An aircraft engine, comprising: a first wall and a second wall defining a gaspath between the first wall and the second wall, the gaspath extending around a central axis, each of the first wall and the second wall having a gaspath side facing the gaspath and an opposed side facing away from the gaspath; struts circumferentially distributed around the central axis, the struts extending across the gaspath, a strut of the struts having an airfoil including a leading edge, a trailing edge, a first end secured to the first wall, and a second end secured to the second wall; and protrusions extending from a baseline surface of the opposed side of the first wall, the protrusions increasing a thickness of the first wall, a protrusion of the protrusions overlapping a location where the leading edge or the trailing edge meets the gaspath side of the first wall.
AIRCRAFT ENGINE STRUTS WITH STIFFENING PROTRUSIONS
MATS REACTEURS D'AERONEF COMPRENANT DES SAILLIES DE RAIDISSEMENT
2023-08-11
Patent
Elektronische Ressource
Englisch
Trust struts arrangement for an aircraft engine mount
Europäisches Patentamt | 2017
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