发明名称 Oxygen supply system for an aircraft
摘要 An oxygen supply system for an aircraft includes a control valve, a reservoir bag, a respiration device and a sensor device, wherein the control valve is designed in such a way that oxygen can be supplied to the reservoir bag until a predetermined quantity of oxygen is adjusted in the reservoir bag. The respiration device may be designed in such a way that breathing gas can be provided for a passenger. The sensor device may be designed in such a way that an exhalation is detectable. The reservoir bag may be designed in such a way that a predetermined quantity of oxygen can be metered into the reservoir bag during the exhalation. The reservoir bag may be designed in such a way that breathing gas can be supplied to the respiration device in a pulse-like fashion. The oxygen supply system may include a first and a second operation mode.
申请公布号 US8517018(B2) 申请公布日期 2013.08.27
申请号 US20080600006 申请日期 2008.05.13
申请人 WENZEL JUERGEN;WITTKOWSKI MARTIN;DEUTSCHER WALTER;SCHECKER JOERN;LUKS NORBERT;KNAAK SIMON;AIRBUS OPERATIONS GMBH 发明人 WENZEL JUERGEN;WITTKOWSKI MARTIN;DEUTSCHER WALTER;SCHECKER JOERN;LUKS NORBERT;KNAAK SIMON
分类号 A62B7/00;A61M16/00;A62B18/02 主分类号 A62B7/00
代理机构 代理人
主权项
地址