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公开(公告)号：US09482277B2
公开(公告)日：2016-11-01
申请号：US14584505
申请日：2014-12-29
CPC分类号： F16C33/124 , F16C17/024 , F16C32/0603 , F16C32/0607 , F16C33/1005 , F16C33/121 , F16C2204/44 , F16C2223/70 , F16C2360/44 , F16C2380/26
摘要： An air bearing shaft for a cabin air compressor includes a first edge and a second edge, a surface extending between the first edge and the second edge, and chrome plating on the surface between the first edge and the second edge. L1 is a first distance from the first edge of the air bearing shaft to a first end of the chrome plating. L2 is a second distance from the first edge of the air bearing shaft to a second end of the chrome plating.
摘要翻译： 用于机舱空气压缩机的空气轴承轴包括第一边缘和第二边缘，在第一边缘和第二边缘之间延伸的表面以及在第一边缘和第二边缘之间的表面上的镀铬。 L1是从空气轴承轴的第一边缘到镀铬的第一端的第一距离。 L2是从空气轴承轴的第一边缘到镀铬的第二端的第二距离。
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公开(公告)号：US20160186806A1
公开(公告)日：2016-06-30
申请号：US14584505
申请日：2014-12-29
CPC分类号： F16C33/124 , F16C17/024 , F16C32/0603 , F16C32/0607 , F16C33/1005 , F16C33/121 , F16C2204/44 , F16C2223/70 , F16C2360/44 , F16C2380/26
摘要： An air bearing shaft for a cabin air compressor includes a first edge and a second edge, a surface extending between the first edge and the second edge, and chrome plating on the surface between the first edge and the second edge. L1 is a first distance from the first edge of the air bearing shaft to a first end of the chrome plating. L2 is a second distance from the first edge of the air bearing shaft to a second end of the chrome plating.
摘要翻译： 用于机舱空气压缩机的空气轴承轴包括第一边缘和第二边缘，在第一边缘和第二边缘之间延伸的表面以及在第一边缘和第二边缘之间的表面上的镀铬。 L1是从空气轴承轴的第一边缘到镀铬的第一端的第一距离。 L2是从空气轴承轴的第一边缘到镀铬的第二端的第二距离。
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公开(公告)号：US20150337894A1
公开(公告)日：2015-11-26
申请号：US14652973
申请日：2013-12-16
申请人： Masato YOSHINO , Hiroki FUJIWARA
发明人： Masato YOSHINO , Hiroki FUJIWARA
CPC分类号： F16C17/024 , F01D25/16 , F01D25/166 , F02C3/08 , F02C7/06 , F02C7/08 , F05D2220/32 , F05D2220/40 , F16C27/02 , F16C32/0607 , F16C33/101 , F16C43/02 , F16C2360/23 , F16C2360/24
摘要： A foil bearing includes an outer member (11), and a plurality of foils (13) that are mounted to an inner circumferential surface (11a) of the outer member (11) and directly face the inner circumferential surface (11a) of the outer member (11) in a radial direction without interposition of another member (such as back foils). The foils (13) each include: holding portions (13a, 13b) that are formed at both circumferential ends and held while in contact with the outer member (11); and a body portion (13c) that is formed circumferentially between the holding portions (13a, 13b) and has a bearing surface (A). At least an end portion on one side in a circumferential direction of the body portion (13c) is raised radially inward with respect to the inner circumferential surface (11a) of the outer member (11).
摘要翻译： 箔片轴承包括外部构件（11）和安装到外部构件（11）的内周面（11a）并直接面向外部构件（11）的内周面（11a）的多个箔片（13） （11），而不插入另一个部件（例如背部箔片）。 箔片（13）各自包括：保持部（13a，13b），其形成在两个圆周端并与外部构件（11）接触时保持; 以及在所述保持部（13a，13b）之间周向形成并具有支承面（A）的主体部（13c）。 主体部（13c）的圆周方向一侧的至少一端部相对于外侧部件（11）的内周面（11a）向内侧径向升高。
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4.发明申请METHOD OF AND A DEVICE FOR PROTECTING A MOTOR IN A POD AGAINST SHAFT BENDING SHOCKS 审中-公开用于保护电机中的电动机的方法和装置，用于防止扭转冲击公开(公告)号：US20150054367A1
公开(公告)日：2015-02-26
申请号：US14344524
申请日：2012-09-10
申请人： ROLLS-ROYCE AB
发明人： Andreas Eriksson , Anders Lobell , Per Nahnfeldt , Gunnar Styrud
CPC分类号： H02K7/083 , B23P15/003 , B63B43/18 , B63B2211/06 , B63H23/321 , B63H2005/1258 , B63H2023/322 , F16C17/14 , F16C17/20 , F16C32/0607 , F16C39/02 , F16C41/004 , F16C2326/30 , H02K7/09 , H02K7/102 , H02K13/02 , H02K17/22 , Y10T29/49696
摘要： A method of and a device for protecting an electric motor (4) in a pod unit (1) for propulsion of marine vessels against shaft bending shocks when the blades (2) of the pod propeller hit ice blocks or other hard objects, said motor (4) having a drive shaft (3), a rotor (41) and a stator (42), said shocks tending to momentarily bend the drive shaft (3) to such an extent that the rotor (41) will come into contact with the stator (42). In accordance with the present invention, the rotor (41) is prevented from coming in detrimental contact with the stator (42) by providing at least two members (61, 62), which together form a radial plain bearing (6) having mating arcuate bearing surfaces (611 and 621, respectively), which during normal operation of the motor (4) are spaced from one another by a gap and come in contact with one another only at extreme loads with short durations. One of the members (61, 62) is an inner member (61) having a circular circumference that constitutes one (611) of the bearing surfaces (611, 621). The arcuate bearing surface (611) of the inner member (61) is coaxial with the rotor (41) and rotary therewith, and at least one of the other members is an outer member (62), which fixed in relation to the stator (42) and has its arcuate bearing surface (621) coaxial there with.
摘要翻译： 一种用于保护荚果单元（1）中的电动机（4）的方法和装置，用于当桨形螺旋桨的叶片（2）撞击冰块或其它硬物体时推进船舶抵抗轴弯曲冲击，所述马达 （4）具有驱动轴（3），转子（41）和定子（42），所述冲击趋向于使驱动轴（3）暂时弯曲到转子（41）将与 定子（42）。 根据本发明，通过提供至少两个构件（61,62），防止转子（41）与定子（42）发生有害接触，这两个构件一起形成具有配合弓形的径向滑动轴承（6） 在马达（4）的正常操作期间，轴承表面（611和621分别）彼此间隔开并且在极短的持续时间内彼此接触。 构件（61,62）中的一个是具有构成一个（611）的支承面（611,621）的圆周的内构件（61）。 内部构件（61）的弓形轴承表面（611）与转子（41）同轴并与其一起旋转，并且至少一个其它构件是外部构件（62），其相对于定子（ 42），并且其弓形轴承表面（621）与其同轴。
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公开(公告)号：US12104644B2
公开(公告)日：2024-10-01
申请号：US17746007
申请日：2022-05-17
发明人： Keun Ryu , Hyun Sung Jung
CPC分类号： F16C32/0633 , F16C17/18 , F16C32/0607 , F16C32/0688
摘要： Provided is a floating-sleeve hybrid fluid bearing. The floating-sleeve hybrid fluid bearing may comprise: a bearing housing which is mounted by ring-coupling to the outer circumferential surface of a rotary shaft; and a floating sleeve which is mounted between the rotary shaft and the bearing housing so that there is a gap between the floating sleeve and the rotary shaft, and between the floating sleeve and the bearing housing, wherein the rotation of the floating sleeve is constrained by the bearing housing during the rotation of the rotary shaft, and one side of the floating sleeve in the circumferential direction is open in the radial direction.
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6.发明公开公开(公告)号：US20230219120A1
公开(公告)日：2023-07-13
申请号：US18184776
申请日：2023-03-16
发明人： Guangbin GAO
CPC分类号： B08B5/02 , B08B7/0035 , B08B13/00 , F16C32/0607
摘要： A cover plate bearing device, a cover plate cleaning device, and a cover plate cleaning method. The cover plate bearing device includes a main body and a gas channel provided on the main body; the main body includes two side walls separated in a first direction, a bottom wall connected with the side walls, and a receiving cavity enclosed and formed by the side walls and the bottom wall; the shape of the receiving cavity matches that of the curved cover plate; at least one gas outlet of the gas channel are provided on the side wall; and the gas channel being adapted for blowing gas with a preset angle towards a side of the side wall facing away from the bottom wall, to prevent a moving fluid from eroding the functional coating of the curved cover plate.
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公开(公告)号：US20190017547A1
公开(公告)日：2019-01-17
申请号：US16030927
申请日：2018-07-10
申请人： Stein Seal Company
发明人： Glenn M. Garrison
CPC分类号： F16C32/0662 , F01D11/04 , F01D25/22 , F05D2250/75 , F16C32/0607 , F16C32/0625 , F16C2360/23 , F16J15/40 , F16J15/441 , F16J15/442
摘要： A circumferential seal assembly capable of dividing a gas into separate flow paths before communication between a rotatable runner and a pair of seal rings is presented. The assembly includes an annular seal housing, a rotatable runner, a pair of annular seal rings, and a plurality of groove structures. Each groove structure separates a source flow communicated into a feed groove so that a portion enters at least two grooves to form a longitudinal flow therein. Each groove includes at least two adjoining steps defined by base walls. The base walls are arranged along the groove to decrease depthwise opposite to rotation of the rotatable runner. Two adjoining base walls are disposed about a base shoulder. Each base shoulder locally redirects the longitudinal flow to form an outward radial flow in the direction of one annular seal ring. The base walls are bounded by and intersect a pair of side walls. Each side wall includes at least one side shoulder which narrows the groove widthwise and locally redirects the longitudinal flow away from the side wall to form a lateral flow in the direction of the other side wall. Each reduction to the volume of the gas at the downstream end of each groove structure increases pressure and enhances the stiffness of a thin-film layer between each annular seal ring and the rotatable runner.
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公开(公告)号：US20170122205A1
公开(公告)日：2017-05-04
申请号：US14924888
申请日：2015-10-28
CPC分类号： F02C7/06 , F01D25/22 , F02K3/06 , F05D2230/90 , F05D2240/50 , F05D2240/53 , F05D2240/61 , F16C17/02 , F16C17/028 , F16C32/0607 , F16C32/0625 , F16C33/1005 , F16C33/101 , F16C2360/23 , Y02T50/671
摘要： Embodiments of a gas bearing for aircraft engines are provided herein. In some embodiments, a gas bearing may include a first shaft; a second shaft disposed concentrically about the first shaft; and a protrusion extending from at least one of an inner surface of the first shaft or the outer surface of the second shaft to form a gap between the first shaft and the second shaft.
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公开(公告)号：US09631556B2
公开(公告)日：2017-04-25
申请号：US15158894
申请日：2016-05-19
申请人： Masato Yoshino , Hiroki Fujiwara
发明人： Masato Yoshino , Hiroki Fujiwara
CPC分类号： F16C17/024 , F01D25/16 , F01D25/166 , F02C3/08 , F02C7/06 , F02C7/08 , F05D2220/32 , F05D2220/40 , F16C27/02 , F16C32/0607 , F16C33/101 , F16C43/02 , F16C2360/23 , F16C2360/24
摘要： A foil bearing includes an outer member (11), and a plurality of foils (13) that are mounted to an inner circumferential surface (11a) of the outer member (11) and directly face the inner circumferential surface (11a) of the outer member (11) in a radial direction without interposition of another member (such as back foils). The foils (13) each include: holding portions (13a, 13b) that are formed at both circumferential ends and held while in contact with the outer member (11); and a body portion (13c) that is formed circumferentially between the holding portions (13a, 13b) and has a bearing surface (A). At least an end portion on one side in a circumferential direction of the body portion (13c) is raised radially inward with respect to the inner circumferential surface (11a) of the outer member (11).
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公开(公告)号：US20170058951A1
公开(公告)日：2017-03-02
申请号：US14836406
申请日：2015-08-26
发明人： Rodrigo Rodriguez Erdmenger , Christopher Edward Wolfe , Vittorio Michelassi , Quang Tue Nguyen Tran , Nathan Evan McCurdy Gibson
CPC分类号： F16C32/0622 , F16C32/0607 , F16C32/0618 , F16C2360/23 , F16C2361/00 , F16J15/34 , F16J15/40
摘要： Gas bearing for an aspirating seal assembly is disclosed. The gas bearing includes a bearing body having a bearing surface. The gas bearing further includes a first through-hole disposed in the bearing body, and a plurality of second through-holes spaced apart from each other and disposed around the first through-hole. The first through-hole is characterized by a size, and a first central axis. Each second through-hole is characterized by a size, and a second central axis. The second central axis of each second through-hole in the plurality of second through-holes intersects the first central axis at an angle in a range from about 30 degrees to about 150 degrees or at an angle in a range from about −30 degrees to about −150 degrees. Size of at least one through-hole in the plurality of second through-holes is different from the size of the first through-hole.
摘要翻译： 公开了用于吸气密封组件的气体轴承。 气体轴承包括具有支承面的轴承体。 气体轴承还包括设置在轴承体中的第一通孔和彼此间隔开并设置在第一通孔周围的多个第二通孔。 第一通孔的特征在于尺寸和第一中心轴线。 每个第二通孔的特征在于尺寸和第二中心轴。 多个第二通孔中的每个第二通孔的第二中心轴与第一中心轴以大约30度至大约150度的角度相交，或者在约-30度到 约-150度。 多个第二通孔中的至少一个通孔的尺寸与第一通孔的尺寸不同。
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