Method and device for suppressing the formation of ice on structures at the air intake of a turbomachine

• US 9,708,929 B2
• Filed: 06/17/2014
• Issued: 07/18/2017
• Est. Priority Date: 06/18/2013
• Status: Active Grant

• Current Assignee: Ansaldo Energia Switzerland AG (Ansaldo Energia SPA)
• Original Assignee: Ansaldo Energia Switzerland AG (Ansaldo Energia SPA)
• Inventors: Szwedowicz, Jaroslaw Leszek, Bauer, Andreas, Neubauer, Marcus, Schwarzendahl, Sebastian Marc
• Primary Examiner(s): Bui Pho, Pascal M
• Assistant Examiner(s): FORD, RENE D
• Application Number:
  US14/306,314
• Publication Number:
  US 20140366552A1
• Time in Patent Office: 1,127 Days
• CPC Class Codes: F01D 25/02 De-icing means for engines having icing phenomena
• CPC Class Codes: F02C 7/047 Heating to prevent icing
• CPC Class Codes: F03G 7/08 recovering energy derived from swinging, rolling, pitching or like movements, e.g. from the vibrations of a machine
• CPC Class Codes: F05D 2260/407 through piezoelectric conversion
• CPC Class Codes: F25C 5/08 by heating bodies in contact with the ice

Abstract

The application relates to a method and a device for suppressing ice formation on intake structures of a compressor, particularly the compressor of a gas turbine. The technical aim of the present invention is to provide a method and a device for suppressing the formation of ice on said structures, which avoid the disadvantages of known solutions, such as a reduction of the performance of the gas turbine, and have a simple and broad applicability. According to the present invention the mechanical vibratory energy of said structures during operation is converted into electrical energy by a piezoelectric element, firmly applied to said structure, and in a connected electrical circuit the generated electrical energy is then converted into thermal energy by an ohmic resistor and this thermal energy is conducted to at least a portion of the structure for suppressing ice formation. Excess energy may be transmitted by a transmitter to other circuits in adjacent structures.

Claims

1. A method for suppressing ice formation on a surface of at least one turbomachine structure during operation of the turbomachine, the method comprising:

converting mechanical vibratory energy of at least one first structure of the turbomachine into electrical energy via at least one piezoelectric element connected to the structure,

wirelessly transmitting a signal based on the electric energy converted from the mechanical vibratory energy of the at least one first structure,

receiving the signal by at least one heat generating circuit attached to at least one second structure of the turbomachine,

generating, by the heat generating circuit, thermal energy from the signal received by the heat generating circuit, and

conducting the thermal energy generated via the heat generating circuit to a second structure of the turbomachine to which the heat generating circuit is attached to suppress ice formation on the second structure to which the heat generating circuit is attached.

2. The method according to claim 1, wherein mechanical vibrations of the structure result in deforming the at least one piezoelectric element to convert the mechanical vibratory energy of the at least one first structure into an electrical voltage to initiate an electrical current in an electrical circuit connected to the at least one piezoelectric element, the method also comprising:

converting the electrical current into thermal energy by an ohmic resistor of the electrical circuit and conducting this thermal energy to the at least one first structure.

3. The method according to claim 1, comprising:

a transmitter of an external energy delivery system transmitting the signal to transmit power by contactless energy transfer to at least one receiver of the heat generating circuit.

4. The method according to claim 1, wherein the heat generating circuit is an electrical circuit that comprises a receiver and a resistor that is connected to the receiver so that the resistor generates heat from the signal received by the heat generating circuit via the receiver of the heat generating circuit.

5. The method according to claim 1, wherein more than one piezoelectric element is coupled to the at least one first structure, the method comprising:

adjusting the piezoelectric elements to one or more resonance frequencies.

6. The method according to claim 1, wherein the turbomachine is a compressor of a stationary gas turbine plant for power generation.

7. The method according to claim 1, comprising:

coupling the at least one piezoelectric element to said at least one first structure of the turbomachine and connecting each piezoelectric element to an electrical circuit having an ohmic resistor.

8. The method according to claim 7, wherein the electrical circuit additionally comprises a transmitter.

9. The method according to claim 8, wherein the electrical circuit of the at least one first structure and the transmitter of the electrical circuit is configured to transmit the signal to transmit power by contactless energy transfer.

10. The method according to claim 9, wherein the at least one first structure is a rotating blade and the second structure is an inlet guide vane and/or a stator part of an intake of a compressor of the turbomachine.

11. The method according to claim 8, wherein the transmitter of the electrical circuit sends the signal to a receiver of an external energy delivery system.

12. The method according to claim 11, wherein the external energy delivery device comprises at least the receiver, an electrical power source and a transmitter for contactless energy transfer configured to transmit the signal.

13. The method according to claim 12, wherein the transmitter of the external energy delivery system transmits the signal to transmit power by contactless energy transfer to at least one receiver of the heat generating circuit, the heat generating circuit being configured as an electrical circuit.

14. A device for conducting the method according to claim 1, the device comprising:

a casing with an intake section to receive an airflow;

a rotor surrounded by the casing,

a row of inlet guide vanes connected to the casing, and

a row of rotating blades connected to the rotor,

a piezoelectric element and an electrical circuit connected to the piezoelectric element, the piezoelectric element connected to one of an inlet guide vane of the row of inlet guide vanes and a rotating blade of the row of rotating blades, and

wherein the electrical circuit is configured to wirelessly transmit a signal for sending to at least one of;

heat generating circuits connected to the inlet guide vanes and heat generating circuits connected to the rotating blades, the signal configured to facilitate actuation of the heat generating circuits for the generation of heat to suppress ice formation.

15. The device according to claim 14, wherein the piezoelectric element is connected to the electrical circuit such that vibrations due to ice formation deform the piezoelectric element to generate an electrical voltage to cause the electrical circuit to wirelessly transmit the signal.

16. The device according to claim 14, wherein the electrical circuit is attached to an outer surface or an inner surface of a structure of a turbomachine or is embedded within the structure of the turbomachine.

17. The device according to claim 14, wherein the electrical circuit includes at least one resistor or at least one ohmic resistor.

18. The device according to claim 14, wherein the electrical circuit comprises at least a transmitter.

19. The device according to claim 18, wherein the electrical circuit is connected to the casing, the rotating blade of the row of rotating blades, or the inlet guide vane of the row of inlet guide vanes.

20. The device according to claim 19, wherein the electrical circuit is connected to the rotating blade of the row of rotating blades.

21. The device according to claim 19, wherein a transmitter of the electrical circuit is designed to send the signal to receivers of the heat generating circuits connected to the inlet guide vanes and receivers of the heat generating circuits connected to the rotating blades.

22. The device according to claim 14, comprising:

an external energy delivery system that comprises a receiver for receiving the signal, an electrical power source and a transmitter for contactless energy transfer transmission to the heat generating circuits connected to the rotating blades and the heat generating circuits connected to the inlet guide vanes.

23. The device according to claim 22, wherein each of the heat generating circuits comprises an electrical circuit that comprises a receiver connected to a resistor.

24. The device according to claim 14, wherein the piezoelectric element and the electrical circuit connected to the piezoelectric element are designed as a module.

25. The device according to claim 24, wherein the module additionally comprises an ohmic resistor and/or a transmitter.