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Inlet nose cone assembly, inlet nose cone assembly repair kit, and inlet nose cone assembly repair method

机译:进气口鼻锥组件,进气口鼻锥组件维修套件和进气口鼻锥组件维修方法

摘要

An inlet nose cone assembly for a gas turbine comprises an inlet nose cone 15 formed of a composite material having a flange 100 extending radially inward from a first circumferentially extending location 80 for attachment to a rotor disk; an aft fairing 105 formed of a composite material having a first stiffness to mass ratio, the aft fairing 105 being integral with the inlet nose cone 15 and extending in cantilevered fashion rearward from the first circumferentially extending location; a circumferentially continuous outer ring 90 formed of a material having a second stiffness to mass ratio that is greater than the first stiffness to mass ratio of the aft fairing 105, the outer ring 99 having an interior surface attached to the exterior surface of the aft fairing and the exterior surface of the inlet nose cone. IMAGE
机译:一种用于燃气轮机的进气鼻锥组件,包括由复合材料形成的进气鼻锥15,该进气鼻锥15具有从第一周向延伸位置80径向向内延伸以连接至转子盘的凸缘100。后整流罩105由具有第一刚度质量比的复合材料形成,后整流罩105与入口鼻锥15成一体并且以悬臂方式从第一周向延伸位置向后延伸。圆周连续的外环90,该外环90由第二刚性/质量比大于后整流罩105的第一刚性/质量比的材料形成,外环99的内表面附接到后整流罩的外表面和入口鼻锥的外表面。 <图像>

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