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Device for limiting flow of fluid circulating between high temperature and low-temperature zones of pneumatic circuit in engine of aircraft, has thermosensitive device whose deformation limits flow of fluid according to fluid temperature
Device for limiting flow of fluid circulating between high temperature and low-temperature zones of pneumatic circuit in engine of aircraft, has thermosensitive device whose deformation limits flow of fluid according to fluid temperature
The device has a thermosensitive device (5) adapted to be deformed passively according to temperature of fluid circulating on level of the thermosensitive device. The deformation modifies cross-section of stream discharge of the fluid in a fluid circuit and limits flow of the fluid according to the temperature of the fluid to the level of the thermosensitive device. The thermosensitive device is of a type having a bistable behavior, and includes a thermal switch supporting a valve and acts as a thermosensitive capsule with thermal dilation with/without phase shift. An independent claim is also included for a method for controlling temperature of a fluid circulating in a fluid circuit.
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