IP Library Granted Patent US 10,180,074
Granted Patent B2
US 10,180,074 · App. 11/275,188 · Granted Jan 15, 2019

Wireless monitoring system

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Quick Facts
Patent No.
US 10,180,074
App. No.
11/275,188
Granted
Jan 15, 2019
Kind
B2
Abstract

A system and method for remotely monitoring the operation of a turbine includes a remote device having a power module connected to a sensor and a transmitter. The remote device is powered by the power module and connected to a system such that the remote device is self-powered. The remote device wirelessly transmits information acquired by the sensor out of the turbine.

Claims (33)

1. A turbine comprising:

a shroud;

a compressor;

highly pressurized air exiting said compressor;

a combustor introducing highly atomized fuel to said pressurized air;

a sensor positioned in the shroud and configured to monitor a condition of the turbine;

a transmitter connected to the sensor and configured to transmit data acquired by the sensor; and

a power source configured to generate sufficient electrical energy to power the sensor and the transmitter from thermal energy during operation of the turbine,

wherein the transmitter further comprises a receiver constructed to wirelessly receive information from a location remote the turbine.

2. A turbine comprising:

a turbine component;

a sensor positioned in the turbine component and configured to monitor a condition of the turbine;

a transmitter connected to the sensor and configured to transmit data acquired by the sensor; and

a power source configured to generate sufficient electrical energy to power the sensor and the transmitter from thermal energy during operation of the turbine,

wherein the transmitter further comprises a receiver constructed to wirelessly receive information from a location remote the turbine,

wherein said power source is not electrically connected to any device external to said turbine, and

wherein the power source is a thermoelectric device and is in thermal communication with at least two temperatures associated with at least two of a flow of gas through the shroud; a flow of gas through the turbine; a flow of gas through a cooling passage of at least one of a fin, a blade, and a vane; a thermal gradient across the power source by conduction heat transfer in a solid material of the turbine; and a thermal gradient directed to the thermoelectric device by at least one of a heat pipe and a high conductivity heat spreader.

3. A turbine comprising:

a turbine component;

a sensor positioned in the turbine component and configured to monitor a condition of the turbine;

a transmitter connected to the sensor and configured to transmit data acquired by the sensor; and

a power source configured to generate sufficient electrical energy to power the sensor and the transmitter from thermal energy during operation of the turbine,

wherein the transmitter further comprises a receiver constructed to wirelessly receive information from a location remote the turbine,

wherein said power source is not electrically connected to any device external to said turbine, and

further comprising a heat exchanger attached to at least one of a heat-in side and a heat-out side of the power source.

4. A blade for a turbine engine, comprising:

a body, the body having an outer surface subject to a pressurized flow of a gas through the turbine engine and a passage formed in the body configured to allow passage of a flow of coolant through the body; and

a sensor package provided on the outer surface, the sensor package comprising:

a sensor configured to monitor a condition associated with operation of the turbine engine;

a power module configured to generate an electrical signal from one of a temperature differential and a temperature gradient during operation of a turbine; and

a transmitter attached to the first sensor and powered by the electrical signal generated by the power module, the transmitter configured to wirelessly transmit data acquired by the first sensor remote from the turbine, wherein the power module generates the electrical signal from a thermal gradient or a temperature differential between the flow of coolant in the passage and the pressurized flow of gas on the outer surface,

wherein the power module comprises a heat-in surface, a heat-out surface, and a plurality of semiconductor legs between the heat-in and heat-out surfaces, the plurality of semiconductor legs including at least one n-type leg and at least one p-type leg that are coupled electrically in series and thermally in parallel, and

wherein the power module further comprises a first heat exchanger in thermal contact with the heat-in surface and a second heat exchanger in thermal contact with the heat out-surface.

Assignments (2)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Dec 6, 2018
From: GENERAL ELECTRIC COMPANY
To: GE GLOBAL SOURCING LLC
Reel/Frame 047700/0636 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Dec 19, 2005
From: ARIK, MEHMET; MCKENNEY, KURTIS GIFFORD; LITER, SCOTT GAYTON; DASGUPTA, SAMHITA
To: GENERAL ELECTRIC COMPANY
Reel/Frame 016911/0849 →