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    INSERT ELEMENT FOR CLOSING AN OPENING INSIDE A WALL OF A HOT GAS PATH COMPONENT OF A GAS TURBINE AND METHOD FOR ENHANCING OPERATIONAL BEHAVIOUR OF A GAS TURBINE
    3.
    发明申请
    INSERT ELEMENT FOR CLOSING AN OPENING INSIDE A WALL OF A HOT GAS PATH COMPONENT OF A GAS TURBINE AND METHOD FOR ENHANCING OPERATIONAL BEHAVIOUR OF A GAS TURBINE 有权
    用于封闭气体涡轮机的热气道组件内的开启的插入元件和用于增强气体涡轮机的操作行为的方法

    公开(公告)号：US20140147251A1

    公开(公告)日：2014-05-29

    申请号：US14087569

    申请日：2013-11-22

    Applicant: ALSTOM Technology Ltd

    Inventor： Felix REINERT ,  Guenter Ambrosy ,  Matthias Hoebel ,  Jeffrey De Jonge

    IPC: F02C7/24

    CPC classification number: F23R3/007 ,  F23R3/002 ,  F23R2900/00005 ,  F23R2900/00014 ,  Y10T29/49318

    Abstract: The invention refers an insert element for closing an opening inside a wall of a hot gas path component of a gas turbine. The insert includes a plate like body with an opening sided surface. The surface provides at least one first area which projects beyond at least one second area of said surface which surrounds the at least one first area frame-like. The at least one first area is encompassed by a circumferential edge corresponding in form and size to the opening such that the circumferential edge and the opening contour limit a gap at least in some areas, while the at least one second area contacts directly or indirectly the wall of the hot gas path component at a rear side facing away from the hot gas path. The plate like body provides at least a first functional layer-system, providing at least one layer made of heat resistant material, defining the first area of the surface (S).

    Abstract translation: 本发明涉及一种用于关闭燃气轮机的热气路径部件的壁内的开口的插入元件。 插入件包括具有开口侧表面的板状主体。 所述表面提供至少一个第一区域，其突出超过所述表面的至少一个第二区域，所述至少一个第二区域围绕所述至少一个第一区域框架状。 所述至少一个第一区域被围绕所述开口的形式和尺寸对应的圆周边缘包围，使得所述周边边缘和所述开口轮廓至少在一些区域中限制间隙，而所述至少一个第二区域直接或间接地接触 所述热气体路径部件的壁位于远离热气体路径的后侧。 板状体提供至少第一功能层系统，提供限定表面（S）的第一区域的至少一层由耐热材料制成的层。

    METHOD FOR POST-WELD HEAT TREATMENT OF WELDED COMPONENTS MADE OF GAMMA PRIME STRENGTHENED SUPERALLOYS
    5.
    发明申请
    METHOD FOR POST-WELD HEAT TREATMENT OF WELDED COMPONENTS MADE OF GAMMA PRIME STRENGTHENED SUPERALLOYS 有权
    焊接组件的焊后热处理方法加强加强超级合金

    公开(公告)号：US20140366995A1

    公开(公告)日：2014-12-18

    申请号：US14306348

    申请日：2014-06-17

    Applicant: ALSTOM Technology Ltd.

    Inventor： Thomas Etter ,  Daniel Beckel ,  Thomas Opderbecke ,  Guenter Ambrosy

    IPC: B23K37/00 ,  C21D9/50 ,  C22F1/10

    CPC classification number: C21D9/505 ,  B23K31/02 ,  B23K2101/001 ,  C22F1/10 ,  F01D5/005

    Abstract: The invention relates to a method of post-weld heat treatment of a without a filler material electron beam or laser welded high strength component made of a gamma prime (γ′) strengthened superalloy based on Ni or Co or Fe or combinations thereof. The method consists of the following stepsa) providing the welded component, thenb) heating the welded component by applying a rapid heating-up rate in the range of about 20 to 40° C./min during the entire temperature range from RT up to a temperature T1 of at least 1000° C., thenc) holding the welded component at T1 and then heating the component by applying a slow heating-up rate of about 5° C./min to a final temperature Tf, thend) holding the welded component at Tf for a time tf, wherein isothermal dwell time tf is sufficient for at least partially dissolving the gamma prime phase in the weld and also in the base material surrounding the weld; thene) cooling the component with a cooling rate of about 20° C./min andf) finally optionally applying a precipitation hardening treatment according to the known state of the art

    Abstract translation: 本发明涉及一种无需填充材料电子束或基于Ni或Co或Fe的γ'（γ'）强化超级合金或其组合制成的激光焊接高强度部件的焊后热处理方法。 该方法包括以下步骤：a）提供焊接部件，然后b）通过在从RT向上的整个温度范围内施加约20至40℃/分钟范围内的快速加热速率来加热焊接部件 然后c）将焊接成分保持在T1，然后通过施加约5℃/分钟的缓慢加热速率至最终温度Tf来加热组分，然后d ）将Tf上的焊接部件保持一段时间tf，其中等温停留时间tf足以至少部分地将伽马质相溶解在焊缝中以及围绕焊缝的基体材料中; 然后e）以约20℃/ min的冷却速度冷却组分，f）最后根据已知的现有技术任选地进行沉淀硬化处理

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