Control device for the pitch of blades, and propeller

1. A control device of the pitch of blades of a rotor of a propeller, comprising:

a radial shaft;

a pivot connected to the blade, a foot of the blade being mounted in the pivot, rotation of the radial shaft driving rotation of the pivot for modifying the pitch of the blade;

an insert fixed rigidly to the pivot so as to block a relative displacement of the insert with respect to the pivot, the insert being in direct contact with the radial shaft, the radial shaft being configured to drive in rotation the insert via rotation transmission elements borne respectively on an external surface of the radial shaft and an inner surface of the insert, the insert comprising a fixing flange;

at least one peg passing through the fixing flange of the insert and the pivot for transmission of the rotation of the insert to the pivot; and

a heat insulation element interposed between the fixing flange of the insert and the pivot, a thermal conductivity of the heat insulation element is less than a thermal conductivity of the pivot and a thermal conductivity of the radial shaft.

2. The device according to claim 1 , wherein the insert is fixed to the pivot by at least one screw.

3. The device according to claim 2 , wherein the heat insulation element encloses a circumference of at least one part of the peg or of the at least one screw.

4. The device according to claim 1 , wherein the heat insulation element consists in an air gap.

5. The device according to claim 4 , wherein the air gap has a height of less than or equal to 1 mm.

6. The device according to claim 1 , wherein the heat insulation element includes a material in which the thermal conductivity is less than the thermal conductivity of the pivot and the thermal conductivity of the radial shaft.

7. The device according to claim 6 , wherein the heat insulation element comprises an annular piece comprising:

a central opening, for passage of the radial shaft, and

one or more circumferential openings.

8. The device according to claim 6 , wherein the heat insulation element comprises one or more separate annular pieces enclosing at least one part of the peg or a screw linking the radial shaft to the pivot.

9. The device according to claim 6 , wherein the thermal conductivity of the material of the heat insulation element is between 0.01 and 10 W/m/K at 20° C.

10. A propeller comprising a rotor and blades, and a control device of the pitch of the blades according to claim 1 .

11. A control device of the pitch of blades of a rotor of a propeller, comprising:

a radial shaft;

a pivot connected to the blade, rotation of the radial shaft driving rotation of the pivot for modifying the pitch of the blade;

an insert fixed rigidly to the pivot so as to block a relative displacement of the insert with respect to the pivot, the radial shaft being configured to drive in rotation the insert;

at least one peg passing through the insert and the pivot for transmission of the rotation of the insert to the pivot; and

a heat insulation element arranged between the insert and the pivot, a thermal conductivity of the heat insulation element is less than a thermal conductivity of the pivot and a thermal conductivity of the radial shaft,

wherein the heat insulation element includes a material in which the thermal conductivity is less than the thermal conductivity of the pivot and the thermal conductivity of the radial shaft, and

wherein the thermal conductivity of the material of the heat insulation element is between 0.01 and 10 W/m/K at 20° C.