公开(公告)号：US20150003975A1

公开(公告)日：2015-01-01

申请号：US14491040

申请日：2014-09-19

Applicant: ALSTOM Technology Ltd

Inventor： Sergey SHCHUKIN ,  Robert MARMILIC

IPC: F02C7/12

CPC classification number: F02C7/12 ,  F01D5/18 ,  F01D5/187 ,  F01D25/12 ,  F05D2240/127 ,  F05D2260/2212 ,  F05D2260/22141

Abstract: The disclosure pertains to a cooled wall for separating a hot gas flow path of a gas turbine from a cooling flow including at least one turbulator rib extending from the wall into the cooling flow, and having a height, a width for providing heat transfer enhancement for the cooled wall. The turbulator rib has filets at its root with a filet radius. In order to increase the heat transfer enhancement of the turbulator rib, the filet at the downstream side of turbulator rib is extending into the cooled wall with a penetration depth. Further, the disclosure relates to specific embodiments in which the cooled wall with turbulator ribs is configured as the sidewall of an airfoil, a combustor wall or a heat shield.

Abstract translation: 本发明涉及一种用于将燃气涡轮机的热气体流路与冷却流分离的冷却壁，所述冷却流包括从壁延伸到冷却流中的至少一个湍流肋，并且具有高度，用于提供热传递增强的宽度 冷却的墙壁。 湍流肋在其根部具有锉刀半径。 为了增加湍流肋的传热增强，在湍流肋的下游侧的file口延伸到具有穿透深度的冷却壁中。 此外，本公开涉及其中具有湍流肋的冷却壁被构造为翼型，燃烧器壁或隔热罩的侧壁的具体实施例。

公开(公告)号：US20160076390A1

公开(公告)日：2016-03-17

申请号：US14837078

申请日：2015-08-27

Applicant: ALSTOM Technology Ltd

Inventor： Robert MARMILIC ,  Sergey SHCHUKIN

IPC: F01D9/04 ,  F01D25/12

CPC classification number: F01D9/042 ,  F01D5/14 ,  F01D5/147 ,  F01D5/18 ,  F01D5/187 ,  F01D5/189 ,  F01D5/28 ,  F01D9/041 ,  F01D11/005 ,  F01D25/12 ,  F05D2220/32 ,  F05D2240/12 ,  F05D2240/55 ,  F05D2240/81 ,  F05D2260/201

Abstract: The invention relates to a mounting and sealing arrangement for a guide vane of a gas turbine, which includes a vane carrier for carrying said vanes in a ring-like arrangement, whereby the vanes each comprise an airfoil and an outer diameter platform. The thermal stress is reduced and lifetime improved by providing a separate intermediate mounting element between the vane carrier and the outer diameter platform of each of the vanes, and mounting the intermediate mounting element with an outer side on the vane carrier, whereby the intermediate mounting element abuts with an inner side on the outer diameter platform in a sealing fashion.

Abstract translation: 本发明涉及一种用于燃气轮机的导向叶片的安装和密封装置，其包括用于将所述叶片以环状装置承载的叶片载体，由此叶片各自包括翼型件和外径平台。 通过在叶片承载件和每个叶片的外径平台之间设置单独的中间安装元件，并将中间安装元件安装在叶片承载件上的外侧，从而降低了热应力并提高了使用寿命，从而中间安装元件 以密封方式与外径平台上的内侧邻接。