公开(公告)号：US20160222978A1

公开(公告)日：2016-08-04

申请号：US14917476

申请日：2014-08-04

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Lee M. Drozdenko ,  James O. Hansen ,  Jesse C. Meyer ,  John J. Marcin, JR. ,  Robert M. Shemenski ,  Scot A. Webb ,  Brandon A. Gates ,  Michael A. Morden

IPC: F04D29/38 ,  F04D29/32 ,  F04D29/64 ,  F04D29/02

Abstract: An airfoil member (100) comprising has a substrate (120) along at least a portion of an airfoil (102) of the airfoil member. A sheath (122) has a channel (144) receiving a portion (160) of the substrate. A plurality of separate spacers (320; 380; 400) are between the sheath and the substrate and have a plurality of gaps between the spacers.

Abstract translation: 翼型件（100）包括沿翼型件的翼型（102）的至少一部分具有基底（120）。 护套（122）具有容纳衬底的一部分（160）的通道（144）。 多个分离的间隔物（320; 380; 400）位于护套和衬底之间并且在间隔件之间具有多个间隙。

公开(公告)号：US20190024255A1

公开(公告)日：2019-01-24

申请号：US15656571

申请日：2017-07-21

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： John Harner ,  John D. Riehl ,  William Bogue ,  Gary A. Wigell ,  Brandon A. Gates ,  Michael A. Morden ,  Thomas M. Morin

IPC: C25D11/12 ,  C25D11/26 ,  C25D11/02 ,  C25D11/08 ,  B64F5/40 ,  F02C3/04 ,  F01D5/28

CPC classification number: C25D11/12 ,  B64F5/40 ,  C25D11/022 ,  C25D11/04 ,  C25D11/08 ,  C25D11/26 ,  C25D17/005 ,  F01D5/288 ,  F02C3/04 ,  F05D2230/90

Abstract: A method for anodizing a bonded assembly may include attaching a first electrode to a first component of the bonded assembly, and forming a first oxide layer on the first component. The bonded assembly may comprise the first component and a second component bonded to the first component. The second component may be electrically isolated from the first component.

公开(公告)号：US20150240661A1

公开(公告)日：2015-08-27

申请号：US14628263

申请日：2015-02-22

Applicant: United Technologies Corporation

Inventor： Brian K. Holland ,  Michael A. Morden ,  Brandon A. Gates ,  William Bogue

IPC: F01D25/24 ,  F01D25/00 ,  B23P6/00

CPC classification number: F01D25/24 ,  B23P6/005 ,  B29C73/04 ,  B29C73/26 ,  F01D25/005 ,  F02C9/00 ,  Y02T50/672 ,  Y10T29/49318

Abstract: A method of remanufacturing a liner panel for a gas turbine engine includes removing a bushing from a damaged component; and molding the bushing with a material charge. A liner panel for a gas turbine engine includes a forward fan exit case liner panel with a donor bushing from a damaged forward fan exit case liner panel. A liner panel for a gas turbine engine includes a forward fan exit case liner panel molded from a material charge that includes a multiple of layers. At least one of the multiple of layer includes a discontinuity.

Abstract translation: 一种用于燃气涡轮发动机的衬板的再制造方法包括从损坏的部件移除衬套; 并用材料成型模制衬套。 用于燃气涡轮发动机的衬板包括前风扇出口壳衬里面板，其具有来自损坏的前风扇出口壳衬套板的供体衬套。 用于燃气涡轮发动机的衬板包括由包括多个层的材料装料模制的前风扇出口壳衬里面板。 层的多重中的至少一个包括不连续性。

公开(公告)号：US10458035B2

公开(公告)日：2019-10-29

申请号：US15656571

申请日：2017-07-21

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： John Harner ,  John D. Riehl ,  William Bogue ,  Gary A. Wigell ,  Brandon A. Gates ,  Michael A. Morden ,  Thomas M. Morin

IPC: C25D11/12 ,  B64F5/40 ,  C25D11/02 ,  C25D11/08 ,  C25D11/26 ,  F01D5/28 ,  F02C3/04 ,  C25D11/04 ,  C25D17/00

Abstract: A method for anodizing a bonded assembly may include attaching a first electrode to a first component of the bonded assembly, and forming a first oxide layer on the first component. The bonded assembly may comprise the first component and a second component bonded to the first component. The second component may be electrically isolated from the first component.

公开(公告)号：US20190024671A1

公开(公告)日：2019-01-24

申请号：US15656249

申请日：2017-07-21

Applicant: United Technologies Corporation

Inventor： John Harner ,  John D. Riehl ,  Gary A. Wigell ,  Michael A. Morden ,  Brandon A. Gates

IPC: F04D29/32 ,  F04D29/38 ,  B05C5/02 ,  B05C11/10 ,  B05C13/02 ,  B05D1/02 ,  B05D1/00 ,  B05B1/18

Abstract: A drench system includes a rotating mount to rotate a workpiece, a showerhead to dispense a fluid onto the workpiece; and a tray to collect the fluid and recirculate the fluid to the shower. A method of repairing or remanufacturing a coating includes abrading a surface to at least partially remove a portion of a coating to leave an abraded surface; applying a sol-gel over the abraded surface; applying a corrosion resistant primer onto the sol-gel; and applying an erosion coating onto the corrosion resistant primer.

公开(公告)号：US20150369582A1

公开(公告)日：2015-12-24

申请号：US14767864

申请日：2013-12-18

Applicant: United Technologies Corporation

Inventor： Thomas H. Rogers ,  Randall W. Joyner ,  James R. Murdock ,  Andrew J. Brinks ,  Michael A. Morden

IPC: G01B5/008 ,  F01D9/02 ,  F01D5/28 ,  G01M13/00 ,  F01D5/14

CPC classification number: G01B5/008 ,  F01D5/005 ,  F01D5/141 ,  F01D5/288 ,  F01D9/02 ,  F01D21/003 ,  F05D2220/32 ,  F05D2230/90 ,  F05D2260/83 ,  G01B11/03 ,  G01M13/00

Abstract: A method of inspecting components between a pre-coated state and a post-coated state is provided. The method entails providing at least first and second datum points onto the component in the pre-coated state, where each of the at least first and second datum points have a substantially hemi-spherical shape and a center point. The center points of each of the at least first and second datum points are utilized for measurement of a selected portion on the component in the pre-coated state. Then, the component is coated. Next, the center points of each of the at least first and second datum points are utilized for measurement of the selected portion on the component in the post-coated state. The pre-coated state measurements and the post-coated state measurements are then correlated for inspection purposes.

Abstract translation: 提供了一种在预涂状态和后涂状态之间检查部件的方法。 该方法需要在预涂覆状态下将至少第一和第二基准点提供到部件上，其中至少第一和第二基准点中的每一个具有基本上半球形的形状和中心点。 所述至少第一和第二基准点中的每一个的中心点被用于测量预包装状态下的部件上的选定部分。 然后，涂覆该组分。 接下来，使用至少第一和第二基准点中的每一个的中心点来测量后涂覆状态下的部件上的选定部分。 然后将预涂层状态测量和后涂状态测量相关以进行检查。

公开(公告)号：US10458428B2

公开(公告)日：2019-10-29

申请号：US14917476

申请日：2014-08-04

Applicant: United Technologies Corporation

Inventor： Lee M. Drozdenko ,  James O. Hansen ,  Jesse C. Meyer ,  John J. Marcin, Jr. ,  Robert M. Shemenski ,  Scot A. Webb ,  Brandon A. Gates ,  Michael A. Morden

IPC: F04D29/38 ,  F01D5/28 ,  F01D5/14 ,  F04D29/02 ,  F04D29/32 ,  F04D29/64

Abstract: An airfoil member (100) comprising has a substrate (120) along at least a portion of an airfoil (102) of the airfoil member. A sheath (122) has a channel (144) receiving a portion (160) of the substrate. A plurality of separate spacers (320; 380; 400) are between the sheath and the substrate and have a plurality of gaps between the spacers.

公开(公告)号：US10094242B2

公开(公告)日：2018-10-09

申请号：US14628263

申请日：2015-02-22

Applicant: United Technologies Corporation

Inventor： Brian K. Holland ,  Michael A. Morden ,  Brandon A. Gates ,  William Bogue

IPC: B29C73/04 ,  F01D25/24 ,  F02C9/00 ,  B23P6/00 ,  F01D25/00 ,  B29C73/26

Abstract: A method of remanufacturing a liner panel for a gas turbine engine includes removing a bushing from a damaged component; and molding the bushing with a material charge. A liner panel for a gas turbine engine includes a forward fan exit case liner panel with a donor bushing from a damaged forward fan exit case liner panel. A liner panel for a gas turbine engine includes a forward fan exit case liner panel molded from a material charge that includes a multiple of layers. At least one of the multiple of layer includes a discontinuity.

公开(公告)号：US09927220B2

公开(公告)日：2018-03-27

申请号：US14767864

申请日：2013-12-18

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Thomas H. Rogers ,  Randall W. Joyner ,  James R. Murdock ,  Andrew J. Brinks ,  Michael A. Morden

IPC: G01B5/008 ,  F01D9/02 ,  F01D5/28 ,  G01M13/00 ,  F01D5/14 ,  F01D5/00 ,  G01B11/03 ,  F01D21/00

CPC classification number: G01B5/008 ,  F01D5/005 ,  F01D5/141 ,  F01D5/288 ,  F01D9/02 ,  F01D21/003 ,  F05D2220/32 ,  F05D2230/90 ,  F05D2260/83 ,  G01B11/03 ,  G01M13/00

Abstract: A method of inspecting components between a pre-coated state and a post-coated state is provided. The method entails providing at least first and second datum points onto the component in the pre-coated state, where each of the at least first and second datum points have a substantially hemi-spherical shape and a center point. The center points of each of the at least first and second datum points are utilized for measurement of a selected portion on the component in the pre-coated state. Then, the component is coated. Next, the center points of each of the at least first and second datum points are utilized for measurement of the selected portion on the component in the post-coated state. The pre-coated state measurements and the post-coated state measurements are then correlated for inspection purposes.

公开(公告)号：US20160215784A1

公开(公告)日：2016-07-28

申请号：US14917485

申请日：2014-08-04

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Lee M. Drozdenko ,  James O. Hansen ,  Maria C. Kirejczyk ,  Scot A. Webb ,  Jesse C. Meyer ,  Brandon A. Gates ,  Richard B. Bergethon ,  Michael A. Morden

IPC: F04D29/02 ,  F04D29/32 ,  F04D29/64 ,  F04D29/38

CPC classification number: F04D29/023 ,  F01D5/288 ,  F04D29/324 ,  F04D29/325 ,  F04D29/388 ,  F04D29/644 ,  F05D2240/303 ,  F05D2300/173 ,  F05D2300/174 ,  F05D2300/6033

Abstract: An airfoil member (100) comprising has a substrate (120) along at least a portion of an airfoil (102) of the airfoil member. A sheath (122) has a channel (144) receiving a portion (160) of the substrate. A scrim (200) is between the substrate and the sheath. A spacer (220) is between the sheath and the substrate and has a plurality of spaced-apart portions (232, 234) with gaps between the spaced-apart portions.

Abstract translation: 翼型件（100）包括沿翼型件的翼型（102）的至少一部分具有基底（120）。 护套（122）具有容纳衬底的一部分（160）的通道（144）。 稀松布（200）在基材和护套之间。 间隔物（220）位于护套和衬底之间并且具有多个间隔开的部分（232,234），其间隔开间隔开的部分。