High speed aerospace generator resilient mount

• US 7,589,447 B2
• Filed: 12/05/2006
• Issued: 09/15/2009
• Est. Priority Date: 12/05/2006
• Status: Active Grant

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Birdi, Balwinder S., Meacham, Walter L., Stout, David E., Down, Edward M., Gradillas, Anna C.
• Primary Examiner(s): Leung; Quyen
• Assistant Examiner(s): Mok; Alex W
• Application Number:
  US11/566,881
• Publication Number:
  US 20080129134A1
• Time in Patent Office: 1,015 Days
• Field of Search: 310/90, 310/51, 384/119, 384/535
• US Class Current: 310/90
• CPC Class Codes: F16C 19/06 with a single row or balls
• CPC Class Codes: F16C 2326/43 Aeroplanes; Helicopters in general B64C
• CPC Class Codes: F16C 2380/26 Dynamo-electric machines or combinations therewith, e.g. electro-motors and generators in general H02K
• CPC Class Codes: F16C 27/04 Ball or roller bearings, e.g. with resilient rolling bodies
• CPC Class Codes: H02K 5/1732 radially supporting the rotary shaft at both ends of the rotor H02K5/1737 takes precedence
• CPC Class Codes: H02K 7/16 for operation above the critical speed of vibration of the rotating parts

Abstract

Centering rings may be used to modify the combined resonance of a rotor and its support assembly to migrate the rotor critical speeds such that they can be engineered out of the rotor operating speed range. The centering rings of the present invention may be useful for any rotating electrical machinery, especially high speed aerospace applications, such as generators and starter-generators.

Claims

1. A high speed rotating electrical machinery, comprising:

a rotor;

a first bearing supporting the rotor;

a housing supporting the first bearing; and

a first centering ring positioned between the first bearing and the housing that deflects due to the vibration of the rotor, wherein the first centering ring comprises;

a flange in the shape of a cylindrical disk, with the flange having a uniform thickness and integral with a first end of the first centering ring and the flange attached to the housing;

a tube spring having a cylindrical shape and a uniform thickness, with the tube spring attached to the flange; and

a plurality of slots forming radial openings through the tube spring, the slots being sealed at a first end by the flange and the slots, at the second opposite end, being sealed by virtue of continuing only partially in an axial direction through the tube spring;

whereby

the number and size of the slots are selected such that the first centering ring exhibits a radial stiffness that will migrate rotor critical speeds outside of an operating speed range of the high speed rotating electrical machinery by selectively absorbing more or less vibrations of the rotor according to the radial stiffness of the centering ring.

2. The high speed rotating electrical machinery according to claim 1, wherein the flange is attached to the housing with bolts.

3. The high speed rotating electrical machinery according to claim 1, wherein the first centering ring is located at one of a drive end or an opposite drive end of the rotor.

4. The high speed rotating electrical machinery according to claim 1, further comprising:

a second bearing supporting the rotor; and

a second centering ring positioned between the second bearing and the housing.

5. The high speed rotating electrical machinery according to claim 1, wherein the centering ring has a stiffness between about 5 klb/in and about 1000 klb/in.

6. The high speed rotating electrical machinery according to claim 1, wherein the rotating electrical machinery is one of a generator or a starter-generator.

7. The high speed rotating electrical machinery according to claim 1, wherein the centering ring has non-isotropic stiffness.