Fan-cooled electrical machine with axial thrust compensation

Patent metadata

Field	Value
Publication number	US-10218245-B2
Application number	US-201414916471-A
Country	US
Kind code	B2
Filing date	Mar 6, 2014
Priority date	Sep 3, 2013
Publication date	Feb 26, 2019
Grant date	Feb 26, 2019

Abstract

A rotating machinery equipment is disclosed, including a rotating electrical machine having a stator (1) and a rotating shaft (7), whereon a rotor (11) is mounted. The machinery equipment further includes a cooling fan (23) comprised of a rotating impeller (33) mounted on the rotating shaft (7) for co-rotation therewith. Cooling gas passages (45, 47) are provided for delivering compressed cooling gas through the stator and rotor. The cooling gas is delivered by the impeller (33) into a cooling-gas distribution chamber (31). The pressure of the cooling gas in the cooling-gas distribution chamber generates an axial force balancing the axial thrust generated on the electrical machine by the cooling gas flow.

First claim

What is claimed is:

1. A rotating machinery equipment comprising a rotating electrical machine comprising:
a stator;
a rotating shaft;
a rotor mounted on the rotating shaft and rotating therewith;
a cooling fan comprised of a rotating impeller having a gas inlet and a gas outlet and mounted at a first end of the rotating shaft and rotating therewith;
a thrust disk integrally rotating with the impeller, the thrust surface being located on the thrust disk; and
cooling gas passages for delivering compressed cooling gas through the stator and rotor;

wherein a cooling-gas distribution chamber is provided between the cooling fan and the stator and rotor, in fluid communication with the cooling fan and the cooling gas passages, compressed cooling gas delivered by the cooling fan being received in the cooling-gas distribution chamber and distributed therefrom to the cooling gas passages; and
wherein the cooling fan is provided with a thrust surface facing the stator and rotor, gas pressure in the cooling-gas distribution chamber acting on the thrust surface, generating an axial force (AT) on the rotating shaft, the axial force being oriented in a direction opposite the cooling gas flow through the stator and rotor.

2. The rotating machinery equipment of claim 1 , further comprising a turbomachine drivingly connected to a second end of the rotating shaft.

3. The rotating machinery equipment of claim 2 , wherein a load coupling is arranged between the electrical machine and the turbomachine.

4. The rotating machinery equipment of claim 3 , wherein the load coupling comprises a flexible shaft coupling.

5. The rotating machinery equipment according to claim 2 , wherein the electrical machine and the turbomachine are housed in a common enclosure.

6. The rotating machinery equipment according to claim 2 , wherein the electrical machine and the turbomachine are housed in separate enclosures.

7. The rotating machinery equipment according to claim 1 , wherein the cooling fan comprises a stationary diffuser at the gas outlet of the impeller.

8. The rotating machinery equipment according to claim 1 , further comprising an inlet manifold, through which cooling gas enters the gas inlet of the impeller, and wherein the inlet manifold has a cross section which decreases along flow direction.

9. The rotating machinery equipment of claim 1 , wherein the thrust disk has an outer diameter larger than an outer diameter of the impeller.

10. The rotating machinery equipment according to claim 1 , further comprising a seal, preferably a non-contact seal, more preferably a labyrinth seal, between an outer peripheral edge of the thrust disk and a stationary component of the cooling-gas distribution chamber.

11. The rotating machinery equipment according to claim 1 , further comprising a seal, preferably a non-contact seal, more preferably a labyrinth seal, between an outer peripheral edge of the impeller and a stationary component of the cooling-gas distribution chamber.

12. The rotating machinery equipment according to claim 1 , wherein the rotating shaft has a larger-diameter end portion, whereon the impeller is keyed, and a smaller diameter portion co-acting with a sealing arrangement, which seals the cooling-gas distribution chamber against the rotating shaft, and wherein an annular shoulder between the smaller diameter portion and the larger diameter portion forms an auxiliary thrust surface, whereon the gas pressure in the cooling-gas distribution chamber acts.

13. A method for reducing an axial thrust on a rotating machinery equipment comprising a rotating electrical machine having a stator, a rotating shaft, a rotor mounted on the rotating shaft and rotating therewith, and a cooling fan arranged for generating a pressurized cooling gas flow across a gap between the rotor and the stator, the cooling fan comprised of a rotating impeller having an impeller inlet and an impeller outlet and arranged on the rotating shaft, the method comprising:
building up a gas pressure by receiving cooling gas in a cooling-gas distribution chamber; and, with the cooling gas pressure, generating an axial force (AT) acting upon the shaft, the axial force being oriented in a direction opposite the flow direction of the cooling gas through the gap between the rotor and the stator;
accelerating a cooling gas flow in the impeller and increasing a static pressure of the cooling gas from the inlet to the outlet of the impeller;
slowing down the cooling gas flow and increasing the static pressure thereof through a diffuser arranged between the impeller outlet and the cooling-gas distribution chamber.

14. The method of claim 13 , wherein the rotating machinery equipment further comprises a turbomachine, connected preferably through a load coupling to the electrical machine, and wherein the fan is mounted on the rotating shaft opposite the turbomachine.

15. A method for reducing an axial thrust on a rotating machinery equipment comprising a rotating electrical machine having a stator, a rotating shaft, and a rotor mounted on the rotating shaft and rotating therewith; the method comprising:
using a cooling fan comprised of a rotating impeller having an impeller inlet and an impeller outlet and arranged on the rotating shaft;
rotating the impeller and delivering compressed cooling gas in a cooling-gas distribution chamber;
delivering cooling gas in a cooling-gas flow direction from the cooling-gas distribution chamber towards the rotor and stator;
generating, with the compressed cooling gas in the cooling-gas distribution chamber, a balancing axial force, the balancing axial force acting on the shaft in a direction opposite a cooling-gas flow direction;
accelerating a cooling gas flow in the impeller and increasing a static pressure of the cooling gas from the inlet to the outlet of the impeller;
slowing down the cooling gas flow and increasing the static pressure thereof through a diffuser arranged between the impeller outlet and the cooling-gas distribution chamber.

16. The method of claim 15 , further comprising recovering gas pressure downstream of the diffuser to increase the static pressure of in the cooling-gas distribution chamber above the static pressure of the cooling gas at the outlet of the diffuser.

17. The method of claim 15 , wherein the rotating machinery equipment further comprises a turbomachine, connected preferably through a load coupling to the electrical machine, and wherein the fan is mounted on the rotating shaft opposite the turbomachine.

Assignees

• Nuovo Pignone Srl

Inventors

• Oxman Ilia
• Michelassi Vittorio

Classifications

• F04D25/06

  the pump being electrically driven (F04D25/08 takes precedence) · CPC title

• H02K7/1823

  structurally associated with turbines or similar engines · CPC title

• F04D29/5806

  Cooling the drive system · CPC title

• F04D29/0516

  balancing pistons · CPC title

• H02K9/06 Primary

  with fans or impellers driven by the machine shaft · CPC title