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1.发明申请ADDITIVELY MANUFACTURED CASTING ARTICLES FOR MANUFACTURING GAS TURBINE ENGINE PARTS 审中-公开用于制造气体涡轮发动机零件的大量制造铸件公开(公告)号：US20160184884A1
公开(公告)日：2016-06-30
申请号：US14870443
申请日：2015-09-30
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Thomas N. SLAVENS , Mark F. ZELESKY , JinQuan XU , Joel H. WAGNER
CPC classification number: B22C9/24 , B22C1/00 , B22C9/02 , B22C9/10 , B22C9/106 , B22D29/002 , B22F3/1055 , B22F5/009 , B22F5/04 , B29C64/153 , B33Y10/00 , B33Y80/00 , F01D5/18 , F05D2230/30 , Y02P10/292 , Y02P10/295
Abstract: A casting article according to another exemplary aspect of the present disclosure includes, among other things, a circuit forming portion including an interior channel and an outer shell body that surrounds the interior channel. An engineered failure feature is formed in the outer shell body and is configured to increase compressibility of the casting article during a casting process.
Abstract translation: 根据本公开另一示例性方面的铸造制品除了别的以外包括包括内部通道的电路形成部分和围绕内部通道的外部壳体。 在外壳体中形成工程破坏特征，并且构造成在铸造过程中增加铸件的压缩性。
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公开(公告)号：US20150354372A1
公开(公告)日：2015-12-10
申请号：US14759761
申请日：2013-01-24
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： San QUACH , Thomas N. SLAVENS
CPC classification number: F01D5/187 , F01D5/147 , F05D2250/185 , F05D2250/314 , F05D2260/201
Abstract: A component for a gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a body portion that includes a first wall spaced apart from a second wall. At least one rib extends between the first wall and the second wall and at least one aperture extends through the at least one rib. The at least one aperture is angled relative to a radial axis of the at least one rib.
Abstract translation: 根据本公开的示例性方面的用于燃气涡轮发动机的部件尤其包括主体部分，其包括与第二壁间隔开的第一壁。 至少一个肋在第一壁和第二壁之间延伸，并且至少一个孔延伸穿过至少一个肋。 所述至少一个孔相对于所述至少一个肋的径向轴线成角度。
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3.发明申请GAS TURBINE ENGINE COMPONENT HAVING VASCULAR ENGINEERED LATTICE STRUCTURE 审中-公开具有瓦斯工程尺寸结构的气体涡轮发动机部件公开(公告)号：US20150345396A1
公开(公告)日：2015-12-03
申请号：US14655059
申请日：2013-03-15
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Mark F. ZELESKY , Joel H. WAGNER , Tracy A. PROPHETER-HINCKLEY , Michael F. BLAIR , Thomas N. SLAVENS , Dominic J. MONGILLO
CPC classification number: F01D5/186 , B22F3/1055 , B23P15/26 , B33Y10/00 , B33Y70/00 , B33Y80/00 , F01D5/147 , F01D5/18 , F01D5/183 , F01D5/184 , F01D5/187 , F01D9/02 , F01D11/08 , F01D25/08 , F01D25/12 , F01D25/24 , F02C7/18 , F05D2250/185 , F05D2260/204 , F23R3/002 , F23R2900/03043 , Y10T29/49318
Abstract: A component according to an exemplary aspect of the present disclosure includes, among other things, a wall and a vascular engineered lattice structure formed inside of the wall. The vascular engineered lattice structure includes at least one of a hollow vascular structure and a solid vascular structure configured to communicate fluid through the vascular engineered lattice structure.
Abstract translation: 根据本公开的示例性方面的部件尤其包括形成在壁内部的壁和血管工程格子结构。 血管工程化晶格结构包括中空血管结构和固体血管结构中的至少一个，其被配置为使流体通过血管工程化晶格结构传播。
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Patent Agency Ranking
4.发明申请ADDITIVELY MANUFACTURED CASTING ARTICLES FOR MANUFACTURING GAS TURBINE ENGINE PARTS 审中-公开用于制造气体涡轮发动机零件的大量制造铸件公开(公告)号：US20160121389A1
公开(公告)日：2016-05-05
申请号：US14870430
申请日：2015-09-30
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Thomas N. SLAVENS , Mark F. ZELESKY , JinQuan XU , Joel H. WAGNER
CPC classification number: B22C9/10 , B22C1/00 , B22C1/181 , B22C9/106 , B22D29/002 , B22F3/1055 , B22F5/009 , B22F5/04 , B28B1/001 , B28B7/346 , B29C64/153 , B33Y10/00 , B33Y80/00 , F01D5/187 , F01D9/041 , F01D25/12 , F05D2220/32 , F05D2230/21 , F05D2240/12 , F05D2240/30 , F05D2300/13 , F05D2300/16 , Y02P10/292 , Y02P10/295
Abstract: A casting article according to an exemplary aspect of the present disclosure includes, among other things, a circuit forming portion and an interior channel formed inside of the circuit forming portion. The interior channel defines a leaching path that extends at least partially through the circuit forming portion.
Abstract translation: 根据本公开的示例性方面的铸造制品尤其包括形成在电路形成部分内部的电路形成部分和内部通道。 内部通道限定了至少部分地延伸通过电路形成部分的浸出路径。
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公开(公告)号：US20150377029A1
公开(公告)日：2015-12-31
申请号：US14765390
申请日：2014-01-31
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Mosheshe Camara-Khary BLAKE , Lisa K. OSBORNE , Thomas N. SLAVENS
CPC classification number: F01D5/141 , F01D5/18 , F01D5/181 , F01D5/187 , F01D9/065 , F01D25/08 , F05D2240/11 , F05D2240/127 , F05D2250/71 , F05D2260/2212 , F05D2260/22141
Abstract: A component for a gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a wall that forms a portion of an outer periphery of at least one cavity and at least one curved turbulator that extends from said wall.
Abstract translation: 根据本公开的示例性方面的用于燃气涡轮发动机的部件尤其包括形成至少一个空腔的外周的一部分的壁和从所述壁延伸的至少一个弯曲的湍流器。
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6.发明申请公开(公告)号：US20160333702A1
公开(公告)日：2016-11-17
申请号：US15112497
申请日：2015-01-26
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Thomas N. SLAVENS , Brooks E. SNYDER
CPC classification number: F01D5/187 , F01D9/02 , F01D11/08 , F01D25/12 , F01D25/30 , F05D2220/32 , F05D2230/211 , F05D2230/31 , F05D2240/35 , F05D2260/204 , F05D2260/205 , F05D2260/2214 , F23R3/002 , F23R2900/03045 , Y02T50/676
Abstract: A component according to an exemplary aspect of the present disclosure includes, among other things, a pedestal that traverses a flow channel disposed between a first wall and a second wall. The pedestal includes at least one interior bore configured to communicate a cooling fluid inside of the pedestal.
Abstract translation: 根据本公开的示例性方面的部件包括穿过设置在第一壁和第二壁之间的流动通道的基座。 基座包括至少一个内孔，其构造成在基座内部连通冷却流体。
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7.发明申请GAS TURBINE ENGINE COMPONENT COOLING CAVITY WITH VORTEX PROMOTING FEATURES 审中-公开气体涡轮发动机组件冷却空气与VORTEX促销功能公开(公告)号：US20160312624A1
公开(公告)日：2016-10-27
申请号：US15102335
申请日：2014-11-17
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Nicholas M. LORICCO , James T. AUXIER , Brooks E. SNYDER , Thomas N. SLAVENS
CPC classification number: F01D5/189 , F01D5/187 , F01D5/284 , F01D9/02 , F01D11/08 , F01D25/12 , F05D2220/32 , F05D2230/50 , F05D2240/12 , F05D2240/30 , F05D2240/35 , F05D2250/25 , F05D2260/2212 , F05D2260/2214 , F05D2260/22141 , F05D2300/13 , F05D2300/20 , F23R3/002 , Y02T50/676
Abstract: A component according to an exemplary aspect of the present disclosure includes, among other things, a body, a wall extending inside of the body and a plurality of vortex promoting features arranged in a helical pattern along the wall.
Abstract translation: 根据本公开的示例性方面的部件包括主体，在主体内部延伸的壁和沿着壁布置成螺旋形图案的多个涡流促进特征。
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8.发明申请GAS TURBINE ENGINE COMPONENT HAVING VASCULAR ENGINEERED LATTICE STRUCTURE 审中-公开具有瓦斯工程尺寸结构的气体涡轮发动机部件公开(公告)号：US20150345304A1
公开(公告)日：2015-12-03
申请号：US14654676
申请日：2013-03-15
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Dominic J. MONGILLO , Tracy A. PROPHETER-HINCKLEY , Mark F. ZELESKY , Joel H. WAGNER , Thomas N. SLAVENS
IPC: F01D5/18
CPC classification number: F01D5/186 , B22F3/1055 , B23P15/26 , B33Y10/00 , B33Y70/00 , B33Y80/00 , F01D5/147 , F01D5/18 , F01D5/183 , F01D5/184 , F01D5/187 , F01D9/02 , F01D11/08 , F01D25/08 , F01D25/12 , F01D25/24 , F02C7/18 , F05D2250/185 , F05D2260/204 , F23R3/002 , F23R2900/03043 , Y10T29/49318
Abstract: A component according to an exemplary aspect of the present disclosure includes, among other things a wall and a vascular engineered lattice structure formed inside of the wall. The vascular engineered lattice structure defines a hollow vascular structure configured to communicate a fluid through the vascular engineered lattice structure. The vascular engineered lattice structure has at least one inlet hole and at least one outlet hole that communicates the fluid into and out of the hollow vascular structure.
Abstract translation: 根据本公开的示例性方面的部件尤其包括形成在壁内部的壁和血管工程格子结构。 血管工程格子结构限定了中空血管结构，其构造成使流体通过血管工程化晶格结构。 血管工程格子结构具有至少一个入口孔和至少一个出口孔，其将流体与中空血管结构连通。
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