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1.发明授权公开(公告)号：US08727733B2
公开(公告)日：2014-05-20
申请号：US13116068
申请日：2011-05-26
申请人： Anthony Constantine Thermos , Govindarajan Rengarajan , William John Miller , Max Robert Farson , Scott Yiming Yu
发明人： Anthony Constantine Thermos , Govindarajan Rengarajan , William John Miller , Max Robert Farson , Scott Yiming Yu
IPC分类号： F01D5/32
CPC分类号： F01D5/323 , F01D5/3007 , F01D5/326 , F04D29/322 , F05D2220/3219 , F05D2250/411 , F05D2260/33 , F05D2260/36
摘要： A rotor blade and blade retention key assembly includes: a radially outer airfoil, a shank and a radially inner attachment dovetail. The attachment dovetail has a radially innermost surface formed with a notch at one axial end thereof, and a retention key is received in the notch, and rotatable from a retracted position where a retention key portion is substantially flush with the radially innermost surface, to an extended position where the retention key portion projects inwardly from said radially innermost surface and into a recess or pocket formed in a rotor wheel slot to prevent axial movement of the blade within the slot.
摘要翻译： 转子叶片和叶片保持键组件包括：径向外翼面，柄和径向内部附接燕尾。 附件燕尾有一径向最内表面，在其一个轴向端部形成有凹口，并且保持键被容纳在凹口中，并且可从保持键部分基本上与径向最内表面齐平的缩回位置旋转到 延伸位置，其中保持键部分从所述径向最内表面向内突出并且形成在形成在转子轮槽中的凹部或凹穴中，以防止所述刀片在所述槽内的轴向移动。
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2.发明申请公开(公告)号：US20120301308A1
公开(公告)日：2012-11-29
申请号：US13116068
申请日：2011-05-26
申请人： Anthony Constantine THERMOS , Govindarajan RENGARAJAN , William John MILLER , Max Robert FARSON , Scott Yiming YU
发明人： Anthony Constantine THERMOS , Govindarajan RENGARAJAN , William John MILLER , Max Robert FARSON , Scott Yiming YU
IPC分类号： F01D5/30
CPC分类号： F01D5/323 , F01D5/3007 , F01D5/326 , F04D29/322 , F05D2220/3219 , F05D2250/411 , F05D2260/33 , F05D2260/36
摘要： A rotor blade and blade retention key assembly includes: a radially outer airfoil, a shank and a radially inner attachment dovetail. The attachment dovetail has a radially innermost surface formed with a notch at one axial end thereof, and a retention key is received in the notch, and rotatable from a retracted position where a retention key portion is substantially flush with the radially innermost surface, to an extended position where the retention key portion projects inwardly from said radially innermost surface and into a recess or pocket formed in a rotor wheel slot to prevent axial movement of the blade within the slot.
摘要翻译： 转子叶片和叶片保持键组件包括：径向外翼面，柄和径向内部附接燕尾。 附件燕尾有一径向最内表面，在其一个轴向端部形成有凹口，并且保持键被容纳在凹口中，并且可从保持键部分基本上与径向最内表面齐平的缩回位置旋转到 延伸位置，其中保持键部分从所述径向最内表面向内突出并且形成在形成在转子轮槽中的凹部或凹穴中，以防止所述刀片在所述槽内的轴向移动。
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公开(公告)号：US20100329863A1
公开(公告)日：2010-12-30
申请号：US12494610
申请日：2009-06-30
申请人： Nicholas Joseph Kray , David W. Crall , Daniel E. Mollmann , Donald Lee Gardner , Marcia Boyle Johnson , Howard P. Weaver , Max Robert Farson
发明人： Nicholas Joseph Kray , David W. Crall , Daniel E. Mollmann , Donald Lee Gardner , Marcia Boyle Johnson , Howard P. Weaver , Max Robert Farson
CPC分类号： F01D5/20 , F01D11/122 , F05D2240/303 , F05D2240/307 , Y02T50/672 , Y10T29/4932
摘要： A method for reducing tip rub loads in a rotor blade is described having the steps of selecting a location of contact between the rotor blade and a static structure; selecting a location on the blade for incorporating a tip-cutter; selecting a cutter-profile for the tip-cutter; and incorporating the tip-cutter on the selected location on the blade such that tip-cutter is capable of removing a portion of the static structure during a tip rub such that tip rub loads are facilitated to be reduced.
摘要翻译： 描述了一种用于减小转子叶片中的尖端摩擦负荷的方法，其具有选择转子叶片和静态结构之间的接触位置的步骤; 选择刀片上的一个位置以结合尖端切割器; 选择尖端铣刀的刀具轮廓; 并将尖端切割器结合在刀片上的选定位置，使得尖端切割器能够在尖端摩擦期间移除静态结构的一部分，从而有助于降低尖端摩擦载荷。
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公开(公告)号：US08662834B2
公开(公告)日：2014-03-04
申请号：US12494610
申请日：2009-06-30
申请人： Nicholas Joseph Kray , David W. Crall , Daniel E. Mollmann , Donald Lee Gardner , Marcia Boyle Johnson , Howard P. Weaver , Max Robert Farson
发明人： Nicholas Joseph Kray , David W. Crall , Daniel E. Mollmann , Donald Lee Gardner , Marcia Boyle Johnson , Howard P. Weaver , Max Robert Farson
IPC分类号： F01D11/12
CPC分类号： F01D5/20 , F01D11/122 , F05D2240/303 , F05D2240/307 , Y02T50/672 , Y10T29/4932
摘要： A method for reducing tip rub loads in a rotor blade is described having the steps of selecting a location of contact between the rotor blade and a static structure; selecting a location on the blade for incorporating a tip-cutter; selecting a cutter-profile for the tip-cutter; and incorporating the tip-cutter on the selected location on the blade such that tip-cutter is capable of removing a portion of the static structure during a tip rub such that tip rub loads are facilitated to be reduced.
摘要翻译： 描述了一种用于减小转子叶片中的尖端摩擦负荷的方法，其具有选择转子叶片和静态结构之间的接触位置的步骤; 选择刀片上的一个位置以结合尖端切割器; 选择尖端铣刀的刀具轮廓; 并将尖端切割器结合在刀片上的选定位置，使得尖端切割器能够在尖端摩擦期间移除静态结构的一部分，从而有助于降低尖端摩擦载荷。
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公开(公告)号：US08657570B2
公开(公告)日：2014-02-25
申请号：US12494595
申请日：2009-06-30
申请人： Nicholas Joseph Kray , David W. Crall , Daniel E. Mollmann , Donald Lee Gardner , Marcia Boyle Johnson , Howard P. Weaver , Max Robert Farson
发明人： Nicholas Joseph Kray , David W. Crall , Daniel E. Mollmann , Donald Lee Gardner , Marcia Boyle Johnson , Howard P. Weaver , Max Robert Farson
IPC分类号： F01D11/12
CPC分类号： F01D11/122 , F01D5/20 , F05D2220/36 , F05D2240/303 , F05D2240/307 , Y02T50/672
摘要： An airfoil for use in a rotor assembly is disclosed, the airfoil having a tip-cutter located on a sidewall near a tip portion, wherein the tip-cutter is capable of removing a portion of an abradable material during a tip rub. In another embodiment, an airfoil has a tip-grinder located on the tip portion, wherein the tip-grinder capable of removing a portion of an abradable material during a tip rub. In another embodiment, an airfoil has a tip-rake that facilitates reducing loading induced to said airfoil during tip rubs.
摘要翻译： 公开了一种用于转子组件的翼型件，翼型件具有位于靠近顶端部分的侧壁上的尖端切割器，其中尖端切割器能够在尖端摩擦期间去除可磨损材料的一部分。 在另一个实施例中，翼型件具有位于尖端部分上的尖端磨床，其中尖端磨床能够在尖端摩擦期间去除可磨损材料的一部分。 在另一个实施例中，翼型件具有尖耙，其有助于减少在尖端摩擦期间引起的所述翼型的载荷。
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公开(公告)号：US07476086B2
公开(公告)日：2009-01-13
申请号：US11209085
申请日：2005-08-22
申请人： Aspi Rustom Wadia , Peter Nicholas Szucs , Max Robert Farson , Virginia Louise Wilson , William Joseph Solomon
发明人： Aspi Rustom Wadia , Peter Nicholas Szucs , Max Robert Farson , Virginia Louise Wilson , William Joseph Solomon
IPC分类号： B64C27/46
CPC分类号： F02K3/06 , F01D5/141 , F04D29/324 , F05D2220/326 , F05D2220/327 , F05D2220/36 , F05D2250/70 , F05D2250/71 , F05D2250/711 , F05D2250/712 , Y02T50/672 , Y02T50/673 , Y10S416/05
摘要： A fan blade includes an airfoil having opposite pressure and suction sides extending in span between a root and tip, and extending in chord between opposite leading and trailing edges. From root toward tip, the airfoil includes increasing stagger and decreasing camber, and increasing chord length to barrel the airfoil along both the leading and trailing edges. The airfoil further includes forward aerodynamic sweep at the tip, and non-forward aerodynamic sweep between the maximum barrel and the root.
摘要翻译： 风扇叶片包括具有相反压力和吸力侧的翼型件，其在根部和尖端之间的跨度中延伸，并且在相对的前缘和后缘之间延伸成弦。 从根部到尖端，翼型件包括增加的交错和减小的弯度，并且增加弦长以使得沿着前缘和后缘的翼型滚动。 翼型件还包括尖端的向前空气动力学扫掠，以及最大筒体和根部之间的非向前空气动力学扫掠。
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公开(公告)号：US20100329875A1
公开(公告)日：2010-12-30
申请号：US12494595
申请日：2009-06-30
申请人： Nicholas Joseph Kray , David W. Crall , Daniel E. Mollmann , Donald Lee Gardner , Marcia Boyle Johnson , Haward P. Weaver , Max Robert Farson
发明人： Nicholas Joseph Kray , David W. Crall , Daniel E. Mollmann , Donald Lee Gardner , Marcia Boyle Johnson , Haward P. Weaver , Max Robert Farson
CPC分类号： F01D11/122 , F01D5/20 , F05D2220/36 , F05D2240/303 , F05D2240/307 , Y02T50/672
摘要： An airfoil for use in a rotor assembly is disclosed, the airfoil having a tip-cutter located on a sidewall near a tip portion, wherein the tip-cutter is capable of removing a portion of an abradable material during a tip rub. In another embodiment, an airfoil has a tip-grinder located on the tip portion, wherein the tip-grinder capable of removing a portion of an abradable material during a tip rub. In another embodiment, an airfoil has a tip-rake that facilitates reducing loading induced to said airfoil during tip rubs.
摘要翻译： 公开了一种用于转子组件的翼型件，翼型件具有位于靠近顶端部分的侧壁上的尖端切割器，其中尖端切割器能够在尖端摩擦期间去除可磨损材料的一部分。 在另一个实施例中，翼型件具有位于尖端部分上的尖端磨床，其中尖端磨床能够在尖端摩擦期间去除可磨损材料的一部分。 在另一个实施例中，翼型件具有尖耙，其有助于减少在尖端摩擦期间引起的所述翼型的载荷。
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