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11. 发明授权

US08104708B2 Suspension for mounting a turbojet engine on an aircraft 有权
标题翻译：悬挂在飞机上安装涡轮喷气发动机
公开(公告)号：US08104708B2
公开(公告)日：2012-01-31
申请号：US12329136
申请日：2008-12-05
申请人： Pierre-Alain Jean-Marie Philippe Hugues Chouard , Guillaume Lefort
发明人： Pierre-Alain Jean-Marie Philippe Hugues Chouard , Guillaume Lefort
IPC分类号： F02C7/20
CPC分类号： B64D27/26 , B64D2027/268
摘要： The present invention relates to an isostatic suspension for mounting a turbojet engine on a pylon of an aircraft, the turbojet engine comprising a front fan, an intermediate casing downstream of the fan with an outer shell and a hub interconnected by radial arms, and an exhaust casing with an outer shell on the same axis XX, the suspension comprising a front attachment on the intermediate casing, a rear attachment with at least two rear attachment links connected to the outer shell of the exhaust casing, a pair of thrust bars being fixed at their upstream ends to the hub of the intermediate casing. It is characterized in that the plane formed by the two links of the rear attachment is inclined with respect to the plane of the exhaust casing.
摘要翻译：技术领域本发明涉及一种用于将涡轮喷气发动机安装在飞机的塔架上的等静压悬架，该涡轮喷气发动机包括前风扇，具有外壳的风扇下游的中间壳体和通过径向臂互连的轮毂，以及排气壳体，其具有在相同轴线XX上的外壳，悬架包括在中间壳体上的前部附件，后部附件，其具有连接到排气壳体的外部壳体的至少两个后部附接链节，一对推杆固定在它们的上游端到达中间壳体的毂。其特征在于，由后附件的两个连杆形成的平面相对于排气套的平面倾斜。

12. 发明申请

US20110001002A1 SUSPENSION FOR MOUNTING A TURBOJET ENGINE ON AN AIRCRAFT 有权
标题翻译：用于在飞机上安装涡轮发动机的悬架
公开(公告)号：US20110001002A1
公开(公告)日：2011-01-06
申请号：US12329136
申请日：2008-12-05
申请人： Pierre-Alain Jean-Marie Philippe Hugues CHOUARD , Guillaume LEFORT
发明人： Pierre-Alain Jean-Marie Philippe Hugues CHOUARD , Guillaume LEFORT
IPC分类号： B64D27/00
CPC分类号： B64D27/26 , B64D2027/268
摘要： The present invention relates to an isostatic suspension for mounting a turbojet engine on a pylon of an aircraft, the turbojet engine comprising a front fan, an intermediate casing downstream of the fan with an outer shell and a hub interconnected by radial arms, and an exhaust casing with an outer shell on the same axis XX, the suspension comprising a front attachment on the intermediate casing, a rear attachment with at least two rear attachment links connected to the outer shell of the exhaust casing, a pair of thrust bars being fixed at their upstream ends to the hub of the intermediate casing. It is characterized in that the plane formed by the two links of the rear attachment is inclined with respect to the plane of the exhaust casing.
摘要翻译：技术领域本发明涉及一种用于将涡轮喷气发动机安装在飞机的塔架上的等静压悬架，该涡轮喷气发动机包括前风扇，风扇下游的外壳和通过径向臂互连的轮毂和排气壳体，其具有在相同轴线XX上的外壳，悬架包括在中间壳体上的前部附件，后部附件，其具有连接到排气壳体的外部壳体的至少两个后部附接链节，一对推杆固定在它们的上游端到达中间壳体的毂。其特征在于，由后附件的两个连杆形成的平面相对于排气套的平面倾斜。

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