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ROTOR FAN turbojet-powered aircraft

机译:转子风扇涡轮喷气发动机

摘要

FIELD: transport.;SUBSTANCE: fan rotor contains fan blades (15) attached to periphery of wheel (13). Each blade has blade tail engaged with groove in this wheel and held in it by main fixture (28). The main fixture is engaged with slots (34) formed adjacent to superposed end of corresponding groove and on each its side to counteract blade tail movement in axial direction. The main fixture (28) is connected with additional fixture differing from the main fixture. Additional fixture is spaced from the main fixture by predetermined distance. The additional fixture (32) is located between the main fixture and superposed end of blade tail engaged with groove. The additional fixture (32) preferably is thin wall.;EFFECT: invention allows fixture to dissipate impact energy and minimise damage to adjacent blades and parts while keeping structure simple and cheap.;6 cl, 6 dwg
机译:领域:运输;实体:风扇转子的风扇叶片(15)固定在轮(13)的外围。每个叶片的叶片尾部与该轮上的凹槽啮合,并由主固定装置(28)固定在其中。主夹具与邻近相应凹槽的叠置端并在其每一侧上形成的槽(34)接合,以抵消叶片沿轴向的尾部移动。主固定装置(28)与不同于主固定装置的附加固定装置连接。附加固定装置与主固定装置间隔预定距离。附加固定装置(32)位于主固定装置和与凹槽接合的叶片尾部的重叠端之间。额外的固定装置(32)最好是薄壁。效果:本发明允许固定装置消散冲击能量,并最大程度地减少对相邻叶片和零件的损坏,同时保持结构简单和便宜。; 6 cl,6 dwg

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