A turboshaft engine includes an inlet, a swirl frame mounted downstream of the inlet, and an inlet seal mounted to one of the inlet and the swirl frame extending toward the other of the inlet and the swirl frame. The inlet seal includes a support member and an elastomeric member extending from a first end portion coupled to the support member to a second, cantilevered end portion.
Inlet seal for a turboshaft engine
2020-04-28
Patent
Elektronische Ressource
Englisch
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