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公开(公告)号:US12084977B1
公开(公告)日:2024-09-10
申请号:US18484062
申请日:2023-10-10
发明人: Timothy Unton
CPC分类号: F01D11/122 , F01D11/127 , F01D21/045 , F01D25/24 , F01D25/28 , F04D29/526 , F05D2220/36 , F05D2260/31 , F05D2300/522 , F05D2300/603 , F05D2300/6031 , F05D2300/6034
摘要: A fan case assembly adapted for use with a gas turbine engine includes a fan case and a fan track liner. The fan case that extends circumferentially about an axis. The fan track liner extends circumferentially at least partway about the axis and is coupled with the fan case. The fan track liner includes an abradable section and a core section located radially outward of the abradable section. The core section defines a triply periodic minimal surface geometry.
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公开(公告)号:US12071959B1
公开(公告)日:2024-08-27
申请号:US18461705
申请日:2023-09-06
发明人: Hien Duong , Christopher Chiang
CPC分类号: F04D29/526 , F04D29/324 , F02C3/06 , F05D2220/323
摘要: A compressor for an aircraft engine, has: a gaspath extending around a central axis between a radially-inner wall and a radially-outer wall; a rotor having blades circumferentially distributed around the central axis, the blades having airfoils extending from roots to tips along a span and extending from leading edges to trailing edges along a chord, the airfoils extending across the gaspath; grooves defined in an inner face of the radially-outer wall, circumferentially distributed around the central axis, and having groove lengths extending in a first direction having a circumferential component relative to the central axis, the grooves located between the leading edges and the trailing edges of the airfoils; and slots defined in the inner face of the radially-outer wall, circumferentially distributed around the central axis, and having slot lengths extending in a second direction having an axial component relative to the central axis, the slots projecting from the grooves.
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公开(公告)号:US20240271637A1
公开(公告)日:2024-08-15
申请号:US18493093
申请日:2023-10-24
发明人: Yuki FURUTANI
CPC分类号: F04D29/526 , F04D19/002 , F04D29/541
摘要: An axial fan includes: an impeller including a rotating part, and a blade part connected to the rotating part; a bellmouth including a flat part orthogonal to an extension direction of a rotation axis of the rotating part; a rising part rising from the flat part; and an opening along which the rising part extends, the impeller being located in the opening, the rising part surrounding the impeller, the bellmouth including a plurality of grooves located at a surface of the bellmouth, the surface of the bellmouth being connected to an inner surface of the rising part, the inner surface of the rising part facing the blade part of the impeller, the plurality of grooves being located in at least a corner portion connecting the flat part and the rising part, the plurality of grooves extending in a direction crossing the flat part.
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公开(公告)号:US11905973B2
公开(公告)日:2024-02-20
申请号:US17846854
申请日:2022-06-22
发明人: Yi Wen Chen , Yung Ching Huang , Shang-Chih Yang
CPC分类号: F04D29/663 , F04D19/002 , F04D29/326 , F04D29/522 , F04D29/526 , F04D29/329
摘要: A fan assembly including a fan frame and an impeller. The fan frame includes a frame body and a first peripheral protruding plate and has an air inlet and an air outlet. The first peripheral protruding plate protrudes from a side of the frame body and forms an air channel together with the frame body. The first peripheral protruding plate is configured to reduce a noise made by the fan assembly. The air inlet is in fluid communication with the air outlet via the air channel. The impeller is rotatably disposed on the frame body and located in the air channel. The protruding height of the first peripheral protruding plate relative to the frame body ranges from 50 to 100 percent of an overall axial thickness of the impeller.
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公开(公告)号:US11788558B2
公开(公告)日:2023-10-17
申请号:US17272735
申请日:2019-08-28
发明人: Florent Louis Andre Rognin , Clement Bourolleau , Serge Domingues , Vincent Pascal Fiore , Anwer Siraj
CPC分类号: F04D29/665 , F04D29/522 , F04D29/526 , F05D2220/323 , F05D2230/30
摘要: A fan casing for an aircraft turbomachine, the casing including a one-piece annular body, the one piece annular body including a radially internal annular surface, a first annular portion of which is made of an abradable material, wherein a second annular portion of the internal surface comprises blind holes conferring acoustic properties to the second portion.
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公开(公告)号:US11746793B2
公开(公告)日:2023-09-05
申请号:US17100952
申请日:2020-11-23
申请人: Yung Shun Chiu
发明人: Yung Shun Chiu
IPC分类号: F04D29/52 , F04D29/048 , F04D25/08 , F04D25/06 , F04D29/40
CPC分类号: F04D25/0606 , F04D25/06 , F04D29/403 , F04D29/526 , F04D25/08 , F04D29/048
摘要: A fan includes an annular frame, a rail assembly, a driving member and blades. The blades are connected to the driving member. The driving member is electromagnetically movable along the magnetic levitation assembly that extends along an edge of the annular frame. The driving member does not contact the annular frame or the magnetic levitation assembly so that when the fan is used, the magnetic levitation assembly is energized to generate an electromagnetic force between the magnetic levitation assembly and the driving member to move the driving member along the edge of the annular frame to drive the blades to rotate. Therefore, the blades can be rotated without having to use any motor behind the annular frame, thereby reducing the volume of the fan.
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公开(公告)号:US11732612B2
公开(公告)日:2023-08-22
申请号:US17560225
申请日:2021-12-22
CPC分类号: F01D25/26 , F01D9/065 , F01D21/045 , F01D25/24 , F04D29/526 , F04D29/685 , F05D2220/32 , F05D2230/60 , F05D2240/14 , F05D2260/60
摘要: A fan case assembly adapted for use with a gas turbine engine includes a fan track liner and an annular case. The fan track liner extends circumferentially at least partway about a central axis of the gas turbine engine. The annular case is configured to support the fan track liner at a radial position relative to the central axis. The fan case assembly further includes an air recirculation duct configured to redirect air around the fan track liner.
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公开(公告)号:US11702194B1
公开(公告)日:2023-07-18
申请号:US16898583
申请日:2020-06-11
IPC分类号: B64C37/00 , B64C11/00 , B60F5/02 , F04D29/32 , B64C25/66 , F04D29/52 , B64C25/36 , B64C25/40 , B64C25/32 , F01D15/00
CPC分类号: B64C25/66 , B60F5/02 , B64C11/001 , B64C25/36 , B64C25/405 , B64C37/00 , F04D29/526 , B60F2301/04 , F01D15/00 , F04D29/326
摘要: A convertible ducted fan engine and mounting system. The convertible ducted fan engine has a shroud encircling a mechanical fan. The convertible ducted fan engine includes a fluid-propulsion configuration in which the mechanical fan rotates freely with respect to the shroud to produce thrust through fluid flow, and a drive-wheel configuration in which the shroud rotates about the rotational axis.
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公开(公告)号:US20190186498A1
公开(公告)日:2019-06-20
申请号:US16280101
申请日:2019-02-20
发明人: Oliver HAAF , Thomas HELI , Daniel GEBERT , Peter RIEGLER , Valerius SCHAAF
CPC分类号: F04D29/281 , F04D27/001 , F04D29/4226 , F04D29/526 , F05D2250/52 , G01F1/115 , H02K9/06
摘要: A radial fan has a housing with a motor-drivable fan wheel. The fan wheel generates an air volume flow during operation. The housing has a blow-out portion (4) with an impeller (5). The impeller (5) has a plurality of impeller blades (7) spaced apart in the circumferential direction. The impeller (5) is driven by the air volume flow generated by the fan wheel.
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公开(公告)号:US20180313363A1
公开(公告)日:2018-11-01
申请号:US15921460
申请日:2018-03-14
CPC分类号: F04D19/002 , F04D29/164 , F04D29/526 , F04D29/541 , F05D2250/51
摘要: Briefly, embodiments of a fan for moving a volume of compressible fluid from an upstream side to a downstream side may comprise a vortex circulation channel formed within a shroud substantially surrounding the blades of the fan. As a portion of one or more blades of the fan moves within the vortex circulation channel, a vortex that is formed and confined within the channel may reduce formation of a vortex within the fan working area, thereby bringing about an increase in a volume of the compressible fluid capable of being moved by the fan. In an embodiment, a fin or other protrusion disposed on a tip portion of a blade may additionally increase flow of a compressible fluid through a fan. In an embodiment, use of a wraparound leading edge of a fan shroud may bring about further increases in volume of compressible fluid flow.
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