Cooling arrangement for a generator
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United States of America Patent
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Feb 15, 2022
Grant Date -
Feb 4, 2021
app pub date -
Mar 28, 2019
filing date -
Apr 10, 2018
priority date (Note) -
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status (Latency Note)
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Abstract
A generator arranged to be driven by an aircraft engine. The generator including a rotor. The rotor includes an inlet for receiving a fluid, a plurality of outlets configured to release the fluid from a radially outer region of the rotor, and a fluid distribution arrangement arranged to direct fluid from the inlet to one or more of the plurality of outlets. The fluid distribution arrangement is configured to selectively distribute fluid to one or more of the plurality of outlets in dependence on an operational parameter of the rotor.
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