中科微点-全球专利检索

  1. Login
  2. Sign Up

Search Results

13 records (took 0.023 seconds)

    HYBRID METAL FAN BLADE
    1.
    发明申请
    HYBRID METAL FAN BLADE 审中-公开
    混合金属风扇叶片

    公开(公告)号：WO2014196987A3

    公开(公告)日：2015-02-26

    申请号：PCT/US2013046819

    申请日：2013-06-20

    Applicant: UNITED TECHNOLOGIES CORP

    Inventor： DEAL JAMES L ,  SCHIRRA JOHN J ,  DROZDENKO LEE ,  GRAVES WILLIAM R ,  HANSEN JAMES O ,  WEISSE MICHAEL A ,  WATSON THOMAS J

    IPC: F01D5/14 ,  F01D5/28 ,  F04D29/38

    CPC classification number: F01D5/288 ,  F01D5/147 ,  F04D29/023 ,  F04D29/324 ,  F05D2220/36 ,  F05D2230/23 ,  F05D2240/303 ,  F05D2300/121 ,  F05D2300/124 ,  F05D2300/174 ,  Y02T50/672

    Abstract: 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.

    Abstract translation: 风扇叶片包括翼型部分和鞘部分。 护套部分具有鞘头部分，第一护套侧面和第二护套侧面，两个侧面从前鞘部分向翼伸出。 护套部分结合到翼型部分，使得鞘头部分覆盖前翼型边缘，限定叶片前缘。 第一护套侧面覆盖靠近翼型件前缘的第一翼型件表面的一部分，共同限定叶片抽吸表面。 第二护套侧面覆盖靠近翼型件前缘的第二翼型件表面的一部分，共同限定叶片压力表面。 第一种金属材料是含有约0.5wt％至约3.0wt％的锂的铝合金。

    GROUNDING FOR FAN BLADES ON AN UNDERBLADE SPACER
    2.
    发明申请
    GROUNDING FOR FAN BLADES ON AN UNDERBLADE SPACER 审中-公开
    在无障碍间隔件上接地风扇叶片

    公开(公告)号：WO2014105257A3

    公开(公告)日：2014-10-23

    申请号：PCT/US2013065335

    申请日：2013-10-17

    Applicant: UNITED TECHNOLOGIES CORP

    Inventor： DROZDENKO LEE ,  PENDA ALLAN R

    IPC: F01D5/30 ,  F01D5/14 ,  F01D25/00 ,  F02C7/00 ,  F04D29/00

    CPC classification number: F01D21/14 ,  F01D5/3007 ,  F04D29/023 ,  F04D29/322 ,  F05D2220/36 ,  F05D2260/95 ,  F05D2300/121 ,  F05D2300/133 ,  F05D2300/50 ,  F05D2300/614

    Abstract: A fan rotor includes a rotor body with at least one slot receiving a fan blade. The fan blade has an outer surface, at least at some areas, formed of a first material and an airfoil extending from a dovetail. The dovetail is received in the slot. A spacer is positioned radially inwardly of the dovetail biasing the fan blade against the slot. The spacer includes a grounding element, which is in contact with a portion of the dovetail formed of a second material that is more electrically conductive than the first material. The grounding element 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 grounding and rotating elements form a ground path from the portion of the dovetail into the rotor.

    Abstract translation: 风扇转子包括具有至少一个接收风扇叶片的槽的转子主体。 风扇叶片至少在一些区域具有由第一材料和从燕尾延伸的翼型件形成的外表面。 燕尾槽收纳在插槽中。 间隔件定位在燕尾榫的径向内侧，将风扇叶片偏压在狭槽上。 间隔件包括接地元件，该接地元件与由比第一材料更导电的第二材料形成的燕尾榫的一部分接触。 接地元件与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。 第一材料与第三材料相比导电性较差。 接地元件和旋转元件形成从燕尾部分到转子的接地路径。

    HYBRID METAL FAN BLADE
    4.
    发明专利
    HYBRID METAL FAN BLADE 未知

    公开(公告)号：SG173944A1

    公开(公告)日：2011-09-29

    申请号：SG2010089142

    申请日：2010-12-03

    Applicant: UNITED TECHNOLOGIES CORP

    Inventor： DEAL JAMES L ,  SCHIRRA JOHN J ,  DROZDENKO LEE ,  GRAVES WILLIAM R ,  HANSEN JAMES O

    Abstract: A fan blade is disclosed comprising a lightweight metallic airfoil portion and a high-strength sheath portion. The airfoil portion has a forward airfoil edge, a first airfoil surface, and a second airfoil surface. 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.Fig 2.

    ROOT SPACER FOR ARRANGING BETWEEN A ROTOR DISK AND A ROOT OF A ROTOR BLADE
    7.
    发明公开
    ROOT SPACER FOR ARRANGING BETWEEN A ROTOR DISK AND A ROOT OF A ROTOR BLADE 审中-公开
    转子盘与转子片一个脚的安装面接口

    公开(公告)号：EP2935785A4

    公开(公告)日：2015-12-16

    申请号：EP13863945

    申请日：2013-12-18

    Applicant: UNITED TECHNOLOGIES CORP

    Inventor： DROZDENKO LEE ,  GRAVES WILLIAM R

    IPC: F01D5/02 ,  F01D5/30 ,  F02C7/00

    CPC classification number: F01D5/3092 ,  F01D5/3007 ,  F05D2220/36

    Abstract: A rotor assembly is provided that includes a rotor blade, a root spacer, and a rotor disk with a slot. The rotor blade includes a blade root arranged within the slot. The blade root includes a root base segment and a pair of root side segments. The root base segment is laterally separated from the rotor disk by the root side segments. The root spacer is arranged within the slot, and includes a side surface that extends radially between an inner surface and an outer surface. The side surface is approximately laterally aligned with an intersection between the root base segment and a first of the root side segments. The outer surface engages the root base segment.

Patent Agency Ranking