发明申请
- 专利标题: Aircraft fuel tank and sensor system
- 专利标题(中): 飞机油箱和传感器系统
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申请号: US11226805申请日: 2005-09-14
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公开(公告)号: US20070234795A1公开(公告)日: 2007-10-11
- 发明人: Kenichi Goto
- 申请人: Kenichi Goto
- 申请人地址: JP Tokyo
- 专利权人: Honda Motor Co., Ltd.
- 当前专利权人: Honda Motor Co., Ltd.
- 当前专利权人地址: JP Tokyo
- 主分类号: G01F22/00
- IPC分类号: G01F22/00 ; G01F23/00 ; B64D37/06 ; B64D37/08 ; B64D43/00
摘要:
The aircraft tank and gauge system of the present invention provides a fuel tank with a gauge chamber located generally aligned with the tank center of gravity and that has a general vertical orientation when the aircraft is level. The gauge chamber extends from the top of the tank to a height generally equivalent to a high collection point on the tank and/or extends from the bottom of the tank to a height generally equivalent to a low collection point on the tank. As the aircraft pitches and rolls, fuel within a complex-shaped tank, will be measured by a sensor in the gauge chamber. In order to prevent any type of vapor blockage in the gauge chamber, a first vent extends from the bottom of the gauge chamber to the low collection point of the tank and a second vent extends from the top of the gauge chamber to the high collection point of the tank.
公开/授权文献
- US07334464B2 Aircraft fuel tank and sensor system 公开/授权日:2008-02-26
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