公开(公告)号：US09561555B2

公开(公告)日：2017-02-07

申请号：US13729286

申请日：2012-12-28

Applicant: United Technologies Corporation

Inventor： James M. Koonankeil ,  Edward F. Pietraszkiewicz ,  Karl A. Schachtner ,  Kevin J. Klinefelter ,  Markus W. Fritch ,  Jason Daley

IPC: B23H1/00 ,  F01D5/18 ,  B23H7/26 ,  B23H7/30 ,  B23H9/10

CPC classification number: B23H1/00 ,  B23H7/265 ,  B23H7/30 ,  B23H9/10 ,  F01D5/187 ,  F05D2230/12 ,  F05D2240/12 ,  F05D2240/81 ,  Y02T50/676 ,  Y10T29/49323 ,  Y10T29/49341

Abstract: A method of machining cooling holes in a component includes the steps of inserting an electro discharge machining guide that houses an electrode into an internal cavity of a component, and machining a cooling hole into a wall of the component with the electrode. A gas turbine engine component includes first and second spaced apart walls providing an internal cavity. The first wall has outer and inner surfaces. The inner surface faces the internal cavity. A cooling hole extends through the first wall from the inner surface to the outer surface. The cooling hole includes entry and exit openings respectively provided in the inner and outer surfaces. The exit opening includes a cross-sectional area that is smaller than a cross-sectional area of the entry opening.

Abstract translation: 在部件中加工冷却孔的方法包括以下步骤：将容纳电极的放电加工引导件插入部件的内部空腔中，并用电极将冷却孔加工到部件的壁中。 燃气涡轮发动机部件包括提供内腔的第一和第二隔开的壁。 第一个墙壁有外表面和内表面。 内表面面向内腔。 冷却孔从内表面到外表面延伸穿过第一壁。 冷却孔包括分别设置在内表面和外表面上的入口和出口。 出口开口包括比入口开口的横截面面积小的横截面面积。

公开(公告)号：US09470605B2

公开(公告)日：2016-10-18

申请号：US14183807

申请日：2014-02-19

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： James M. Koonankeil

IPC: G01M15/14 ,  G01N25/72 ,  F01D21/00 ,  G01M99/00 ,  F01D5/00 ,  F01D5/18 ,  F01D5/28

CPC classification number: G01M15/14 ,  F01D5/005 ,  F01D5/186 ,  F01D5/288 ,  F01D21/003 ,  F05D2220/32 ,  F05D2260/202 ,  F05D2260/83 ,  G01M99/002 ,  G01N25/72

Abstract: An airfoil has an of internal cooling channel, and cooling holes extending from the internal cooling channel to an outer skin. Air is injected into the cooling channel, and then into an inlet of the cooling hole. The exit of the air from an outlet of the cooling hole at the outer skin is monitored to determine whether the outlet is blocked. A location of the inlet of the cooling hole is determined by utilizing the determined location of the outlet, in combination with a known angle through which the cooling hole extends.

Abstract translation: 机翼具有内部冷却通道，以及从内部冷却通道延伸到外部皮肤的冷却孔。 将空气注入冷却通道，然后进入冷却孔的入口。 监测空气从外皮的冷却孔的出口的出口，以确定出口是否被堵塞。 通过利用确定的出口位置与冷却孔延伸通过的已知角度的组合来确定冷却孔入口的位置。

公开(公告)号：US20150315930A1

公开(公告)日：2015-11-05

申请号：US14702840

申请日：2015-05-04

Applicant: United Technologies Corporation

Inventor： James M. Koonankeil ,  Edward F. Pietraszkiewicz

IPC: F01D25/12

CPC classification number: F01D25/12 ,  F01D5/186 ,  F01D5/187 ,  F05D2220/32 ,  F05D2230/20 ,  Y10T29/49236

Abstract: An airfoil body includes an airfoil wall defined between an internal cavity surface and an external airfoil surface. A pad extends from the internal cavity surface. A cooling hole extends from the external airfoil surface, through the airfoil wall and through the pad for fluid communication through the airfoil wall.

Abstract translation: 翼型体包括限定在内腔表面和外部翼面之间的翼型壁。 垫从内腔表面延伸。 冷却孔从外部翼面表面延伸穿过翼型壁并穿过垫，以便通过翼型壁流体连通。

公开(公告)号：US20140294136A1

公开(公告)日：2014-10-02

申请号：US14219106

申请日：2014-03-19

Applicant: United Technologies Corporation

Inventor： James M. Koonankeil ,  Gordon Miller Reed ,  Rodney H. Warner

IPC: G01N23/04

CPC classification number: G01N23/046 ,  G01N2223/63

Abstract: A method of non-destructively inspecting an article includes scanning an article to produce a computerized three-dimensional representation of an internal feature of the article. A measurement characteristic of the internal feature is then generated from a plurality of cross-sections through the computerized three-dimensional representation of the internal feature. The measurement characteristic is then used to determine whether the internal feature meets a design criterion.

Abstract translation: 不破坏性地检查物品的方法包括扫描物品以产生物品的内部特征的计算机化三维表示。 然后通过内部特征的计算机化三维表示从多个横截面产生内部特征的测量特性。 然后测量特性用于确定内部特征是否符合设计标准。

公开(公告)号：US20140183164A1

公开(公告)日：2014-07-03

申请号：US13729328

申请日：2012-12-28

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： James M. Koonankeil ,  Markus W. Fritch ,  Jason Daley ,  Edward F. Pietraszkiewicz ,  Karl A. Schachtner ,  Kevin J. Klinefelter

IPC: B23H1/04

CPC classification number: B23H1/04 ,  B23H7/26 ,  B23H9/10 ,  B23H9/14

Abstract: An electro discharge machining system includes a guide having first and second portions that are non-colinear with respect to one another. A consumable electrode is housed within the guide and configured to drill cooling holes in a component. A controller is programmed to position the guide and electrode to a desired position with respect to the component. An electro discharge machining guide includes first and second portions that are non-colinear with respect to one another and that include a passage configured to receive an electrode.

Abstract translation: 放电加工系统包括具有相对于彼此不共线的第一和第二部分的引导件。 消耗性电极容纳在引导件内并构造成钻出部件中的冷却孔。 编程控制器以将引导件和电极相对于部件定位到期望的位置。 电放电加工引导件包括相对于彼此非共线的第一和第二部分，并且包括构造成接收电极的通道。