Exhaust liner deflection limiter

1. A deflection limiter system comprising:

a spacer comprising:

a chimney having a first side and a second side opposite of the first side and further including an aperture wherein the aperture extends from the first side to the second side, and wherein the aperture is oblong in cross-sectional shape, the oblong cross-sectional shape defining a major dimension and a minor dimension;

a flange, the flange being disposed on the first side; and

at least one anti-rotation tab, the anti-rotation tab being disposed on the second side near an edge of the second side; and

a bolt having a T-shape, the bolt comprising:

an elongate shaft, the shaft extending along an axis and having a diameter; and

a head connected to an end of the shaft, the head having at least one straight edge;

wherein the at least one straight edge engages with the anti-rotation tab, thereby preventing rotation of the T-bolt about the axis;

wherein the diameter of the bolt is smaller than the major dimension of the aperture such that a gap exists between the bolt and spacer when the spacer is inserted over the bolt.

2. The deflection limiter system of claim 1 , wherein the bolt further includes external threads, the threads being circumferential on the elongate shaft at a distal end from the head.

3. The deflection limiter system of claim 2 , further including a nut, wherein the nut includes internal threads, the internal threads having dimensions that allow the nut to threadably matably engage with the external threads on the bolt.

4. The deflection limiter system of claim 3 , wherein the nut is a self-locking nut.

5. The deflection limiter system of claim 1 , wherein the major dimension is greater than the minor dimension.

6. The deflection limiter system of claim 1 , wherein the bolt is manufactured from a nickel alloy.

7. The deflection limiter system of claim 1 , wherein the spacer is manufactured from a nickel alloy.

8. The deflection limiter system of claim 1 , wherein the deflection limiter system is positioned in an exhaust duct of a gas turbine engine to attach an exhaust liner to a static structure.

9. A method for connecting a deflection limiter system to an exhaust sidewall liner, the method comprising:

inserting a T-bolt through a first aperture and a rectangular, second aperture, the T-bolt having a head with at least one straight edge and a shape corresponding to the first aperture and the second aperture, the head being connected to an end of an elongate shaft, and the first aperture being in a static structure section and the second aperture being on a concealed side of a hollow exhaust liner, proximate to the first aperture;

rotating the T-bolt approximately a quarter-turn;

placing a spacer onto the elongate shaft, the spacer comprising:

a chimney with an aperture extending from a first end to a second end for receiving the elongate shaft;

a flange disposed on the first end of the chimney; and

an anti-rotation tab disposed on the second end of the chimney near an edge of the second end;

wherein a diameter of the elongate shaft is less than a major dimension of the aperture of the spacer such that a gap exists between the bolt and spacer when the spacer is inserted over the bolt; and

inserting the spacer into the first aperture and the second aperture such that the straight edge engages with the anti-rotation tab, thereby preventing rotation of the T-bolt.

10. The method of claim 9 , further comprising attaching a nut to the T-bolt such that internal threads of the nut threadably matably engage with external threads of the T-bolt.

11. The method of claim 10 , wherein the nut is a self-locking nut.

12. The method of claim 10 , wherein the nut is manufactured from a nickel alloy.

13. The method of claim 9 , wherein the T-bolt is manufactured from a nickel alloy.

14. The method of claim 9 , wherein the spacer is manufactured from a nickel alloy.

15. A system for limiting deflection of an exhaust sidewall liner on a variable geometry exhaust duct, the system comprising:

the exhaust sidewall liner;

a static structure; and

an exhaust liner deflection limiter connecting the exhaust sidewall liner to the static structure, the exhaust liner deflection limiter comprising:

a spacer positioned in the static structure, the spacer comprising:

a chimney having a first side and a second side opposite of the first side and further including an aperture wherein the aperture extends from the first side to the second side;

a flange, the flange being disposed on the first side; and

at least one anti-rotation tab, the anti-rotation tab being disposed on the second side near an edge of the second side;

a stud having a head and a shaft, the head being positioned in the exhaust sidewall liner and the shaft extending through the spacer; and

a fastener connected to the shaft to secure the exhaust sidewall liner to the static structure;

wherein the chimney aperture is oblong in cross-sectional shape, the oblong defining a major dimension and a minor dimension; and

wherein a diameter of the shaft is less than the major dimension of the chimney aperture such that a gap exists between the bolt and spacer when the spacer is inserted over the bolt.

16. The system of claim 15 , wherein the major dimension is greater than the minor dimension by an amount that accommodates lateral shift between the static structure and the exhaust sidewall liner.

17. The system of claim 15 , wherein the static structure aperture dimension is greater than the chimney dimension by an amount that accommodates lateral shift between the static structure and the exhaust sidewall liner.

18. The system of claim 15 , wherein the spacer is manufactured from a nickel alloy.