公开(公告)号：US20060073348A1

公开(公告)日：2006-04-06

申请号：US10959843

申请日：2004-10-06

Applicant: Gilbert Farmer ,  James Groeschen

Inventor： Gilbert Farmer ,  James Groeschen

IPC: B32B15/04

CPC classification number: C25D5/022 ,  C09D5/44 ,  C25D7/00 ,  C25D13/04 ,  F23D2213/00 ,  F23R2900/00018 ,  Y10T428/31678

Abstract: A method of applying a wear coat to a surface portion of a fuel assembly. The engine component is dipped in wax and a desired portion of the wax is removed with a fluid. The removed wax exposes a surface of the component. This surface can then be electroplated with a wear coat while the non-exposed surfaces are protected from electrodeposition.

Abstract translation: 将耐磨涂层施加到燃料组件的表面部分的方法。 将发动机部件浸入蜡中，用流体除去蜡的所需部分。 去除的蜡暴露组件的表面。 然后可以用耐磨涂层对该表面进行电镀，同时防止未暴露的表面电沉积。

公开(公告)号：US20070119182A1

公开(公告)日：2007-05-31

申请号：US11290115

申请日：2005-11-30

Applicant: Robert Czachor ,  James Groeschen ,  Jason Hoppa

Inventor： Robert Czachor ,  James Groeschen ,  Jason Hoppa

IPC: F23R3/60

CPC classification number: F02C3/14 ,  F01D25/28 ,  F05D2230/60 ,  F05D2230/642 ,  F23R3/60

Abstract: A method for assembling a gas turbine engine includes coupling a first structure within the gas turbine engine, wherein the first structure includes a plurality of sockets extending from a radially outer surface of the first structure, and coupling a second structure to the first structure by inserting a radial pin through the second structure and into each respective socket such that the first structure is aligned axially, circumferentially, and with respect to an engine centerline axis extending through the gas turbine engine, where the position of the pins relative to the second structure is adjustable.

Abstract translation: 一种用于组装燃气涡轮发动机的方法，包括联接在燃气涡轮发动机内的第一结构，其中第一结构包括从第一结构的径向外表面延伸的多个插座，并且通过插入第二结构将第二结构 径向销穿过第二结构并进入每个相应的插座，使得第一结构沿轴向，周向地和相对于延伸穿过燃气涡轮发动机的发动机中心线轴线对准，其中销相对于第二结构的位置是 可调。