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公开(公告)号：US20130098451A1
公开(公告)日：2013-04-25
申请号：US13278900
申请日：2011-10-21
申请人： David Scott Krug
发明人： David Scott Krug
IPC分类号： F16K31/18
CPC分类号： B64D37/32 , B64D37/22 , F16K24/048 , F16K31/22 , Y10T137/0318 , Y10T137/053 , Y10T137/7358 , Y10T137/7485
摘要： A fuel system for an aircraft has a vent system. The system has a conduit opening into the fuel section. The system has a member connected to the conduit at a proximal end. The member has a seal plate within the conduit sealing the opening into the fuel section when a buoyant section at a distal end rises along with the seal plate through the member with a rise in fluid level within the fuel section.
摘要翻译： 用于飞行器的燃料系统具有排气系统。 该系统具有通向燃料部分的导管。 系统具有在近端连接到导管的构件。 当在远端的浮力部分与密封板一起通过该构件而升高燃料部分内的液位时，该构件具有在导管内的密封板将开口密封到燃料部分中。
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公开(公告)号：US08789794B2
公开(公告)日：2014-07-29
申请号：US13219389
申请日：2011-08-26
申请人： David Scott Krug
发明人： David Scott Krug
CPC分类号： B64D37/32 , Y10T137/7481
摘要： A method and apparatus comprising a tube, an opening in the tube, and a valve associated with the opening. The tube is configured to carry an inert gas in a fuel tank. The valve is configured to control an amount of the inert gas that exits the opening based on a level of fuel relative to the opening.
摘要翻译： 一种包括管，管中的开口和与开口相关联的阀的方法和装置。 管被配置为在燃料箱中携带惰性气体。 阀构造成基于相对于开口的燃料水平来控制离开开口的惰性气体的量。
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公开(公告)号：US20130048144A1
公开(公告)日：2013-02-28
申请号：US13219389
申请日：2011-08-26
申请人： David Scott Krug
发明人： David Scott Krug
CPC分类号： B64D37/32 , Y10T137/7481
摘要： A method and apparatus comprising a tube, an opening in the tube, and a valve associated with the opening. The tube is configured to carry an inert gas in a fuel tank. The valve is configured to control an amount of the inert gas that exits the opening based on a level of fuel relative to the opening.
摘要翻译： 一种包括管，管中的开口和与开口相关联的阀的方法和装置。 管被配置为在燃料箱中携带惰性气体。 阀构造成基于相对于开口的燃料水平来控制离开开口的惰性气体的量。
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公开(公告)号：US08596289B2
公开(公告)日：2013-12-03
申请号：US13278900
申请日：2011-10-21
申请人： David Scott Krug
发明人： David Scott Krug
IPC分类号： F16K31/18
CPC分类号： B64D37/32 , B64D37/22 , F16K24/048 , F16K31/22 , Y10T137/0318 , Y10T137/053 , Y10T137/7358 , Y10T137/7485
摘要： A fuel system for an aircraft has a vent system. The system has a conduit opening into the fuel section. The system has a member connected to the conduit at a proximal end. The member has a seal plate within the conduit sealing the opening into the fuel section when a buoyant section at a distal end rises along with the seal plate through the member with a rise in fluid level within the fuel section.
摘要翻译： 用于飞行器的燃料系统具有排气系统。 该系统具有通向燃料部分的导管。 该系统具有在近端连接到导管的构件。 当在远端的浮力部分与密封板一起通过该构件而升高燃料部分内的液位时，该构件具有在导管内的密封板将开口密封到燃料部分中。
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