Cooling of turboalternator for hybrid motor vehicle

• US 5,789,824 A
• Filed: 05/02/1996
• Issued: 08/04/1998
• Est. Priority Date: 05/02/1996
• Status: Expired due to Term

• Current Assignee: FCA US LLC (Stellantis NV)
• Original Assignee: Chrysler Corporation (Stellantis NV)
• Inventors: Heitmann, Arnold M., Selfors, Brian J.
• Primary Examiner(s): Stephan, Steven L.
• Assistant Examiner(s): Ponomarenko, Nicholas
• Application Number:
  US08/642,084
• Time in Patent Office: 824 Days
• Field of Search: 290/52, 290/54, 290/43, 290/45, 60/668, 60/698, 60/716, 180/65.1, 180/65.3, 180/65.2, 180/65.4, 180/301
• US Class Current: 290/52
• CPC Class Codes: B60L 50/15 with additional electric power supply with capacitors charged by engine-driven generators B60L50/40; with batteries charged by engine-driven generators B60L50/61
• CPC Class Codes: F01D 15/10 Adaptations for driving, or combinations with, electric generators
• CPC Class Codes: F02C 3/085 the turbine being of the radial-flow type (radial-radial) F02C3/05 takes precedence
• CPC Class Codes: F02C 6/20 Adaptations of gas-turbine plants for driving vehicles
• CPC Class Codes: Y02T 10/70 Energy storage systems for electromobility, e.g. batteries
• CPC Class Codes: Y02T 10/7072 Electromobility specific charging systems or methods for batteries, ultracapacitors, supercapacitors or double-layer capacitors

Abstract

A turboalternator for a hybrid motor vehicle includes at least one compressor, at least one turbine, at least one alternator having a rotor and being disposed between the at least one compressor and the at least one turbine, and a common shaft having a longitudinal axis and interconnecting the at least one compressor and the at least one alternator and the at least one turbine. The common shaft is integral and formed as one-piece with the rotor. The turboalternator also includes a structure for cooling the at least one alternator having at least one fluid flow channel extending longitudinally through the rotor and being spaced radially from the longitudinal axis of the common shaft.

Claims

1. A turboalternator for a hybrid motor vehicle comprising:

at least one compressor;

at least one turbine;

at least one alternator having a rotor and being disposed between said at least one compressor and said at least one turbine;

a common shaft having a longitudinal axis and interconnecting said at least one compressor and said at least one alternator and said at least one turbine said common shaft being integral and formed as one-piece with said rotor; and

means for cooling said at least one alternator comprising at least one fluid flow channel extending longitudinally through said rotor, said at least one fluid flow channel being spaced radially from the longitudinal axis of said common shaft.

2. A turboalternator as set forth in claim 1 including at least one first bearing supporting a first end of said common shaft.

3. A turboalternator as set forth in claim 2 including at least one second bearing supporting a second end of said common shaft.

4. A turboalternator as set forth in claim 1 including a hydrodynamic axial bearing and a hydrodynamic rotary bearing supporting each end of said common shaft.

5. A turboalternator as set forth in claim 1 including a pump disposed on opposite ends of said alternator rotor to pump fluid through said at least one fluid flow channel.

6. A turboalternator as set forth in claim 5 wherein said pump is a Barske pump.

7. A turboalternator for a hybrid motor vehicle comprising:

at least one compressor;

at least one turbine;

at least one alternator having a rotor and being disposed between said at least one compressor and said at least one turbine;

a common shaft having a longitudinal axis and interconnecting said at least one compressor and said at least one alternator and said at least one turbine, said common shaft being integral and formed as one-piece with said rotor; and

means for cooling said at least one alternator comprising at least one fluid flow channel extending longitudinally through said rotor, said at least one fluid flow channel being spaced radially from the longitudinal axis of said common shaft, and a Barske pump disposed about each end of said rotor and communicating with said at least one fluid flow channel to assist in pumping fluid through said at least one fluid flow channel at high speeds of said rotor without changing a phase of the fluid.