Guide device for an aircraft turbine engine
AssigneeSafran Aircraft Engines
InventorsRemy LE GALL, Daniele CACCIAPUOTI
Life of this patent
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Abstract
A guide device for an aircraft turbine engine, the guide device includes a metal body provided with at least one attachment tab including an opening configured to receive a screw or the like; a guide pad made of a plastic or composite material, this pad provided with a first surface bonded to a first surface of the body and a second opposing surface which is free and which is configured to form a sliding guide surface, wherein the metal body includes through-holes which open onto the first surface of the body and in that the guide pad includes studs which project from the first surface of the pad and which are respectively engaged and crimped in the holes of the body.
Claims14
A guide device for an aircraft turbine engine, comprising:
- a metal body comprising at least one attachment tab including an orifice (75) configured to receive a screw or the like, this metal body comprising a first surface,
- a guide pad which is made from a plastic or composite material, this pad comprising a first surface bonded to said first surface of the body and a second opposite surface which is free and which is configured to form a sliding guide surface,
- wherein said metal body comprises through holes which open onto the first surface of the body, and in that said guide pad comprises studs which project from said first surface of the pad and which are respectively engaged and crimped in the holes of said body.
Dependencies are inferred from the claim text.