ADAPTIVE MACHINING TURBOMACHINE BLADE SHROUD HARD FACE
    3.
    发明申请
    ADAPTIVE MACHINING TURBOMACHINE BLADE SHROUD HARD FACE 有权
    自适应加工涡轮机叶片硬质面

    公开(公告)号:US20170044900A1

    公开(公告)日:2017-02-16

    申请号:US14824566

    申请日:2015-08-12

    Abstract: A system for adaptively machining a shroud of a blade used in a turbomachine is provided. The system may include a computer system including a module(s) configured to: extract geometric location data from a 3D model of the shroud after use in the turbomachine, the 3D model created by digitizing using a digitizing device. The geometric location data includes geometric location data of a hard face plane of the shroud exposed to wear during turbomachine operation and of a non-worn surface adjacent to the hard face plane substantially unexposed to wear during turbomachine operation. Comparing the geometric location data of the non-worn surface from the three-dimensional model to a manufacturing model of the blade determines a change in position of the non-worn surface from use of the blade in the turbomachine. The change in position is used to modify a machining instruction used by a machining device to repair the hard face plane.

    Abstract translation: 提供一种用于自动加工用于涡轮机中的叶片的护罩的系统。 该系统可以包括计算机系统,其包括被配置为:在使用涡轮机之后从护罩的3D模型中提取几何位置数据的模块,通过使用数字化装置进行数字化创建的3D模型。 几何位置数据包括在涡轮机操作期间暴露于磨损的护罩的硬面平面的几何位置数据和在涡轮机操作期间基本上未暴露于磨损的与硬面平面相邻的未磨损表面。 将来自三维模型的非磨损表面的几何位置数据与刀片的制造模型进行比较,确定在磨损机器中使用刀片时未磨损表面的位置的变化。 位置变化用于修改加工装置使用的加工指令来修复硬面平面。

    PRESSURE MASKERS AND PRESSURE MASKING SYSTEMS
    5.
    发明申请
    PRESSURE MASKERS AND PRESSURE MASKING SYSTEMS 有权
    压力屏蔽和压力屏蔽系统

    公开(公告)号:US20130174923A1

    公开(公告)日:2013-07-11

    申请号:US13826017

    申请日:2013-03-14

    Abstract: Pressure maskers for masking at least one passageway of an article include a body portion that surrounds at least a portion of the article around the at least one passageway, at least one fluid inlet connected to the body portion that provides a conduit for pressurized masking fluid to pass from an exterior of the pressure masker to an interior of the pressure masker, wherein the article is at least partially disposed within the interior of the pressure masker, and at least one seal that seals the body portion at least partially around the article such that the pressurized masking fluid that enters the interior of the pressure masker is at least partially forced through the at least one passageway.

    Abstract translation: 用于掩蔽制品的至少一个通道的压力掩模包括围绕所述至少一个通道围绕所述制品的至少一部分的主体部分,连接到所述主体部分的至少一个流体入口,其提供用于加压掩蔽流体的管道 从压力屏蔽器的外部通过到压力掩蔽器的内部,其中制品至少部分地设置在压力掩蔽器的内部,以及至少一个密封件,其至少部分地围绕物品密封身体部分,使得 进入压力屏蔽器内部的加压掩模流体至少部分地被迫穿过至少一个通道。

    COOLING HOLE CLEANING METHOD AND APPARATUS
    7.
    发明申请
    COOLING HOLE CLEANING METHOD AND APPARATUS 有权
    冷却孔清洁方法和装置

    公开(公告)号:US20170058695A1

    公开(公告)日:2017-03-02

    申请号:US15349283

    申请日:2016-11-11

    Abstract: Blockages of turbomachine cooling circuit cooling holes resulting from coating processes can be removed by introducing a cleaning agent into the cooling circuit. The cooling circuit can be connected to a cleaning agent supply under pressure, adding force on the blockage to chemical action by the cleaning agent. The cleaning agent is chemically reactive with the coating material and substantially chemically non-reactive with the underlying material of the cooling circuit and other parts of the turbomachine. A neutralization agent can also be introduced to reduce toxicity and/or action of the cleaning agent. A turbomachine cooling hole cleaning method includes introducing a cleaning agent into a cooling circuit of a turbomachine part, pressurizing the cleaning agent in the cooling circuit until a first defined condition is met, and introducing a neutralization agent to the turbomachine part while the cleaning agent is applied to the cooling circuit.

    Abstract translation: 可以通过将清洁剂引入冷却回路来除去由涂布过程产生的涡轮机冷却回路冷却孔的堵塞。 冷却回路可以在压力下连接到清洁剂供应源上,从而增加阻塞作用力,使清洁剂产生化学作用。 清洁剂与涂层材料具有化学反应性,并且与冷却回路和涡轮机的其它部分的基础材料基本上化学上不反应。 还可以引入中和剂以减少清洁剂的毒性和/或作用。 涡轮机冷却孔清洗方法包括将清洗剂引入到涡轮机部件的冷却回路中,对冷却回路中的清洗剂进行加压,直到满足第一限定条件,并将中和剂引入涡轮机部件,同时清洗剂为 应用于冷却回路。

    METHOD FOR REMOVING AN END CAP OF A COMBUSTOR CAP ASSEMBLY
    10.
    发明申请
    METHOD FOR REMOVING AN END CAP OF A COMBUSTOR CAP ASSEMBLY 审中-公开
    用于移除燃烧器盖组件的端盖的方法

    公开(公告)号:US20150059177A1

    公开(公告)日:2015-03-05

    申请号:US14010638

    申请日:2013-08-27

    CPC classification number: F23R3/46 F23R3/60 F23R2900/00019 Y10T29/49346

    Abstract: A method for removing an end cap assembly from a combustor cap assembly includes inserting a push rod through an opening in a back plate portion of the cap assembly. One end of the push rod is engaged with a radial support feature of the end cap assembly and a substantially linear force is applied to the push rod. The force is distributed to the radial support feature, thereby preventing damage to a cap plate portion of the end cap assembly.

    Abstract translation: 从燃烧器盖组件移除端盖组件的方法包括将推杆穿过盖组件的后板部分中的开口插入。 推杆的一端与端盖组件的径向支撑部件接合,并且基本上线性的力被施加到推杆上。 力被分配到径向支撑特征,从而防止对端盖组件的盖板部分的损坏。

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