Gas turbine combustor control system
A technology of gas turbine and combustor, which is applied in the direction of turbine/propulsion fuel delivery system, fuel control of turbine/propulsion device, gas turbine device, etc., and can solve the problem of harmful gas turbine system and downstream components
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
Embodiment approach 2
[0116] Embodiment 2. The gas turbine system of Embodiment 1, comprising: an oxidant flow path configured to deliver oxidant flow to the turbine combustor, and an oxygen sensor disposed along the oxidant flow path, wherein the oxygen sensor is communicatively connected to the controller , and the oxygen sensor is configured to determine oxidant composition information.
Embodiment approach 3
[0117] Embodiment 3. The gas turbine system of any preceding Embodiment, wherein the oxidant composition information comprises a concentration of oxygen in the oxidant.
Embodiment approach 4
[0118] Embodiment 4. The gas turbine system of any preceding embodiment, comprising an oxidant flow meter disposed along the oxidant flow path, wherein the oxidant flow meter is communicatively connected to the controller, and the oxidant flow meter is configured to determine oxidant flow information.
PUM
Login to View More Abstract
Description
Claims
Application Information
Login to View More 