BIMETAL THERMO MECHANICAL ACTUATOR
A bimetal thermo mechanical actuator ( 10 ) includes a multi-layer bimetal structure ( 22 ) that includes a plurality of bimetal structures ( 12 ). Each bimetal structure ( 12 ) includes a pair of metals, a structural metal ( 14 ) and a driving metal ( 16 ) that are bonded together along a bonded interface ( 18 ) with the pair of metals forming one layer. A sliding interface ( 20 ) is between each pair of metals. The multi-layer bimetal structure ( 22 ) has a shape that has at least one arch. The multi-layer bimetal structure ( 22 ) includes a first end ( 24 ) and a second end ( 26 ), an inner edge ( 40 ) and an inner radius ( 42 ), an outer edge ( 44 ) and an outer radius ( 46 ). A first pivot head ( 28 ) is connected to the first end ( 24 ) and a second pivot head ( 34 ) is connected to the second end ( 26 ) of the multi-layer bimetal structure ( 22 ). Each pivot head includes a through-hole ( 30 ) located approximately center. The multi-layer bimetal structure ( 22 ) expands and contracts with temperatures changes.
1 . A bimetal thermo mechanical actuator comprising:
a multi-layer bimetal structure comprising a plurality of bimetal structures, wherein each bimetal structure comprises a pair of metals, a structural metal and a driving metal, bonded together along a bonded interface, with the pair of metals forming one layer, wherein a sliding interface is there between each pair of metals, wherein the multi-layer bimetal structure has a shape with at least one arch having a first end and a second end on opposite ends of a length of the multi-layer bimetal structure, an inner edge and inner radius, an outer edge and an outer radius; and
a first pivot head connected to the first end and a second pivot head connected to the second end of the multi-layer bimetal structure, wherein each pivot head includes a through-hole located approximately center of each pivot head,
wherein the multi-layer bimetal structure expands and contracts with temperature changes.
2 . The bimetal thermo mechanical actuator according to claim 1 , wherein each bimetal structure varies in thickness compared to other bimetal structures within the multi-layer bimetal structure.
3 . The bimetal thermo mechanical actuator according to claim 1 , wherein the multi-layer bimetal structure is bent in an approximately semi-circle shape.
4 . The bimetal thermo mechanical actuator; according to claim 1 , wherein the multi-layer bimetal structure is bent in a shape that has multiple curves.
5 . The bimetal thermo mechanical actuator according to claim 1 , wherein the multi-layer bimetal structure is bent in multiple directions.
6 . The bimetal thermo mechanical actuator according to claim 1 , further comprising a heating/cooling element attached to the multi-layer bimetal structure.
7 . A method for adjusting a clearance distance, comprising:
positioning a bimetal thermo mechanical actuator between a stationary component and a moved component, the bimetal thermo mechanical actuator comprising:
a multi-layer bimetal structure comprising a plurality of bimetal structures, wherein each bimetal structure comprises a pair of metals, a structural metal and a driving metal, bonded together along a bonded interface with the pair of metals forming one layer, wherein a sliding interface is between each pair of metals, wherein the multi-layer bimetal structure has a shape with at least one arch having a first end and a second end, an inner edge and inner radius, an outer edge and an outer radius; and
a first pivot head connected to the first end; and a second pivot head connected to the second end of the multi-layer bimetal structure, wherein each pivot head includes a through-hole located approximately center of each pivot head,
wherein the multi-layer bimetal structure expands and contracts with temperature changes;
mounting the first pivot head or the second pivot head to the moved component, wherein pivot head is mounted through the through-hole of the pivot head to the moved component; and
increasing/decreasing a local temperature surrounding the bimetal thermo mechanical actuator, wherein the bimetal thermo mechanical actuator expands or contracts based on the direction of the temperature change, wherein the expansion or contraction of the bimetal thermo mechanical actuator moves the moved component along one axis closing a gap between two components.
8 . The method according to claim 7 , wherein the moved component is a gas turbine compressor vane, wherein one pivot head mounts in a lower part of the gas turbine compressor vane and the other pivot head mounts to a moving upper part of the vane.
9 . The method according to claim 7 , wherein the moved component is a gas turbine vane, wherein one pivot head mounts in the gas turbine vane and the other pivot head mounts to a moving top of the turbine vane.
10 . The method according to claim 7 , wherein the stationary component is a gas turbine frame, wherein one pivot head mounts to the gas turbine frame and the other pivot head mounts to the moved component.