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1. 发明授权

US07445179B2 Engine assembly for aircraft 有权
标题翻译：飞机发动机总成
公开(公告)号：US07445179B2
公开(公告)日：2008-11-04
申请号：US11527622
申请日：2006-09-27
申请人： Lionel Diochon , Frederic Journade , Laurent LaFont , Mickael Sarrato , Alain Razafindrabe
发明人： Lionel Diochon , Frederic Journade , Laurent LaFont , Mickael Sarrato , Alain Razafindrabe
IPC分类号： B64D29/00
CPC分类号： B64D27/26 , B64D2027/268
摘要： The invention relates to an engine suspension pylon for an aircraft including a rigid structure provided with a box (24), this pylon also including an engine aft attachment (8) provided with an attachment body (38), and a thrust resistance device (9) generated by the engine. The rigid structure according to the invention includes an offset rib (35) for the attachment body (38), this rib (35) being mounted fixed on the box (24) between the box and the engine (2) and carrying the attachment body. Furthermore, the device (9) includes a thrust resistance spar (9b) of which the forward end is mounted fixed on the rib (35), and the aft end is mounted fixed on the box.
摘要翻译：本发明涉及一种用于飞行器的发动机悬挂塔，其包括设置有箱体（24）的刚性结构，该塔架还包括设置有附接体（38）的发动机后部附件（8）和推力阻力装置（9））。根据本发明的刚性结构包括用于附接体（38）的偏移肋（35），该肋（35）固定在箱体和发动机（2）之间的箱体（24）上并承载附着体。此外，装置（9）包括固定在肋（35）上的前端安装的推力阻力梁（9b），后端安装在箱体上。

2. 发明申请

US20070069069A1 Engine assembly for aircraft 有权
标题翻译：飞机发动机总成
公开(公告)号：US20070069069A1
公开(公告)日：2007-03-29
申请号：US11527622
申请日：2006-09-27
申请人： Lionel Diochon , Frederic Journade , Laurent LaFont , Mickael Sarrato , Alain Razafindrabe
发明人： Lionel Diochon , Frederic Journade , Laurent LaFont , Mickael Sarrato , Alain Razafindrabe
IPC分类号： B64D27/00
CPC分类号： B64D27/26 , B64D2027/268
摘要： The invention relates to an engine suspension pylon for an aircraft including a rigid structure provided with a box (24), this pylon also including an engine aft attachment (8) provided with an attachment body (38), and a thrust resistance device (9) generated by the engine. The rigid structure according to the invention includes an offset rib (35) for the attachment body (38), this rib (35) being mounted fixed on the box (24) between the box and the engine (2) and carrying the attachment body. Furthermore, the device (9) includes a thrust resistance spar (9b) of which the forward end is mounted fixed on the rib (35), and the aft end is mounted fixed on the box.
摘要翻译：本发明涉及一种用于飞行器的发动机悬挂塔，其包括设置有箱体（24）的刚性结构，该塔架还包括设置有附接体（38）的发动机后部附件（8）和推力阻力装置（9））。根据本发明的刚性结构包括用于附接体（38）的偏移肋（35），该肋（35）固定在箱体和发动机（2）之间的箱体（24）上并承载附着体。此外，装置（9）包括固定在肋（35）上的前端安装的推力阻力梁（9b），后端安装在箱体上。

3. 发明授权

US08038092B2 Engine assembly for aircraft 有权
标题翻译：飞机发动机总成
公开(公告)号：US08038092B2
公开(公告)日：2011-10-18
申请号：US12088450
申请日：2006-09-26
申请人： Lionel Diochon , Jean-Michel Cetout , Laurent LaFont
发明人： Lionel Diochon , Jean-Michel Cetout , Laurent LaFont
IPC分类号： B64D27/00
CPC分类号： B64D27/26 , B64D2027/264 , B64D2027/266
摘要： An aircraft engine assembly including a turbojet engine, an engine mount, and a plurality of engine attachments. The engine attachments include first and second forward attachments fixed to a fan case and located symmetrically in relation to a plane defined by a longitudinal axis of the turbojet engine and a vertical direction thereof, both forward attachments configured to transfer loads exerted in a longitudinal direction of the turbojet engine and in the vertical direction thereof. Moreover, each of the two forward attachments includes a shear pin mounted on the case and going through two walls of a clevis fixed on the engine mount.
摘要翻译：包括涡轮喷气发动机，发动机支架和多个发动机附件的飞机发动机组件。发动机附件包括固定到风扇壳体并相对于由涡轮喷气发动机的纵向轴线及其垂直方向限定的平面对称地定位的第一和第二前部附件，两个前部附件构造成传递沿纵向方向施加的载荷涡轮喷气发动机和其垂直方向。此外，两个前置附件中的每一个包括安装在壳体上并穿过固定在发动机支架上的U形夹的两个壁的剪切销。

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