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A turbine wheel having an axis of rotation and including: a disk having a periphery and a side face; a plurality of blades assembled on the disk, each blade having a blade root and a first hook oriented radially and defining a first groove that opens radially towards the axis of rotation of the turb

A turbine wheel having an axis of rotation and including: a disk having a periphery and a side face; a plurality of blades assembled on the disk, each blade having a blade root and a first hook oriented radially and defining a first groove that opens radially towards the axis of rotation of the turbine wheel. The disk includes a series of second hooks oriented radially and defining a second groove that opens radially towards the axis of rotation of the turbine wheel. An axial retaining ring for placing in the first and second grooves includes a tab for placing between two adjacent blade roots to limit movements of the ring in azimuth.

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1. A turbine wheel having an axis of rotation and comprising: a disk having a periphery and a side face;a plurality of blades assembled on the disk, each blade including a root of the blade and a first hook projecting axially therefrom, the first hook being oriented radially and defining a first gro

1. A turbine wheel having an axis of rotation and comprising: a disk having a periphery and a side face;a plurality of blades assembled on the disk, each blade including a root of the blade and a first hook projecting axially therefrom, the first hook being oriented radially and defining a first groove that opens radially towards the axis of rotation of the turbine wheel;the disk including a series of second hooks projecting axially from its side face on a same side as the first hooks, each second hook being oriented radially and defining a second groove that opens radially towards the axis of rotation of the turbine wheel; andan axial retaining ring including at least one tab and configured to be arranged in the first groove and in the second groove to retain the blades axially relative to the disk, the ring presenting an outer annular portion from which the tab does not extend, and the tab occupying an inner annular portion of the ring,wherein the tab is configured to be arranged between two roots of adjacent blades so as to limit movements of the ring in azimuth,wherein a depth of the second groove is less than a distance between the outer peripheral edge of the of the ring and the tab such that the outer peripheral edge of the ring cooperates with a bottom of the second groove and the tab is radially spaced apart from a free edge of the second hook with a first minimum clearance, the first minimum clearance being greater than a radial deformation of the ring at the tab when the turbine wheel is in operation, andwherein a bottom of the first groove is radially further from the axis of rotation than the bottom of the second groove such that the outer peripheral edge of the ring is spaced apart from the bottom of the first groove by a second minimum clearance while the outer peripheral edge of the ring cooperates with the bottom of the second groove, the second minimum clearance being greater than the radial deformation of the ring between the first and second hooks. 2. A turbine wheel according to claim 1, wherein the tab projects axially from an axial face of the ring. 3. A turbine wheel according to claim 1, wherein the tab is placed on an inner annular portion of the ring. 4. A turbine wheel according to claim 1, wherein the tab is configured to be placed between the first hooks of two adjacent roots of blade. 5. A turbine wheel according to claim 1, wherein the first hook of each blade projects radially from the root of the blade. 6. A turbine wheel according to claim 1, wherein the root of each blade is engaged in a housing that opens out into the periphery of the disk, the housings being separated by teeth, with each second hook projecting from one of the teeth. 7. A turbine wheel according to claim 1, wherein the tab presents contact faces configured to make plane-on-plane contact with bearing faces of two roots of blades that limit movement of the ring in azimuth. 8. A turbine wheel according to claim 1, wherein the ring presents a slot diametrically opposite from the tab. 9. A turbine wheel according to claim 1, wherein the ring presents a general shape of an annulus having an axis, with the center of gravity of the ring being situated on the axis. 10. A turbine wheel according to claim 1, wherein the ring cooperates radially solely with the second hooks. 11. A turbine engine including a turbine wheel according to claim 1. 12. A turbine wheel according to claim 1, wherein the outer annular portion of the ring and the inner annular portion of the ring are separated by a chamfer that is provided on an inner peripheral edge of an axial face supporting the tab.