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TURBINE ENGINE WITH TRANSVERSE-FLOW HYDRAULIC TURBINES HAVING REDUCED TOTAL LIFT FORCE

机译:横向流动液压涡轮的涡轮发动机总升力降低

摘要

The invention relates to a turbine engine (55) that includes at least firstand second lift turbine stacks (53A, 53B)with transverse flow. The shafts of adjacent turbines in the first stack areconnected by a first coupling device adapted for compensatingspace misalignments, and the shafts of adjacent turbines in the first stackare connected by a second coupling device adaptedfor compensating for space misalignments. The turbine engine includes a device(46, 48) for supporting the first and second turbinestacks, which is symmetrical to said plane, and a control device (220A, 220B,224) adapted for permanently maintaining the symmetrybetween the first and second turbine stacks relative to the plane, and formaintaining the rotation speeds of the first and secondturbine stacks at equal values in opposite rotation directions.
机译:本发明涉及一种涡轮发动机(55),其至少包括第一和第二个提升涡轮机烟囱(53A,53B)横向流动。第一组中相邻涡轮的轴是通过适于补偿的第一耦合装置连接空间未对准以及第一堆中相邻涡轮的轴通过适合的第二连接装置连接用于补偿空间偏差。涡轮发动机包括装置(46、48)用于支撑第一和第二涡轮机相对于所述平面对称的堆栈和控制装置(220A,220B,224)适用于永久保持对称相对于飞机在第一和第二涡轮机堆之间保持第一和第二的旋转速度涡轮在相反的旋转方向上以相等的值堆叠。

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