Thermally actuated passive gas turbine engine compartment...

F - Mech Eng,Light,Heat,Weapons – 02 – C

Patent

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Details

F02C 7/12 (2006.01) F01D 25/08 (2006.01) F01P 1/06 (2006.01) F01P 11/00 (2006.01)

Patent

CA 2720607

A thermally actuated venting system includes a thermally actuated vent for opening a vent outlet in a gas turbine engine associated compartment with a passive thermal actuator located in the compartment based on a temperature of the compartment. Outlet may be located at or near a top of a core engine compartment, a fan compartment, or a pylon compartment. Actuator may be operably connected to a hinged door of vent for opening outlet. Actuator may be actuated by a phase change material disposed in a chamber and having a liquid state below a predetermined actuation temperature and a gaseous state above the predetermined actuation temperature. Actuator may include a thermal fuse for closing door during a fire. Thermal fuse may include at least a portion of piston rod or a cylinder wall of actuator being made of a fuse material having a melting point substantially above the predetermined actuation temperature.

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