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公开(公告)号:US10661297B2
公开(公告)日:2020-05-26
申请号:US16032803
申请日:2018-07-11
Applicant: United Technologies Corporation
Inventor: James W. Neal , Kevin W. Schlichting , Brian T. Hazel , David A. Litton , Eric Jorzik , Michael J. Maloney
Abstract: An embodiment of a method includes retaining a first workpiece and a second workpiece selectively on a workpiece fixture disposed within a deposition chamber. The workpiece fixture includes tooling including a first workpiece holder, a second workpiece holder, and a first hollow wall. The first workpiece is separated from the second workpiece using the first hollow wall. Energy is selectively applied and directed within the deposition chamber, from an energy source toward a first crucible, the first crucible including a plurality of walls defining an upper recess contiguous with, and disposed directly above a first lower recess, at least the upper recess open to an interior of the deposition chamber. During the step of selectively applying and directing energy, a gas valve is controlled to maintain a partial vacuum in the deposition chamber of greater than 2 Pa to control a size and overlap of at least one coating zone formed around each of the at least one workpiece.
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公开(公告)号:US20190202742A1
公开(公告)日:2019-07-04
申请号:US16298217
申请日:2019-03-11
Applicant: United Technologies Corporation
Inventor: Mario P. Bochiechio , David A. Litton , Michael J. Maloney
IPC: C04B35/488 , F01D5/28 , C04B35/50 , C23C16/44 , C23C4/134 , C04B41/52 , C04B41/50 , C04B41/00 , C04B41/89 , C04B41/87 , C23C14/22 , C23C28/04 , C23C28/00
CPC classification number: C04B35/4885 , C04B35/50 , C04B41/009 , C04B41/5042 , C04B41/52 , C04B41/87 , C04B41/89 , C04B2235/3224 , C23C4/134 , C23C14/22 , C23C16/44 , C23C28/042 , C23C28/32 , C23C28/321 , C23C28/3215 , C23C28/3455 , F01D5/284 , F01D5/288 , F05D2300/21 , C04B35/00 , C04B35/80 , C04B41/5031 , C04B41/5045 , C04B41/51
Abstract: A thermal barrier coating for a turbine engine component contains neodymia, optionally alumina, and zirconia. The thermal barrier coating has resistance to CMAS attack and a low thermal conductivity.
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公开(公告)号:US20170101874A1
公开(公告)日:2017-04-13
申请号:US14880846
申请日:2015-10-12
Applicant: United Technologies Corporation
Inventor: James W. Neal , Michael J. Maloney , Kevin W. Schlichting , Brian T. Hazel , David A. Litton , Eric Jorzik
CPC classification number: F01D5/288 , B32B9/005 , B32B2250/02 , C04B35/48 , C04B35/62222 , C04B2237/348 , C23C14/083 , C23C14/30 , F01D25/005 , F02C3/04 , F05D2220/323 , F05D2230/31 , F05D2240/12 , F05D2240/30 , F05D2240/35 , F05D2240/55 , F05D2300/134 , F05D2300/135 , F05D2300/15 , F05D2300/606
Abstract: An article includes a substrate and a multi-layered ceramic barrier coating on a substrate. The coating includes, from the substrate outward, a first layer of a low-dopant ceramic material and a second layer high-dopant ceramic material. The first layer has a columnar microstructure and the second layer has a branched columnar microstructure.
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公开(公告)号:US20160060748A1
公开(公告)日:2016-03-03
申请号:US14774489
申请日:2014-03-14
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor: Brian T. Hazel , Michael J. Maloney , James W. Neal , David A. Litton
CPC classification number: C23C14/30 , C23C14/228 , C23C14/243 , C23C14/246 , C23C14/505
Abstract: A deposition apparatus (20) comprising: a chamber (22); a process gas source (62) coupled to the chamber; a vacuum pump (52) coupled to the chamber; at least two electron guns (26); one or more power supplies (30) coupled to the electron guns; a plurality of crucibles (32,33,34) positioned or positionable in an operative position within a field of view of at least one said electron gun; and a part holder (170) having at least one operative position for holding parts spaced above the crucibles by a standoff height H. The standoff height H is adjustable in a range including at least 22 inches.
Abstract translation: 一种沉积设备(20),包括:腔室(22); 耦合到所述室的处理气体源(62); 耦合到所述室的真空泵(52); 至少两个电子枪(26); 耦合到电子枪的一个或多个电源(30); 多个坩埚(32,33,34),其定位或定位在至少一个所述电子枪的视野内的操作位置; 以及具有至少一个操作位置的部件保持器(170),用于将间隔在坩埚上方的部件保持在间隔高度H上。间隔高度H在包括至少22英寸的范围内是可调节的。
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公开(公告)号:US20160017154A1
公开(公告)日:2016-01-21
申请号:US14771893
申请日:2013-12-30
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor: Christopher W. Strock , Michael J. Maloney
CPC classification number: C09D5/08 , C08K3/08 , C08K3/38 , C08K2003/0812 , C08K2003/0862 , C08K2003/0881 , C08K2003/385 , C23C4/04 , C23C30/00
Abstract: An abradable coating for application to a gas turbine engine part is formed from a titanium aluminide alloy, a filler material, and porosity. The coating may be applied to a part such as a casing made from a titanium alloy.
Abstract translation: 用于燃气涡轮发动机部件的可磨损涂层由钛铝化合物,填料和孔隙形成。 可以将涂层施加到诸如由钛合金制成的外壳的部件上。
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公开(公告)号:US20150361556A1
公开(公告)日:2015-12-17
申请号:US14736834
申请日:2015-06-11
Applicant: United Technologies Corporation
Inventor: James W. Neal , David A. Litton , Brian T. Hazel , Michael J. Maloney , Eric M. Jorzik
IPC: C23C16/46 , C23C16/455 , C23C16/458 , C23C14/22
CPC classification number: C23C16/463 , C23C14/22 , C23C14/50 , C23C14/505 , C23C14/56 , C23C16/455 , C23C16/458 , C23C16/46
Abstract: A deposition apparatus comprises: an infeed chamber; a preheat chamber; a deposition chamber; and optionally at least one of a cooldown chamber and an outlet chamber. At least a first of the preheat chamber and the cooldown chamber contains a buffer system for buffering workpieces respectively passing to or from the deposition chamber.
Abstract translation: 沉积设备包括:进料室; 一个预热室; 沉积室; 以及可选的冷却室和出口室中的至少一个。 预热室和冷却室中的至少第一个包含用于缓冲分别通过或离开沉积室的工件的缓冲系统。
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公开(公告)号:US11365473B2
公开(公告)日:2022-06-21
申请号:US16527250
申请日:2019-07-31
Applicant: United Technologies Corporation
Inventor: Brian T. Hazel , Michael J. Maloney , James W. Neal , David A. Litton
Abstract: A deposition apparatus (20) comprising: a chamber (22); a process gas source (62) coupled to the chamber; a vacuum pump (52) coupled to the chamber; at least two electron guns (26); one or more power supplies (30) coupled to the electron guns; a plurality of crucibles (32,33,34) positioned or positionable in an operative position within a field of view of at least one said electron gun; and a part holder (170) having at least one operative position for holding parts spaced above the crucibles by a standoff height H. The standoff height H is adjustable in a range including at least 22 inches.
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公开(公告)号:US10822951B2
公开(公告)日:2020-11-03
申请号:US15656960
申请日:2017-07-21
Applicant: United Technologies Corporation
Inventor: Brian T. Hazel , Kevin W. Schlichting , Michael J. Maloney
Abstract: Disclosed herein is a method comprising mixing a carrier liquid with particles and/or with a particle precursor to form a suspension or solution respectively; where the particles comprise a metal oxide; and where the particle precursor comprises a metal salt; injecting the suspension or solution through a plasma flame; and depositing the particles and/or the particle precursor onto a substrate to form an first abradable coating; where the first abradable coating comprises a plurality of cracks or voids that are substantially perpendicular to the substrate surface, where the substrate is a hub surface of a gas turbine engine or where the substrate is a cantilever stator.
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公开(公告)号:US10724133B2
公开(公告)日:2020-07-28
申请号:US15265102
申请日:2016-09-14
Applicant: United Technologies Corporation
Inventor: James W. Neal , Michael J. Maloney , Kevin W. Schlichting , Eric Jorzik , David A. Litton
IPC: C23C14/30 , C23C14/24 , C23C14/22 , C23C14/54 , H01J37/305
Abstract: An electron beam vapor deposition process for depositing coatings includes placing a source coating material in a crucible of a vapor deposition apparatus; energizing the source coating with an electron beam raster pattern that delivers a controlled power density to the material in the crucible forming a vapor cloud from the source coating material; and depositing the source coating material onto a surface of a work piece.
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公开(公告)号:US10597330B2
公开(公告)日:2020-03-24
申请号:US16298217
申请日:2019-03-11
Applicant: United Technologies Corporation
Inventor: Mario P. Bochiechio , David A. Litton , Michael J. Maloney
IPC: C04B35/488 , C23C16/44 , C23C14/22 , F01D5/28 , C23C28/04 , C23C28/00 , C04B35/50 , C04B41/87 , C04B41/89 , C04B41/00 , C04B41/50 , C04B41/52 , C23C4/134
Abstract: A thermal barrier coating for a turbine engine component contains neodymia, optionally alumina, and zirconia. The thermal barrier coating has resistance to CMAS attack and a low thermal conductivity.
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