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公开(公告)号:US20240287911A1
公开(公告)日:2024-08-29
申请号:US18173989
申请日:2023-02-24
Applicant: GENERAL ELECTRIC COMPANY
Inventor: Benjamin Thomas Van Oflen , Gary Willard Bryant, Jr. , Michael John Franks , Elzbieta Kryj-Kos , Nicholas Joseph Kray , Arthur William Sibbach
CPC classification number: F01D5/3007 , F01D5/282 , F05D2220/32 , F05D2240/24 , F05D2240/30
Abstract: A turbine engine having a disk and a composite airfoil assembly. The disk having a slot. The composite airfoil assembly having an airfoil portion, a dovetail portion, and a roll snubber. The dovetail portion having a radially inner surface. The roll snubber being provided on the radially inner surface. The radially inner surface spaced from the slot to define a gap therebetween.
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公开(公告)号:US11668207B2
公开(公告)日:2023-06-06
申请号:US15316577
申请日:2015-04-23
Applicant: GENERAL ELECTRIC COMPANY
Inventor: Jason David Shapiro , Jan Christopher Schilling , Michael John Franks
CPC classification number: F01D25/246 , F01D25/12 , F01D25/24 , F05D2220/32 , F05D2250/131 , F05D2300/50212 , Y02T50/60
Abstract: A shroud hanger assembly or shroud assembly is provided for dimensionally incompatible components wherein the assembly includes a multi-piece hanger, for example having a forward hanger portion and a rearward hanger portion. A cavity is formed between the parts; wherein a shroud may be positioned which is formed of a low coefficient of thermal expansion material. The hanger and shroud may be formed of the same material or differing materials in order to better match the thermal growth between the hanger and the shroud. When the shroud is positioned within the hanger opening or cavity, one of the forward and rearward hanger portions may be press fit or otherwise connected into the other of the forward and rearward hanger portion.
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公开(公告)号:US10309244B2
公开(公告)日:2019-06-04
申请号:US15102370
申请日:2014-12-04
Applicant: General Electric Company
Inventor: Jason David Shapiro , Roger Lee Doughty , Michael John Franks
Abstract: A shroud and shroud hanger are provided wherein at least the shroud is formed of ceramic matrix composite material. The shroud and hanger extend in a circumferential direction. A generally C-shaped clip extends radially to retain the hanger and shroud together.
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14.
公开(公告)号:US10196937B2
公开(公告)日:2019-02-05
申请号:US14984418
申请日:2015-12-30
Applicant: General Electric Company
Inventor: John Joseph Wunsch , Michael John Franks , Danielle Marie Greenfield , Michael Stephens Bodey , Randall Maurice Prather
Abstract: A composite duct panel assembly is provided. The composite duct panel assembly includes a composite duct panel having a curved cross-section in a circumferential direction and a width based on the panel including a portion of a circumference of an annular bypass duct. In one embodiment, at least two adjacent corners of the panel are greater than 90°. In one embodiment, the panel includes a circumferential flange along a circumferential edge and an axial flange along an axial edge, and the assembly further includes a corner bracket coupled to the panel, the circumferential flange, and the axial flange. The corner bracket includes a flange corner having an approximate 90° angle, the flange corner extending the axial flange and the circumferential flange to an intersection at a corner of the panel.
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