公开(公告)号：WO2014137422A1

公开(公告)日：2014-09-12

申请号：PCT/US2013/071694

申请日：2013-11-25

Applicant: ROLLS-ROYCE NORTH AMERICANTECHNOLOGIES, INC.

Inventor： SIEGEL, William, L. ,  RODRIGUEZ, Rigoberto, Jorge

IPC: B64D41/00 ,  H02J4/00

CPC classification number: B60R16/03 ,  B60L11/02 ,  B60L2200/10 ,  B60R16/0215 ,  B64D33/00 ,  B64D41/00 ,  B64D2013/0614 ,  B64D2221/00 ,  H01B7/423 ,  H01B9/0605 ,  H02J4/00 ,  Y02T50/44

Abstract: An aircraft, comprising: a wing; a fuselage coupled to the wing; an engine (34) coupled to at least one of the fuselage and the wing; an electrical load (20) associated with the aircraft during flight operations; a generator (32) coupled to the engine and configured to generate electrical power for the electrical load; a conductor (38) electrically disposed between the electrical load and the generator; a conduit (46) configured to house the conductor; and a dielectric gas (44) disposed in the conduit; wherein the conduit (46) is configured to envelop the conductor (38) in the dielectric gas (44).

Abstract translation: 一架飞机，包括：一架翼; 机身与机翼相连; 耦合到机身和机翼中的至少一个的发动机（34）; 在飞行操作期间与飞机相关联的电力负载（20）; 发电机（32），其耦合到所述发动机并且被配置为产生用于所述电负载的电力; 电气设置在电负载和发电机之间的导体（38）; 导管（46），其构造成容纳所述导体; 以及设置在所述导管中的电介质气体（44） 其中所述导管（46）构造成包围所述电介质气体（44）中的导体（38）。