Thermal switch with activation indicator
AssigneeHoneywell International Inc.
InventorsByron G. Scott, George D. Davis
Life of this patent
Estimating the term…
Abstract
A temperature sensitive indicator 24 in the form of a label or decal is affixed to the outside of a thermal switch 20. The temperature sensitive label provides a permanent record of the temperature limits exposed to the thermal switch. The temperature sensitive material changes colors when the thermal switch is exposed to its predetermined temperature limit. The changed color provides a quick and clear indication of an event that caused switch activation. The color indication on the outside surface of the switch also provides a visual indication that is easy to acquire and inspect without the need to have physical access to the switch itself.
Claims9
An overheat sensing system for sensing the thermal condition of the turbine bleed air duct system in an airplane, said overheat sensing system comprising:
- a thermal switch coupled to the turbine bleed air duct system for detecting when an external threshold temperature associated with said thermal switch has been reached, wherein said external threshold temperature is caused from other than an electric current through said switch;
- and
- a temperature sensing material coupled to the surface of said thermal switch for indicating if said thermal switch has been exposed to temperatures above the threshold temperature associated with the turbine bleed air duct system.
A method of sensing a prior thermal condition of one or more components of a device, said method comprising:
- coupling a temperature sensing material to a thermal switch to form a thermal switch apparatus, said temperature sensing material selected to change color at a threshold temperature;
- coupling said thermal switch apparatus to the components of the device;
- changing the color of said temperature sensing material when exposed to an external threshold temperature caused from other than an electric current through said thermal switch;
- and
- identifying by visual inspection of the temperature sensing material whether said thermal switch apparatus has been exposed to said external threshold temperature.
A method of sensing a prior thermal condition of an aircraft turbine bleed air duct system, said method comprising:
- coupling a temperature sensing material to a thermal switch to form a thermal switch apparatus, said temperature sensing material selected to change color at a threshold temperature corresponding to a high-temperature condition in the bleed air duct system;
- coupling said thermal switch apparatus to the components of the bleed air duct system;
- changing the color of said temperature sensing material when exposed to said threshold temperature caused from other than an electric current through said thermal switch;
- and
- identifying by visual inspection of the temperature sensing material whether said thermal switch apparatus has been exposed to said external threshold temperature.
Dependencies are inferred from the claim text.