Turbine assembly with auxiliary wheel

Patent metadata

Field	Value
Publication number	US-2018320522-A1
Application number	US-201715587310-A
Country	US
Kind code	A1
Filing date	May 4, 2017
Priority date	May 4, 2017
Publication date	Nov 8, 2018
Grant date	—

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 method of balancing a rotor assembly, the method comprising:
affixing an auxiliary wheel to a rotor disc, the auxiliary wheel comprising an annular balance land; coupling the rotor disc with a coaxial driveshaft; spinning the driveshaft to rotate the auxiliary wheel and the rotor disc as a unit;
estimating a center of rotation of the unit; and
grinding the annular balance land of the auxiliary wheel based on a difference between the estimated center of rotation of the unit and a central axis of the driveshaft.

2 . The method of claim 1 , further comprising circumferentially rotating the auxiliary wheel with respect to the rotor disc based on the estimated center of rotation of the unit.

3 . The method of claim 1 , wherein prior to the grinding step, a maximum radial thickness of the auxiliary wheel is equal to a maximum radial thickness of the annular balance land.

4 . The method of claim 1 , wherein the rotor disc comprises an annular mount and the step of affixing the auxiliary wheel to the rotor disc comprises placing the auxiliary wheel around the annular mount.

5 . The method of claim 4 , wherein the step of affixing the auxiliary wheel to the rotor disc results in an interference fit between an inner diameter of the auxiliary wheel and an outer diameter of the mount.

6 . The method of claim 5 , wherein the step of affixing the auxiliary wheel to the rotor disc comprises heating the auxiliary wheel, performing the step of placing the auxiliary wheel around the annular mount, and allowing the auxiliary wheel to cool.

7 . The method of claim 6 , wherein the auxiliary wheel defines an aperture with an entry portion and a locking portion, the mount comprises a radially extending tab, and the step of placing the auxiliary wheel around the annular mount comprises passing the radially extending tab through the entry portion of the aperture and into the locking portion of the aperture.

8 . The method of claim 7 , wherein the step of heating the auxiliary wheel comprises heating the auxiliary wheel at least until a width of the entry portion of the aperture exceeds a width of the radially extending tab; and
the step of allowing the auxiliary wheel to cool comprises allowing the auxiliary wheel to cool at least until the width of the entry portion of the aperture contracts to become smaller than the width of the radially extending tab.

9 . The method of claim 8 , wherein the aperture defined in the auxiliary wheel is “T” shaped.

10 . The method of claim 8 , wherein the rotor disc is a turbine disc and the method further comprises securing turbine blades to the rotor disc.

11 . The method of claim 1 , wherein the auxiliary wheel is magnetic and the rotor disc is non-magnetic.

12 . The method of claim 1 , wherein the auxiliary wheel comprises an annular target portion comprising an alternating sequence of teeth and channels;

13 . A rotor assembly comprising:
a rotor disc; an auxiliary wheel affixed to the rotor disc and comprising an annular balance land.

14 . The rotor assembly of claim 13 , wherein the auxiliary wheel is directly mounted to the rotor disc.

15 . The rotor assembly of claim 14 , wherein the balance land radially protrudes from the auxiliary wheel.

16 . The rotor assembly of claim 15 , wherein the balance land outwardly radially protrudes from the auxiliary wheel.

17 . The rotor assembly of claim 16 , wherein a maximum radial thickness of the auxiliary wheel is equal to a maximum radial thickness of the balance land.

18 . The rotor assembly of claim 15 , wherein the balance land, when viewed in a cross section, is plateau-shaped.

19 . The rotor assembly of claim 18 , wherein a radial outer surface of the balance land is deformed from subtractive machining.

20 . The rotor assembly of claim 19 , wherein the auxiliary wheel is seated on an axially extending and annular mount of the rotor disc.

Assignees

• Rolls Royce Corp

Inventors

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

Classifications

• F01D5/027 Primary

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

• F05D2260/30

  Retaining components in desired mutual position · CPC title

• F05D2220/32

  in gas turbines · CPC title

• F05D2230/60

  Assembly methods · CPC title

• F05D2240/24

  for turbines · CPC title