Quasi-cylindrical sound-insulation wall for turbojet engine nacelle in airplane, has alveolar structure with cylindrical configuration without discontinuity, and carried by another structure formed of juxtaposed sectors fixed end to end
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Year of Publication 28.08.2009
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Year of Publication 28.08.2009
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método para deposição in situ de um revestimento por fabricação aditiva, sistema para deposição de material filamentar, e, revestimento de parede de turbomáquina suscetível de abrasão
NORMAN BRUNO ANDRÉ JODET, EDITH-ROLAND FOTSING, JACKY NOVI MARDJONO, JÉREMY PAUL FRANCISCO GONZALEZ, ANNIE ROSS, ARNAUD DUBOURG, DANIEL THERRIAULT
Year of Publication 17.11.2020
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Year of Publication 17.11.2020
Patent