Rotor assembly

Patent metadata

Field	Value
Publication number	US-9926940-B2
Application number	US-201013203155-A
Country	US
Kind code	B2
Filing date	Feb 10, 2010
Priority date	Feb 24, 2009
Publication date	Mar 27, 2018
Grant date	Mar 27, 2018

Abstract

A rotor assembly that includes a shaft and an impeller and/or a rotor core. The shaft is secured within a bore in the impeller and/or the rotor core by an adhesive such that the concentricity of the shaft is smaller than that of the bore. A method of manufacturing the rotor assembly is also described.

First claim

The invention claimed is:

1. A rotor assembly comprising a shaft, at least one impeller, and a rotor core, the shaft being adhered within a bore of the at least one impeller and the rotor core by the method comprising:
adhering the shaft within a bore in the at least one impeller and rotor core by an adhesive such that the concentricity of the shaft relative to the at least one impeller and rotor core is smaller than that of the bore, and wherein the adhesive is applied to an outer surface of the shaft.

2. The rotor assembly of claim 1 , wherein the ratio of the concentricities of the shaft and the bore is no greater than 0.9.

3. The rotor assembly of claim 1 , wherein the impeller is formed of plastic.

4. The rotor assembly of claim 1 , wherein the concentricity of the shaft is no greater than 0.07 mm.

5. The rotor assembly of claim 1 wherein the concentricity of the shaft relative to a centerline of the impeller is smaller than the concentricity of the bore in the impeller relative to the centerline of the impeller, and the concentricity of the shaft relative to a centerline of the rotor core is smaller than the concentricity of the bore in the rotor core relative to the centerline of the rotor core.

6. The rotor assembly of claim 5 , wherein the rotor assembly comprises a bearing cartridge located between the impeller and the rotor core.

7. The rotor assembly of claim 5 , wherein the rotor core is formed of a rare-earth magnetic material.

8. A method of manufacturing a rotor assembly comprising:
providing a shaft;
providing at least one of an impeller and a rotor core; and
adhering the shaft within a bore in the at least one impeller and rotor core such that the concentricity of the shaft relative to the at least one impeller and rotor core is smaller than that of the bore,
wherein adhering the shaft within the bore comprises applying an adhesive to the shaft and inserting the shaft into the bore while rotating the shaft relative to the at least one impeller and rotor core.

9. The method of claim 8 , wherein the method comprises mounting each of the shaft and the at least one impeller and rotor core in one half of a jig, the two halves of the jig being aligned, and bringing the two halves of the jig together while rotating one half of the jig relative to the other half of the jig.

10. The method of claim 8 , wherein the radius of the shaft has a first concentricity, the radius of the bore has a second concentricity the bore has a third concentricity, and the method comprises providing at least one of the impeller and rotor core with a bore of nominal radius greater than the nominal radius of the shaft by at least the sum of the first, second and third concentricities.

11. The method of claim 10 , wherein the method comprises providing at least one of the impeller and rotor core with a bore of nominal radius greater than the nominal radius of the shaft by at least the sum of the first, second and third concentricities and a nominal radial gap that encourages wicking of the adhesive between the shaft and bore.

12. The method of claim 8 , wherein the ratio of the concentricities of the shaft and the bore is no greater than 0.9.

13. The method of claim 8 , wherein the concentricity of the shaft is no greater than 0.07 mm.

14. A rotor assembly comprising a shaft, an impeller, a rotor core and a bearing assembly, wherein the impeller and the rotor core are secured to the shaft at opposite ends of the shaft and the bearing cartridge is secured to the shaft between the impeller and the rotor core, and the shaft is secured within a bore of at least one of the impeller and the rotor core by the method comprising:
adhering the shaft within a bore in the impeller and the rotor core by an adhesive such that the concentricity of the shaft relative to the one impeller and rotor core is smaller than that of the bore, and wherein the adhesive is applied to an outer surface of the shaft.

Assignees

• Mockridge Richard Iain
• Dyson Technology Ltd

Inventors

• Mockridge Richard Iain

Classifications

• F16D1/068 Primary

  involving gluing, welding or the like · CPC title

• F04D29/622

  Adjusting the clearances between rotary and stationary parts · CPC title

• F04D29/263 Primary

  mounting fan or blower rotors on shafts · CPC title

• F04D29/626

  Mounting or removal of fans · CPC title

• F04D29/266 Primary

  mounting compressor rotors on shafts · CPC title