专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 发明授权

US08256708B2 Device for attaching an aircraft engine comprising a thrust force take-up device with a compact design 有权
标题翻译：用于附接具有紧凑设计的推力牵引装置的飞机发动机的装置
公开(公告)号：US08256708B2
公开(公告)日：2012-09-04
申请号：US12674555
申请日：2008-08-22
申请人： Emmanuel Guillet , Jean-Marc Martinou , Pascal Gardes
发明人： Emmanuel Guillet , Jean-Marc Martinou , Pascal Gardes
IPC分类号： B64D27/00
CPC分类号： B64D27/26 , B64D2027/264 , B64D2027/268
摘要： An aircraft engine attachment device including a rigid structure and a mechanism attaching the engine on the rigid structure, the attachment mechanism including a rear engine attachment and a device for taking-up thrust forces generated by the engine. The rear engine attachment is attached to the rigid structure by two lateral fittings attached to the rigid structure. The force take-up device includes two connecting rods mechanically connected to a spreader beam by a mechanical connection, a connection fitting attached to the rear engine attachment and mechanically connected to the rigid structure by a thrust pin, the lateral fittings including a stop mechanism to limit pivoting of the spreader beam if a connecting rod breaks and ensuring transmission of thrust forces to the rigid structure.
摘要翻译：一种飞机发动机附接装置，包括刚性结构和将发动机附接在刚性结构上的机构，所述附接机构包括后部发动机附件和用于吸收由发动机产生的推力的装置。后部发动机附件通过附接到刚性结构的两个侧向配件附接到刚性结构。力吸收装置包括通过机械连接机械地连接到吊架梁的两个连杆，连接到后发动机附件的连接配件并通过推力销机械地连接到刚性结构件，该横向配件包括止动机构如果连杆断裂并确保将推力传递到刚性结构，则吊具梁的极限枢转。

2. 发明申请

US20110114786A1 DEVICE FOR ATTACHING AN AIRCRAFT ENGINE COMPRISING A THRUST FORCE TAKE-UP DEVICE WITH A COMPACT DESIGN 有权
标题翻译：用于连接包含具有紧凑设计的推力装置的飞机发动机的装置
公开(公告)号：US20110114786A1
公开(公告)日：2011-05-19
申请号：US12674555
申请日：2008-08-22
申请人： Emmanuel Guillet , Jean-Marc Martinou , Pascal Gardes
发明人： Emmanuel Guillet , Jean-Marc Martinou , Pascal Gardes
IPC分类号： B64D27/02 , B64D27/26
CPC分类号： B64D27/26 , B64D2027/264 , B64D2027/268
摘要： An aircraft engine attachment device including a rigid structure and a mechanism attaching the engine on the rigid structure, the attachment mechanism including a rear engine attachment and a device for taking-up thrust forces generated by the engine. The rear engine attachment is attached to the rigid structure by two lateral fittings attached to the rigid structure. The force take-up device includes two connecting rods mechanically connected to a spreader beam by a mechanical connection, a connection fitting attached to the rear engine attachment and mechanically connected to the rigid structure by a thrust pin, the lateral fittings including a stop mechanism to limit pivoting of the spreader beam if a connecting rod breaks and ensuring transmission of thrust forces to the rigid structure.
摘要翻译：一种飞机发动机附接装置，包括刚性结构和将发动机附接在刚性结构上的机构，所述附接机构包括后部发动机附件和用于吸收由发动机产生的推力的装置。后部发动机附件通过附接到刚性结构的两个侧向配件附接到刚性结构。力吸收装置包括通过机械连接机械地连接到吊架梁的两个连杆，连接到后发动机附件的连接配件并通过推力销机械地连接到刚性结构件，该横向配件包括止动机构如果连杆断裂并确保将推力传递到刚性结构，则吊具梁的极限枢转。

3. 发明授权

US08205826B2 Device for attaching an aircraft engine and aircraft comprising at least one such device 有权
标题翻译：用于连接包括至少一个这种装置的飞机发动机和飞行器的装置
公开(公告)号：US08205826B2
公开(公告)日：2012-06-26
申请号：US12594455
申请日：2008-04-11
申请人： Stephane Combes , Emmanuel Guillet
发明人： Stephane Combes , Emmanuel Guillet
IPC分类号： B64D27/00
CPC分类号： B64D27/26 , B64D2027/268
摘要： A device for attaching an aircraft engine including a thrust force take-up device that includes a main fitting to be fixed to an engine mounting beam fixed to a box structure, an additional fitting fixed to the main fitting, and two load reacting link rods connected to the main fitting by a balance beam, each of the link rods being connected to the balance beam by a first longitudinal end by a first mechanical connection that has at least one axis of rotation, each of the link rods being connected to the additional fitting by a second longitudinal end by a second mechanical connection that has at least one axis of rotation, the second mechanical connection having play, the first and second mechanical connections having at least one axis of rotation in common.
摘要翻译：一种用于附接飞行器发动机的装置，包括：推力牵引装置，其包括固定到固定到箱结构的发动机安装梁的主配件，固定到主配件的附加配件以及连接的两个负载反作用连杆通过平衡梁到主配件，每个连杆通过具有至少一个旋转轴线的第一机械连接件通过第一纵向端连接到平衡梁上，每个连杆连接到附加配件通过具有至少一个旋转轴线的第二机械连接的第二纵向端，所述第二机械连接具有打开，所述第一和第二机械连接具有至少一个共同旋转轴线。

4. 发明申请

US20100116926A1 DEVICE FOR ATTACHING AN AIRCRAFT ENGINE AND AIRCRAFT COMPRISING AT LEAST ONE SUCH DEVICE 有权
标题翻译：用于连接飞机发动机的设备和包含至少一个此类设备的飞机
公开(公告)号：US20100116926A1
公开(公告)日：2010-05-13
申请号：US12594455
申请日：2008-04-11
申请人： Stephane Combes , Emmanuel Guillet
发明人： Stephane Combes , Emmanuel Guillet
IPC分类号： B64D27/00
CPC分类号： B64D27/26 , B64D2027/268
摘要： A device for attaching an aircraft engine including a thrust force take-up device that includes a main fitting to be fixed to an engine mounting beam fixed to a box structure, an additional fitting fixed to the main fitting, and two load reacting link rods connected to the main fitting by a balance beam, each of the link rods being connected to the balance beam by a first longitudinal end by a first mechanical connection that has at least one axis of rotation, each of the link rods being connected to the additional fitting by a second longitudinal end by a second mechanical connection that has at least one axis of rotation, the second mechanical connection having play, the first and second mechanical connections having at least one axis of rotation in common.
摘要翻译：一种用于附接飞行器发动机的装置，包括：推力牵引装置，其包括固定到固定到箱结构的发动机安装梁的主配件，固定到主配件的附加配件以及连接的两个负载反作用连杆通过平衡梁到主配件，每个连杆通过具有至少一个旋转轴线的第一机械连接件通过第一纵向端连接到平衡梁上，每个连杆连接到附加配件通过具有至少一个旋转轴线的第二机械连接的第二纵向端，所述第二机械连接具有打开，所述第一和第二机械连接具有至少一个共同旋转轴线。

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式