| 摘要 |
A locking spacer assembly in a gap between adjacent blade structures (22) in a turbine engine includes opposed side edge members(48,50), opposed end members (100,102), and a cap member (130). The side edge members include a recessed portion along a top surface thereof and define a groove along an inner edge. The end members include opposed tongue members that are received within the grooves of the respective side edge members to prevent radial movement of the end members relative to the side edge members. The end members further include a projection extending from an inner edge thereof toward the opposed end member. The cap member is received by the recessed portions of the side edge members, wherein rotation of the cap member causes notches of the cap member to receive the projections of the end members to prevent radial movement of the cap member relative to the end members. |
