公开(公告)号：WO2015069335A3

公开(公告)日：2015-07-23

申请号：PCT/US2014049576

申请日：2014-08-04

Applicant: UNITED TECHNOLOGIES CORP

Inventor： DROZDENKO LEE M ,  HANSEN JAMES O ,  KIREJCZYK MARIA C ,  WEBB SCOT A ,  MEYER JESSE C ,  GATES BRANDON A ,  BERGETHON RICHARD B ,  MORDEN MICHAEL A

IPC: F01D5/14 ,  F02K3/06 ,  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: 翼型构件（100）包括沿着翼型构件的翼型（102）的至少一部分的基板（120）。 护套（122）具有接收基底的一部分（160）的通道（144）。 稀松布（200）位于基材和护套之间。 间隔件（220）位于护套和基底之间，并具有多个在间隔开的部分之间具有间隙的间隔开的部分（232,234）。

公开(公告)号：EP3044419A4

公开(公告)日：2017-04-19

申请号：EP14843035

申请日：2014-08-04

Applicant: UNITED TECHNOLOGIES CORP

Inventor： DROZDENKO LEE M ,  HANSEN JAMES O ,  MEYER JESSE C ,  MARCIN JR JOHN J ,  SHEMENSKI ROBERT M ,  WEBB SCOT A ,  GATES BRANDON A ,  MORDEN MICHAEL A

IPC: F01D5/18 ,  F01D25/12 ,  F02C7/12 ,  F04D29/38 ,  F04D29/58

CPC classification number: F04D29/388 ,  F01D5/147 ,  F01D5/282 ,  F01D5/288 ,  F04D29/023 ,  F04D29/324 ,  F04D29/325 ,  F04D29/644 ,  F05D2220/36 ,  F05D2240/303 ,  F05D2300/173 ,  F05D2300/174 ,  F05D2300/433 ,  F05D2300/614

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: 包括沿翼型件的翼型件（102）的至少一部分具有基底（120）的翼型件（100）。 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：EP2972077A4

公开(公告)日：2016-11-16

申请号：EP13877533

申请日：2013-12-18

Applicant: UNITED TECHNOLOGIES CORP

Inventor： ROGERS THOMAS H ,  JOYNER RANDALL W ,  MURDOCK JAMES R ,  BRINKS ANDREW J ,  MORDEN MICHAEL A

IPC: G01B5/008 ,  F01D5/14 ,  F01D5/28 ,  F01D21/00 ,  G01B11/03 ,  G01B13/00 ,  G01M13/00

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.

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所选部分。 然后将预涂状态测量和后涂状态测量相关以用于检查目的。

公开(公告)号：EP3044417A4

公开(公告)日：2016-12-14

申请号：EP14860986

申请日：2014-08-04

Applicant: UNITED TECHNOLOGIES CORP

Inventor： DROZDENKO LEE M ,  HANSEN JAMES O ,  KIREJCZYK MARIA C ,  WEBB SCOT A ,  MEYER JESSE C ,  GATES BRANDON A ,  BERGETHON RICHARD B ,  MORDEN MICHAEL A

IPC: F01D5/14 ,  F02K3/06 ,  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.