Starting and controlling speed of a two spool gas turbine engine
AssigneeHoneywell International Inc.
InventorsRay McGinley, Alan Luebs
Life of this patent
Estimating the term…
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AssigneeHoneywell International Inc.
InventorsRay McGinley, Alan Luebs
Estimating the term…
Two spool gas turbine engines are often used to drive variable speed loads, such as an electric generator, or the fan/propeller of aircraft engines. The gas turbine engine must be designed to withstand transient speed and temperature conditions which are encountered when sudden changes to the load on the generator, fan, or propeller occur. By adding a relatively small motor/generator to the gas generator spool of the gas turbine engine, the compressor speed and airflow can be quickly adjusted to compensate for external load changes. This reduces the severity and duration of the transient conditions, resulting in decreased operation and reliability problems such as overspeed, compressor surge, and high turbine temperature. The motor/generator may also be used as an engine starting device.
An apparatus for controlling the rotational speed of a power turbine shaft, comprising:
(canceled)
An apparatus for controlling the speed of a two spool gas turbine engine comprising:
An apparatus for controlling the speed of a drive shaft of an electrical generator attached to a power turbine shaft of a two spool gas turbine engine comprising:
A two spool gas turbine engine comprising:
A method for controlling the speed of a two spool gas turbine engine comprising:
28-31. (canceled)
Dependencies are inferred from the claim text.