Invention Grant
US08950170B2 Aircraft fuel system cooling flow device 有权
飞机燃油系统冷却流量装置

Aircraft fuel system cooling flow device
Abstract:
A cooling system includes a housing having an aperture intersecting a passage that includes first and second passage portions. A plug is arranged in the aperture in an interference fit in a first position at a first temperature condition to block the passage and fluidly separate the first and second passage portions. A biasing element is arranged in the housing and is configured to move the plug from the first position to a second position at a second temperature condition to fluidly connect the first and second passage portions.
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