Electric heating for turbomachinery clearance control powered by hybrid energy storage system

1. A clearance control system for a gas turbine engine, comprising:

a rotor blade;

an outer structure disposed radially outward from the rotor blade;

a heating element configured to cause the outer structure to be heated in response to electric current being supplied to the heating element,

wherein a gap between the rotor blade and the outer structure is at least one of increased, decreased, and maintained in response to the outer structure being heated;

a hybrid electric power source configured to supply the electric current to the heating element;

a first converter in electronic communication with the hybrid electric power source;

a second converter configured to receive DC power from the first converter and supply the heating element with electrical power; and

a controller configured to regulate the electric current being supplied to the heating element.

2. The clearance control system of claim 1 , wherein the hybrid electric power source comprises at least one of a battery, a supercapacitor, and an ultracapacitor.

3. The clearance control system of claim 1 , wherein the hybrid electric power source includes a capacitor and a battery, and the first converter is in electronic communication with the battery and the capacitor.

4. The clearance control system of claim 3 , wherein the first converter is configured to regulate power between the battery and the capacitor.

5. The clearance control system of claim 4 , wherein the capacitor comprises at least one of a supercapacitor or an ultracapacitor.

6. The clearance control system of claim 3 , wherein the hybrid electric power source further comprises a generator.

7. The clearance control system of claim 6 , wherein the generator comprises an auxiliary generator driven by one of a low speed spool or a high speed spool of the gas turbine engine.

8. The clearance control system of claim 6 , wherein the generator is configured to charge at least one of the battery or the capacitor in response to at least one of the battery or the capacitor being depleted of electrical energy.

9. The clearance control system of claim 1 , wherein the second converter comprises a DC-AC inverter and the heating element is configured to cause the outer structure to be heated via induction heating.

10. The clearance control system of claim 1 , further comprising a valve assembly configured to meter a cooling air flow to the outer structure.

11. The clearance control system of claim 10 , wherein the controller is configured to coordinate the cooling air flow and the electric current being supplied to the heating element to control a size of the gap.

12. The clearance control system of claim 11 , wherein the controller coordinates the cooling air flow via valve position control of the valve assembly.

13. The clearance control system of claim 12 , wherein the controller is configured to:

send a first control signal to a power electronics for varying the electric current supplied to the heating element to cause the outer structure to move in a first radial direction; and

send a second control signal to the valve assembly for varying the cooling air flow supplied to the outer structure to cause the outer structure to move in a second radial direction;

wherein the first radial direction is opposite the second radial direction.

14. The clearance control system of claim 1 , wherein the heating element is configured to heat up the outer structure by resistive heating.

15. The clearance control system of claim 1 , wherein the hybrid electric power source comprises a battery and a capacitor.

16. The clearance control system of claim 1 , wherein the second converter is configured to supply the heating element with the electrical power for controlling the gap between the rotor blade and the outer structure.

17. The clearance control system of claim 1 , wherein the controller is in electronic communication with the second converter.