Inlet cone for an aircraft turbine engine
AssigneeSafran Aircraft Engines
InventorsMarion Michele PENVERNE, Jean-Marc Claude PERROLLAZ, Manuel Rui EVORA, Baptiste Rene Roger BATONNET
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Abstract
An inlet cone for an aircraft turbine engine is configured to be rotated about an axis (X). The inlet cone includes a frustoconical body and a tip made of elastically deformable material fixed to a smaller-diameter end of the body. The body includes through-housings distributed around the axis, and parts made of elastically deformable material located in the through-housings. Each of the parts made of elastically deformable material has at least one peripheral flange for retaining the part in the corresponding through-housing. The peripheral flange bears against an internal surface of the body.
Claims14
An inlet cone for an aircraft turbine engine, said inlet cone being configured to be driven in rotation about an axis (X) and comprising a body of frustoconical shape and a tip made of elastically deformable material fixed to an end of smaller diameter of said body,
- the body comprising through-housings distributed around the axis (X) and parts made of elastically deformable material located in said through-housings,
- wherein each of the parts made of elastically deformable material comprises at least one peripheral rim for retaining said part in the corresponding through housing, said at least one peripheral rim bearing on an internal surface of said body.
Dependencies are inferred from the claim text.