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Aircraft having M-Wing and Gull Wing Configurations

机译:具有M翼和鸥翼构型的飞机

摘要

An aircraft includes a fuselage coupled to a wing having a dihedral root section with first and second outboard sections pivotably coupled to respective outboard ends thereof. A thrust array is coupled to the wing. A power system is operably associated with the thrust array to provide power to each of a plurality of propulsion assemblies. A flight control system is operably associated with the thrust array and the wing. The flight control system is operable to control the thrust output from the propulsion assemblies and the configuration of the wing. In a thrust-borne vertical lift mode, the wing has an M-wing configuration with the center of gravity of the aircraft located between the outboard sections of the wing. In a wing-borne forward flight mode, the wing has a gull wing configuration with the center of gravity of the aircraft located below the outboard sections of the wing.
机译:一种飞机,包括连接到机翼的机身,该机翼具有二面角的根部,第一和第二外侧部可枢转地连接到其相应的外侧端。推力阵列连接到机翼。动力系统与推力阵列可操作地相关联以向多个推进组件中的每一个提供动力。飞行控制系统可操作地与推力阵列和机翼相关联。该飞行控制系统可操作以控制来自推进组件的推力输出和机翼的构造。在推力式垂直升力模式下,机翼为M机翼配置,飞机的重心位于机翼的外侧部分之间。在机翼前飞模式中,机翼具有鸥翼构造,飞机的重心位于机翼外侧部分下方。

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