Assembly Comprising a Nacelle Panel and a Member Forming a Ball
AssigneeSafran Nacelles
InventorsJean-Baptiste DELARUE, Bertrand Léon Marie DESJOYEAUX, Moncef M'HASNI
Life of this patent
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Abstract
An assembly including a nacelle panel of an aircraft engine, the nacelle panel including an outer skin, an inner skin and a central layer interposed between the outer skin and the inner skin, and the nacelle panel having a free inner enclosure contiguous with the outer skin, and a member forming a link including one or more degrees of freedom, the member being attached to the nacelle panel solely by one or both of the outer skin and the inner skin, and the member extending facing the free inner enclosure.
Claims24
An assembly comprising:
- a nacelle panel of an aircraft engine,
- the nacelle panel comprising an outer skin, an inner skin and a central layer interposed between the outer skin and the inner skin, and
- the nacelle panel having a free inner enclosure contiguous with the outer skin;
- and
- a member forming a link comprising at least one degree of freedom,
- the member being attached to the nacelle panel solely by at least one of the outer skin and the inner skin, and
- the member extending facing the free inner enclosure.
A method for manufacturing an assembly for a nacelle of an aircraft engine, the method comprising:
- producing a panel comprising an outer skin, an inner skin and a central layer interposed between the outer skin and the inner skin, the panel having an inner enclosure contiguous with the outer skin;
- and
- attaching a member to the panel solely by at least one of the outer skin and the inner skin, the member forming a link comprising at least one degree of freedom and extending facing the inner enclosure, the panel and the member forming the assembly for the nacelle of the aircraft engine.
Dependencies are inferred from the claim text.