Dynamoelectric machine rotor ventilation

• US 6,552,452 B2
• Filed: 10/19/2001
• Issued: 04/22/2003
• Est. Priority Date: 10/26/2000
• Status: Expired due to Fees

• Current Assignee: General Electric Canada (GE Aerospace)
• Original Assignee: General Electric Canada (GE Aerospace)
• Inventors: Ferguson, James Harold
• Primary Examiner(s): Mullins, Burton S.
• Application Number:
  US09/982,231
• Publication Number:
  US 20020050748A1
• Time in Patent Office: 550 Days
• Field of Search: 310/52, 310/58, 310/59, 310/61, 310/62
• US Class Current: 310/61
• CPC Class Codes: H02K 1/325 between salient poles
• CPC Class Codes: H02K 9/12 wherein the cooling medium circulates freely within the casing

Abstract

A dynamoelectric machine has a stator member, a rotor member, a first shroud and a second shroud. The first shroud and the second shroud members are mounted to the rotor adjacent respective first and second end portions of the rotor for rotation with the rotor. The first and second shrouds extend radially over and are spaced from the respective radially extending first and second end portions of the rotor to respectively define radial inlet and outlet paths therewith. The first and second shrouds each have a first radially inner end adjacent and spaced from the shaft to define a gas inlet or outlet, respectively, and a second radial outer end mounted to the rotor adjacent and spaced apart the ventilation ducts for communicating gas between the ventilation ducts and the inlet and outlet paths. The second outlet shroud is spaced further from the shaft than the inlet shroud so as to facilitate the gas flowing in the inlet shroud and out the outlet shroud during normal machine operation. Fan motors are provided at the inlet and outlet of the shrouds to direct gas flow. The present invention provides for an improvement in windage loss by angularly accelerating the gas prior to entering the ventilation ducts of the rotor and an additional improvement by partially reclaiming energy at the outlet shroud energy by angularly decelerating the gas flow.

Claims

1. A dynamoelectric machine comprising:

a stator member;

a rotor member mounted within the stator member on an axially extending shaft, the rotor member having spaced apart radially extending first and second end portions and a plurality of spaced apart ventilation ducts each extending between the first and second end portions in a substantially axial direction;

a first shroud member mounted to the rotor adjacent the first end portion of the rotor for rotation therewith, the first shroud extending radially over and spaced from the radially extending first end portion of rotor to define a radial gas inlet path therewith, the first shroud having a first radially inner end portion adjacent to and spaced from the shaft to define a gas inlet and a second radial outer end portion mounted to the rotor for directing gas into the ventilation ducts, and the first shroud member rotating with the rotor to angularly accelerate the moving gas along the radial gas inlet path and into the ventilation ducts; and

,

a second shroud member mounted to the rotor adjacent the second end portion of the rotor for rotation therewith, the second shroud extending radially over and spaced from the radially extending second end portion of rotor to define a radial gas outlet path therewith, the second shroud having a second radially inner end portion adjacent to and spaced from the shaft to define a gas outlet and a second radial outer end portion mounted to the rotor adjacent the spaced apart ventilation ducts for receiving gas exiting the ventilation ducts, and the second shroud member rotating with the rotor to decelerate angularly the gas exiting the ventilation ducts and traveling along the radial gas outlet path.

2. The dynamoelectric machine of claim 1 wherein the rotor includes a plurality of spaced apart poles adjacent an air gap with the stator member, adjacent ones of the poles having an axially extending interpolar space and a cover member extending between the poles across the interpolar spaces to define the ventilation ducts.

3. The dynamoelectric machine of claim 1 wherein the machine is a sealed rotor dynamoelectric machine.

4. The dynamoelectric machine of claim 1 wherein each of the first and second shrouds has a curved rim surface adjacent respective first and second radially outer end portions to redirect gas flow respectively between radial and axial flow, and axial and radial flow.

5. The dynamoelectric machine of claim 1 further including a blower motor adjacent one of the gas inlet, gas outlet and both to direct gas flow into the gas inlet, along the radial gas inlet path, axially along the ventilation ducts, along the radial gas outlet path and out the gas outlet.

6. The dynamoelectric machine of claim 1 wherein second outlet shroud extends radially towards the shaft a predetermined distance less than the first inlet shroud.