-
公开(公告)号：US11698001B2
公开(公告)日：2023-07-11
申请号：US17201054
申请日：2021-03-15
发明人： Yathiraj Kasal , Reha Gomuc , Abhay Naik , Donald G. Godfrey
IPC分类号： F01D21/04 , F01D25/24 , F04D29/52 , B33Y80/00 , B22F3/15 , B22F10/00 , B33Y40/00 , B22F10/28
CPC分类号： F01D21/045 , B22F3/15 , B22F10/00 , B33Y80/00 , F01D25/24 , B22F10/28 , B33Y40/00 , F05D2220/32 , F05D2230/31 , F05D2300/10
摘要： A containment system for a gas turbine engine includes an outer containment ring having a first projection that extends radially inward and an inner containment ring having at least a second projection that extends radially outward toward the outer containment ring. The second projection is offset and spaced apart from the first projection to define a chamber in a first state. The containment system includes a lattice defined within the chamber that spans the chamber, and the lattice is integrally formed with each of the outer containment ring and the inner containment ring. A density of the lattice varies in at least one of an axial direction and a radial direction. The second projection is configured to interlock with the first projection in a second state.
-
公开(公告)号：US11015482B2
公开(公告)日：2021-05-25
申请号：US16200946
申请日：2018-11-27
发明人： Yathiraj Kasal , Reha Gomuc , Abhay Naik , Donald G. Godfrey
摘要： A containment system for a gas turbine engine includes an outer containment ring having a first projection that extends radially inward and an inner containment ring having at least a second projection that extends radially outward toward the outer containment ring. The second projection is offset and spaced apart from the first projection to define a chamber in a first state. The containment system includes a lattice defined within the chamber that spans the chamber, and the lattice is integrally formed with each of the outer containment ring and the inner containment ring. The second projection is configured to interlock with the first projection in a second state.
-
公开(公告)号：US10178800B2
公开(公告)日：2019-01-08
申请号：US15474486
申请日：2017-03-30
发明人： Saravana Mahalingam , Abhay Naik , Yathiraj Kasal , Rakesh Hota , Rajendra Prasad Vrukshavai , Mathews Leslie Kuriakose , Ravi Anekal Radhakrishnan
摘要： A support structure for an electronic component a chassis and a standoff that is attached to the chassis. The standoff is configured to support the electronic component and separate the electronic component at a distance away from the chassis. The standoff is configured to receive heat generated by the electronic component. The standoff includes a fluid passageway. The fluid passageway is configured to allow a cooling fluid to flow therethrough for convective heat transfer from the standoff to the cooling fluid.
-
公开(公告)号：US20200165936A1
公开(公告)日：2020-05-28
申请号：US16200946
申请日：2018-11-27
发明人： Yathiraj Kasal , Reha Gomuc , Abhay Naik , Donald G. Godfrey
摘要： A containment system for a gas turbine engine includes an outer containment ring having a first projection that extends radially inward and an inner containment ring having at least a second projection that extends radially outward toward the outer containment ring. The second projection is offset and spaced apart from the first projection to define a chamber in a first state. The containment system includes a lattice defined within the chamber that spans the chamber, and the lattice is integrally formed with each of the outer containment ring and the inner containment ring. The second projection is configured to interlock with the first projection in a second state.
-
公开(公告)号：US20210222588A1
公开(公告)日：2021-07-22
申请号：US17201054
申请日：2021-03-15
发明人： Yathiraj Kasal , Reha Gomuc , Abhay Naik , Donald G. Godfrey
摘要： A containment system for a gas turbine engine includes an outer containment ring having a first projection that extends radially inward and an inner containment ring having at least a second projection that extends radially outward toward the outer containment ring. The second projection is offset and spaced apart from the first projection to define a chamber in a first state. The containment system includes a lattice defined within the chamber that spans the chamber, and the lattice is integrally formed with each of the outer containment ring and the inner containment ring. A density of the lattice varies in at least one of an axial direction and a radial direction. The second projection is configured to interlock with the first projection in a second state.
-
公开(公告)号：US10913538B2
公开(公告)日：2021-02-09
申请号：US16268559
申请日：2019-02-06
发明人： Daniel C. Birchak , Albert Kang , Darrell Horner , John Perek , Abhay Naik , Jagadeesh Hariwal , William F. Ryan , Doug Smith , Bharath Chandra G , Saravana Mahalingam
摘要： Outflow valve (OFV) assemblies including non-metallic frames and enhanced attachment features are provided. In embodiments, the OFV assembly includes a non-metallic frame to which at least one valve door is pivotally mounted. The non-metallic frame may, in turn, include a generally rectangular frame body, a central opening through the frame body, an outer peripheral flange extending around at least a portion of the frame body. Frame attachment interfaces are distributed or spaced around the outer peripheral flange of the non-metallic frame. The frame attachment interfaces include fastener openings and elevated platform regions, which project from an inboard side of the outer peripheral flange and through which the fastener openings extend. Base plates seat against the elevated platform regions. Fasteners engage the base plates and extend through the fastener openings to an outboard side of the outer peripheral flange to attach the OFV assembly to an aircraft fuselage.
-
7.发明申请公开(公告)号：US20200247549A1
公开(公告)日：2020-08-06
申请号：US16268559
申请日：2019-02-06
发明人： Daniel C. Birchak , Albert Kang , Darrell Horner , John Perek , Abhay Naik , Jagadeesh Hariwal , William F. Ryan , Doug Smith , Bharath Chandra G , Saravana Mahalingam
摘要： Outflow valve (OFV) assemblies including non-metallic frames and enhanced attachment features are provided. In embodiments, the OFV assembly includes a non-metallic frame to which at least one valve door is pivotally mounted. The non-metallic frame may, in turn, include a generally rectangular frame body, a central opening through the frame body, an outer peripheral flange extending around at least a portion of the frame body. Frame attachment interfaces are distributed or spaced around the outer peripheral flange of the non-metallic frame. The frame attachment interfaces include fastener openings and elevated platform regions, which project from an inboard side of the outer peripheral flange and through which the fastener openings extend. Base plates seat against the elevated platform regions. Fasteners engage the base plates and extend through the fastener openings to an outboard side of the outer peripheral flange to attach the OFV assembly to an aircraft fuselage.
-
公开(公告)号：US10598038B2
公开(公告)日：2020-03-24
申请号：US15819473
申请日：2017-11-21
IPC分类号： F01D11/02 , F01D11/12 , F16J15/447 , F01D5/02 , F01D9/02
摘要： A labyrinth seal for a gas turbine engine is provided. The labyrinth seal includes a stator and a rotor spaced apart from the stator. The rotor includes a first tooth at a first side having a first radial height, and a second tooth between the first tooth and a second side. The second tooth has a second radial height that is different than the first radial height. The rotor includes a third tooth between the first tooth and the second side having a third radial height that is substantially the same as the first radial height. A first clearance between a first tip of the first tooth and the stator is different than a second clearance between a second tip of the second tooth and the stator, and a third clearance between a third tip of the third tooth and the stator is substantially the same as the first clearance.
-
公开(公告)号：US20190153884A1
公开(公告)日：2019-05-23
申请号：US15819473
申请日：2017-11-21
CPC分类号： F01D11/02 , F01D5/02 , F01D9/02 , F01D11/122 , F05D2220/32 , F05D2240/55 , F05D2250/18 , F16J15/4472
摘要： A labyrinth seal for a gas turbine engine is provided. The labyrinth seal includes a stator and a rotor spaced apart from the stator. The rotor includes a first tooth at a first side having a first radial height, and a second tooth between the first tooth and a second side. The second tooth has a second radial height that is different than the first radial height. The rotor includes a third tooth between the first tooth and the second side having a third radial height that is substantially the same as the first radial height. A first clearance between a first tip of the first tooth and the stator is different than a second clearance between a second tip of the second tooth and the stator, and a third clearance between a third tip of the third tooth and the stator is substantially the same as the first clearance.
-
10.发明申请公开(公告)号：US20180288900A1
公开(公告)日：2018-10-04
申请号：US15474486
申请日：2017-03-30
发明人： Saravana Mahalingam , Abhay Naik , Yathiraj Kasal , Rakesh Hota , Rajendra Prasad Vrukshavai , Mathews Leslie Kuriakose , Ravi Anekal Radhakrishnan
CPC分类号： H05K7/20263 , H05K7/1427 , H05K7/20272
摘要： A support structure for an electronic component a chassis and a standoff that is attached to the chassis. The standoff is configured to support the electronic component and separate the electronic component at a distance away from the chassis. The standoff is configured to receive heat generated by the electronic component. The standoff includes a fluid passageway. The fluid passageway is configured to allow a cooling fluid to flow therethrough for convective heat transfer from the standoff to the cooling fluid.
-
-
-
-
-
-
-
-
-
搜索结果
12 条记录 (耗时 0.02 秒)
