A spinner for a gas turbine engine comprises an outer shell for defining an airflow path when mounted in a gas turbine engine. An inner surface is provided with a plurality of webs. A gas turbine engine and a fan section for a gas turbine engine are also disclosed.
Gas turbine engine with reinforced spinner
27.08.2019
Patent
Elektronische Ressource
Englisch
Europäisches Patentamt | 2020
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