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US 2012/0247108 A1Published application
Combustor probe for gas turbine
AssigneeGeneral Electric Company
InventorsBryan Wesley Romig, Jonathan Hale Kegley, Robert Wade Clifford, Derrick Walter Simons
Life of this patent
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Abstract
Embodiments of the present disclosure are directed towards a turbine combustor probe having a combustion dynamics monitoring probe configured to monitor combustion dynamics within a turbine combustor. The turbine combustor probe also has a gas sampling sleeve configured to collect a gas sample from an airflow path between a liner and a flow sleeve of the turbine combustor.
Claims20
A system, comprising:
- a turbine combustor;
- and
- a combustor probe, comprising:
- a combustion dynamics monitoring probe configured to monitor combustion dynamics within the turbine combustor;
- and
- a gas sampling sleeve configured to collect a gas sample from an airflow path between a liner and a flow sleeve of the turbine combustor.
3 more elements
A turbine combustor probe, comprising:
- a gas sampling sleeve configured to collect a gas sample from an air flow in a turbine combustor;
- and
- a combustion dynamics probe configured to monitor combustion dynamics in the turbine combustor, wherein the combustion dynamics probe is disposed within the gas sampling sleeve, and an annular passage is disposed between the combustion dynamics probe and the gas sampling sleeve.
A turbine combustor probe sleeve, comprising:
- a gas sampling tube operatively coupled to a gas sample cavity, wherein the gas sampling tube and the gas sample cavity are configured to receive a combustor probe and to collect a gas sample from an air flow in a turbine combustor.
Dependencies are inferred from the claim text.