-
公开(公告)号：US20250059894A1
公开(公告)日：2025-02-20
申请号：US18476474
申请日：2023-09-28
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Abhijeet Jayshingrao Yadav , Frank Worthoff , Nicholas Joseph Kray , Nitesh Jain , Balaraju Suresh
Abstract: A turbine engine including a fan section, a compressor section, a combustion section, and a turbine section in serial flow arrangement. The turbine engine further including a composite airfoil assembly. The composite airfoil assembly having an outer wall, a composite body at least partially defining the outer wall, and a tip cap at least partially defining the outer wall.
-
公开(公告)号：US20240151147A1
公开(公告)日：2024-05-09
申请号：US17979853
申请日：2022-11-03
Applicant: General Electric Company
Inventor： Gary Willard Bryant, Jr. , Nicholas Joseph Kray , Ming Xie , Elzbieta Kryj-Kos , Douglas Lorrimer Armstrong , Nicholas M. Daggett , Frank Worthoff , Scott Roger Finn
IPC: F01D5/28
CPC classification number: F01D5/282 , F05D2220/32 , F05D2230/60 , F05D2300/603
Abstract: The present disclosure relates to an airfoil assembly for a turbine engine and methods of assembly thereof. The airfoil assembly generally includes a composite airfoil and a spar. The composite airfoil has a pressure side and a suction side extending in an axial direction between a leading edge and a trailing edge defining a chordwise direction and extending radially between a root and a tip defining a spanwise direction and having a span-length. The spar includes a first portion including a first material and a second portion joined at an interface with the first portion. The second portion further includes a second material, different from the first material, joined to the first portion at an interface. The method generally includes joining the first portion with the second portion at the interface; and assembling the spar with the composite airfoil.
-
公开(公告)号：US20200291812A1
公开(公告)日：2020-09-17
申请号：US16891665
申请日：2020-06-03
Applicant: General Electric Company
Inventor： Frank Worthoff , Benjamin James Roby , Scott Roger Finn
Abstract: An apparatus a multiple layer structure having a sub-portion defining an impact zone, and having an inner composite fiber layer, an outer composite fiber layer overlying the inner composite fiber layer, and a woven glass layer, where the inner composite fiber layer, outer composite fiber layer, and the woven glass layer overly the impact zone.
-
公开(公告)号：US20190136711A1
公开(公告)日：2019-05-09
申请号：US15805467
申请日：2017-11-07
Applicant: General Electric Company
Inventor： Frank Worthoff , Benjamin James Roby , Scott Roger Finn
Abstract: An apparatus and method for a multiple layer fan casing surrounding a fan having a plurality of circumferentially spaced blades rotatable about a rotational axis and having a sub-portion defining a blade impact zone, the multiple layers comprising an inner fiber layer confronting the blades, an outer fiber layer overlying the inner carbon layer, a glass layer sandwiched between the inner and outer composite fiber layers.
-
-
-
Search Results
14
records
(took 0.015 seconds)
