公开(公告)号：US20120153752A1

公开(公告)日：2012-06-21

申请号：US13316832

申请日：2011-12-12

申请人： Martin HAAS ,  Jochen Huebl ,  Roland Mager

发明人： Martin HAAS ,  Jochen Huebl ,  Roland Mager

IPC分类号： H02K11/02 ,  H05K9/00 ,  H05K13/04

CPC分类号： H05K9/0018 ,  B60T8/368 ,  H01H50/10 ,  H02K5/225 ,  H02K7/14 ,  H02K11/024 ,  H02K11/026 ,  Y10T29/49009

摘要： An actuator apparatus is described as having a stator device, a cover device, a contact device and an attenuation device. The stator device and the cover device are joined in such a manner so that a hollow space is formed between the stator device and the cover device. The cover device has an opening, through which the contact device is guided into the hollow space, so that the contact device runs at least partially in the hollow space and at least partially in the cover device. The attenuation device is positioned in the opening in such a manner so that a high-frequency electromagnetic radiation that travels through the opening is more highly attenuated by the attenuation device than the radiation would be attenuated without the presence of the attenuation device.

摘要翻译： 致动器装置被描述为具有定子装置，盖装置，接触装置和衰减装置。 定子装置和盖装置以这样的方式接合，使得在定子装置和盖装置之间形成中空空间。 盖装置具有开口，接触装置通过该开口被引导到中空空间中，使得接触装置至少部分地在中空空间中延伸并且至少部分地在覆盖装置中延伸。 衰减装置以这样的方式定位在开口中，使得穿过开口的高频电磁辐射被衰减装置高度衰减，而不会衰减衰减装置。

公开(公告)号：US20090155067A1

公开(公告)日：2009-06-18

申请号：US11956460

申请日：2007-12-14

申请人： Martin HAAS

发明人： Martin HAAS

IPC分类号： F01D1/02

CPC分类号： F02C7/045 ,  B64D33/02 ,  B64D2033/0226 ,  B64D2033/0286 ,  F05D2240/127

摘要： A nacelle assembly for a turbine engine has a cowl. The cowl extends along an axis and has an exterior surface spaced from an interior surface. The interior surface forms an air inlet for directing airflow to the turbine engine. A turbulator for creating turbulence is disposed on one of the interior surface and the exterior surface.

摘要翻译： 用于涡轮发动机的机舱组件具有整流罩。 整流罩沿轴线延伸并且具有与内表面间隔开的外表面。 内表面形成用于将气流引导到涡轮发动机的空气入口。 用于产生湍流的湍流器设置在内表面和外表面之一上。