Hybrid cycle high pressure compressor and turbine engine including such a compressor

1. A cycle HP compressor for a turbine engine, said compressor comprising:

a plurality of rotor wheels and rectifiers arranged alternately, from upstream to downstream successively in a principal direction of air flow through the compressor, a first rotor wheel a first rectifier and a second rotor wheel,

a separation slot set between the first rectifier and the second rotor wheel in order to supply the turbine engine with a secondary air flux,

wherein the first rectifier is a double grid rectifier comprising a grid of vanes upstream as well as a grid of vanes downstream,

wherein said grids of vanes upstream and downstream are associated respectively with variable setting systems upstream and downstream controlled in autonomous manner,

wherein each vane of each of the upstream and downstream grids of the first rectifier is capable of being pivoted around an axis of rotation extending closely radially, and

wherein for each vane of the upstream grid, the axis of rotation is located close to a trailing edge of said vane, and for each vane of the downstream grid, the axis of rotation is located close to a leading edge of said vane.

2. A cycle HP compressor according to claim 1 , wherein for each vane of the upstream grid, the axis of rotation is located in a downstream portion of the latter beginning at the level of two thirds of a chord of said vane, and wherein for each vane of the downstream grid, the axis of rotation is located in an upstream portion of the latter, ending at the level of a third of a chord of said vane.

3. A cycle HP compressor according to claim 2 , wherein in transversal cross-section taken along any plane located upstream of the first rectifier, on any circle C centered on a principal longitudinal axis of the compressor and intercepting the upstream and downstream grids of vanes, a length L 1 of an arc of a circle defined by the axis of rotation of any vane of the upstream grid as well as by the axis of rotation of the vane of the downstream grid the closest to any vane of the upstream grid, and a length L 2 of an arc of a circle defined by the axes of rotation of two consecutive vanes of the upstream grid, are such that L 1 is less than or equal to a third of L 2 .

4. A cycle HP compressor according to claim 3 , wherein a length L 3 of an arc of a circle defined by the rotation axes of two consecutive vanes of the downstream grid is equal to the length L 2 .

5. A cycle turbine engine comprising a hybrid cycle HP compressor according to claim 2 .

6. A cycle HP compressor according to claim 1 , wherein in transversal cross-section taken along any plane located upstream of the first rectifier, on any circle C centered on a principal longitudinal axis of the compressor and intercepting the upstream and downstream grids of vanes, a length L 1 of an arc of a circle defined by the axis of rotation of any vane of the upstream grid as well as by the axis of rotation of the vane of the downstream grid the closest to any vane of the upstream grid, and a length L 2 of an arc of a circle defined by the axes of rotation of two consecutive vanes of the upstream grid, are such that L 1 is less than or equal to a third of L 2 .

7. A cycle HP compressor according to claim 6 , wherein a length L 3 of an arc of a circle defined by the rotation axes of two consecutive vanes of the downstream grid is equal to the length L 2 .

8. A cycle turbine engine comprising a hybrid cycle HP compressor according to claim 7 .

9. A cycle turbine engine comprising a hybrid cycle HP compressor according to claim 6 .

10. A cycle turbine engine comprising a hybrid cycle HP compressor according to claim 1 .