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Turbine engine with low lift global force transverse hydraulic turbines

机译:具有低升程全力横向水力涡轮机的涡轮发动机

摘要

The invention relates to a turbine engine that includes at least first and second lift turbine stacks with transverse flow. The shafts of adjacent turbines in the first stack are connected by a first coupling device adapted for compensating space misalignments, and the shafts of adjacent turbines in the first stack are connected by a second coupling device adapted for compensating for space misalignments. The turbine engine includes a device for supporting the first and second turbine stacks, which is symmetrical to said plane, and a control device adapted for permanently maintaining the symmetry between the first and second turbine stacks relative to the plane, and for maintaining the rotation speeds of the first and second turbine stacks at equal values in opposite rotation directions.
机译:涡轮发动机技术领域本发明涉及一种涡轮发动机,其至少包括具有横向流的第一和第二提升涡轮机堆。第一烟囱中的相邻涡轮的轴通过适于补偿空间偏差的第一联接装置连接,并且第一烟囱中的相邻涡轮的轴通过适于校正空间偏差的第二联接装置连接。该涡轮发动机包括:用于支撑相对于所述平面对称的第一和第二涡轮机堆的装置;以及控制装置,其适于永久地保持第一和第二涡轮机堆之间相对于平面的对称性,并且用于维持旋转速度。在相反的旋转方向上,第一和第二涡轮机烟囱的角度相等。

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