Component with spar assembly for turbine engine

A component and blade assembly for a turbine engine, the component having a wall defining an interior and defining an outer surface extending radially between a leading edge and a trailing edge to define a chordwise direction and extending between a hub and a tip to define a spanwise direction. A metal spar extends in a spanwise direction from the hub into the interior, the metal spar defining a socket. The composite spar extends in a spanwise direction between a spar root and a spar tip, the spar root being received in the socket. The component also has a reinforcement. 一种用于涡轮发动机的部件和叶片组件，该部件具有界定内部并且限定外表面的壁，外表面在前缘和后缘之间径向延伸以限定弦向方向，并且在毂和尖端之间延伸以限定翼展方向。金属翼梁在翼展方向上从毂延伸到内部中，金属翼梁限定承窝。复合翼梁在翼展方向上在翼梁根部和翼梁尖端之间延伸，翼梁根部接收在承窝中。该部件还具有加强件。