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11.发明授权FAN BLADE AND GROUNDING ELEMENT, CORRESPONDING ROTOR AND GAS TURBINE ENGINE 有权风叶和接地元件，相应的转子和燃气涡轮发动机
公开(公告)号：EP2900931B1
公开(公告)日：2017-11-08
申请号：EP13841756.3
申请日：2013-09-23
CPC分类号： F01D25/00 , B64D45/02 , F01D5/30 , F01D5/3007 , F01D25/007 , F05D2220/36 , F05D2270/54 , Y02T50/671 , Y02T50/673
摘要： A rotor has a rotor body with at least one slot receiving a blade. The blade has an outer surface, at least at some areas, formed of a first material and having an airfoil extending from a dovetail. The dovetail is received in the slot. A diode is in contact with a portion of the dovetail formed of a second material that is more electrically conductive than the first material. The diode is in contact with a rotating element that rotates with the rotor. The rotating element is formed of a third material. The first material is less electrically conductive than the third material. The diode and the rotating element together form a ground path from the portion of the dovetail into the rotor. An engine and a fan blade are also disclosed.
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公开(公告)号：EP3019638A1
公开(公告)日：2016-05-18
申请号：EP14822973.5
申请日：2014-07-09
摘要： A composition comprises, in weight percent: Al as a largest constituent; 3.0-6.0 Cr; 1.5-4.0 Mn; 0.1-3.5 Co; and 0.3-2.0 Zr.
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公开(公告)号：EP2867473A2
公开(公告)日：2015-05-06
申请号：EP13886385.7
申请日：2013-06-20
发明人： DEAL, James L. , SCHIRRA, John J. , DROZDENKO, Lee , GRAVES, William R. , HANSEN, James O. , WEISSE, Michael A. , WATSON, Thomas J.
摘要： A fan blade comprises an airfoil portion and a sheath portion. The sheath portion has a sheath head section, a first sheath flank, and a second sheath flank, both flanks extending chordwise from the forward sheath section. The sheath portion is bonded to the airfoil portion such that the sheath head section covers the forward airfoil edge, defining a blade leading edge. The first sheath flank covers a portion of the first airfoil surface proximate the airfoil forward edge, jointly defining a blade suction surface. The second sheath flank covers a portion of the second airfoil surface proximate the airfoil forward edge, jointly defining a blade pressure surface. The first metallic material is an aluminum alloy containing between about 0.5 wt% and about 3.0 wt% of lithium.
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公开(公告)号：EP2809884A2
公开(公告)日：2014-12-10
申请号：EP13743677.0
申请日：2013-01-10
摘要： A method of making an aluminum airfoil includes brazing a first airfoil piece and a second airfoil piece together using a braze material that includes an element selected from magnesium and zinc, to form a braze joint between the first airfoil piece and the second airfoil piece. At least one of the first airfoil piece or the second airfoil piece has an aluminum alloy composition that includes greater than 0.8% by weight of zinc.
摘要翻译： 一种制备铝翼型的方法包括钎焊第一翼型件和第二翼型件一起使用，其包括从镁和锌中选择的元素的钎焊材料，以形成所述第一翼型件和第二翼型件件之间形成钎焊接头。 第一翼型件或第二翼型件中的至少一个具有包含大于0.8重量％的锌的铝合金组合物。
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公开(公告)号：EP2901023B1
公开(公告)日：2019-10-30
申请号：EP13864424.0
申请日：2013-09-25
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公开(公告)号：EP3354766A1
公开(公告)日：2018-08-01
申请号：EP18153751.5
申请日：2018-01-26
CPC分类号： B22F1/0059 , B22F2301/052 , B22F2301/15 , B22F2301/205 , B22F2303/01 , B22F2303/05 , B22F2999/00 , C23C4/06 , C23C24/04 , F01D5/288 , F05D2230/90 , F05D2300/611
摘要： A coated article comprising: a substrate; and a coating on the substrate comprising: a metallic matrix comprising, by weight: Al as a largest constituent; 1.9-6.0 Cr; 1.0-4.0 Mn; 0.1-3.5 Co; and 0.2-2.0 Zr; and a filler and optionally porosity.
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公开(公告)号：EP3090128A2
公开(公告)日：2016-11-09
申请号：EP14882461.8
申请日：2014-11-19
发明人： CERNATESCU, Iuliana , WATSON, Thomas J. , HANSEN, James O. , FURRER, David Ulrich , SALVA, Randy P.
CPC分类号： F01D5/28 , C30B29/52 , F01D5/147 , F05D2220/36 , F05D2250/74 , F05D2300/173 , F05D2300/605 , F05D2300/606 , Y02T50/673
摘要： An airfoil includes an airfoil body that extends at least between leading and trailing edges, first and second sides, and radially inner and outer ends. The airfoil body includes an aluminum alloy that has a controlled crystallographic texture with respect to a predefined three-dimensional coordinate system. The airfoil can be used in the fan of a gas turbine engine.
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18.发明公开
公开(公告)号：EP2900931A1
公开(公告)日：2015-08-05
申请号：EP13841756.3
申请日：2013-09-23
CPC分类号： F01D25/00 , B64D45/02 , F01D5/30 , F01D5/3007 , F01D25/007 , F05D2220/36 , F05D2270/54 , Y02T50/671 , Y02T50/673
摘要： A rotor has a rotor body with at least one slot receiving a blade. The blade has an outer surface, at least at some areas, formed of a first material and having an airfoil extending from a dovetail. The dovetail is received in the slot. A diode is in contact with a portion of the dovetail formed of a second material that is more electrically conductive than the first material. The diode is in contact with a rotating element that rotates with the rotor. The rotating element is formed of a third material. The first material is less electrically conductive than the third material. The diode and the rotating element together form a ground path from the portion of the dovetail into the rotor. An engine and a fan blade are also disclosed.
摘要翻译： 转子具有转子体，其具有容纳叶片的至少一个槽。 至少在一些区域，叶片具有由第一材料形成并具有从燕尾形延伸的翼型件的外表面。 燕尾接收在槽中。 二极管与由与第一材料相比更导电的第二材料形成的燕尾形部分接触。 二极管与转子一起旋转的旋转元件接触。 旋转元件由第三材料形成。 第一种材料比第三种材料导电性差。 二极管和旋转元件一起形成从燕尾的部分到转子的接地路径。 还公开了一种发动机和风扇叶片。
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