-
公开(公告)号：US20170044931A1
公开(公告)日：2017-02-16
申请号：US14826498
申请日：2015-08-14
Applicant: United Technologies Corporation
Inventor： Paul M. Lutjen , Carson A. Roy Thill , Dominic J. Mongillo, JR. , Kevin D. Tracy , Jeffrey A. Perry , Thurman C. Dabbs
CPC classification number: F01D25/12 , F01D11/08 , F05D2220/32 , F05D2240/11 , F05D2240/24 , F05D2250/74 , F05D2260/20
Abstract: A gas turbine engine includes a turbine section including a plurality of blade outer air seals (BOAS) disposed therein, the BOAS including a BOAS body including a plurality of cooling holes defined in substantial conformance with a set of Cartesian coordinates as set forth in at least one of Table 1 and Table 2.
Abstract translation: 燃气涡轮发动机包括涡轮部分，其包括设置在其中的多个叶片外部空气密封件（BOAS），所述BOAS包括BOAS主体，该BOAS主体包括基本上符合一组笛卡尔坐标定义的多个冷却孔，至少如 表1和表2之一。
-
52.发明申请公开(公告)号：US20160376896A1
公开(公告)日：2016-12-29
申请号：US14903467
申请日：2014-06-17
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Brandon W. Spangler , Dominic J. Mongillo, JR.
CPC classification number: F01D5/187 , F01D9/041 , F01D11/08 , F01D25/12 , F05D2220/32 , F05D2230/00 , F05D2230/21 , F05D2240/81 , F05D2260/202 , F05D2260/204 , F05D2260/205 , Y02T50/676
Abstract: A gas turbine engine component includes a structure having a wall that provides an exterior surface. A first cooling passage is arranged adjacent to and interiorly of the wall. A second cooling passage is arranged in the wall and provides a first fluid flow direction. A resupply channel is arranged in the wall and is fluidly interconnected to the second cooling passage. A resupply hole fluidly interconnects the first cooling passage and the resupply channel. The resupply channel is transverse relative to the second cooling passage to provide a second fluid flow direction that extends from the resupply hole to the second cooling passage.
Abstract translation: 燃气涡轮发动机部件包括具有提供外表面的壁的结构。 第一冷却通道布置成与壁的内部和内部相邻。 第二冷却通道布置在壁中并提供第一流体流动方向。 补给通道布置在壁中并且流体地互连到第二冷却通道。 补给孔流体地互连第一冷却通道和补给通道。 补给通道相对于第二冷却通道是横向的，以提供从补给孔延伸到第二冷却通道的第二流体流动方向。
-
Patent Agency Ranking
公开(公告)号：US20160208618A1
公开(公告)日：2016-07-21
申请号：US14600048
申请日：2015-01-20
Applicant: United Technologies Corporation
Inventor： Benjamin F. Hagan , Ryan Alan Waite , Bryan P. Dube , Dominic J. Mongillo, JR.
CPC classification number: F01D5/187 , F01D5/147 , F01D5/18 , F01D5/225 , F01D9/041 , F01D9/065 , F01D25/12 , F05D2220/32 , F05D2230/211 , F05D2240/12 , F05D2240/30 , F05D2240/81 , F05D2260/202 , F05D2260/22141
Abstract: An airfoil includes a platform that has platform leading and trailing ends, lateral side faces, and inner and outer faces. An airfoil portion extends outwardly from the inner face of the platform. The airfoil portion includes airfoil leading and trailing ends and side walls that join the airfoil leading and trailing ends. The platform includes a cooling passage that has an inlet at a forward location, outlet slots at the platform trailing end, and an intermediate passage portion that extends from the inlet to the outlet slots. The intermediate passage portion includes a common manifold region that feeds the outlet slots.
Abstract translation: 机翼包括具有平台前端和后端，侧面以及内外表面的平台。 翼面部分从平台的内表面向外延伸。 机翼部分包括翼型件的前端和后端以及连接翼型件前端和后端的侧壁。 该平台包括一个冷却通道，该冷却通道在前部位置具有一个入口，在该平台后端具有一个出口槽，以及一个从入口延伸到出口槽的中间通道部分。 中间通道部分包括供给出口槽的公共歧管区域。
-
公开(公告)号：US20160151829A1
公开(公告)日：2016-06-02
申请号：US14904991
申请日：2014-07-02
Applicant: UNITED TECHNOLOGIES CORPORATION
Abstract: A method of preparing a casting article for use in manufacturing a gas turbine engine part according to an exemplary aspect of the present disclosure includes, among other things, communicating a powdered material to an additive manufacturing system and preparing a casting article that includes at least one trunk and a skin core that extends from the at least one trunk out of the powdered material.
Abstract translation: 根据本公开的示例性方面，制备用于制造燃气涡轮发动机部件的铸造制品的方法包括将粉末材料连接到添加剂制造系统并且制备包括至少一个 躯干和皮肤芯，其从至少一条干线延伸出粉末状材料。
-
公开(公告)号：US20160047264A1
公开(公告)日：2016-02-18
申请号：US14735415
申请日：2015-06-10
Applicant: United Technologies Corporation
Inventor： Christopher R. Joe , Paul M. Lutjen , Dominic J. Mongillo, JR.
IPC: F01D11/08
CPC classification number: F01D11/08 , F05D2230/90 , F05D2250/292 , F05D2260/202 , Y02T50/676
Abstract: A blade outer air seal member includes a distinct body that has two circumferential sides, a leading edge and a trailing edge, and a gas path side and a radially outer side opposite the gas path side. A ceramic coating is initially disposed on a portion of the gas path side. The ceramic coating includes a forward coating portion and an aft coating portion. The gas path side has a bare area axially separating the forward coating portion and the aft coating portion. The bare area excludes any of the ceramic coating. One or more cooling passages have an outlet that opens at the bare area. The cooling passage extends in the body in an axial direction under the ceramic coating.
Abstract translation: 叶片外部空气密封构件包括具有两个周向侧面，前缘和后缘以及与气体路径侧相对的气体通道侧和径向外侧的不同体。 最初将陶瓷涂层设置在气体路径侧的一部分上。 陶瓷涂层包括前涂层部分和后涂部分。 气体通道侧具有使前部涂布部分和后部涂布部分轴向分离的裸露区域。 裸露的区域不包括任何陶瓷涂层。 一个或多个冷却通道具有在裸露区域开口的出口。 冷却通道在陶瓷涂层下在轴向方向上延伸。
-
公开(公告)号：US20160023272A1
公开(公告)日：2016-01-28
申请号：US14706425
申请日：2015-05-07
Applicant: United Technologies Corporation
Inventor： Dominic J. Mongillo, JR. , Tracy A. Propheter-Hinckley , JinQuan Xu
IPC: B22F3/105 , B23K26/00 , B23K26/342 , F01D9/06 , B22F5/00 , B22F5/04 , B22F7/06 , F01D5/18 , B23K15/00 , B22F1/00
CPC classification number: B22F3/1055 , B22F1/0003 , B22F5/009 , B22F5/04 , B22F5/10 , B22F7/06 , B23K15/0086 , B23K15/0093 , B23K26/0006 , B23K26/342 , B23K2103/26 , B23K2103/50 , B23K2103/52 , B23K2103/54 , B33Y10/00 , B33Y80/00 , C04B35/622 , C04B2235/6026 , C04B2235/665 , C04B2235/94 , C04B2235/963 , F01D5/185 , F01D5/187 , F01D9/065 , F05D2230/31 , F05D2240/31 , F05D2260/2212 , F05D2260/22141 , F05D2300/516 , Y02P10/295
Abstract: In a first embodiment, a hollow gas turbine engine workpiece comprises first and second walls formed via additive manufacturing, and a cooling passage defined between the first and second walls by a surface of the first and second walls having arithmetic average surface roughness of at least 100 μin (0.0025 mm). In a second embodiment, a method of manufacture of a gas turbine engine component comprises depositing successive layers of pulverant material via additive manufacturing to form first and second walls defining a cooling passage therebetween, and loading a grain size of the pulverant material to produce lattice convective cooling design networks of various size and proportions with each having a range of relative roughness values, 0.10
Abstract translation: 在第一实施例中，中空燃气涡轮发动机工件包括通过添加剂制造形成的第一和第二壁，以及由第一和第二壁的表面限定在第一和第二壁之间的冷却通道，其具有至少100的算术平均表面粗糙度 μin（0.0025mm）。 在第二实施例中，制造燃气涡轮发动机部件的方法包括通过添加剂制造沉积连续的粉碎材料层，以形成在其间限定冷却通道的第一和第二壁，并加载粉碎材料的晶粒尺寸以产生晶格对流 各种尺寸和比例的冷却设计网络，其各自具有一定范围的相对粗糙度值，0.10
-
57.发明申请公开(公告)号：US20140212297A1
公开(公告)日：2014-07-31
申请号：US13728069
申请日：2012-12-27
Applicant: United Technologies Corporation
Inventor： Travis Goeller , Erik R. Granstrand , Irwin D. Singer , Dominic J. Mongillo, JR. , Edward F. Pietraszkiewicz
IPC: F01D5/18
CPC classification number: F01D5/188 , F01D5/187 , F05D2250/185 , F05D2260/22141 , Y02T50/676
Abstract: A gas turbine engine component includes a structure having a cooling passage providing upstream and downstream portions separated from one another by an inner wall and fluidly connected by a bend. First and second trip strips are respectively arranged in the upstream and downstream portions. The first trip strips are arranged at a first spacing from one another. The second trip strips are arranged at a second spacing from one another. A turbulence promoter is arranged in the bend and at a third spacing from the first trip strips that is different than the first spacing. The turbulence promoter is arranged at a fourth spacing from the second trip strips that is different than the second spacing.
Abstract translation: 燃气涡轮发动机部件包括具有冷却通道的结构，该冷却通道提供通过内壁彼此分离并通过弯曲部流体连接的上游和下游部分。 第一和第二跳闸条分别布置在上游和下游部分中。 第一行程条以彼此之间的第一间距布置。 第二跳闸条以相互间隔开的第二间隔布置。 湍流促进器布置在弯曲中并且以与第一间隔不同的第一跳闸带的第三间隔布置。 湍流促进器被布置在与第二间隔不同的第二跳闸带的第四间隔处。
-
-
-
-
-
-
Search Results
57
records
(took 0.018 seconds)
