-
公开(公告)号：US20120097761A1
公开(公告)日：2012-04-26
申请号：US12863477
申请日：2009-01-09
IPC分类号： F02K1/70
CPC分类号： F02K1/72 , B64C7/02 , B64D29/06 , F05D2220/36 , F05D2300/612 , Y02T50/672
摘要： The invention relates to a twelve-hour structure for a thrust reverser, that comprises a half beam (1) capable of holding a reverser half cowling and including a plurality of hinge yokes (9c) for rotatingly mounting said half beam (1) on a nacelle-holding mast. The half beam (1) is at least partially made of a composite material.
摘要翻译： 本发明涉及一种用于推力反向器的十二小时结构，其包括能够保持反向器半罩的半梁（1），并且包括多个铰链轭（9c），用于将所述半梁（1）旋转地安装在 机舱桅杆 半梁（1）至少部分地由复合材料制成。
-
公开(公告)号：US09157395B2
公开(公告)日：2015-10-13
申请号：US12863477
申请日：2009-01-09
CPC分类号： F02K1/72 , B64C7/02 , B64D29/06 , F05D2220/36 , F05D2300/612 , Y02T50/672
摘要： The invention relates to a twelve-hour structure for a thrust reverser, that comprises a half beam (1) capable of holding a reverser half cowling and including a plurality of hinge yokes (9c) for rotatingly mounting said half beam (1) on a nacelle-holding mast. The half beam (1) is at least partially made of a composite material.
摘要翻译： 本发明涉及一种用于推力反向器的十二小时结构，其包括能够保持反向器半罩的半梁（1），并且包括多个铰链轭（9c），用于将所述半梁（1）旋转地安装在 机舱桅杆 半梁（1）至少部分地由复合材料制成。
-
公开(公告)号：US08273204B2
公开(公告)日：2012-09-25
申请号：US12864377
申请日：2008-09-22
申请人： Jean-Bernard Vache
发明人： Jean-Bernard Vache
IPC分类号： B29C65/48
CPC分类号： F02C7/24 , B29C65/48 , B29C65/5057 , B29C66/022 , B29C66/0222 , B29C66/1142 , B29C66/223 , B29C66/725 , B29C67/0044 , B29C2793/0081 , B29K2995/0002 , B29L2031/608 , B31D3/0292 , B64D2033/0206 , F05D2230/23 , F05D2230/60 , F05D2230/64 , F05D2260/96 , Y10T156/1002 , Y10T156/1003
摘要： The invention relates to a method for joining a first acoustic panel (2), having a cellular structure of the honeycomb type, with a second acoustic panel (2), wherein said method comprises the steps of: inserting at least one mandrel, (5, 8) having a shape adapted to the cells (3), into at least one cell (3) located in the vicinity of a junction edge (6) of the acoustic panel; passing a roller (12) on said junction edge of the acoustic panel; joining the junction edge of the acoustic panel together with a junction edge (6′) of the second panel and connecting the same by applying a linking means.
摘要翻译： 本发明涉及一种用于将具有蜂窝型蜂窝结构的第一声学面板（2）与第二声学面板（2）接合的方法，其中所述方法包括以下步骤：将至少一个心轴（5 ，8）具有适于所述电池（3）的形状，形成位于所述隔音板的接合边缘（6）附近的至少一个电池（3）中; 在所述声学板的所述接合边缘上通过辊（12）; 将声学面板的接合边缘与第二面板的接合边缘（6'）连接并通过施加连接装置将其连接在一起。
-
公开(公告)号：US20110011972A1
公开(公告)日：2011-01-20
申请号：US12934670
申请日：2009-02-20
申请人： Jean-Bernard Vache
发明人： Jean-Bernard Vache
IPC分类号： B64D27/26
CPC分类号： B64D27/26 , B64D2027/264 , Y02T50/44
摘要： The invention relates to an effort recovery structure (101) of a connecting strut for attaching a turboreactor to the wing system of an aircraft. Said structure comprises a first lateral block (102) and a second lateral block (103) to be attached to the wing system of the aircraft, and a spigot fastener to be attached to the turboreactor, said lateral blocks (102, 103) surrounding an essentially long central plate (104) following the main axis (105) of the structure (101). The central plate (104) is connected to the spigot fastener and is produced from a metal or an alloy that can resist a temperature of at least 1000° C. over a period of at least 15 minutes, such as to recover the static and dynamic efforts generated by the turboreactor according to the main axis (105). The invention also relates to a connecting strut for attaching a turboreactor to a wing system of an aircraft, comprising such a primary structure (101).
摘要翻译： 本发明涉及一种用于将涡轮反应器附接到飞机的翼系统的连接支柱的努力恢复结构（101）。 所述结构包括第一横向块（102）和附接到飞行器的翼系统的第二横向块（103），以及附接到涡轮反应器的接头紧固件，所述横向块（102,103）围绕着 基本上长的中心板（104）沿着结构（101）的主轴线（105）。 中心板（104）连接到接头紧固件，并且由金属或合金制成，其可以在至少15分钟的时间内抵抗至少1000℃的温度，例如恢复静态和动态 由涡轮反应器根据主轴（105）产生的努力。 本发明还涉及一种用于将涡轮反应器附接到飞行器的翼系统的连接支柱，包括这种主结构（101）。
-
公开(公告)号：US20100294422A1
公开(公告)日：2010-11-25
申请号：US12864377
申请日：2008-09-22
申请人： Jean-Bernard Vache
发明人： Jean-Bernard Vache
IPC分类号： B31D3/02
CPC分类号： F02C7/24 , B29C65/48 , B29C65/5057 , B29C66/022 , B29C66/0222 , B29C66/1142 , B29C66/223 , B29C66/725 , B29C67/0044 , B29C2793/0081 , B29K2995/0002 , B29L2031/608 , B31D3/0292 , B64D2033/0206 , F05D2230/23 , F05D2230/60 , F05D2230/64 , F05D2260/96 , Y10T156/1002 , Y10T156/1003
摘要： The invention relates to a method for joining a first acoustic panel (2), having a cellular structure of the honeycomb type, with a second acoustic panel (2), wherein said method comprises the steps of: inserting at least one mandrel, (5, 8) having a shape adapted to the cells (3), into at least one cell (3) located in the vicinity of a junction edge (6) of the acoustic panel; passing a roller (12) on said junction edge of the acoustic panel; joining the junction edge of the acoustic panel together with a junction edge (6′) of the second panel and connecting the same by applying a linking means.
摘要翻译： 本发明涉及一种用于将具有蜂窝型蜂窝型结构的第一声学面板（2）与第二声学面板（2）接合的方法，其中所述方法包括以下步骤：将至少一个心轴（5 ，8）具有适于所述电池（3）的形状，形成位于所述隔音板的接合边缘（6）附近的至少一个电池（3）中; 在所述声学板的所述接合边缘上通过辊（12）; 将声学面板的接合边缘与第二面板的接合边缘（6'）连接并通过施加连接装置将其连接在一起。
-
公开(公告)号：US07004725B2
公开(公告)日：2006-02-28
申请号：US10416161
申请日：2001-11-29
CPC分类号： F02C7/00
摘要： A device for centering a component positioned inside and rotationally secured at its end to a turbine hollow shaft positioned in a gas turbine engine. The device includes a sheath enclosing and solidly joined to the component, and an elastic ring interposed between the sheath and the shaft. The ring includes a plurality of pairs of opposed shoes extending radially outwardly therefrom and configured to radially expand so as to extend against an inner portion of the shaft. The shoes include thin, elastic cylindrical walls having an external diameter configured slightly less than the internal diameter of the shaft prior to assembly onto the shaft, and arranged to expand to the inner wall of the shaft when assembled thereon.
摘要翻译： 定位在内部并将其端部旋转地固定到位于燃气涡轮发动机中的涡轮空心轴的部件的装置。 该装置包括包封并牢固地连接到部件的护套，以及插入护套和轴之间的弹性环。 环包括多对相对的鞋，其从其径向向外延伸并且构造成径向膨胀以抵靠轴的内部部分延伸。 鞋包括薄的弹性圆柱形壁，其具有在组装到轴之前稍微小于轴的内径的外径，并且被布置成当组装在其上时扩展到轴的内壁。
-
-
-
-
-
搜索结果
6 条记录 (耗时 0.018 秒)