Vane lever arm for a variable area vane arrangement

1. A variable area vane arrangement, comprising:

a stator vane including a shaft having an axis; and

a vane lever arm that rotates the stator vane about the axis, and includes a base, a first tab and a second tab, wherein

the base is arranged laterally between the first tab and the second tab;

the first tab laterally overlaps the base; and

the second tab includes an aperture and laterally overlaps the base and the first tab;

wherein the shaft extends through the aperture and is connected to the base;

wherein the first tab extends from the base to a first anti-rotation element;

wherein the second tab includes a second anti-rotation element that partially defines the aperture;

wherein the shaft is arranged between and engages the first anti-rotation element and the second anti-rotation element;

wherein the second tab includes a third anti-rotation element that partially defines the aperture;

wherein the third anti-rotation element is separated from the shaft by a gap during a first mode of operation, and engages the shaft during a second mode of operation; and

wherein the shaft is arranged between the second anti-rotation element and the third anti-rotation element.

2. The vane arrangement of claim 1 , wherein the vane lever arm further includes an arm portion that extends longitudinally from the base.

3. The vane arrangement of claim 1 , wherein the first tab is located adjacent the shaft.

4. The vane arrangement of claim 1 , wherein the first tab overlaps the aperture.

5. The vane arrangement of claim 1 , wherein the first anti-rotation element is configured as a substantially planar surface that contacts a substantially planar surface of the shaft.

6. The vane arrangement of claim 1 , wherein the second anti-rotation element is configured as a substantially planar surface that contacts a substantially planar surface of the shaft.

7. The vane arrangement of claim 1 , wherein

at least one of the first tab and the second tab each include an intermediate portion and an end portion;

the intermediate portion extends between the base and the end portion; and

the end portion overlaps the base.

8. The vane arrangement of claim 7 , wherein the intermediate portion is curved, and the end portion is substantially planar.

9. The vane arrangement of claim 1 , wherein the base includes a second aperture, and the shaft extends through the second aperture.

10. The vane arrangement of claim 1 , further comprising a vane platform including a second aperture, wherein the stator vane further includes a turbine engine airfoil, and wherein the shaft extends from the airfoil, through the second aperture, to the vane lever arm.

11. A variable area vane arrangement, comprising:

a stator vane including a shaft having an axis; and

a vane lever arm that rotates the stator vane about the axis, and includes a base, a first tab and a second tab, wherein

the base is arranged between the first tab and the second tab;

the first tab extends from the base to a first anti-rotation element; and

the second tab includes an aperture and a second anti-rotation element that partially defines the aperture;

wherein the shaft extends through the aperture, is connected to the base, and is arranged between the first anti-rotation element and the second anti-rotation element;

wherein the second tab includes a third anti-rotation element that partially defines the aperture;

wherein the third anti-rotation element is separated from the shaft by a gap during a first mode of operation, and engages the shaft during a second mode of operation; and

wherein the shaft is arranged between the second anti-rotation element and the third anti-rotation element.

12. The vane arrangement of claim 11 , wherein the first tab overlaps the base, and the second tab overlaps the base and the first tab.

13. The vane arrangement of claim 12 , wherein the first tab overlaps the aperture.

14. The vane arrangement of claim 11 , wherein

at least one of the first tab and the second tab each include an intermediate portion and an end portion;

the intermediate portion extends between the base and the end portion; and

the end portion overlaps the base.

15. The vane arrangement of claim 11 , further comprising a vane platform including a second aperture, wherein the stator vane further includes a turbine engine airfoil, and wherein the shaft extends from the airfoil, through the second aperture, to the vane lever arm.

16. A variable area vane arrangement, comprising:

a stator vane including a shaft; and

a vane lever arm configured to rotate the stator vane about an axis of the shaft, the vane lever arm including an arm portion, a base, a first tab and a second tab;

the arm portion projecting out from the base and away from the shaft;

the base extending and connected laterally between the first tab and the second tab;

the first tab connected to the arm portion through the base independent of the second tab, and the first tab laterally overlapping the base;

the second tab connected to the arm portion through the base independent of the first tab, and the second tab including an aperture and laterally overlapping the base and the first tab;

wherein the shaft extends through the aperture and is connected to the base.

17. The vane arrangement of claim 16 , wherein

the first tab extends from the base to a first anti-rotation element;

the second tab includes a second anti-rotation element that partially defines the aperture; and

the shaft is arranged between and engages the first anti-rotation element and the second anti-rotation element.

18. The vane arrangement of claim 17 , wherein

the second tab includes a third anti-rotation element that partially defines the aperture;

the third anti-rotation element is separated from the shaft by a gap during a first mode of operation, and engages the shaft during a second mode of operation; and

the shaft is arranged between the second anti-rotation element and the third anti-rotation element.