Generators with open loop active cooling

Patent metadata

Field	Value
Publication number	US-9985501-B2
Application number	US-201414172074-A
Country	US
Kind code	B2
Filing date	Feb 4, 2014
Priority date	Aug 16, 2013
Publication date	May 29, 2018
Grant date	May 29, 2018

Abstract

A rotor body for a high-speed generator includes a rotor body with interior and exterior surfaces, a coolant inlet and outlet, and a rotor cooling path for actively cooling the rotor body. The coolant inlet and outlet extend between the interior and exterior surfaces. An interior segment of the rotor cooling path fluidly couples the coolant inlet and coolant outlet and is bounded by the rotor body interior surface. An exterior segment of the cooling path is bounded by the rotor body exterior surface and fluidly couples the coolant outlet an environment external to the rotor body.

First claim

What is claimed is:

1. A rotor for a high-speed generator, comprising:
a rotor body defining:
an interior surface and opposed exterior surface;
a coolant inlet and outlet extending between the interior and exterior surfaces; and

a rotor cooling path including (i) an interior cooling path segment bounded by the rotor body interior surface and fluidly coupling the coolant inlet to the coolant outlet, and (ii) an exterior cooling path segment bounded by the rotor body exterior surface and fluidly coupling the coolant outlet to an external environment for open loop cooling the rotor body; and
a cryogenic fuel supply in fluid communication with the coolant inlet.

2. A rotor as recited in claim 1 , wherein the coolant inlet is configured to fluidly couple the rotor body to a cryogenic fuel supply.

3. A rotor as recited in claim 1 , wherein the coolant inlet is configured to fluidly couple the rotor body to a hydrogen, oxygen, xenon, or helium supply.

4. A rotor a recited in claim 1 , further comprising a baffle coupled to the rotor body inner surface and dividing an interior cavity of the rotor body into a plurality of coolant channels extending between the coolant inlet and the coolant outlet.

5. A rotor as recited in claim 1 , wherein the rotor body defines a plurality of coolant outlets disposed along an axial length of the rotor body.

6. A rotor recited in claim 1 , wherein the rotor body defines a plurality of coolant outlets disposed about a circumference of the rotor body.

7. A rotor as recited in claim 1 , wherein the coolant outlet is bounded by a sidewall extending between the interior and exterior surfaces of the rotor body through a thickness of the rotor body.

8. A rotor as recited in claim 4 , wherein the sidewall intersects a longitudinal axis of the rotor body obliquely such that the coolant outlet is oriented toward a first end portion of the rotor body.

9. A rotor as recited in claim 4 , wherein the sidewall intersects a longitudinal axis of the rotor body obliquely such that the coolant outlet is oriented toward a second end portion of the rotor body.

10. A rotor as recited in claim 4 , wherein the sidewall defines a coolant outlet axis oriented radially outward and towards a direction of rotation of the rotor body.

11. A rotor as recited in claim 4 , wherein the sidewall defines a coolant outlet axis oriented radially outward and opposite a direction of rotation of the rotor body.

12. A turbo-alternator, comprising:
a rotor as recited in claim 1 ;
a stator with an inner surface opposing the rotor body exterior surface and bounding the exterior cooling path segment of the rotor cooling path; and
a cooling path fluidly coupled to the rotor cooling path including a supply orifice and an exhaust orifice, wherein the supply orifice is configured to fluidly couple with a pressurized coolant source for actively cooling the rotor body, wherein the exhaust orifice is fluidly coupled to an external environment for open loop cooling.

13. A turbo-alternator as recited in claim 12 , wherein the coolant inlet is configured to cool bearings supporting the rotor body using coolant flow traversing the coolant inlet.

14. A turbo-alternator as recited in claim 13 , wherein the cooling path includes a speed control valve fluidly coupled between the supply orifice and the coolant inlet of the rotor body.

15. A turbo-alternator as recited in claim 14 , wherein the speed control valve is fluidly coupled to the rotor body through a first coolant inlet and a second coolant inlet.

16. A turbo-alternator as recited in claim 15 , wherein the first and second coolant inlets are arranged on opposite ends of the rotor body.

17. A method of cooling a generator, comprising:
receiving hydrogen coolant from a vehicle fuel supply at an inlet of a rotor body;
flowing the hydrogen coolant through the rotor body along a coolant path including (i) an interior cooling path segment bounded by the rotor body interior surface and fluidly coupling the coolant inlet to the coolant outlet, and (ii) an exterior cooling path segment bounded by the rotor body exterior surface; and
exhausting the hydrogen coolant into the environment external to the vehicle by flowing the hydrogen coolant through a coolant outlet fluidly coupling the exterior cooling path segment to the external environment.

18. A rotor as recited in claim 1 , further comprising a pump fluidly coupling the cryogenic fuel supply to the coolant inlet.

19. A rotor as recited in claim 1 , wherein the cryogenic fuel supply is fluidly coupled to the coolant inlet in blow down arrangement.

Assignees

• Hamilton Sundstrand Corp

Inventors

• Ribarov Lubomir A
• Downing Robert S
• Himmelmann Richard A

Classifications

• H02K1/32

  with channels or ducts for flow of cooling medium · CPC title

• H02K9/197 Primary

  in which the rotor or stator space is fluid-tight, e.g. to provide for different cooling media for rotor and stator · CPC title

• H02K9/19

  for machines with closed casing and closed-circuit cooling using a liquid cooling medium, e.g. oil · CPC title