METHOD AND DEVICE FOR SUPPRESSING THE FORMATION OF ICE ON STRUCTURES AT THE AIR INTAKE OF A TURBOMACHINE
First Claim
1. Method for suppressing ice formation on the surface of a turbomachine structure, particularly an intake structure of a compressor, during its operation, the method comprising at least the steps of piezoelectrically converting mechanical vibratory energy of said structure into electrical energy, converting the generated electrical energy into thermal energy and conducting this thermal energy to at least a portion of the structure.
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Accused Products
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.
27 Citations
25 Claims
- 1. Method for suppressing ice formation on the surface of a turbomachine structure, particularly an intake structure of a compressor, during its operation, the method comprising at least the steps of piezoelectrically converting mechanical vibratory energy of said structure into electrical energy, converting the generated electrical energy into thermal energy and conducting this thermal energy to at least a portion of the structure.
Specification