Fan stagger angle for dirt rejection
    5.
    发明授权
    Fan stagger angle for dirt rejection 有权
    风扇交错角度排污

    公开(公告)号:US09115649B2

    公开(公告)日:2015-08-25

    申请号:US13176473

    申请日:2011-07-05

    摘要: A gas turbine engine includes a spool, a turbine coupled to drive the spool, a propulsor coupled to be rotated about an axis by the turbine through the spool, and a gear assembly coupled between the propulsor and the spool such that rotation of the turbine drives the propulsor at a different speed than the spool. The propulsor includes a hub and a row of propulsor blades that extend from the hub. Each of the propulsor blades has a span between a root at the hub and a tip, and a chord between a leading edge and a trailing edge. The chord forms a stagger angle α with the axis, and the stagger angle α is less than 15° at a position along the propulsor blade that is within an inboard 20% of the span.

    摘要翻译: 燃气涡轮发动机包括阀芯,联接以驱动阀芯的涡轮机,被连接以通过阀芯绕涡轮机绕轴旋转的推进器,以及联接在推进器和阀芯之间的齿轮组件,使得涡轮机驱动 推进器的速度不同于阀芯。 推进器包括从轮毂延伸的轮毂和一排推杆叶片。 每个推进器叶片具有在轮毂的根部与顶端之间的跨度,以及前缘和后缘之间的弦。 弦与轴线形成交错角α,并且在沿着推进刀片的位置处的交错角α小于15°,该推进角度在跨度的20%内。

    High turning fan exit stator
    6.
    发明授权
    High turning fan exit stator 有权
    高转向风扇出口定子

    公开(公告)号:US08438832B1

    公开(公告)日:2013-05-14

    申请号:US13407857

    申请日:2012-02-29

    IPC分类号: F02K3/02

    摘要: A turbine engine includes a fan section that rotates about a longitudinal axis and a compressor section. The turbine engine also includes a fan exit stator located between the fan section and the compressor section, the fan exit stator including an airfoil. The airfoil defines an entrance angle with respect to a leading edge of the airfoil and a line parallel to the longitudinal axis, and the airfoil defines an exit angle with respect to a trailing edge of the airfoil and a line parallel to the longitudinal axis. A difference between the entrance angle and the exit angle is between about 45° and about 65°. The turbine engine also includes a turbine section, and a portion of the compressor section is driven by a portion of the turbine section.

    摘要翻译: 涡轮发动机包括围绕纵向轴线和压缩机部分旋转的风扇部分。 涡轮发动机还包括位于风扇部分和压缩机部分之间的风扇出口定子,风扇出口定子包括翼型件。 翼型件相对于翼型件的前缘和平行于纵向轴线的线限定入口角,并且翼型件相对于翼型件的后缘和平行于纵向轴线的线限定出口角。 入射角和出射角之间的差异在大约45°和大约65°之间。 涡轮发动机还包括涡轮部分,并且压缩机部分的一部分由涡轮部分的一部分驱动。

    Variable compressor stator vane having extended fillet
    8.
    发明申请
    Variable compressor stator vane having extended fillet 有权
    可变压缩机定子叶片具有延伸的圆角

    公开(公告)号:US20080101935A1

    公开(公告)日:2008-05-01

    申请号:US11590297

    申请日:2006-10-31

    IPC分类号: F01D11/00

    CPC分类号: F01D5/147 F01D5/16 F01D17/162

    摘要: An example variable stator vane assembly includes at least one button, a vane airfoil adjacent to the button, and a fillet defined between the button and the airfoil. In one example, the fillet defines a constant radius and extends beyond the button at least greater than a distance of 60% of a length of an overhang portion of the vane airfoil.

    摘要翻译: 示例性可变定子叶片组件包括至少一个按钮,与按钮相邻的叶片翼型件和在按钮和翼型之间限定的圆角。 在一个示例中,圆角限定了恒定的半径,并且延伸超过按钮至少大于叶片翼型的突出部分的长度的60%的距离。

    FAN STAGGER ANGLE FOR DIRT REJECTION
    9.
    发明申请
    FAN STAGGER ANGLE FOR DIRT REJECTION 有权
    风扇防护角风扇角

    公开(公告)号:US20130011266A1

    公开(公告)日:2013-01-10

    申请号:US13176473

    申请日:2011-07-05

    IPC分类号: F01D5/14

    摘要: A gas turbine engine includes a spool, a turbine coupled to drive the spool, a propulsor coupled to be rotated about an axis by the turbine through the spool, and a gear assembly coupled between the propulsor and the spool such that rotation of the turbine drives the propulsor at a different speed than the spool. The propulsor includes a hub and a row of propulsor blades that extend from the hub. Each of the propulsor blades has a span between a root at the hub and a tip, and a chord between a leading edge and a trailing edge. The chord forms a stagger angle α with the axis, and the stagger angle α is less than 15° at a position along the propulsor blade that is within an inboard 20% of the span.

    摘要翻译: 燃气涡轮发动机包括阀芯,联接以驱动阀芯的涡轮机,被连接以通过阀芯绕涡轮机绕轴旋转的推进器,以及联接在推进器和阀芯之间的齿轮组件,使得涡轮机驱动 推进器的速度不同于阀芯。 推进器包括从轮毂延伸的轮毂和一排推杆叶片。 每个推进器叶片具有在轮毂的根部与顶端之间的跨度,以及前缘和后缘之间的弦。 弦与轴线形成交错角α,并且在沿着推进刀片的位置处的交错角α小于15°,该推进角度在跨度的20%内。