-
公开(公告)号：US20170191493A1
公开(公告)日：2017-07-06
申请号：US14985169
申请日：2015-12-30
Applicant: General Electric Company
Inventor： Nicholas Joseph Kray , Jan Christopher Schilling , Nitesh Jain , Abhijit Roy
CPC classification number: F04D29/324 , F01D5/147 , F01D5/282 , F01D5/30 , F01D11/008 , F04D29/023 , F04D29/322 , F05D2220/32 , F05D2230/20 , F05D2230/23 , F05D2230/60 , F05D2240/30 , F05D2240/80 , F05D2260/30 , F05D2300/603 , Y02T50/672 , Y02T50/673
Abstract: A composite blade assembly and a method of assembling a composite blade are provided. The composite blade assembly includes a composite blade having a radially inner root. A composite blade assembly includes a first platform and a circumferentially adjacent second platform abutting the first platform at a platform joint. Each of the first platform and the second platform includes a radially outer surface and a radially inwardly extending attachment member. The platform joint includes a slot extending through adjacent edges of the first platform and the second platform. The slot is configured to receive the radially inner root and the radially inner root is configured to be sandwiched between the attachment members. The blade assembly includes an adhesive system configured to join the radially inner root of the composite blade and the attachment members into a unitary structure, and a retaining clip configured to bias the attachment members towards each other.
-
公开(公告)号：US12012859B2
公开(公告)日：2024-06-18
申请号：US17894881
申请日：2022-08-24
Applicant: General Electric Company
Inventor： Raghuveer Chinta , Abhijit Roy , Vaishnav Raghuvaran , Srinivas Nuthi , Ravindra Shankar Ganiger
IPC: F01D11/22
CPC classification number: F01D11/22 , F05D2220/32 , F05D2240/55
Abstract: Disclosed herein are example variable flowpath casings for blade tip clearance control. An example casing for a turbine engine includes a first annular substrate extending along an axial direction; a second annular substrate positioned radially inward relative to the first annular substrate, the second annular substrate movably coupled to the first annular substrate; and an actuator coupled to the second annular substrate such that a force applied by the actuator moves the second annular substrate relative to the first annular substrate to adjust a tip clearance.
-
公开(公告)号：US11719103B1
公开(公告)日：2023-08-08
申请号：US17715360
申请日：2022-04-07
Applicant: General Electric Company
Inventor： Abhijit Roy , Nicholas Joseph Kray
CPC classification number: F01D5/282 , B29C70/081 , B32B5/02 , B32B5/26 , F01D5/147 , B29C70/342 , B32B2250/20 , B32B2250/40 , B32B2260/023 , B32B2260/046 , B32B2262/0261 , B32B2262/101 , B32B2262/103 , B32B2262/105 , B32B2262/106 , B32B2262/16 , B32B2603/00 , F05D2220/32 , F05D2230/20 , F05D2300/6034
Abstract: Composite components, such as gas turbine engine airfoils, and methods of forming composite components are provided. For example, a composite component of a gas turbine engine comprises a plurality of continuous fiber layers, each continuous fiber layer formed from a plurality of continuous fibers disposed in a matrix material, and a chopped fiber layer comprising a plurality of chopped fibers formed as a filmed sheet. The chopped fiber layer is laid up with the plurality of continuous fiber layers to form the composite component. A method for forming a composite component comprises laying up a plurality of continuous fiber layers, each continuous fiber layer comprising continuous fibers disposed in a matrix material; laying up a chopped fiber layer with the plurality of continuous fiber layers, the layup of the plurality of continuous fiber layers and the chopped fiber layer forming a reinforced layup; and curing the reinforced layup.
-
Patent Agency Ranking
公开(公告)号：US12281577B2
公开(公告)日：2025-04-22
申请号：US18657420
申请日：2024-05-07
Applicant: General Electric Company
Inventor： Raghuveer Chinta , Abhijit Roy , Vaishnav Raghuvaran , Srinivas Nuthi , Ravindra Shankar Ganiger
IPC: F01D11/22
Abstract: Disclosed herein are example variable flowpath casings for blade tip clearance control. An example casing for a turbine engine includes a first annular substrate extending along an axial direction; a second annular substrate positioned radially inward relative to the first annular substrate, the second annular substrate movably coupled to the first annular substrate; and an actuator coupled to the second annular substrate such that a force applied by the actuator moves the second annular substrate relative to the first annular substrate to adjust a tip clearance.
-
公开(公告)号：US20240301802A1
公开(公告)日：2024-09-12
申请号：US18657420
申请日：2024-05-07
Applicant: General Electric Company
Inventor： Raghuveer Chinta , Abhijit Roy , Vaishnav Raghuvaran , Srinivas Nuthi , Ravindra Shankar Ganiger
IPC: F01D11/22
CPC classification number: F01D11/22 , F05D2220/32 , F05D2240/55
Abstract: Disclosed herein are example variable flowpath casings for blade tip clearance control. An example casing for a turbine engine includes a first annular substrate extending along an axial direction; a second annular substrate positioned radially inward relative to the first annular substrate, the second annular substrate movably coupled to the first annular substrate; and an actuator coupled to the second annular substrate such that a force applied by the actuator moves the second annular substrate relative to the first annular substrate to adjust a tip clearance.
-
公开(公告)号：US20240011408A1
公开(公告)日：2024-01-11
申请号：US17894881
申请日：2022-08-24
Applicant: General Electric Company
Inventor： Raghuveer Chinta , Abhijit Roy , Vaishnav Raghuvaran , Srinivas Nuthi , Ravindra Shankar Ganiger
IPC: F01D11/22
CPC classification number: F01D11/22 , F05D2220/32 , F05D2240/55
Abstract: Disclosed herein are example variable flowpath casings for blade tip clearance control. An example casing for a turbine engine includes a first annular substrate extending along an axial direction; a second annular substrate positioned radially inward relative to the first annular substrate, the second annular substrate movably coupled to the first annular substrate; and an actuator coupled to the second annular substrate such that a force applied by the actuator moves the second annular substrate relative to the first annular substrate to adjust a tip clearance.
-
公开(公告)号：US11286807B2
公开(公告)日：2022-03-29
申请号：US16145656
申请日：2018-09-28
Applicant: General Electric Company
Inventor： Nitesh Jain , Abhijit Roy , Kishore Budumuru , Nicholas Joseph Kray
Abstract: A blade for a propulsion apparatus that includes a body formed of a first material having opposed pressure and suction sides, and extending in span between a root and a boundary, and extending in chord between a leading edge and a trailing edge. A tip region that is formed of a second material and that is positioned such that it extends from the body and defines a tip. The tip region joins the body at the boundary. The tip region is configured to fail when a predetermined force is applied to the tip such that the tip separates from the blade and defines a fused tip.
-
公开(公告)号：US10145382B2
公开(公告)日：2018-12-04
申请号：US14985169
申请日：2015-12-30
Applicant: General Electric Company
Inventor： Nicholas Joseph Kray , Jan Christopher Schilling , Nitesh Jain , Abhijit Roy
Abstract: A composite blade assembly and a method of assembling a composite blade are provided. The composite blade assembly includes a composite blade having a radially inner root. A composite blade assembly includes a first platform and a circumferentially adjacent second platform abutting the first platform at a platform joint. Each of the first platform and the second platform includes a radially outer surface and a radially inwardly extending attachment member. The platform joint includes a slot extending through adjacent edges of the first platform and the second platform. The slot is configured to receive the radially inner root and the radially inner root is configured to be sandwiched between the attachment members. The blade assembly includes an adhesive system configured to join the radially inner root of the composite blade and the attachment members into a unitary structure, and a retaining clip configured to bias the attachment members towards each other.
-
-
-
-
-
-
-
Search Results
8
records
(took 0.017 seconds)
