公开(公告)号：US09957824B2

公开(公告)日：2018-05-01

申请号：US14776473

申请日：2014-03-14

Applicant: United Technologies Corporation

Inventor： Carl Brian Klinetob ,  Stephen J. Lindahl ,  Myron L. Klein ,  Andrew Pope ,  William Richard Ganoe, Jr. ,  Thomas D. Kasprow ,  Douglas J. Morgan

IPC: F01D5/16 ,  F01D9/04 ,  F01D5/26 ,  F01D25/06

CPC classification number: F01D9/041 ,  F01D5/16 ,  F01D5/26 ,  F01D25/06 ,  F05D2230/60 ,  F05D2240/12 ,  F05D2240/123 ,  F05D2240/124 ,  F05D2260/96 ,  F05D2300/121 ,  F05D2300/171

Abstract: A stationary guide vane includes a top platform, a bottom platform, and a vane body located between the top platform and the bottom platform. The vane body includes one or more cavities formed on a side wall of the vane body. One or more of the cavities are filled with vibration damping material and a vane cover is bonded to the vane body over the one or more containers.

公开(公告)号：US20170292530A1

公开(公告)日：2017-10-12

申请号：US15095441

申请日：2016-04-11

Applicant: United Technologies Corporation

Inventor： Andrew Pope

IPC: F04D29/38 ,  B32B15/14 ,  B32B15/04 ,  F04D29/32

CPC classification number: F04D29/388 ,  B32B15/043 ,  B32B15/14 ,  B32B2262/103 ,  B32B2262/106 ,  B32B2603/00 ,  F01D5/147 ,  F01D5/282 ,  F04D29/325 ,  Y02T50/672

Abstract: The present disclosure provides methods and systems for an airfoil of a gas turbine engine. An airfoil of a gas turbine engine may comprise an airfoil body having a body contact surface, and an airfoil edge coupled to the body contact surface, wherein at least one of the airfoil body or airfoil edge comprises a fiber metal laminate.

公开(公告)号：US20150369067A1

公开(公告)日：2015-12-24

申请号：US14765274

申请日：2014-03-10

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Andrew Pope ,  John P. Lucashu ,  Jason Leroux ,  Carl Brian Klinetob ,  Thomas B. Hyatt

IPC: F01D9/02

CPC classification number: F01D9/02 ,  F01D9/042 ,  F01D25/246 ,  F01D25/28 ,  F02C7/20 ,  F05D2220/32 ,  F05D2230/60 ,  F05D2240/80 ,  F05D2260/94 ,  Y02T50/671 ,  Y02T50/673

Abstract: A guide vane includes an airfoil with a first end and a second end. A platform is disposed at a first end of the airfoil, and a K-gusset is disposed on the platform opposite the airfoil. The K-gusset includes four bosses and ribs extending between the bosses in a “K” configuration.

Abstract translation: 导向叶片包括具有第一端和第二端的翼型件。 在翼型件的第一端设置有平台，并且在与翼型件相对的平台上设置有K型角撑板。 K型角撑板包括在“K”构型的凸台之间延伸的四个凸台和肋条。

公开(公告)号：US20210156825A1

公开(公告)日：2021-05-27

申请号：US16690639

申请日：2019-11-21

Applicant: United Technologies Corporation

Inventor： David R. Lyders ,  Andrew Pope ,  Christopher Avery ,  Daniel A. Rodrigues

IPC: G01N29/11 ,  G01N29/30

Abstract: An inspection feature for an adhesive bond portion between parts of a component comprising the inspection feature extending from a surface of the part of the component a predetermined bond line thickness, the inspection feature having a density configured to imitate a defect of the adhesive bond portion responsive to a non-destructive inspection scan.

公开(公告)号：US10947989B2

公开(公告)日：2021-03-16

申请号：US16597644

申请日：2019-10-09

Applicant: United Technologies Corporation

Inventor： Andrew Pope

IPC: F04D29/38 ,  F04D29/32 ,  B32B15/14 ,  B32B15/04 ,  F01D5/14 ,  F01D5/28

Abstract: The present disclosure provides methods and systems for an airfoil of a gas turbine engine. An airfoil of a gas turbine engine may comprise an airfoil body having a body contact surface, and an airfoil edge coupled to the body contact surface, wherein at least one of the airfoil body or airfoil edge comprises a fiber metal laminate.

公开(公告)号：US10087766B2

公开(公告)日：2018-10-02

申请号：US14765274

申请日：2014-03-10

Applicant: United Technologies Corporation

Inventor： Andrew Pope ,  John P. Lucashu ,  Jason Leroux ,  Carl Brian Klinetob ,  Thomas B. Hyatt

IPC: F03D11/04 ,  F03B3/18 ,  F03D1/04 ,  F03D3/04 ,  F01D9/02 ,  F01D9/04 ,  F01D25/24 ,  F01D25/28 ,  F02C7/20

Abstract: A guide vane includes an airfoil with a first end and a second end. A platform is disposed at a first end of the airfoil, and a K-gusset is disposed on the platform opposite the airfoil. The K-gusset includes four bosses and ribs extending between the bosses in a “K” configuration.

公开(公告)号：US20160333710A1

公开(公告)日：2016-11-17

申请号：US14776473

申请日：2014-03-14

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Carl Brian Klinetob ,  Stephen J. Lindahl ,  Myron L. Klein ,  Andrew Pope ,  William Richard Ganoe, JR. ,  Thomas D. Kasprow ,  Douglas J. Morgan

IPC: F01D9/04 ,  F01D25/06

CPC classification number: F01D9/041 ,  F01D5/16 ,  F01D5/26 ,  F01D25/06 ,  F05D2230/60 ,  F05D2240/12 ,  F05D2240/123 ,  F05D2240/124 ,  F05D2260/96 ,  F05D2300/121 ,  F05D2300/171

Abstract: A stationary guide vane includes a top platform, a bottom platform, and a vane body located between the top platform and the bottom platform. The vane body includes one or more cavities formed on a side wall of the vane body. One or more of the cavities are filled with vibration damping material and a vane cover is bonded to the vane body over the one or more containers.

Abstract translation: 固定导叶包括顶部平台，底部平台和位于顶部平台和底部平台之间的叶片体。 叶片体包括形成在叶片体的侧壁上的一个或多个空腔。 一个或多个空腔填充有减震材料，并且叶片盖在一个或多个容器上结合到叶片主体。

公开(公告)号：US11053953B2

公开(公告)日：2021-07-06

申请号：US15886121

申请日：2018-02-01

Applicant: United Technologies Corporation

Inventor： Andrew Pope

IPC: F01D5/14 ,  B32B15/04 ,  F04D29/54 ,  F02K3/06 ,  B32B15/14 ,  F01D9/04

Abstract: A structural guide vane including a vane body contact surface and a vane edge, wherein at least one of the vane body contact surface or the vane edge comprises a fiber metal laminate.

公开(公告)号：US20190234424A1

公开(公告)日：2019-08-01

申请号：US15886121

申请日：2018-02-01

Applicant: United Technologies Corporation

Inventor： Andrew Pope

IPC: F04D29/54 ,  F02K3/06 ,  B32B15/14

CPC classification number: F04D29/542 ,  B32B15/043 ,  B32B15/14 ,  B32B2603/00 ,  F01D9/041 ,  F02K3/06 ,  F05D2220/32 ,  F05D2230/10 ,  F05D2230/31 ,  F05D2240/12 ,  F05D2300/173 ,  F05D2300/174 ,  F05D2300/603

Abstract: A structural guide vane including a vane body contact surface and a vane edge, wherein at least one of the vane body contact surface or the vane edge comprises a fiber metal laminate.

公开(公告)号：US20180058469A1

公开(公告)日：2018-03-01

申请号：US15245137

申请日：2016-08-23

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Andrew Pope ,  Peter V. Tomeo

IPC: F04D29/38 ,  F04D19/00 ,  F04D29/34 ,  F04D29/32 ,  F02C3/04 ,  F02K3/06

Abstract: A fan blade assembly for a gas turbine engine is provided. The fan blade assembly having: a non-linear composite airfoil; and a metal root removably attached to the non-linear composite airfoil.