Guide assembly for an aircraft propulsion unit
AssigneeSafran Nacelles
InventorsPierre PELLERIN, Cedric François Pierre RENAULT
Life of this patent
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Abstract
A guide assembly for an aircraft propulsion unit, the guide assembly having a first element and at least one guide element attached to the first element. The guide element includes a bottom wall, two lateral walls connected together by the bottom wall, and an opening defined between the bottom wall and the lateral walls. The opening is configured to receive at least partly a second element configured to move relative to the guide element. The guide element can further include at least one pair of gripping tongues cooperating with holding members of the first element to retain the guide element on the first element.
Claims15
A guide assembly for an aircraft propulsion unit, the guide assembly comprising:
- a first element having holding members;
- and
- at least one guide element attached to the first element, the guide element having a generally elongated shape along a longitudinal axis between a first longitudinal end and a second longitudinal end, the guide element comprising:
- a bottom wall;
- two lateral walls connected together by the bottom wall;
- and
- an opening delimited between the bottom wall and the lateral walls, the opening configured to receive at least partly a second element configured to move relative to the guide element,
- wherein the guide element further comprises at least one pair of gripping tongues cooperating with the holding members of the first element to retain the guide element on the first element, and
- wherein the holding members are grooves, each groove receiving a tongue of the at least one pair of gripping tongues of the guide element.
Dependencies are inferred from the claim text.