Invention Grant
- Patent Title: Aircraft fuel system cooling flow device
- Patent Title (中): 飞机燃油系统冷却流量装置
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Application No.: US13042538Application Date: 2011-03-08
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Publication No.: US08950170B2Publication Date: 2015-02-10
- Inventor: Bruce Paradise
- Applicant: Bruce Paradise
- Applicant Address: US CT Windsor Locks
- Assignee: Hamilton Sundstrand Corporation
- Current Assignee: Hamilton Sundstrand Corporation
- Current Assignee Address: US CT Windsor Locks
- Agency: Carlson, Gaskey & Olds, P.C.
- Main IPC: F02C7/12
- IPC: F02C7/12 ; F01D25/08 ; F16K17/38 ; F16K99/00 ; F02C7/22 ; F16K31/00 ; F02C7/232

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.
Public/Granted literature
- US20120227409A1 AIRCRAFT FUEL SYSTEM COOLING FLOW DEVICE Public/Granted day:2012-09-13
Information query
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