Bladed rotor for a gas turbine engine
    1.
    发明授权
    Bladed rotor for a gas turbine engine 失效
    用于气体涡轮发动机的叶片转子

    公开(公告)号:US3719439A

    公开(公告)日:1973-03-06

    申请号:US3719439D

    申请日:1971-04-06

    申请人: ROLLS ROYCE

    IPC分类号: F01D5/22 F01D5/24

    CPC分类号: F01D5/22 F01D5/24

    摘要: A BLADED ROTOR FOR A GAS TURBINE ENGINE HAS A ROW OF BLADES, EACH BLADE HAVING TWO PART SPHERICALLY FACED DEPRESSIONS OF OPPOSITE FACES AND HOLES THROUGH THE BLADE THICKNESS WHICH LEAD INTO THE DEPRESSIONS. TIE MEMBERS EXTEND BETWEEN ADJACENT BLADES, THE ENDS OF THE TIE MEMBERS PASSING THROUGH THE HOLES AND BEING RETAINED BY PART SPHERICALLY FACE NUTS WHICH ENGAGE IN THE PART SPHERICAL DEPRESSIONS. THE TIE MEMBERS ARE THUS ALLOWED TO MOVE RELATIVE TO THE BLADES AND TO TAKE UP THE NATURAL POSITION WITHOUT STRESSING THE BLADE UNDULY.

    Bladed rotor for a gas turbine engine
    2.
    发明授权
    Bladed rotor for a gas turbine engine 失效
    用于气体涡轮发动机的叶片转子

    公开(公告)号:US3708244A

    公开(公告)日:1973-01-02

    申请号:US3708244D

    申请日:1971-04-09

    申请人: ROLLS ROYCE

    IPC分类号: F01D5/22 F01D5/10 F01D5/24

    CPC分类号: F01D5/22

    摘要: A bladed rotor for a gas turbine engine comprising a row of blades in which each blade is tied to the next adjacent blade by a Z-shaped metal tie having a center section which is inwardly curved such that centrifugal forces acting on itself are evidenced as compressive stresses within the tie and end limbs or lugs extending from the center section in opposite directions generally chordally of the blades and each being attached to the blades by bolts spaced apart transversely of the blade, the bolts extending through the blade to also attach a similar limb or lug to the opposite blade face.

    摘要翻译: 一种用于燃气涡轮发动机的叶片转子,其包括一排叶片,其中每个叶片通过Z形金属扎带固定在下一个相邻叶片上,该Z形金属扎带具有向内弯曲的中心部分,使得作用在其上的离心力被证明为压缩 从中心部分沿相反方向延伸的连接件和端部四肢或突出部内的应力通常与叶片并排,并且每个通过与叶片横向间隔开的螺栓附接到叶片,螺栓延伸穿过叶片,以连接相似的肢体 或凸耳到相对的刀片面。