Method and apparatus for preventing overspeed in a gas turbine
Patent
·
OSTI ID:7308858
A method and apparatus for preventing overspeed in a gas turbine in response to the rapid loss of applied load is disclosed. The method involves diverting gas from the inlet of the turbine, bypassing the same around the turbine and thereafter injecting the diverted gas at the turbine exit in a direction toward or opposing the flow of gas through the turbine. The injected gas is mixed with the gas exiting the turbine to thereby minimize the thermal shock upon equipment downstream of the turbine exit.
- Assignee:
- Energy Research and Development Administration
- Patent Number(s):
- US 3998047
- OSTI ID:
- 7308858
- Resource Relation:
- Patent File Date: Filed date 18 Apr 1975; Other Information: PAT-APPL-569,351
- Country of Publication:
- United States
- Language:
- English
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