公开(公告)号：US20110006534A1

公开(公告)日：2011-01-13

申请号：US12738675

申请日：2008-10-23

申请人： Jean-Luc Achard ,  Didier Imbault ,  Ali Tourabi

发明人： Jean-Luc Achard ,  Didier Imbault ,  Ali Tourabi

IPC分类号： F03B13/10 ,  F01K23/00

CPC分类号： F03B17/063 ,  F05B2240/93 ,  Y02E10/28 ,  Y02E10/38 ,  Y10S415/907

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.

摘要翻译： 本发明涉及一种涡轮发动机，其包括具有横向流动的至少第一和第二提升涡轮机组。 第一堆叠中的相邻涡轮机的轴通过适于补偿空间不对准的第一联接装置连接，并且第一堆叠中的相邻涡轮机的轴通过适于补偿空间未对准的第二联接装置连接。 涡轮发动机包括用于支撑与所述平面对称的第一和第二涡轮机叠层的装置，以及适于永久地保持第一和第二涡轮机叠层相对于该平面之间的对称性并用于保持转速的控制装置 的第一和第二涡轮机组在相反的旋转方向上具有相等的值。

公开(公告)号：US08827631B2

公开(公告)日：2014-09-09

申请号：US12738675

申请日：2008-10-23

申请人： Jean-Luc Achard ,  Didier Imbault ,  Ali Tourabi

发明人： Jean-Luc Achard ,  Didier Imbault ,  Ali Tourabi

IPC分类号： F03B13/10 ,  F03B17/06

CPC分类号： F03B17/063 ,  F05B2240/93 ,  Y02E10/28 ,  Y02E10/38 ,  Y10S415/907

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.

摘要翻译： 本发明涉及一种涡轮发动机，其包括具有横向流动的至少第一和第二提升涡轮机组。 第一堆叠中的相邻涡轮机的轴通过适于补偿空间不对准的第一联接装置连接，并且第一堆叠中的相邻涡轮机的轴通过适于补偿空间未对准的第二联接装置连接。 涡轮发动机包括用于支撑与所述平面对称的第一和第二涡轮机叠层的装置，以及适于永久地保持第一和第二涡轮机叠层相对于该平面之间的对称性并用于保持转速的控制装置 的第一和第二涡轮机组在相反的旋转方向上具有相等的值。