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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 present invention relates to a turbine engine (55) comprising at least a first and a second lift type cross-flow turbine stack (53A, 53B). The axes of adjacent turbines in the first stack are connected by a first coupling device configured to compensate for spatial misalignment and the axes of adjacent turbines in the first stack are connected by a second coupling device configured to compensate for spatial misalignment. The turbine engine includes devices (46, 48) for supporting the first and second turbine stacks, and control devices (220A, 220B) configured to permanently maintain symmetry between the first and second turbine stacks , 224), which control device is configured to maintain the rotational speeds of the first and second turbine stacks at the same magnitude in the opposite direction.
机译:涡轮发动机(55)技术领域本发明涉及一种涡轮发动机(55),该涡轮发动机(55)至少包括第一和第二升程式错流涡轮烟囱(53A,53B)。第一堆中的相邻涡轮机的轴线通过配置为补偿空间不对准的第一联接装置连接,并且第一堆中的相邻涡轮机的轴线通过构造为补偿空间不对准的第二联接装置连接。涡轮发动机包括用于支撑第一涡轮机堆和第二涡轮机堆的装置(46、48)以及构造成永久地保持第一涡轮机堆和第二涡轮机堆224之间的对称性的控制装置(220A,220B),该控制装置被构造成保持在相反方向上,第一和第二涡轮机堆栈的旋转速度相同。

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