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1. 发明授权

US08851424B2 Systems and methods to provide compliance with structural load requirements for aircraft with additional fuel tankage 有权
标题翻译：提供符合附加燃油箱的飞机结构载荷要求的系统和方法
公开(公告)号：US08851424B2
公开(公告)日：2014-10-07
申请号：US13095615
申请日：2011-04-27
申请人： Weber Brito Barbosa , Paulo Henrique Hasmann , Luciano Magno Fragola Barbosa
发明人： Weber Brito Barbosa , Paulo Henrique Hasmann , Luciano Magno Fragola Barbosa
IPC分类号： B64C17/10 , B64D37/16 , B64D37/10 , B64D37/04 , B64D37/20
CPC分类号： B64D37/04 , B64C17/10 , B64D37/10 , B64D37/16 , B64D37/20
摘要： Methods and systems are provided to comply with structural load requirements applicable to aircraft additional fuel tank systems. A plurality of aircraft fuel tanks may be positioned adjacent to one another, preferably within the fuselage (e.g., a cargo compartment) of the aircraft so as to be disposed generally along a longitudinal axis of the aircraft. The tank body defining an interior space for holding aircraft fuel, an intercommunication conduit assembly between the fuel tank modules configured to refuel and transfer fuel from the tank modules by a cascade mode and an intentional air-filled ullage space are operatively associated with the tank body to prevent an overpressure condition within the interior space of the fuel tank body. The intentional air-filled ullage is obtained through the predetermined positioning of the terminal open end of the intercommunication tube inside the respective fuel tank module. The intentional air-filled ullage can be configured in all or in only some of the fuel tank modules according to the design of the auxiliary fuel tanks or aircraft structural loads requirements.
摘要翻译：提供方法和系统以符合适用于飞机附加燃料箱系统的结构载荷要求。多个飞行器燃料箱可以彼此相邻地定位，优选地位于飞行器的机身（例如，货舱）内，以便大致沿飞机的纵向轴线设置。所述罐主体限定用于保持飞机燃料的内部空间，构造成通过级联模式和有意充满气体的空间空间来从燃料箱模块加油和转移燃料的燃料箱模块之间的相互通信导管组件与罐体以防止燃料箱体的内部空间内的过压状态。通过相应的燃料箱模块内的相互连通管的端子开口端的预定位置来获得有意充气的空载。根据辅助油箱的设计或飞行器结构载荷要求，可以在全部或仅部分燃油箱模块中配置有意的充气排空。

2. 发明申请

US20110272526A1 SYSTEMS AND METHODS TO PROVIDE COMPLIANCE WITH STRUCTURAL LOAD REQUIREMENTS FOR AIRCRAFT WITH ADDITIONAL FUEL TANKAGE 有权
标题翻译：提供符合附加燃料舱航空器结构性载荷要求的系统和方法
公开(公告)号：US20110272526A1
公开(公告)日：2011-11-10
申请号：US13095615
申请日：2011-04-27
申请人： Weber Brito BARBOSA , Paulo Henrique HASMANN , Luciano Magno Fragola BARBOSA
发明人： Weber Brito BARBOSA , Paulo Henrique HASMANN , Luciano Magno Fragola BARBOSA
IPC分类号： B64D37/04 , B64D37/06 , B64D37/16
CPC分类号： B64D37/04 , B64C17/10 , B64D37/10 , B64D37/16 , B64D37/20
摘要： Methods and systems are provided to comply with structural load requirements applicable to aircraft additional fuel tank systems. A plurality of aircraft fuel tanks may be positioned adjacent to one another, preferably within the fuselage (e.g., a cargo compartment) of the aircraft so as to be disposed generally along a longitudinal axis of the aircraft. The tank body defining an interior space for holding aircraft fuel, an intercommunication conduit assembly between the fuel tank modules configured to refuel and transfer fuel from the tank modules by a cascade mode and an intentional air-filled ullage space are operatively associated with the tank body to prevent an overpressure condition within the interior space of the fuel tank body. The intentional air-filled ullage is obtained through the predetermined positioning of the terminal open end of the intercommunication tube inside the respective fuel tank module. The intentional air-filled ullage can be configured in all or in only some of the fuel tank modules according to the design of the auxiliary fuel tanks or aircraft structural loads requirements.
摘要翻译：提供方法和系统以符合适用于飞机附加燃料箱系统的结构载荷要求。多个飞行器燃料箱可以彼此相邻地定位，优选地位于飞行器的机身（例如，货舱）内，以便大致沿飞机的纵向轴线设置。所述罐主体限定用于保持飞机燃料的内部空间，构造成通过级联模式和有意充满气体的空间空间来从燃料箱模块加油和转移燃料的燃料箱模块之间的相互通信导管组件与罐体以防止燃料箱体的内部空间内的过压状态。通过相应的燃料箱模块内的相互连通管的端子开口端的预定位置来获得有意充气的空载。根据辅助油箱的设计或飞行器结构载荷要求，可以在全部或仅部分燃油箱模块中配置有意的充气排空。

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