公开(公告)号：WO2015017405A1

公开(公告)日：2015-02-05

申请号：PCT/US2014/048607

申请日：2014-07-29

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： HOLLAND, Brian K. ,  BOGUE, William ,  DENTON, Jeffrey

IPC: F02C9/48 ,  F02K3/06 ,  G01N21/17 ,  G01N21/35

CPC classification number: B23K31/02 ,  F01D5/005 ,  F02K1/78 ,  F05D2230/232 ,  F05D2230/40 ,  F05D2300/133 ,  F05D2300/174 ,  F05D2300/701 ,  G01N21/3563 ,  G01N21/552 ,  G01N21/94 ,  G01N2021/3595 ,  G01N2201/0221

Abstract: A method of immobilizing a contaminant within a component includes identifying the contaminate; and thermally processing the component via a specific thermal cycle related to the contaminate. A method of repairing a component includes immobilizing a contaminant within the component; and weld repairing the component subsequent to immobilizing the contaminant. An aerospace component includes a honeycomb structure with a thermally decomposed contaminate and a weld repair.

Abstract translation: 将组分中污染物固定的方法包括识别污染物; 并通过与污染物相关的特定热循环热处理该组件。 修复部件的方法包括将污染物固定在所述部件内; 并在固定污染物之后焊接修补部件。 航空航天部件包括具有热分解污染物和焊接修复的蜂窝结构。

公开(公告)号：WO2015026798A1

公开(公告)日：2015-02-26

申请号：PCT/US2014/051651

申请日：2014-08-19

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： HOLLAND, Brian K. ,  DENTON, Jeffrey ,  BOGUE, William

IPC: F16B43/00 ,  F16B5/04 ,  F02C7/20 ,  F01D25/00

CPC classification number: F01D25/24 ,  B29C73/06 ,  B29C2073/268 ,  F01D25/005 ,  F02C7/00 ,  F05D2230/80 ,  F05D2260/31 ,  F05D2300/603 ,  F16B5/01 ,  F16B11/006 ,  F16B43/00

Abstract: An annular bushing includes an annular cylindrical portion with a flange that defines a fastener aperture along an axis. A multiple of spacers extend from an outer surface of the annular cylindrical portion and the flange. The multiple of spacers are operable to control a bond line thickness.

Abstract translation: 环形衬套包括环形圆柱形部分，其具有沿轴线限定紧固件孔的凸缘。 多个间隔件从环形圆柱形部分和凸缘的外表面延伸。 多个间隔件可操作以控制粘结线厚度。

公开(公告)号：EP3276145B1

公开(公告)日：2019-06-05

申请号：EP17183236.3

申请日：2017-07-26

Applicant: United Technologies Corporation

Inventor： HOLLAND, Brian K.

IPC: F02C7/04

公开(公告)号：EP3036445B1

公开(公告)日：2019-12-18

申请号：EP14838458.9

申请日：2014-08-19

Applicant: United Technologies Corporation

Inventor： HOLLAND, Brian K. ,  DENTON, Jeffrey ,  BOGUE, William

IPC: F16B43/00 ,  F16B5/04 ,  F02C7/20 ,  F01D25/00

公开(公告)号：EP3027872A1

公开(公告)日：2016-06-08

申请号：EP14832816.4

申请日：2014-07-29

Applicant: United Technologies Corporation

Inventor： HOLLAND, Brian K. ,  BOGUE, William ,  DENTON, Jeffrey

IPC: F02C9/48 ,  F02K3/06 ,  G01N21/17 ,  G01N21/35

CPC classification number: B23K31/02 ,  F01D5/005 ,  F02K1/78 ,  F05D2230/232 ,  F05D2230/40 ,  F05D2300/133 ,  F05D2300/174 ,  F05D2300/701 ,  G01N21/3563 ,  G01N21/552 ,  G01N21/94 ,  G01N2021/3595 ,  G01N2201/0221

Abstract: A method of immobilizing a contaminant within a component includes identifying the contaminate; and thermally processing the component via a specific thermal cycle related to the contaminate. A method of repairing a component includes immobilizing a contaminant within the component; and weld repairing the component subsequent to immobilizing the contaminant. An aerospace component includes a honeycomb structure with a thermally decomposed contaminate and a weld repair.

公开(公告)号：EP3249163A1

公开(公告)日：2017-11-29

申请号：EP17172282.0

申请日：2017-05-22

Applicant: United Technologies Corporation

Inventor： HOLLAND, Brian K.

IPC: F01D5/30 ,  B64C11/14 ,  F01D5/00 ,  B29C73/10

Abstract: A system and method for nose cone edge delamination repair is provided. A nose cone (110;310) may comprise an outer skirt (111) having an aft edge (113), a flange (112), and a pin landing (114). The system and method may comprise trimming the aft edge (113) of the nose cone (110;310) to form a repaired edge (316). A first layer (417) of fiberglass may be placed over repaired edge (316). A second layer (418) of fiber glass may be placed over the first layer (417) and the repaired edge (316). The first layer (417) and second layer (418) may be trimmed to create a spot face (519) to allow for lower tolerances when installing the nose cone (110;310) into a gas turbine engine (100).

Abstract translation: 提供了用于鼻锥边缘分层修复的系统和方法。 鼻锥（110; 310）可以包括具有后边缘（113），凸缘（112）和销平台（114）的外裙部（111）。 该系统和方法可以包括修剪鼻锥体（110; 310）的后缘（113）以形成修复的边缘（316）。 玻璃纤维的第一层（417）可以放置在修复的边缘（316）上方。 玻璃纤维的第二层（418）可以放置在第一层（417）和修复的边缘（316）上。 当将头锥体（110; 310）安装到燃气涡轮发动机（100）中时，可修整第一层（417）和第二层（418）以形成斑点面（519）以允许较低的公差。

公开(公告)号：EP3036445A1

公开(公告)日：2016-06-29

申请号：EP14838458.9

申请日：2014-08-19

Applicant: United Technologies Corporation

Inventor： HOLLAND, Brian K. ,  DENTON, Jeffrey ,  BOGUE, William

IPC: F16B43/00 ,  F16B5/04 ,  F02C7/20 ,  F01D25/00

Abstract: An annular bushing includes an annular cylindrical portion with a flange that defines a fastener aperture along an axis. A multiple of spacers extend from an outer surface of the annular cylindrical portion and the flange. The multiple of spacers are operable to control a bond line thickness.

公开(公告)号：EP3249163B1

公开(公告)日：2020-01-08

申请号：EP17172282.0

申请日：2017-05-22

Applicant: United Technologies Corporation

Inventor： HOLLAND, Brian K.

IPC: F01D5/30 ,  B64C11/14 ,  F01D5/00 ,  B29C73/10

公开(公告)号：EP3276145A1

公开(公告)日：2018-01-31

申请号：EP17183236.3

申请日：2017-07-26

Applicant: United Technologies Corporation

Inventor： HOLLAND, Brian K.

IPC: F02C7/04

CPC classification number: F02C7/04 ,  B64D27/10 ,  F02K3/06 ,  F04D19/002 ,  F04D29/329 ,  F05D2220/32 ,  F05D2230/31 ,  F05D2240/12 ,  F05D2260/30 ,  F05D2300/601 ,  F05D2300/603 ,  F05D2300/6034 ,  Y02T50/672

Abstract: Aspects of the disclosure are directed to an inlet cap 312, comprising: a first lug slot 324D located proximate a perimeter of the inlet cap 312, and a second lug slot 324F located proximate the perimeter of the inlet cap 312 and located peripherally adjacent to the first lug slot 324D, where the first lug slot 324D includes a first ply 324D-1 to 324D-8, the second lug slot 324E includes a second ply 324E-1 to 324E-8 that is different from the first ply 324D-1 to 324D-8, and at least a third ply (324D-8, 324D-9, 324D-10) is common to the first lug slot 324D and the second lug slot 324E.

Abstract translation: 本公开的多个方面涉及一种入口盖312，其包括：位于入口盖312的周边附近的第一凸耳槽324D和位于入口盖312的周边附近且位于圆周地邻近于入口盖312的第二凸耳槽324F 第一凸耳槽324D，其中第一凸耳槽324D包括第一帘布层324D-1至324D-8，第二凸耳槽324E包括与第一帘布层324D-1至324D-8不同的第二帘布层324E-1至324E-8。 324D-8以及至少第三层（324D-8,324D-9,324D-10）对于第一凸耳槽324D和第二凸耳槽324E是共同的。

公开(公告)号：EP3263836A1

公开(公告)日：2018-01-03

申请号：EP17178206.3

申请日：2017-06-27

Applicant: United Technologies Corporation

Inventor： HOLLAND, Brian K.

IPC: F01D5/00

CPC classification number: F01D5/005 ,  B23P15/02 ,  B23P15/04 ,  B32B38/10 ,  B32B43/006 ,  F01D5/147 ,  F04D29/324 ,  F04D29/38 ,  F05D2220/32 ,  F05D2220/36 ,  F05D2230/10 ,  F05D2230/23 ,  F05D2230/70 ,  F05D2230/80 ,  F05D2230/90 ,  F05D2240/303 ,  F05D2300/121 ,  F05D2300/133 ,  F05D2300/603 ,  Y02T50/672

Abstract: Aspects of the disclosure are directed to milling a nose of a first shield (204) of a blade to leave at least one strip (208a,b) of the first shield (208) coupled to a blade body (204), subsequent to the milling, applying a cryogenic technique to the blade to weaken a bond between the first shield (208) and the blade body (204), and subsequent to the applying of the cryogenic technique, removing the at least one strip (208a,b) of the first shield (208) from the blade body (204).

Abstract translation: 本公开的多个方面涉及铣削刀片的第一防护罩（204）的鼻部，以使第一防护罩（208）的至少一个条带（208a，208b）联接至刀片主体（204） 研磨，将低温技术应用于所述叶片以减弱所述第一防护件（208）与所述叶片主体（204）之间的结合，并且在施加所述低温技术之后，去除所述至少一个带材（208a，208b） 从所述刀身（204）的所述第一护罩（208）。