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公开(公告)号：WO2015069673A1
公开(公告)日：2015-05-14
申请号：PCT/US2014/063977
申请日：2014-11-05
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： MCCAFFREY, Michael G. , ALVANOS, Ioannis , ABBOTT, Michael G. , COOK, III, Grant O.
CPC classification number: F01D5/147 , F01D5/18 , F01D5/282 , F01D5/284 , F01D5/326 , F02C3/04 , F02C7/12 , F05D2220/32 , F05D2230/236 , F05D2230/51 , F05D2240/11 , F05D2240/12 , F05D2300/6033 , Y02T50/672
Abstract: An airfoil component includes a first segment that has a first piece of a mount and a first piece of an airfoil. The first segment is formed of a first ceramic-based material. A second segment includes a second piece of the mount and a second piece of the airfoil. The second segment is formed of a second ceramic-based material. The first and second segments are bonded together along a bond joint such that the first and second pieces of the mount are bonded to each other and the first and second pieces of the airfoil are bonded to each other.
Abstract translation: 机翼部件包括具有第一安装座和第一翼片的第一段。 第一段由第一陶瓷基材料形成。 第二段包括第二段安装件和第二段翼型件。 第二段由第二陶瓷基材料形成。 第一和第二段沿着接合接头结合在一起，使得第一和第二安装件彼此接合并且第一和第二翼片彼此接合。
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公开(公告)号：WO2014031202A2
公开(公告)日：2014-02-27
申请号：PCT/US2013/042846
申请日：2013-05-28
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： MCCAFFREY, Michael G. , HASKO, Gregory H. , ABBOTT, Michael G.
CPC classification number: F01D5/147 , C04B37/001 , C04B2237/365 , C04B2237/38 , C04B2237/61 , C04B2237/84 , Y10T29/49336
Abstract: A method of making a platform of a blade includes the steps of creating two platform sections by solidifying a material with a fabric in a mold and positioning a band of fabric around the two platform sections to retain an airfoil and define a blade. The method further includes the step of bonding the two platform sections together by solidifying the material to define a platform of a solid material. The platform is not bonded to the airfoil.
Abstract translation: 制造刀片平台的方法包括以下步骤：通过将模具中的织物固化在模具中并将织物带定位在两个平台部分周围以保持翼型件并限定刀片来创建两个平台部分。 该方法还包括通过固化材料以固定固体材料的平台将两个平台部分结合在一起的步骤。 平台没有粘合到翼型上。
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公开(公告)号：WO2015009388A1
公开(公告)日：2015-01-22
申请号：PCT/US2014/042848
申请日：2014-06-18
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： COOK III, Grant O. , ABBOTT, Michael G. , MCCAFFREY, Michael G.
CPC classification number: F23R3/007 , C09J5/00 , C09J2400/123 , C09J2400/163 , F01D5/284 , F01D9/02 , F01D25/246 , F05D2230/236 , F05D2230/642 , F05D2240/11 , F23R3/002 , F23R3/60 , F23R2900/00005 , F23R2900/00017 , Y02T50/672
Abstract: A gas turbine engine component assembly includes a ceramic component having a first thermal characteristic. A metallic component has a second thermal characteristic. A bonding material secures the ceramic component to the metallic component. The bonding material includes at least one of a transient liquid phase bond and a partial transient liquid phase bond. The bonding material is configured to withstand a shear stress parameter relating to a differential between the first and second thermal characteristics.
Abstract translation: 燃气涡轮发动机部件组件包括具有第一热特性的陶瓷部件。 金属部件具有第二热特性。 粘结材料将陶瓷组分固定在金属组分上。 接合材料包括瞬态液相和部分瞬态液相键中的至少一种。 接合材料被配置为承受与第一和第二热特性之间的差异相关的剪切应力参数。
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公开(公告)号：WO2015009386A1
公开(公告)日：2015-01-22
申请号：PCT/US2014/042744
申请日：2014-06-17
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： COOK, Grant O. III , ABBOTT, Michael G. , MCCAFFREY, Michael G.
CPC classification number: F01D5/284 , F01D5/282 , F01D9/042 , F01D9/044 , F05D2230/23 , F05D2230/236 , F05D2300/6033 , Y02T50/672
Abstract: A gas turbine engine component assembly includes first and second portions, wherein at least one of the first and second portions is a ceramic material. The first portion includes an aperture having a first angled surface. The second portion is disposed within the aperture and includes a second angled surface adjacent to the first angled surface. The first and second angled surfaces lock the first and second portions to one another under a pulling load. A bonding material operatively secures the first and second angled surfaces to one another.
Abstract translation: 燃气涡轮发动机部件组件包括第一和第二部分，其中第一和第二部分中的至少一个是陶瓷材料。 第一部分包括具有第一倾斜表面的孔。 第二部分设置在孔内并且包括与第一倾斜表面相邻的第二倾斜表面。 第一和第二倾斜表面在牵引载荷下将第一和第二部分彼此锁定。 接合材料将第一和第二倾斜表面相互操作地固定。
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5.发明授权
公开(公告)号：EP3162547B1
公开(公告)日：2019-01-09
申请号：EP16192942.7
申请日：2016-10-07
Applicant: United Technologies Corporation
Inventor： ABBOTT, Michael G. , READ, Kathryn S.
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Patent Agency Ranking
公开(公告)号：EP3080401A1
公开(公告)日：2016-10-19
申请号：EP14859735.4
申请日：2014-11-05
Applicant: United Technologies Corporation
Inventor： MCCAFFREY, Michael G. , ALVANOS, Ioannis , ABBOTT, Michael G. , COOK, III Grant O.
CPC classification number: F01D5/147 , F01D5/18 , F01D5/282 , F01D5/284 , F01D5/326 , F02C3/04 , F02C7/12 , F05D2220/32 , F05D2230/236 , F05D2230/51 , F05D2240/11 , F05D2240/12 , F05D2300/6033 , Y02T50/672
Abstract: An airfoil component includes a first segment that has a first piece of a mount and a first piece of an airfoil. The first segment is formed of a first ceramic-based material. A second segment includes a second piece of the mount and a second piece of the airfoil. The second segment is formed of a second ceramic-based material. The first and second segments are bonded together along a bond joint such that the first and second pieces of the mount are bonded to each other and the first and second pieces of the airfoil are bonded to each other.
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7.发明授权
公开(公告)号：EP3056478B1
公开(公告)日：2019-10-09
申请号：EP16155069.4
申请日：2016-02-10
Applicant: United Technologies Corporation
Inventor： ABBOTT, Michael G. , READ, Kathryn S. , HERTEL, Christopher J.
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公开(公告)号：EP3022407B1
公开(公告)日：2020-08-19
申请号：EP14826220.7
申请日：2014-06-18
Applicant: United Technologies Corporation
Inventor： COOK III, Grant O. , ABBOTT, Michael G. , MCCAFFREY, Michael G.
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公开(公告)号：EP3022406A1
公开(公告)日：2016-05-25
申请号：EP14825748.8
申请日：2014-06-17
Applicant: United Technologies Corporation
Inventor： COOK, Grant O. III , ABBOTT, Michael G. , MCCAFFREY, Michael G.
CPC classification number: F01D5/284 , F01D5/282 , F01D9/042 , F01D9/044 , F05D2230/23 , F05D2230/236 , F05D2300/6033 , Y02T50/672
Abstract: A gas turbine engine component assembly includes first and second portions, wherein at least one of the first and second portions is a ceramic material. The first portion includes an aperture having a first angled surface. The second portion is disposed within the aperture and includes a second angled surface adjacent to the first angled surface. The first and second angled surfaces lock the first and second portions to one another under a pulling load. A bonding material operatively secures the first and second angled surfaces to one another.
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公开(公告)号：EP2855856B1
公开(公告)日：2019-01-16
申请号：EP13831702.9
申请日：2013-05-28
Applicant: United Technologies Corporation
Inventor： MCCAFFREY, Michael G. , HASKO, Gregory H. , ABBOTT, Michael G.
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