Thermal sensor
A thermal sensor for an aircraft includes a first electrode, a second electrode, a support layer disposed between the first electrode and the second electrode, and a state changing material is configured to disposed within the support layer, wherein the state changing material transitions between a non-conductive state to a conductive state at a threshold temperature to electrically connect the first and second electrodes.
1. A continuous thermal/overheat sensor for an aircraft, comprising:
a first electrode;
a second electrode;
a support layer disposed between the first electrode and the second electrode; and
a state changing material disposed within the support layer, wherein the state changing material is configured to transition between a non-conductive state to a conductive state at a threshold temperature to electrically connect the first and second electrodes, wherein at least one of the first and second electrodes are plate electrodes.
2. The thermal sensor of claim 1 , wherein the first and second electrodes are made of aluminum.
3. The thermal sensor of claim 1 , wherein the support layer can include at least one of a porous ceramic or a porous high temperature polymer.
4. The thermal sensor of claim 3 , wherein the porous ceramic includes at least one of glass fiber or the high temperature polymer includes polytetrafluoroethylene (PTFE), polyetheretherketone (PEEK), polyetherimide (PEI), polyphenylsulfone (PPSU), or polysulfone (PSU).
5. The thermal sensor of claim 1 , wherein the support layer is an anodized layer of one of the first and second electrodes.
6. The thermal sensor of claim 1 , wherein the state changing material includes a salt mixture.
7. The thermal sensor of claim 6 , wherein the salt mixture includes a chemical ratio of LiNO 3 :NaNO 3 :KNO 3 :NaNO 2 .
8. The thermal sensor of claim 1 , wherein the state changing material is sandwiched between the first electrode and the second electrode, and wherein the state changing material is sealed in between the first electrode and the second electrode by a sealant.
9. A method for manufacturing a continuous thermal/overheat sensor, comprising:
dip coating a support layer using a molten state changing material;
disposing a first and second aluminum plate electrodes on the support layer after dip coating; and
sealing the support layer between the first and second aluminum plate electrodes.
10. The thermal sensor of claim 9 , wherein the sealant includes a perfluoro-elastomer.
11. The method of claim 9 , wherein sealing the support layer includes disposing a sealant on an exposed edge of the support layer and hot pressing the sealant.
12. The method of claim 11 , further comprising hot pressing the first and second electrodes, the support layer, and the sealant together into a sandwich.