Turbojet engine nacelle
View Patent ↗A turbojet engine nacelle includes an air intake structure having a longitudinal outer panel incorporating an air intake lip, a middle structure to which the air intake structure is attached, at least one inner panel including an acoustic shroud, rails guiding the outer panel able to allow a rectilinear movement of the outer panel, and a reinforcing member to react the mechanical loads of the guide rails. In particular, the reinforcing member reacts the loads of the guide rails beyond a predetermined deformation of the guide rails.
1. A turbojet engine nacelle comprising:
an air intake structure to channel a flow of air towards a fan of the turbojet engine and comprising at least one longitudinal outer panel incorporating an air intake lip;
a middle structure surrounding said fan and to which the air intake structure is attached in such a way as to provide aerodynamic continuity;
at least one inner panel comprising an acoustic shroud, fixed at a downstream end to an upstream end of the middle structure forming therewith a fixed structure of the nacelle;
means of guiding the outer panel(s) to allow a substantially rectilinear movement of the outer panel in the upstream direction of the nacelle so as to open the air intake structure; and
reinforcing means to react mechanical loads of the guide means beyond a predetermined deformation thereof as the air intake structure opens,
wherein said reinforcing means only reacts the mechanical loads when a deformation of the guide means occurs.
2. The nacelle according to claim 1 , wherein the predetermined deformation is in at least one direction belonging to a plane substantially perpendicular to a main direction of the guide means.
3. The nacelle according to claim 1 , wherein the reinforcing means have, between them or with an element of the nacelle, a non-zero spacing in an idle position.
4. The nacelle according to claim 3 , wherein the reinforcing means comprise a protruding member fastened on the inner panel and having a non-zero spacing with the guide means in the idle position.
5. The nacelle according to claim 1 , wherein the reinforcing meansare fastened on the inner panel in the shape of an inverted L, the guide means having a non-zero spacing with the lateral portion of the L in an idle position.
6. The nacelle according to claim 1 , wherein the reinforcing means have a load reacting portion with a shape substantially complementary to the guide means, said portion having a non-zero spacing in an idle position with the guide means.
7. The nacelle according to claim 1 , wherein the reinforcing means comprise a protruding member fastened on the guide means and a lug fastened on the inner panel, said protruding member being mounted opposite the lug with a non-zero spacing in an idle position.
8. The nacelle according to claim 1 , wherein the reinforcing means comprise a first member fixed on the outer panel and able to move on a ramp mounted on the inner panel.
9. The nacelle according to claim 8 , wherein the end comprises a roller able to roll on the ramp.
10. The nacelle according to claim 8 , wherein the ramp comprises a stop at the upstream end.
11. The nacelle according to claim 1 , wherein the reinforcing means comprise a first stop member mounted on the guide means and at least one second stop member mounted on the inner panel, said first and second stop members being connected using a connection capable of deforming to react the loads undergone by the guide means.
12. The nacelle according to claim 11 , wherein the connecting means is a connecting rod.
13. The nacelle according to claim 12 , wherein the connecting rod is formed from a metal piece.
14. The nacelle according to claim 12 , wherein the connecting rod comprises an elastically deformable member.