Low diameter turbine rotor clamping arrangement

Patent metadata

Field	Value
Publication number	US-10100642-B2
Application number	US-201514841308-A
Country	US
Kind code	B2
Filing date	Aug 31, 2015
Priority date	Aug 31, 2015
Publication date	Oct 16, 2018
Grant date	Oct 16, 2018

Abstract

A gas turbine engine having turbine discs includes a low diameter turbine rotor clamp for securing the turbine discs together. The rotor clamp includes a clamp sleeve, a clamp cylinder adapted to be threadably engaged to the clamp sleeve to apply an axial force on the turbine discs being coupled together. The rotor clamp includes an anti-score ring positioned between the bore of a turbine disc and the clamp cylinder and a lock tube used to prevent unwanted rotation of the clamp cylinder with respect to the clamp sleeve.

First claim

What is claimed is:

1. A low diameter turbine rotor clamp for securing turbine discs together comprising:
a clamp cylinder having a cylindrical wall section and a threaded section that is adjacent the cylindrical wall section, the clamp cylinder adapted to be positioned within a bore of a first turbine disc;
a clamp sleeve having a cylindrical wall section and a threaded section that is adjacent the cylindrical wall section, the clamp sleeve adapted to be positioned within a bore of a second turbine disc, the threaded section of the clamp sleeve is adapted to threadably engage the threaded section of the clamp cylinder; and
an anti-score ring positioned between the bore of the first turbine disc and the cylindrical wall section of the clamp cylinder, the anti-score ring including an annular sidewall having an outer surface that is sized to engage the bore of the first turbine disc to prevent unwanted wear to the bore;
wherein when the clamp cylinder is threaded and tightened with respect to the clamp sleeve an axial force is applied to the first and second turbine discs.

2. The rotor clamp of claim 1 , wherein the threaded section of the clamp cylinder includes a series of buttress threads.

3. The rotor clamp of claim 2 , wherein the threaded section of the clamp sleeve includes a series of buttress threads.

4. The rotor clamp of claim 1 , wherein the coefficient of expansion of the clamp sleeve is different than the coefficient of expansion of the second turbine disc.

5. The rotor clamp of claim 1 , wherein the anti-score ring includes an annular lip that extends radially outward from the annular sidewall of the anti-score ring that is adapted to engage an axially-facing surface of the second turbine disk to prevent unwanted wear.

6. A low diameter turbine rotor clamp for securing turbine discs together comprising:
a clamp cylinder having a cylindrical wall section and a threaded section that is adjacent the cylindrical wall section, the clamp cylinder adapted to be positioned within a bore of a first turbine disc;
a clamp sleeve having a cylindrical wall section and a threaded section that is adjacent the cylindrical wall section, the clamp sleeve adapted to be positioned within a bore of a second turbine disc, the threaded section of the clamp sleeve is adapted to threadably engage the threaded section of the clamp cylinder;
an anti-score ring positioned between the bore of the first turbine disc and the cylindrical wall section of the clamp cylinder; and
a lock tube positioned within the clamp cylinder and having a first lock tab that engages a notch formed in the cylindrical wall section of the clamp cylinder,
wherein when the clamp cylinder is threaded and tightened with respect to the clamp sleeve an axial force is applied to the first and second turbine discs.

7. The rotor clamp of claim 6 , wherein the lock tube includes a second lock tab that is adapted to engage a slot formed in the cylindrical wall section of the clamp sleeve wherein the lock tube prevents unwanted rotation of the clamp cylinder with respect to the clamp sleeve.

8. The rotor clamp of claim 7 , wherein the slot is elongated and extends through at least a portion of the threaded section of the clamp sleeve.

9. A low diameter turbine rotor clamp for securing turbine discs together comprising:
a clamp cylinder having a cylindrical wall section and a threaded section that is adjacent the cylindrical wall section, the clamp cylinder adapted to be positioned within a bore of a first turbine disc;
a clamp sleeve having a cylindrical wall section and a threaded section that is adjacent the cylindrical wall section, the clamp sleeve adapted to be positioned within a bore of a second turbine disc, the threaded section of the clamp sleeve is adapted to threadably engage the threaded section of the clamp cylinder; and
an anti-score ring positioned between the bore of the first turbine disc and the cylindrical wall section of the clamp cylinder;
wherein when the clamp cylinder is threaded and tightened with respect to the clamp sleeve an axial force is applied to the first and second turbine discs, and wherein the clamp sleeve is press fit into the bore of the second turbine disc.

10. A low diameter turbine rotor clamp for securing turbine discs together comprising:
a clamp cylinder having a cylindrical wall section and a threaded section that is adjacent the cylindrical wall section, the clamp cylinder adapted to be positioned within a bore of a first turbine disc;
a clamp sleeve having a cylindrical wall section and a threaded section that is adjacent the cylindrical wall section, the clamp sleeve adapted to be positioned within a bore of a second turbine disc, the threaded section of the clamp sleeve is adapted to threadably engage the threaded section of the clamp cylinder; and
an anti-score ring positioned between the bore of the first turbine disc and the cylindrical wall section of the clamp cylinder;
wherein when the clamp cylinder is threaded and tightened with respect to the clamp sleeve an axial force is applied to the first and second turbine discs, and wherein the clamp sleeve includes an annular flange at a first end the annular flange having an inner face that is adapted to engage the second turbine disc when the clamp sleeve and clamp cylinder are secured together.

11. The rotor clamp of claim 10 , wherein the clamp cylinder includes an annular flange having an inner face that is adapted to engage the first turbine disc when the clamp sleeve and clamp cylinder are secured together.

12. The rotor clamp of claim 11 , wherein the annular flange of the clamp cylinder is formed to include a series of grooves on an outer face to permit the clamp cylinder to be rotated with respect to the clamp sleeve.

13. A low diameter turbine rotor clamp for securing turbine discs together comprising:
a clamp cylinder having a cylindrical wall section and a threaded section that is adjacent the cylindrical wall section, the clamp cylinder adapted to be positioned within a bore of a first turbine disc;
a clamp sleeve having a cylindrical wall section and a threaded section that is adjacent the cylindrical wall section, the clamp sleeve adapted to be positioned within a bore of a second turbine disc, the threaded section of the clamp sleeve is adapted to threadably engage the threaded section of the clamp cylinder; and
a lock tube including a cylindrical sidewall positioned within the clamp cylinder and a first lock tab extending radially from the cylindrical sidewall to engage a notch formed in the cylindrical wall section of the clamp cylinder such that the lock tube is adapted to prevent unwanted rotation of the clamp cylinder with respect to the clamp sleeve;
wherein when the clamp cylinder is threaded and tightened with respect to the clamp sleeve an axial force is applied to the first and second turbine discs;
wherein the lock tube includes a second lock tab that is adapted to engage a slot formed in the cylindrical wall section of the clamp sleeve wherein the lock tube prevents unwanted rotation of the clamp cylinder with respect to the clamp sleeve; and
wherein the slot is elongated and extends through at least a portion of the threaded section of the clamp sleeve.

14. The rotor clamp of claim 13 , wherein the coefficient of expansion of the clamp sleeve is different than the coefficient of expansion of the second turbine disc.

15. A low diameter turbine rotor clamp for securing turbine discs together comprising:
a clamp cylinder having a cylindrical wall section and a threaded section that is adjacent the cylindrical wall section, th

Assignees

• Rolls Royce Corp

Inventors

• Morrison Daniel K
• Basiletti Matthew P
• Jackson Matthew I

Classifications

• F01D5/025

  Fixing blade carrying members on shafts (attachment of a member on a shaft in general F16D1/06; for non-positive displacement pumps F04D29/00) · CPC title

• F01D5/066 Primary

  Connecting means for joining rotor-discs or rotor-elements together, e.g. by a central bolt, by clamps · CPC title

• Y02T50/672

  Cross-Sectional Technologies · mapped topic

• Y02T50/60

  Efficient propulsion technologies, e.g. for aircraft · CPC title