-
1.发明申请ROTATING INLET COWL FOR A TURBINE ENGINE, COMPRISING AN ECCENTRIC FORWARD END 有权用于涡轮发动机的旋转进气口，包括前进端公开(公告)号：US20120036827A1
公开(公告)日：2012-02-16
申请号：US13262386
申请日：2010-03-29
IPC分类号： F02C7/047
CPC分类号： F02C7/047 , F02C6/206 , F02K3/06 , Y02T50/671 , Y02T50/672 , Y10T137/0536 , Y10T137/0645
摘要： A rotating inlet cowl for a turbine engine, having a rotation axis and for which the forward end is arranged to be eccentric relative to this rotation axis. Furthermore, a forward cone of the cowl is truncated by a truncation surface defining the forward end of the inlet cowl.
摘要翻译： 一种用于涡轮发动机的旋转入口罩，具有旋转轴线，并且前端相对于该旋转轴线布置成偏心。 此外，整流罩的前锥体被限定入口罩的前端的截头表面截断。
-
2.发明授权Engine and pod assembly for an aircraft, equipped with an anti-icing device including a source of radiation and pulse control unit connected to the source of radiation 有权用于飞机的发动机和荚组件，配备有包括辐射源的防冰装置和连接到辐射源的脉冲控制单元公开(公告)号：US08997451B2
公开(公告)日：2015-04-07
申请号：US13256308
申请日：2010-03-12
申请人： François Dufresne de Virel , Michel Pealat , Patrick Joyez , Bruce Pontoizeau , Jean-François Lacuisse , Sylvie Wintenberger
发明人： François Dufresne de Virel , Michel Pealat , Patrick Joyez , Bruce Pontoizeau , Jean-François Lacuisse , Sylvie Wintenberger
摘要： An engine and pod assembly for an aircraft includes a pod receiving an engine having an air intake. A rotating nose cone extends on the nose cone, as well as a device for limiting the formation of ice. The device includes means for creating a circumferential heterogeneity of ice on the nose cone.
摘要翻译： 用于飞行器的发动机和舱组件包括容纳具有进气口的发动机的舱。 旋转的鼻锥在鼻锥上延伸，以及用于限制冰的形成的装置。 该装置包括用于在鼻锥上产生圆周异质性的装置。
-
3.发明授权Rotating inlet cowl for a turbine engine, comprising an eccentric forward end 有权用于涡轮发动机的旋转入口罩，包括偏心的前端公开(公告)号：US08984855B2
公开(公告)日：2015-03-24
申请号：US13262386
申请日：2010-03-31
IPC分类号： F02G3/00 , F02K1/78 , F02K99/00 , F02K3/06 , B64D15/16 , B64D15/00 , F03B15/22 , F03D11/04 , F04D29/60 , F04D29/52 , F02C7/047 , F02C6/20
CPC分类号： F02C7/047 , F02C6/206 , F02K3/06 , Y02T50/671 , Y02T50/672 , Y10T137/0536 , Y10T137/0645
摘要： A rotating inlet cowl for a turbine engine, having a rotation axis and for which the forward end is arranged to be eccentric relative to this rotation axis. Furthermore, a forward cone of the cowl is truncated by a truncation surface defining the forward end of the inlet cowl.
摘要翻译： 一种用于涡轮发动机的旋转入口罩，具有旋转轴线，并且前端相对于该旋转轴线布置成偏心。 此外，整流罩的前锥体被限定入口罩的前端的截头表面截断。
-
4.发明申请ENGINE AND POD ASSEMBLY FOR AN AIRCRAFT, EQUIPPED WITH AN ANTI-ICING DEVICE 有权用于装备有防盗装置的飞机的发动机和油缸组件公开(公告)号：US20120036826A1
公开(公告)日：2012-02-16
申请号：US13256308
申请日：2010-03-12
申请人： Francois Dufresne De Virel , Michel Pealat , Patrick Joyez , Bruce Pontoizeau , Jean-Francois Lacuisse , Sylvie Wintenberger
发明人： Francois Dufresne De Virel , Michel Pealat , Patrick Joyez , Bruce Pontoizeau , Jean-Francois Lacuisse , Sylvie Wintenberger
IPC分类号： F02C7/04
摘要： An engine and pod assembly for an aircraft includes a pod receiving an engine having an air intake. A rotating nose cone extends on the nose cone, as well as a device for limiting the formation of ice. The device includes means for creating a circumferential heterogeneity of ice on the nose cone.
摘要翻译： 用于飞行器的发动机和舱组件包括容纳具有进气口的发动机的舱。 旋转的鼻锥在鼻锥上延伸，以及用于限制冰的形成的装置。 该装置包括用于在鼻锥上产生圆周异质性的装置。
-
-
-
搜索结果
4 条记录 (耗时 0.01 秒)
