Claims
- 1. A tie bolt clamping apparatus, comprising:
a first component designed to rotate; a second component designed to rotate; a tie bolt coupled between said first component and said second component thereby forming a rotatable assembly in which said tie bolt, the first component, and the second component are constraint to rotate together; a shaft supported on said tie bolt and disposed between said first component and said second component; and wherein said tie bolt compresses said first shaft between said first component and said second component such that an axial compressive load on and first shaft is maintained during rotation of said rotatable assembly, thereby preventing mechanical instability.
- 2. The apparatus of claim 1, further comprising a sleeve disposed within said shaft.
- 3. The apparatus of claim 2 wherein said sleeve is not formed from steel.
- 4. The apparatus of claim 2 wherein said sleeve is formed at least in part from material having a coefficient of thermal expansion lower than the coefficient of thermal expansion of steel.
- 5. The apparatus of claim 2 wherein said shaft defines an inset surface formed on at least one of an interior surface and an exterior surface of said shaft.
- 6. The apparatus of claim 2 further including a plate coupled to said shaft.
- 7. The apparatus of claim 2 wherein said sleeve is formed from material which is thermally conductive.
- 8. The apparatus of claim 2, wherein said sleeve is formed from material selected from the group consisting of titanium, titanium alloys and ceramic compositions.
- 9. The apparatus of claim 1 further including a thrust wheel coupled to said shaft.
- 10. A tie bolt clamp apparatus, comprising:
a first component designed to rotate; a second component designed to rotate; a tie bolt coupled between said first component and said second component thereby forming a rotatable assembly in which the tie bolt, the first component, and the second component are constrained to rotate together about an axis defined by an elongated dimension of said tie bolt; a shaft coupled to at least one of said first component and said second component and supported on said tie bolt, said shaft having an interior surface and an exterior surface, said interior surface forming an inset along at least a portion of a length of at least one of said interior surface and said exterior surface; a clamp sleeve supported within said inset; and wherein said tie bolt presses said first sleeve and said clamp sleeve against said first component during rotation such that an axial compressive load on said shaft is maintained.
- 11. The apparatus of claim 10, wherein said clamp sleeve is formed from material having a coefficient of thermal expansion which minimizes deformation of said clamp sleeve such that said axial compressive load is maintained.
- 12. The apparatus of claim 10, wherein said clamp sleeve is formed from material which is thermally conductive.
- 13. The apparatus of claim 10, wherein said clamp sleeve is formed from material selected from the group consisting of titanium, titanium alloys and ceramic compositions.
- 14. The apparatus of claim 10, wherein said shaft includes a thrust wheel.
- 15. The apparatus of claim 10, wherein said sleeve is formed from material having a low coefficient of thermal expansion.
- 16. The apparatus of claim 10, wherein said first component is a compressor element and said second component is a turbine element.
- 17. A method for maintaining a compressive load associated with a rotor shaft, comprising the steps of:
forming a rotational assembly including,
a first component designed to rotate, a second component designed to rotate, a tie bolt coupled between said first component and said second component in which said tie bolt, said first component, and the second component are constrained to rotate together along an axis defined by an elongated dimension of said tie bolt, a shaft supported on said tie bolt, said shaft having at least one portion made of a material with a coefficient of thermal expansion which is lower than coefficients of thermal expansion of at least one of the material of said first component, said second component, and said tie bolt; and rotating said assembly such that said tie bolt compresses said shaft and said first component against said second component such that an axial compressive load is applied to said shaft, whereby said at least one portion minimally deforms and thereby maintains said axial compressive load.
- 18. The method of claim 17, wherein an interior surface of said sleeve defines an inset, and said at least one portion forms a sheath disposed in said inset.
- 19. The method of claim 17, wherein said first component is a compressor element and said second component is a turbine element.
RELATED APPLICATIONS
[0001] This patent application claims the priority of provisional application serial No. 60/245,703, filed Nov. 2, 2000, which provisional application is incorporated by reference herein in its entirety.
Provisional Applications (1)
|
Number |
Date |
Country |
|
60245703 |
Nov 2000 |
US |