Twelve-hour structure for thrust reverser, in particular with grids
The invention relates to a twelve-hour structure for a thrust reverser, that comprises a half beam ( 1 ) capable of holding a reverser half cowling and including a plurality of hinge yokes ( 9 c ) for rotatingly mounting said half beam ( 1 ) on a nacelle-holding mast. The half beam ( 1 ) is at least partially made of a composite material.
1. An aircraft nacelle comprising:
at least one internal fixed half-structure panel defining, with an associated thrust reverser cowl, a cold air flow; and
a twelve-hour structure for thrust reverser comprising a half-beam capable of supporting a reverser half-cowling,
wherein said half-beam comprises a plurality of hinge yokes for rotational assembly of said half-beam on a nacelle-holding mast, and said half-beam is formed at least in part in composite material,
wherein said half-beam and an upper part of the at least one internal fixed half-structure panel form, without mechanical connection, a single unitary part, and wherein the single unitary part is formed by surrounding a foam core or a composite material case of said half-beam with a skin of said at least one internal fixed half-structure panel.
2. The nacelle according to claim 1 , wherein said half-beam also comprises at least one rail for sliding assembly of said half-cowling.
3. The nacelle according to claim 1 , wherein said hinge yokes are formed in a metal alloy.
4. An aircraft nacelle including at least one internal fixed half-structure panel and a twelve-hour structure for thrust reverser, comprising a half-beam capable of supporting a reverser half-cowling and including a plurality of hinge yokes for rotational assembly of said half-beam on a nacelle-holding mast, said half-beam is formed at least in part in composite material,
wherein said half-beam and an upper part of the at least one internal fixed half-structure panel form a single unitary part, and
wherein said half-beam comprises a core including a foam part and a tube in composite material, the core being surrounded in a skin of the at least one internal fixed half-structure panel, and the tube connecting the hinge yokes to each other.
5. The nacelle according to claim 4 , wherein said tube is formed in forged carbon.
6. An aircraft nacelle including at least one internal fixed half-structure panel and a twelve-hour structure for thrust reverser, comprising a half-beam capable of supporting a reverser half-cowling and including a plurality of hinge yokes for rotational assembly of said half-beam on a nacelle-holding mast, said half-beam is formed at least in part in composite material,
wherein said half-beam and an upper part of the at least one internal fixed half-structure panel form a single unitary part, and said half-beam also comprises at least one rail for sliding assembly of the reverser half-cowling and a foam core surrounded in a skin of the at least one internal fixed half-structure panel, and wherein said hinge yokes sandwich said skin.
7. The nacelle according to claim 6 , wherein said hinge yokes are formed in forged carbon.
8. The nacelle according to claim 5 , wherein said hinge yokes are formed in forged carbon.