Turbine assembly with auxiliary wheel

Patent metadata

Field	Value
Publication number	US-10865646-B2
Application number	US-201715587322-A
Country	US
Kind code	B2
Filing date	May 4, 2017
Priority date	May 4, 2017
Publication date	Dec 15, 2020
Grant date	Dec 15, 2020

Abstract

Various embodiments of the present application provide one or more of: (1) auxiliary wheel that (a) enables accurate speed detection of a turbine disc and/or (b) presents a machining surface for balance correction; and/or (2) techniques for mounting an auxiliary wheel to a rotor, such as a turbine disc.

First claim

We claim:

1. A disc and wheel assembly comprising:
(a) a disc comprising:
a mount with a circumferential and radially outwardly facing first mounting surface,
a plurality of radially outwardly extending mounting pins spaced about a circumference of the first mounting surface;

(b) an auxiliary wheel comprising:
a circumferential radially inward facing second mounting surface defining a plurality of mounting slots arranged about a circumference of the second mounting surface, wherein the mounting slots extend through a radial thickness of the auxiliary wheel from the second mounting surface to a circumferential radially outward facing surface of the auxiliary wheel, each of the mounting slots comprising an open and axially extending entry portion and a closed and circumferentially extending retaining portion; wherein each of the mounting pins is disposed in one of the mounting slots and extends radially in the one of the mounting slots through the radial thickness of the auxiliary wheel.

2. The assembly of claim 1 , wherein the auxiliary wheel is carried by the disc in a predetermined axial and radial alignment, the second mounting surface being in an interference engagement with the first mounting surface.

3. The assembly of claim 2 , wherein each of the mounting pins is positioned against a closed end of one of the retaining portions.

4. The assembly of claim 1 , wherein the mounting pins are configured to slide through the entry portions of the mounting slots to reach the retaining portions thereof.

5. The assembly of claim 4 , wherein each mounting pin is radially thicker than each mounting slot.

6. The assembly of claim 1 , wherein each of the mounting slots is T-shaped in the circumferential radially inward facing second mounting surface.

7. The assembly of claim 1 , wherein each of the mounting slots is L-shaped in the circumferential radially inward facing second mounting surface.

8. The assembly of claim 1 , wherein each of the mounting pins is box-shaped.

9. A method of making a disc and wheel assembly,
(a) wherein the disc comprises:
a mount with a circumferential and radially outwardly facing first mounting surface,
a plurality of radially outwardly extending mounting pins spaced about a circumference of the first mounting surface;

(b) wherein the auxiliary wheel comprises:
a circumferential radially inward facing second mounting surface defining a plurality of mounting slots arranged about a circumference of the second mounting surface, wherein the mounting slots extend through a radial thickness of the auxiliary wheel from the radially inward facing second mounting surface to a circumferential radially outward facing surface of the auxiliary wheel, each of the mounting slots comprising an open and axially extending entry portion and a closed and circumferentially extending retaining portion;

the method comprising:
disposing each of the mounting pins in one of the mounting slots such that each of the mounting pins extends radially in the one of the mounting slots through the radial thickness of the auxiliary wheel.

10. The method of claim 9 , comprising;
at least one of: (a) heating the auxiliary wheel to expand the entry portions and (b) cooling the mount to contract the mounting pins; and
while the entry portions are expanded or the mounting pins are contracted, disposing each of the mounting pins in one of the mounting slots.

11. The method of claim 10 , wherein the step of disposing each of the mounting pins in one of the mounting slots comprises:
sliding each of the mounting pins through one the entry portions until reaching one of the retaining portions.

12. The method of claim 11 , wherein the step of disposing each of the mounting pins in one of the mounting slots comprises:
rotating the auxiliary wheel with respect to the disc to clock the mounting pins away from the entry portions.

13. The method of claim 12 , further comprising:
allowing the assembly to return to room temperature;
wherein after the assembly returns to room temperature, surfaces defining opposing axial ends of each retaining slot bear on the mounting pins to disable circumferential movement of each of the mounting pins within the retaining slots.

14. The method of claim 12 , further comprising:
allowing the assembly to return to room temperature;
wherein after the assembly returns to room temperature, the first mounting surface is an interference fit relationship with the second mounting surface.

15. The method of claim 9 , further comprising:
slots,
at least one of: (a) heating the auxiliary wheel and (b) cooling the mount;
performing the step of disposing each of the mounting pins in one of the mounting thereafter, allowing the assembly to return to room temperature;
wherein after the assembly returns to room temperature, the first mounting surface is an interference fit relationship with the second mounting surface.

16. A disc and wheel assembly comprising:
(a) a disc comprising:

a mount with a circumferential first mounting surface,
(b) an auxiliary wheel comprising:
a circumferential second mounting surface
wherein one of the disc and the auxiliary wheel comprise a plurality of radially outwardly facing mounting pins and the other of the disc and the auxiliary wheel defines a plurality of mounting slots, wherein the mounting slots extend through a radial thickness of the auxiliary wheel from the radially inward facing second mounting surface to a circumferential radially outward facing surface of the auxiliary wheel;
each of the mounting pins being disposed in one of the mounting slots such that each of the mounting pins extends radially in the one of the mounting slots through the radial thickness of the auxiliary wheel.

17. The assembly of claim 16 , wherein each mounting slot comprises an open and axially extending entry portion and a closed and circumferentially extending retaining portion.

18. The assembly of claim 17 , wherein the entry portions perpendicularly intersect the retaining portions.

19. The assembly of claim 18 , wherein each of the mounting pins is an interference fit relationship with one of the retaining portions.

20. The assembly of claim 16 , wherein the auxiliary wheel is carried by the disc in a predetermined axial and radial alignment, the second mounting surface being in an interference engagement with the first mounting surface.

Assignees

• Rolls Royce Corp

Inventors

• Snyder Brandon R
• Whitten Michael R
• Sellhorn James E
• Riehle Bradford John

Classifications

• F01D21/02

  Shutting-down responsive to overspeed · CPC title

• F05D2260/30

  Retaining components in desired mutual position · CPC title

• F01D5/027 Primary

  Arrangements for balancing (for balancing rotating bodies in general F16F15/32; for compensating imbalance G01M1/36) · CPC title

• F05D2220/323

  for aircraft propulsion, e.g. jet engines · CPC title

• F01D5/3015

  with side plates · CPC title