Double snapped cover plate for rotor disk
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United States of America Patent
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Oct 29, 2019
Grant Date -
Dec 24, 2015
app pub date -
Jan 30, 2013
filing date -
Jan 30, 2013
priority date (Note) -
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status (Latency Note)
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Abstract
According to an exemplary embodiment of this disclosure, among other possible things a gas turbine engine includes a compressor section, a combustor in fluid communication with the compressor section, a turbine section in fluid communication with the combustor section, a plurality of turbine disks in at least one of the compressor section and the turbine sections, at least one cover plate corresponding to at least one of the turbine disks, each of the cover plates includes, at least two snaps connected via a webbing portion, and a bore region radially inward of the at least two snaps and connected to at least one of the at least two snaps via the webbing portion.
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