公开(公告)号：US20170097234A1

公开(公告)日：2017-04-06

申请号：US15387944

申请日：2016-12-22

Applicant: General Electric Company

Inventor： John David Ward, JR. ,  Bryan Joseph Germann ,  Jason Lee Burnside ,  Gregory Lee Hovis

IPC: G01B21/32 ,  G01M15/14 ,  C23C30/00

CPC classification number: G01B21/32 ,  C23C4/11 ,  C23C24/04 ,  F01D17/04 ,  F05D2230/31 ,  F05D2260/80 ,  F05D2260/83 ,  F05D2270/808 ,  G01B11/165 ,  G01L1/2287 ,  G01M5/0016 ,  G01M5/0041 ,  G01M15/14

Abstract: Methods for manufacturing passive strain indicator on turbine components include providing a turbine component comprising an exterior surface, and, depositing a ceramic material onto a portion of the exterior surface to form a passive strain indicator comprising at least two reference points.

公开(公告)号：US20150346058A1

公开(公告)日：2015-12-03

申请号：US14292015

申请日：2014-05-30

Applicant: General Electric Company

Inventor： John David Ward, JR. ,  Christopher Edward Thompson ,  Bryan Joseph Germann ,  Jason Lee Burnside ,  Gregory Lee Hovis

IPC: G01M15/14 ,  G01L5/00 ,  C04B35/486 ,  C04B35/64 ,  B23K26/36 ,  B23K26/40

CPC classification number: G01M15/14 ,  B23K26/364 ,  B23K26/402 ,  B23K2103/50 ,  C04B35/486 ,  C04B35/64 ,  F01D17/04 ,  F05D2230/13 ,  F05D2230/31 ,  F05D2300/2118 ,  G01B11/165 ,  G01L5/00 ,  G01M5/0016 ,  G01M5/0041 ,  G01M11/081

Abstract: Methods for manufacturing strain sensors on turbine components include providing a turbine component comprising an exterior surface, depositing a ceramic material onto a portion of the exterior surface, and ablating at least a portion of the ceramic material to form a strain sensor comprising at least two reference points.

Abstract translation: 在涡轮机部件上制造应变传感器的方法包括提供包括外表面的涡轮机部件，将陶瓷材料沉积到外表面的一部分上，以及烧蚀陶瓷材料的至少一部分以形成应变传感器，该应变传感器包括至少两个参考 积分

公开(公告)号：US20150346057A1

公开(公告)日：2015-12-03

申请号：US14291922

申请日：2014-05-30

Applicant: General Electric Company

Inventor： John David Ward, JR. ,  Bryan Joseph Germann ,  Jason Lee Burnside ,  Gregory Lee Hovis

IPC: G01M15/14 ,  C23C30/00 ,  G01B21/32

CPC classification number: G01M15/14 ,  C23C4/11 ,  C23C24/00 ,  C23C30/005 ,  F01D17/04 ,  F05D2230/31 ,  F05D2260/80 ,  F05D2260/83 ,  F05D2270/808 ,  G01B21/32 ,  G01L1/2287 ,  G01M5/0016 ,  G01M5/0041

Abstract: Methods for manufacturing strain sensors on turbine components include providing a turbine component comprising an exterior surface, and, depositing a ceramic material onto a portion of the exterior surface to form a strain sensor comprising at least two reference points.

Abstract translation: 在涡轮机部件上制造应变传感器的方法包括提供包括外表面的涡轮机部件，以及将陶瓷材料沉积到外表面的一部分上以形成包括至少两个参考点的应变传感器。