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.
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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 |
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代理人 |
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主权项 |
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地址 |
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