Turbine rotor assembly having a retaining collar for a bayonet mount

Patent metadata

Field	Value
Publication number	US-10968744-B2
Application number	US-201715587319-A
Country	US
Kind code	B2
Filing date	May 4, 2017
Priority date	May 4, 2017
Publication date	Apr 6, 2021
Grant date	Apr 6, 2021

Abstract

A retaining collar is disclosed for a bayonet mount comprising a rotor disc having a male mounting member defining a pair of apertures and an auxiliary annular wheel defining a plurality of mounting slots. The retaining collar comprises a ring-shaped body and a pair of retention pins. The ring-shaped body has a pair of circumferential end portions separated by a circumferential gap, and an arcuate radial outer surface extending circumferentially between the end portions. The body is dimensioned so that the radial outer surface frictionally engages a radial inner surface of a cylindrical male mounting member in the bayonet mount. The pair of retention pins each extend radially outward from one of the circumferential end portions. Each of the retention pins are dimensioned to extend radially outward from the body through one of said apertures and one of said mounting slots.

First claim

What is claimed is:

1. A turbine rotor assembly comprising:
a rotor disc having a male mounting member comprising:
a cylindrical radially inward facing surface;
a cylindrical radially outward facing mounting surface;
a plurality of radially outward extending mounting pins spaced about the circumference of said mounting surface; and
a pair of apertures defined by said male mounting member, each aperture being adjacent one of said mounting pins;

an auxiliary annular wheel having a female mounting member comprising:
a cylindrical radially inward facing mounting surface; and
a plurality of mounting slots defined by said female mounting member and being spaced about the circumference of said female mounting member, each of said mounting slots having an open axially extending portion and a closed circumferentially extending portion, said auxiliary annular wheel being carried by said rotor disc in a predetermined axial and radial alignment wherein said radially inward facing mounting surface of said wheel frictionally engages said radially outward facing mounting surface of said rotor disc and each of said mounting pins is positioned adjacent a closed end of the circumferentially extending portion of one of said mounting slots; and

a retaining collar comprising:
a ring-shaped body having a pair of end portions separated by a gap, and an arcuate radially outward facing surface extending between said end portions; and
a pair of retention pins, each retention pin extending radially outward from one of the end portions, said retaining collar being positioned so that said radially outward facing surface frictionally engages said radially inward facing surface of said male mounting member and each of said retention pins extends radially outward from said body through one of said apertures and one of said mounting slots.

2. The turbine rotor assembly of claim 1 , wherein said cylindrical radially inward facing surface of said male mounting member defines an annular groove having an other cylindrical radially inward facing surface, and wherein said retaining collar is positioned so that said radially outward facing surface of said body frictionally engages said other radially inward facing surface of said groove.

3. The turbine rotor assembly of claim 2 , wherein a plurality of radially outward extending mounting pins is spaced about the circumference of said radially outward facing surface of said male mounting member at intervals of 120 degrees.

4. The turbine rotor assembly of claim 2 , wherein a plurality of radially outward extending mounting pins is spaced about the circumference of said radially outward facing surface of said male mounting member at intervals of 90 degrees.

5. The turbine rotor assembly of claim 1 , wherein said plurality of radially outward extending mounting pins spaced about the circumference of said radially outward facing surface of said male mounting member includes at least one pair of mounting pins having adjacent apertures circumferentially spaced the same distance as said pair of retention pins.

6. The turbine rotor assembly of claim 1 , wherein said ring-shaped body of said retaining collar has a radially varying thickness and a radially thickest portion diametrically opposite the gap.

7. The turbine rotor assembly of claim 1 , wherein said retention collar is formed from a nickel-chromium alloy.

8. The turbine rotor assembly of claim 1 , wherein said ring-shaped body of said retaining collar comprises a machineable surface for balancing the assembly.

Assignees

• Rolls Royce Corp

Inventors

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

Classifications

• F05D2260/33

  with a bayonet coupling · CPC title

• F05D2270/021

  to prevent overspeed · CPC title

• F01D5/027 Primary

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

• F05D2270/03

  in variable speed operation · CPC title

• F05D2270/022

  to prevent underspeed · CPC title