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公开(公告)号：US20160208848A1
公开(公告)日：2016-07-21
申请号：US14914981
申请日：2014-09-10
发明人： Erik Swanson , Patrick O'Meara
CPC分类号： F16C17/024 , F16C17/042 , F16C27/02 , F16C27/04 , F16C43/02 , F16C2202/08 , F16C2220/68 , F16C2220/82 , F16F1/028 , Y10T29/49705
摘要： A wing foil bearing may include one or more wing or tab foil layers. A tab foil layer may comprise a thin material with a two-dimensional array of tab shapes. A tab shape may be defined by a boundary of material separated from the thin material and having an integral edge and a free edge. Tab shapes may include one or more free-state bends relative to the thin material, forming a two-dimensional array of cantilever wings or tabs. Tab arrays may be one or more of various types or two-dimensional arrays, and a tab foil layer may include additional tab arrays and tabs. One or more tab foil layers may be engaged with a mounting surface layer and a counter-surface layer to form a wing foil bearing. Tab foil layers may be stacked and or nested, including partial nesting and complete nesting.
摘要翻译： 翼箔轴承可以包括一个或多个翼片或翼片箔层。 凸片箔层可以包括具有凸片形状的二维阵列的薄材料。 突片形状可以由与薄材料分离并且具有整体边缘和自由边缘的材料的边界限定。 突片形状可以包括相对于薄材料的一个或多个自由状态弯曲，形成悬臂翼或翼片的二维阵列。 标签阵列可以是各种类型或二维阵列中的一种或多种，并且突片箔层可以包括附加的标签阵列和突片。 一个或多个凸片箔层可以与安装表面层和相对表面层接合以形成翼片轴承。 标签箔层可以堆叠或嵌套，包括部分嵌套和完全嵌套。
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公开(公告)号：US10267354B2
公开(公告)日：2019-04-23
申请号：US15960097
申请日：2018-04-23
发明人： Erik Swanson , Patrick O'Meara
摘要： A wing foil bearing may include one or more wing or tab foil layers. A tab foil layer may comprise a thin material with a two-dimensional array of tab shapes. A tab shape may be defined by a boundary of material separated from the thin material and having an integral edge and a free edge. Tab shapes may include one or more free-state bends relative to the thin material, forming a two-dimensional array of cantilever wings or tabs. Tab arrays may be one or more of various types or two-dimensional arrays, and a tab foil layer may include additional tab arrays and tabs. One or more tab foil layers may be engaged with a mounting surface layer and a counter-surface layer to form a wing foil bearing. Tab foil layers may be stacked and or nested, including partial nesting and complete nesting.
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公开(公告)号：US09976594B2
公开(公告)日：2018-05-22
申请号：US14914981
申请日：2014-09-10
发明人： Erik Swanson , Patrick O'Meara
CPC分类号： F16C17/024 , F16C17/042 , F16C27/02 , F16C27/04 , F16C43/02 , F16C2202/08 , F16C2220/68 , F16C2220/82 , F16F1/028 , Y10T29/49705
摘要： A wing foil bearing may include one or more wing or tab foil layers. A tab foil layer may comprise a thin material with a two-dimensional array of tab shapes. A tab shape may be defined by a boundary of material separated from the thin material and having an integral edge and a free edge. Tab shapes may include one or more free-state bends relative to the thin material, forming a two-dimensional array of cantilever wings or tabs. Tab arrays may be one or more of various types or two-dimensional arrays, and a tab foil layer may include additional tab arrays and tabs. One or more tab foil layers may be engaged with a mounting surface layer and a counter-surface layer to form a wing foil bearing. Tab foil layers may be stacked and or nested, including partial nesting and complete nesting.
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公开(公告)号：US20180245625A1
公开(公告)日：2018-08-30
申请号：US15960097
申请日：2018-04-23
发明人： Erik Swanson , Patrick O'Meara
CPC分类号： F16C17/024 , F16C17/042 , F16C27/02 , F16C27/04 , F16C43/02 , F16C2202/08 , F16C2220/68 , F16C2220/82 , F16F1/028 , Y10T29/49705
摘要： A wing foil bearing may include one or more wing or tab foil layers. A tab foil layer may comprise a thin material with a two-dimensional array of tab shapes. A tab shape may be defined by a boundary of material separated from the thin material and having an integral edge and a free edge. Tab shapes may include one or more free-state bends relative to the thin material, forming a two-dimensional array of cantilever wings or tabs. Tab arrays may be one or more of various types or two-dimensional arrays, and a tab foil layer may include additional tab arrays and tabs. One or more tab foil layers may be engaged with a mounting surface layer and a counter-surface layer to form a wing foil bearing. Tab foil layers may be stacked and or nested, including partial nesting and complete nesting.
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