| 摘要 |
A nozzle feature for sealing leakage in a gas turbine engine having a plurality of nozzle segments within the turbine engine which includes a radially inner band, a radially outer band, at least one vane disposed between the radially inner and outer bands, the radially inner band having a first tab formed in said inner band extending radially downwardly from at least one of first and second circumferential ends.
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