公开(公告)号：US20150344145A1

公开(公告)日：2015-12-03

申请号：US14655761

申请日：2013-11-26

Applicant: GENERAL ELECTRIC COMPANY

Inventor： Michael Jay EPSTEIN ,  Paul Bernard STUMBO ,  Robert Harold WEISGERBER

IPC: B64D37/30 ,  F17C3/00

CPC classification number: B64D37/30 ,  B64D37/32 ,  F02C7/14 ,  F02C7/224 ,  F02C9/40 ,  F05D2260/213 ,  F05D2260/98 ,  F17C3/00 ,  Y02T50/44 ,  Y02T50/672 ,  Y02T50/676 ,  Y02T90/44

Abstract: An aircraft having a turbine engine having a bleed air output line, a cryogenic fuel system having a cryogenic fuel tank for storing cryogenic fuel and a supply line operably coupling the tank to the turbine engine, and an on board inert gas generating system (OBIGGS) fluidly coupled to the bleed air output and having a nitrogen rich stream output line and an oxygen rich stream output line.

Abstract translation: 具有具有排气输出管线的涡轮发动机的飞机，具有用于存储低温燃料的低温燃料箱的低温燃料系统和可操作地将罐连接到涡轮发动机的供应管线以及船上惰性气体发生系统（OBIGGS） 流体耦合到放气输出并具有富氮流输出管线和富氧流输出管线。