基板（2）在其边缘区域设有多个开口（6），用于通过冷却空气。开口（6）的中心轴（17）相对于燃烧室壁（4）以较小的角度（α）倾斜。

5. 发明授权

US08938970B2 Gas-turbine combustion chamber with starter film for cooling the combustion chamber wall 有权
标题翻译：燃气轮机燃烧室具有用于冷却燃烧室壁的起动膜
公开(公告)号：US08938970B2
公开(公告)日：2015-01-27
申请号：US12815829
申请日：2010-06-15
申请人： Miklos Gerendas , Sermed Sadig
发明人： Miklos Gerendas , Sermed Sadig
IPC分类号： F02C1/00 , F23R3/06
CPC分类号： F23R3/06 , F23R3/10 , F23R2900/03042
摘要： A gas turbine combustion chamber has a starter film for cooling the combustion chamber wall, and a combustion chamber head, into which cooling air can be introduced and which is confined to the combustion chamber by a heat shield (5). A base plate (2) is arranged at a certain distance from the heat shield (5) and the base plate (2) is provided with several openings (6) in its rim area for passing the cooling air. Center axes (17) of the openings (6) are inclined at a shallow angle (α) relative to the combustion chamber wall (4).
摘要翻译：燃气轮机燃烧室具有用于冷却燃烧室壁的起动膜和燃烧室头部，其中可以通过隔热罩（5）将冷却空气引入其中并被限制在燃烧室中。基板（2）与隔热板（5）隔开一定距离，基板（2）在其边缘区域设有多个开口（6），用于通过冷却空气。开口（6）的中心轴（17）相对于燃烧室壁（4）以较小的角度（α）倾斜。

6. 发明授权

US08677757B2 Combustion chamber head of a gas turbine 失效
标题翻译：燃气轮机的燃烧室头部
公开(公告)号：US08677757B2
公开(公告)日：2014-03-25
申请号：US12774214
申请日：2010-05-05
申请人： Sermed Sadig , Miklos Gerendas
发明人： Sermed Sadig , Miklos Gerendas
IPC分类号： F02C1/00 , F02C7/24
CPC分类号： F23R3/04 , F23M20/005 , F23R3/283 , F23R2900/00014 , F23R2900/03041 , F23R2900/03042 , F23R2900/03043
摘要： A combustion chamber head of a gas turbine has a confinement enclosing a dampening volume (207) and including a combustion chamber-opposite confinement (206) and a combustion chamber-side confinement (210). The combustion chamber-side confinement (210) is provided as perforated wall (210). In the edge area of the combustion chamber-side confinement (210), cooling air can be routed onto the combustion chamber-side confinement (210) via recesses (203) in the confinement (206). This cooling air, which flows along the combustion chamber-side confinement (210), crosses the cooling air flow through the perforated wall (210) in the combustion chamber (101) without mixing with the latter, as both are separated by walls.
摘要翻译：燃气轮机的燃烧室头部具有封闭阻尼体积（207）并包括燃烧室相对限制件（206）和燃烧室侧限制件（210）的限制。燃烧室侧限制（210）设置为穿孔壁（210）。在燃烧室侧限制（210）的边缘区域中，冷却空气可以通过限制（206）中的凹槽（203）被引导到燃烧室侧限制件（210）上。沿着燃烧室侧限制（210）流动的这种冷却空气与通过燃烧室（101）中的穿孔壁（210）的冷却空气流相交而不与后者混合，因为两者都被壁分开。

7. 发明授权

US07059133B2 Dilution air hole in a gas turbine combustion chamber with combustion chamber tiles 失效
标题翻译：具有燃烧室砖的燃气轮机燃烧室内的稀释气孔
公开(公告)号：US07059133B2
公开(公告)日：2006-06-13
申请号：US10400553
申请日：2003-03-28
申请人： Miklos Gerendas
发明人： Miklos Gerendas
IPC分类号： F02C1/00 , F02G3/00
CPC分类号： F23R3/06 , F23R3/002 , F23R2900/03041
摘要： A gas turbine combustion chamber includes combustion chamber tiles 3 attached to a supporting structure 6 of the gas turbine combustion chamber, with each tile possessing at least one dilution air hole 4 which is flush with a dilution air hole of the supporting structure 6, wherein a diameter of the dilution air hole of the supporting structure 6 is considerably larger than a diameter 14 of the dilution air hole 4 of the combustion chamber tile 3.
摘要翻译：燃气轮机燃烧室包括安装在燃气轮机燃烧室的支撑结构6上的燃烧室瓦3，每个瓦片具有与支撑结构6的稀释气孔齐平的至少一个稀释气孔4，其中支撑结构6的稀释气孔的直径比燃烧室瓦3的稀释气孔4的直径14大得多。

8. 发明授权

US06901757B2 Heat shield arrangement with sealing element 失效
标题翻译：带有密封元件的隔热罩
公开(公告)号：US06901757B2
公开(公告)日：2005-06-07
申请号：US10291425
申请日：2002-11-12
申请人： Miklos Gerendas
发明人： Miklos Gerendas
IPC分类号： F23M5/00 , F23M5/04 , F23R3/00 , F02C7/24
CPC分类号： F23M5/04 , F23M5/00 , F23M2900/05005 , F23R3/002 , F23R2900/00012
摘要： A heat shield arrangement includes several tiles 1 and several fasteners 6 for attaching the tiles at a spaced distance to a wall 2 to form an interspace 4 between the wall and the tiles which can be supplied with cooling air. At least one sealing element 3 is positioned between adjacent tiles 1 to provide a seal between rims 5 of the adjacent tiles 1. The rims 5 of the tiles 1 which are to be sealed are maintained at a spaced distance from the wall 2 by the fasteners 6 and the sealing element 3 is positioned remotely from the wall 2 and in abutment with the rims 5 of the tiles 1, with the sealing element 3 being allowed to float over the rims 5.
摘要翻译：隔热罩装置包括多个瓦片1和几个紧固件6，用于将瓦片以间隔距离连接到壁2，以在壁和瓦片之间形成间隙4，间隙4可以被供应冷却空气。至少一个密封元件3定位在相邻的瓦片1之间，以在相邻的瓦片1的边缘5之间提供密封。待密封的瓦1的边缘5通过紧固件6保持与壁2间隔开的距离，并且密封元件3远离壁2定位并且与瓦1的边缘5邻接。密封元件3被允许在边缘5上浮动。

9. 发明授权

US06901756B2 Device for the injection of fuel into the flow wake of swirler vanes 失效
标题翻译：用于将燃料喷射到旋流器叶片的流动尾流中的装置
公开(公告)号：US06901756B2
公开(公告)日：2005-06-07
申请号：US10287718
申请日：2002-11-05
申请人： Miklos Gerendas , Thomas Doerr
发明人： Miklos Gerendas , Thomas Doerr
IPC分类号： F23R3/14 , F23R3/28
CPC分类号： F23R3/14 , F23R3/28
摘要： A device for the injection of fuel into the combustion chamber of a gas turbine includes at least one swirler (1) arranged in an air path with at least one swirler vane (2) and with at least one fuel injection nozzle (3), wherein the fuel injection nozzle (3) is arranged in a wake area of the swirler vane (2) and is separate from the swirler vane (2).
摘要翻译：用于将燃料喷射到燃气涡轮机的燃烧室中的装置包括至少一个与至少一个旋流器叶片（2）和至少一个燃料喷射喷嘴（3）在空气路径中布置的旋流器（1），其中燃料喷射喷嘴（3）布置在旋流器叶片（2）的尾流区域中并且与旋流器叶片（2）分离。

10. 发明申请

US20180272649A1 Multi-Layer NPR Structures 审中-公开
公开(公告)号：US20180272649A1
公开(公告)日：2018-09-27
申请号：US15542481
申请日：2016-01-09
申请人： Christopher BOOTH-MORRISON , Carl J. CARSON , Mehran FARHANGI , Miklos GERENDAS , Thomas Harold GILLESPIE , Matthew Christopher INNES , François-Xavier JETTE , Minh Quan PHAM , Fabian Enrique Sanchez GUERRERO , Megan SCHAENZER , Ali SHANIAN , Evelyne SMITH-ROBERGE , Benoit VILLIEN , President and Fellows of Harvard College
发明人： Katia Bertoldi , Matthew Christopher Innes , Farhad Javid , Minh Quan Pham , Megan Schaenzer , Ali Shanian , Michael J. Taylor
IPC分类号： B32B3/26 , B32B15/01 , B32B7/08
CPC分类号： B32B3/266 , B29C44/357 , B32B3/26 , B32B7/08 , B32B15/01 , C22C1/08 , C22C19/03 , C22C19/05 , C22C19/07
摘要： In some aspects, an auxetic structure includes a first sheet and a second sheet, the first sheet defining therein a plurality of first openings in a first pattern, the plurality of first openings providing a first porosity and the second sheet defining therein a plurality of second openings in a second pattern to provide a second porosity. The second sheet is positioned to overlay the first sheet so that the plurality of second openings at least partially occlude the plurality of first openings to define a plurality of third openings in a third pattern, the plurality of third openings defining a third porosity less than that of the first porosity or the second porosity. The second sheet is connected to the first sheet by a plurality of distinct connection elements.

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