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公开(公告)号：JP5615436B2
公开(公告)日：2014-10-29
申请号：JP2013521804
申请日：2011-07-12
Inventor： ポール エイチ チェース , ポール エイチ チェース , スタンリー ボグゼウスキー , スタンリー ボグゼウスキー
CPC classification number: F23D14/725 , F23N5/123 , F23N2027/36 , F23N2029/02 , F23N2029/12 , F23Q3/00 , F23Q9/00
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公开(公告)号：JP5615362B2
公开(公告)日：2014-10-29
申请号：JP2012524211
申请日：2010-08-09
Inventor： ドニ デュフルネ , ドニ デュフルネ , ペレ ミシェル , ミシェル ペレ , ダン リュシウス ペナシュ , ダン リュシウス ペナシュ
IPC: H01H33/91
CPC classification number: H01H33/901 , H01H2033/907 , H01H2033/908
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公开(公告)号：JP5615035B2
公开(公告)日：2014-10-29
申请号：JP2010115003
申请日：2010-05-19
Inventor： ベアケ オラフ , ベアケ オラフ , ヘリー フランツ−ヨーゼフ , ヘリー フランツ−ヨーゼフ , ミュラー カーステン , ミュラー カーステン , ヨハネス ゼフェリン クロペンブルク ラインハルト , ヨハネス ゼフェリン クロペンブルク ラインハルト
CPC classification number: F01K13/02
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公开(公告)号：JP2014178109A
公开(公告)日：2014-09-25
申请号：JP2014108278
申请日：2014-05-26
Inventor： JAMES W BIRMINGHAM , GLENN D MATTISON , JAMES D SEEBALD , KEVIN J O'BOYLE
IPC: F28D19/04
CPC classification number: F28D19/044 , F28D19/00 , F28F3/025
Abstract: PROBLEM TO BE SOLVED: To provide a heat transfer sheet useful in a rotary regenerative heat exchanger.SOLUTION: A heat transfer sheet for a rotary regenerative heat exchanger comprises: a plurality of sheet spacing members extending along the heat transfer sheet substantially parallel to a direction of a gas flow and defining a portion of a flow passage between two adjacent heat transfer sheets; and undulating surfaces disposed between sheet spacing members adjacent to each other and formed by lobes that become increasingly angled with respect to the sheet spacing members over the length of the heat transfer sheet.
Abstract translation: 要解决的问题：提供一种可用于旋转再生式热交换器的传热片。解决方案：一种用于旋转再生式热交换器的热转印片，包括：多个片材间隔部件，沿着传热片延伸，基本上平行于方向 气流并且限定两个相邻传热片之间的流动通道的一部分; 并且布置在彼此相邻并且由在热传递片的长度上相对于片材间隔部件变得越来越大角度的裂片形成的片材间隔部件之间的起伏表面。
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公开(公告)号：JP2014178026A
公开(公告)日：2014-09-25
申请号：JP2014012742
申请日：2014-01-27
Inventor： YOWELL JEFFERY EDWARD
Abstract: PROBLEM TO BE SOLVED: To provide a roller with geometrical characteristics that is more economical, easily manufactured and less time consuming in manufacture than machined rollers.SOLUTION: A roller 100 for forming heat transfer elements includes a central shaft 110 and a plurality of roller elements 120. Each roller element 120 has a geometrical characteristic formed along an outer periphery thereof. The roller elements 120 are cut from metallic sheets by a method such as laser cutting. The roller elements 120 stacked on the central shaft 110 configure the roller 100 with a circumferential surface 150 corresponding to the geometrical characteristic of the stacked roller elements 120.
Abstract translation: 要解决的问题：提供具有比加工辊更经济，容易制造和较少花费时间的几何特征的辊。解决方案：用于形成传热元件的辊100包括中心轴110和多个辊元件 每个滚子元件120具有沿其外周形成的几何特征。 通过诸如激光切割的方法从金属片切割滚子元件120。 堆叠在中心轴110上的辊元件120将辊100配置成具有对应于叠置的辊元件120的几何特性的圆周表面150。
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Patent Agency Ranking
公开(公告)号：JP2014173600A
公开(公告)日：2014-09-22
申请号：JP2014043975
申请日：2014-03-06
Inventor： OLIA HAMID , SCHLESIER JAN , MICHAEL BREITFELD , PHILIPP BRUNNER
CPC classification number: F01K23/10 , F01K13/02 , F01K23/101 , F02C6/18 , F05D2220/76 , F05D2270/061 , Y02E20/14 , Y02E20/16
Abstract: PROBLEM TO BE SOLVED: To operate a combined cycle power plant equipped with a gas turbine and a steam turbine at a minimum load without producing electric power which is supplied to an electric power system.SOLUTION: A gas turbine 2 is reduced in load to a condition where a compressor 3 is operated at its nominal speed, a steam turbine 12 is reduced in load in coordination with the load reduction of the gas turbine 2 to a condition where the total load exported by a plant 1 to an electric power system 21 is substantially equal to zero, and both the gas turbine 2 and a steam power generation system 10 are connected.
Abstract translation: 要解决的问题：在最小负荷下操作配备有燃气轮机和蒸汽轮机的联合循环发电厂，而不产生供应给电力系统的电力。解决方案：燃气轮机2的负载减小到 在压缩机3以其标称速度运行的情况下，蒸汽轮机12与燃气轮机2的负载减小协调地减小负载，使得由工厂1输出到电力系统21的总负载为 基本上等于零，并且燃气轮机2和蒸汽发电系统10都连接。
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公开(公告)号：JP2014169500A
公开(公告)日：2014-09-18
申请号：JP2014037977
申请日：2014-02-28
Inventor： HOEBEL MATTHIAS DR , ETTER THOMAS , KONTER MAXIME , JULIUS SCHURB
CPC classification number: B23K26/0093 , B22F3/1055 , B22F5/009 , B22F7/06 , B23P6/007 , B23P15/04 , B29C64/386 , B29C64/393 , Y02P10/295 , Y10T428/31678
Abstract: PROBLEM TO BE SOLVED: To provide a method for overcoming disadvantages in an additive manufacturing process such as selective laser melting (SLM).SOLUTION: The invention refers to a method for manufacturing a hybrid component (11) comprising the steps of a) manufacturing a preform (2) as a first part of the hybrid component (11), then b) successively building up on that preform (2) a second part of the component (11) from a metallic powder material (12) by means of an additive manufacturing process by scanning with an energy beam (14), thereby c) establishing a controlled grain orientation in primary and secondary directions of at least a part of the second part of the component (11), d) wherein the controlled secondary grain orientation is realized by applying a specific scanning pattern of the energy beam (14), which is aligned to the cross section profile of the component (11) or to the local load conditions for the component (11).
Abstract translation: 要解决的问题：提供一种在选择性激光熔化（SLM）等添加剂制造工艺中克服缺点的方法。解决方案：本发明涉及一种制造混合部件（11）的方法，包括以下步骤：a） 预成型件（2）作为混合部件（11）的第一部分，然后b）通过添加剂从金属粉末材料（12）连续地在该预制件（2）上建立部件（11）的第二部分， 通过用能量束（14）进行扫描，从而c）在部件（11）的第二部分的至少一部分的初级和次级方向建立受控的晶粒取向，d）其中受控次晶粒取向为 通过施加与部件（11）的横截面轮廓对准的能量束（14）的特定扫描图案或者对于部件（11）的局部负载条件来实现。
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公开(公告)号：JP2014109435A
公开(公告)日：2014-06-12
申请号：JP2013249278
申请日：2013-12-02
Inventor： THOMAS MICHAEL MAURER , URS BENZ , MIRKO RUBEN BOTHIEN
CPC classification number: F23R3/42 , F05D2260/963 , F23M20/005 , F23R3/00 , F23R3/002 , F23R2900/00014
Abstract: PROBLEM TO BE SOLVED: To provide a near-wall cooling system for a damping device of a gas turbine combustor with significantly reduced cooling air mass flow requirements.SOLUTION: An end plate 10 separating a damping volume 9 from a combustion chamber 3 is fixed to an inner wall 5. The end plate 10 is provided with a neck passage 13, and additionally provided with at least one feed plenum 12, 15 for a cooling medium, at least one exit plenum 16 for the cooling medium, and at least one cooling passage 14 enabling a flow of the cooling medium from at least one first feed plenum 12 to a second feed plenum 15 or to the at least one exit plenum 16.
Abstract translation: 要解决的问题：提供一种用于燃气轮机燃烧器的阻尼装置的近壁冷却系统，其具有显着降低的冷却空气质量流量要求。解决方案：将阻尼容积9与燃烧室3分离的端板10固定到 端壁10设置有颈部通道13，并且另外设置有用于冷却介质的至少一个进料室12,15，用于冷却介质的至少一个出口加压室16和至少一个冷却 通道14使冷却介质从至少一个第一进料室12流到第二进料室15或至少一个出口集气室16。
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公开(公告)号：JP2014092162A
公开(公告)日：2014-05-19
申请号：JP2013226285
申请日：2013-10-31
Inventor： URS BENZ , CHRISTOPH APPEL , OLIVER KONRADT , IVAN LENUZZI , ALEN MARKOVIC
CPC classification number: F23R3/002 , F23M5/085 , F23R3/005 , F23R3/06 , F23R2900/00012 , F23R2900/03044
Abstract: PROBLEM TO BE SOLVED: To improve cooling efficiency, lifetime and assembly and disassembly of an impingement-cooled hot gas segment arrangement.SOLUTION: A hot gas segment arrangement includes a hot gas segment, which is removably mounted on a carrier and is subjected at its outside to hot gas and impingement-cooled at its inside. An impingement plate with a plurality of distributed impingement holes is arranged at a distance inside the hot gas segment. Cooling air supply means is provided for loading the impingement plate with pressurized cooling air in order to generate through the impingement holes jets of cooling air, which impinge on the inside of the hot gas segment. The impingement plate is part of a closed receptacle which is supplied with the pressurized cooling air, and the receptacle with the impingement plate is mounted on the carrier independently of the hot gas segment.
Abstract translation: 要解决的问题：提高冷却效率，寿命以及冲击冷却热气体段装置的组装和拆卸。解决方案：热气体段装置包括热气体段，其可拆卸地安装在载体上并经受其 外面是热气体并在其内部进行冲击冷却。 具有多个分布式冲击孔的冲击板布置在热气体段内一段距离处。 提供冷却空气供应装置用于将冲击板加载加压的冷却空气，以便通过撞击在热气体段内部的冷却空气的冲击孔产生。 冲击板是封闭的容器的一部分，其被供应加压的冷却空气，并且具有冲击板的容器独立于热气体段安装在载体上。
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公开(公告)号：JP2014085109A
公开(公告)日：2014-05-12
申请号：JP2013222232
申请日：2013-10-25
Inventor： JOHN PHILIP WOOD , ANDREA CIANI , ANDRE THEUER , PENNELL DOUGLAS ANTHONY , EWALD FREITAG
CPC classification number: F23R3/20 , F02C6/003 , F02C6/02 , F05D2250/12 , F05D2250/13 , F23R3/12 , F23R3/16 , F23R3/18 , F23R3/34 , F23R3/346 , F23R2900/03341
Abstract: PROBLEM TO BE SOLVED: To reduce or avoid limitations in design of downstream components, such as combustion chamber and turbine components, when utilizing a limited burner exit area.SOLUTION: A reheat burner arrangement includes a center body, an annular duct with a prescribed cross-section area, and an intermediate fuel injection plane located along the center body and actively connected to the cross section area of the annular duct. The center body is located upstream of a combustion chamber. The structure of the reheat burner arrangement is defined by various different parameters, and the structure of the reheat burner arrangement is defined by various interrelations.
Abstract translation: 要解决的问题：为了减少或避免在使用有限燃烧器出口区域时下游部件（例如燃烧室和涡轮机部件）的设计上的限制。解决方案：再热燃烧器装置包括中心体，具有规定交叉的环形管道 以及中心燃料喷射平面，该中间燃料喷射平面沿中心体定位并且主动地连接到环形导管的横截面区域。 中心体位于燃烧室的上游。 再热燃烧器装置的结构由各种不同的参数来定义，再热燃烧装置的结构由各种相互关系定义。
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