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公开(公告)号：WO2014088673A3
公开(公告)日：2014-06-12
申请号：PCT/US2013/060085
申请日：2013-09-17
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： KLING, Colin J. , BROWN, Charles W. , QUINN, Christopher M. , DUELM, Shelton O. , TOMEO, Peter V. , HUBBERT, Corey L.
Abstract: A fan hub assembly for a gas turbine engine includes a fan hub that is configured to rotate about an axis. The fan hub has an axially extending aperture and a platform. A fastener is received in the aperture in a slip fit relationship to secure the platform to the fan hub.
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公开(公告)号：WO2015026448A2
公开(公告)日：2015-02-26
申请号：PCT/US2014/045945
申请日：2014-07-09
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： KLING, Colin J. , PARKOS, Joseph , LOMASNEY, Gary M. , BOGUE, William
CPC classification number: G06K19/07749 , B29C37/0025 , B29C64/124 , B29C64/153 , B29C67/0062 , B29C67/0077 , B29C70/42 , B29C70/54 , B29K2079/08 , B29K2105/0058 , B29K2105/12 , B29K2105/251 , B29K2105/253 , B29K2307/04 , B29K2309/08 , B29L2009/008 , B29L2031/082 , B32B27/08 , B32B27/281 , B32B2250/02 , B32B2255/10 , B32B2255/205 , B32B2262/101 , B32B2262/106 , B32B2603/00 , B33Y10/00 , B33Y70/00 , B33Y80/00 , C23C18/1641 , C23C18/1653 , C23C18/1657 , C23C18/166 , C23C18/22 , C23C18/30 , C23C18/32 , C23C28/021 , C23C28/023 , C25D1/003 , C25D1/02 , C25D1/20 , C25D3/02 , C25D5/06 , C25D5/54 , C25D5/56 , C25D7/00 , C25D7/04 , C25D9/02 , C25D17/12 , G01B7/16 , G01D5/12 , G01N3/08 , G01N2203/026 , G01N2203/0268 , G01N2203/0298
Abstract: A method for balancing a rotatable component is disclosed This method comprises and then plating the component to deposit a metal layer onto the component until the component is balanced. In addition, and alternative method for balancing a rotatable component is disclosed. This method comprises attaching a balancing weight to the rotatable component and rotating the component. This is followed by plating the component and the balancing weight to deposit a metal layer onto the balancing weight and the component until the component is balanced.
Abstract translation: 公开了一种用于平衡可旋转部件的方法。该方法包括然后电镀该部件以将金属层沉积到部件上直到部件平衡。 另外，公开了用于平衡可旋转部件的替代方法。 该方法包括将平衡配重附接到可旋转部件并旋转部件。 接着是电镀组件和平衡重量，以在平衡重和组件上沉积金属层，直到组件平衡为止。
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公开(公告)号：WO2014099156A1
公开(公告)日：2014-06-26
申请号：PCT/US2013/068666
申请日：2013-11-06
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： PARKIN, Michael J. , KLING, Colin J.
CPC classification number: F16L55/00 , F01D9/02 , F01D25/005 , F02C7/14 , F05D2300/224 , F05D2300/606 , F05D2300/614 , F16L23/032 , F16L43/008 , F16L47/145 , Y10T29/49286 , Y10T29/49826
Abstract: A duct (78) has: a first non-metallic member (86) extending between a first end and a second end, at least at the first end having an outwardly-projecting flange portion (94); a metallic flange member (90) having a sleeve (180) extending between a first end and a second end and a flange (140) extending outward from the sleeve and having a first face (144) and a second face (142); and a second non-metallic member (88) extending between a first end and a second end having an outwardly-projecting flange (150) portion, the first non-metallic member flange portion mounted to the flange first face and the second non-metallic member flange portion mounted to the flange second face.
Abstract translation: 管道（78）具有：第一非金属构件（86），其在第一端和第二端之间延伸，至少在第一端具有向外突出的凸缘部分（94）; 具有在第一端和第二端之间延伸的套筒（180）的金属法兰构件（90）和从套筒向外延伸并具有第一面（144）和第二面（142）的凸缘（140） 以及第二非金属构件（88），其在具有向外突出的凸缘（150）部分的第一端和第二端之间延伸，所述第一非金属构件凸缘部分安装到所述凸缘第一面和所述第二非金属构件 安装到凸缘第二面的构件凸缘部分。
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公开(公告)号：EP3597862A1
公开(公告)日：2020-01-22
申请号：EP19186635.9
申请日：2019-07-16
Applicant: United Technologies Corporation
Inventor： KLING, Colin J.
Abstract: A fan rotor includes a fan hub and a plurality of fan blades extending radially outwardly from the fan hub. Platforms (106) are positioned intermediate blade sides (122) of adjacent ones of the fan blades (102). Seals (124) are positioned between the blade sides (122) and platform sides (120) of the platforms (106). The seals (124) have an elongated attachment portion (126) bonded to one of the platform sides (120) and the blade sides (122). The seal (124) extends radially outwardly from the elongated attachment portion (126) to a wedge portion (134).
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公开(公告)号：EP2915742B2
公开(公告)日：2019-08-28
申请号：EP15157399.5
申请日：2015-03-03
Applicant: United Technologies Corporation
Inventor： ROACH, James T. , COOK, III, Grant O. , KLING, Colin J. , O'BRIEN, James F. , BUGAJ, Shari L.
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Patent Agency Ranking6.发明公开NOSE CONE WITH AN AFT SUPPORT RING FOR RADIAL ATTACHMENT 审中-公开NASENHAUBE MIT EINEM HINTERENSTÜTZRINGZUR RADIALEN BEFESTIGUNG
公开(公告)号：EP3058198A1
公开(公告)日：2016-08-24
申请号：EP14853438.1
申请日：2014-05-23
Applicant: United Technologies Corporation
Inventor： KLING, Colin J. , CLARKSON, Steven
CPC classification number: F02C7/04 , B64C11/14 , F01D5/066 , F02C3/04 , F05D2220/32 , F05D2260/31 , F05D2260/37
Abstract: A nose cone may have a spinner including a main portion and an axially extending stepped portion. The nose cone may also have an annular aft support ring radially secured to the axially extending stepped portion. The nose cone may further include a fairing, which may be secured to the stepped portion.
Abstract translation: 鼻锥可以具有包括主要部分和轴向延伸的阶梯部分的旋转器。 鼻锥体还可以具有径向固定到轴向延伸的阶梯部分的环形后支撑环。 鼻锥可以进一步包括可以固定到阶梯部分的整流罩。
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公开(公告)号：EP2932053A1
公开(公告)日：2015-10-21
申请号：EP13866439.6
申请日：2013-11-06
Applicant: United Technologies Corporation
Inventor： PARKIN, Michael J. , KLING, Colin J.
CPC classification number: F16L55/00 , F01D9/02 , F01D25/005 , F02C7/14 , F05D2300/224 , F05D2300/606 , F05D2300/614 , F16L23/032 , F16L43/008 , F16L47/145 , Y10T29/49286 , Y10T29/49826
Abstract: A duct has: a first non-metallic member extending between a first end and a second end, at least at the first end having an outwardly-projecting flange portion; a metallic flange member having a sleeve extending between a first end and a second end and a flange extending outward from the sleeve and having a first face and a second face; and a second non-metallic member extending between a first end and a second end having an outwardly-projecting flange portion, the first non-metallic member flange portion mounted to the flange first face and the second non-metallic member flange portion mounted to the flange second face.
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公开(公告)号：EP2915742A1
公开(公告)日：2015-09-09
申请号：EP15157399.5
申请日：2015-03-03
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： ROACH, James T. , COOK, III, Grant O. , KLING, Colin J. , O'BRIEN, James F. , BUGAJ, Shari L.
CPC classification number: F01D9/02 , B64C11/14 , F01D5/02 , F01D5/12 , F02C7/04 , F05D2220/32 , F05D2300/10 , F05D2300/603 , F05D2300/6034 , Y02T50/672
Abstract: A spinner (80) for a gas turbine engine (20) comprises an outer shell (82) for defining an airflow path when mounted in a gas turbine engine (20). An inner surface (84) is provided with a plurality of webs (86). A gas turbine engine (20) and a fan section (22) for a gas turbine engine (20) are also disclosed.
Abstract translation: 用于燃气涡轮发动机（20）的旋转器（80）包括用于在安装在燃气涡轮发动机（20）中时限定气流路径的外壳（82）。 内表面（84）设置有多个腹板（86）。 还公开了一种燃气涡轮发动机（20）和用于燃气涡轮发动机（20）的风扇部分（22）。
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公开(公告)号：EP3252294B1
公开(公告)日：2020-05-06
申请号：EP17174286.9
申请日：2017-06-02
Applicant: United Technologies Corporation
Inventor： McPHAIL, James J. , KLING, Colin J.
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公开(公告)号：EP3477062A1
公开(公告)日：2019-05-01
申请号：EP18203530.3
申请日：2018-10-30
Applicant: United Technologies Corporation
Inventor： KLING, Colin J. , LUSSIER, Darin S. , COSTA, Mark W.
IPC: F01D21/04
Abstract: A gas turbine engine (20) is provided. The gas turbine engine comprising: a fan section (22) having a fan; and a containment zone (100) encircling the fan, the containment zone comprising: a ballistic liner (200; 300; 400) composed of a plurality of ring segments (220a-e; 320a-f) located radially outward of the fan; wherein each of the plurality of ring segments include two opposing circumferential ends (230a, 230b; 330a, 330b), and wherein the plurality of ring segments are arranged circumferentially around the fan section and the circumferential ends of each of the plurality of ring segments meet at joints (240; 330) to form the ballistic liner.
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