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A rotor includes a disk that has slots circumferentially arranged around its periphery. Blades include respective roots that are mounted in respective ones of the slots. The roots are smaller than the slots such that there are circumferential gaps between the roots and circumferential sides of the s

A rotor includes a disk that has slots circumferentially arranged around its periphery. Blades include respective roots that are mounted in respective ones of the slots. The roots are smaller than the slots such that there are circumferential gaps between the roots and circumferential sides of the slots. Wedges are respectively located within the circumferential gaps. The wedges are free floating with regard to the blades and the disk.

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1. A rotor comprising: a disk including slots circumferentially arranged around its periphery;blades including respective roots that are mounted in respective ones of the slots, the roots being smaller than the slots such that there are circumferential gaps between the roots and circumferential side

1. A rotor comprising: a disk including slots circumferentially arranged around its periphery;blades including respective roots that are mounted in respective ones of the slots, the roots being smaller than the slots such that there are circumferential gaps between the roots and circumferential sides of the slots; andwedges respectively located in the circumferential gaps, the wedges being free floating with regard to the blades and the disk and the wedges each having a tapered thickness profile in the respective circumferential gap, with the wedges in contact with either the roots or circumferential sides of the slots at respective contact interfaces, each of the contact interfaces including a curved surface in contact with a flat surface such that there is a point or line of contact between the curved surface and the flat surface. 2. The rotor as recited in claim 1, wherein each of the wedges includes less than three flat sides. 3. The rotor as recited in claim 1, wherein each of the blades includes a ceramic material. 4. The rotor as recited in claim 3, wherein the ceramic material is a multi-layer fiber structure including a ceramic matrix. 5. The rotor as recited in claim 1, wherein each of the wedges includes at least one crowned side. 6. The rotor as recited in claim 1, wherein each of the wedges includes a plurality of crowned sides. 7. The rotor as recited in claim 1, wherein each of the wedges includes sides that are in contact with either the blades or the circumferential sides of the slots, each of the sides being either a flat side or a crowned side such that there is a number N1 of flat sides and a number N2 of crowned sides, and a ratio of N1/N2 is 2 or less. 8. The rotor as recited in claim 7, wherein N1 is 2 and N2 is 1. 9. The rotor as recited in claim 7, wherein N1 is 0 and N2 is 2. 10. The rotor as recited in claim 7, wherein N1 is 2 and N2 is 3. 11. The rotor as recited in claim 7, wherein N1 is 1 and N2 is 2. 12. The rotor as recited in claim 7, wherein N1 is 1 and N2 is 1. 13. The rotor as recited in claim 1, wherein each of the wedges includes a coating thereon that surrounds a core. 14. The rotor as recited in claim 1, including bias members located in respective ones of the slots radially inwardly of the blades, the bias members biasing the blades radially outwardly. 15. The rotor as recited in claim 1, wherein the curved surface is on the wedge. 16. The rotor as recited in claim 15, wherein the roots are flared roots. 17. The rotor as recited in claim 15, wherein blades include respective airfoils and necks connecting the airfoils with the roots, and the wedges each include another curved surface in another contact interface with the necks. 18. The rotor as recited in claim 1, wherein the wedges each include a radially intermediate portion between radially inner and outer ends, and the tapered thickness profile tapers from the radially intermediate portion to each of the radially inner and outer ends. 19. The rotor comprising: a disk including slots circumferentially arranged around it periphery;blades including respective roots that are mounted in respective ones of the slots, the roots being smaller than the slots such that there are circumferential gaps between the roots and circumferential sides of the slots; andwedges respectively located in the circumferential gaps, the wedges being free floating with regard to the blades and the disk,with a width dimension (Q) of a neck of the respective blades, a length dimension (L) of a side of the respective wedges in contact with the circumferential side of the disk, a length dimension (E) of a straight portion of another side of the respective wedges, a length dimension (H) of a straight portion of another, different side of the respective wedges, and overlap dimension (X) between the circumferential side of the disk and the side of the respective wedges that has length dimension (L), a gap dimension (B) between a flared root of the respective blades and the side of the respective wedges that has length dimension (E) at a point of transition between a straight portion and a curved portion, and a gap dimension (W) between the neck and the side of the respective wedges that has length dimension (H) at a point of transition between a straight portion and a curved portion, and including at least one of:W/Q is less than or equal to 0.025,W/H is less than or equal to 0.1,X/L is less than or equal to 0.050, andB/E is less than or equal to 0.080. 20. The rotor as recited in claim 19, wherein each of the wedges included less than three flat sides. 21. The rotor as recited in claim 19, wherein each of the blades includes a ceramic material. 22. The rotor as recited in claim 19, wherein each of the wedges includes a coating therein that surrounds a core. 23. The rotor as recited in claim 19, including bias members located in respective ones of the slots radially inwardly of the blades, the bias members biasing the blades radially outwardly. 24. A gas turbine engine, comprising: optionally, a fana compressor section;a combustor in fluid communication with the compressor section; and a turbine section in fluid communication with the combustor, the turbine section being coupled to drive the compressor section and the fan, at least one of the fan, the turbine section and the compressor section including a disk having slots circumferentially arranged around its periphery, blades including respective roots that are mounted in respective ones of the slots, the roots being smaller than the slots such that there are circumferential gaps between the roots and circumferential sides of the slots, and wedges respectively located within the circumferential gaps, the wedges being free floating with regard to the blades and the disk, with the wedges in contact with either the roots or circumferential sides of the slots at respective contact interfaces, each of the contact interfaces including a curved surface in contact with a flat surface such that there is appoint or line of contact between the curved surface and the flat surface, with a width dimension (Q) of a neck of the respective blades, a length dimension (L) of a side of the respective wedges in contact with the circumferential side of the disk, a length dimension (E) of a straight portion of another side of the respective wedges, a length dimension (H) of a straight portion of another, different side of the respective wedges, and overlap dimension (X) between the circumferential side of the disk and the side of the respective wedges that has length dimension (L), a gap dimension (B) between a flared root of the respective blades and the side of the respective wedges that has length dimension (E) at a point of transition between a straight portion and curved portion, and a gap dimension (W) between the neck and the side of the respective wedges that has length dimension (H) at a point of transition between a straight portion and a curved portion, and including at least one of: W/Q is less than or equal to 0.025,W/H is less than or equal to 0.1,X/L is less than or equal to 0.050, andB/E is less than or equal to 0.080.