Gas turbine generators

• US 11,125,103 B2
• Filed: 09/13/2017
• Issued: 09/21/2021
• Est. Priority Date: 09/13/2016
• Status: Active Grant

• Current Assignee: Delta Cosworth Limited
• Original Assignee: Delta Motorsport Limited
• Inventors: Carpenter, Nicholas, Herring, Scott, Wilksch, Mark
• Primary Examiner(s): Le, Dang D
• Application Number:
  US16/332,881
• Publication Number:
  US 20190360352A1
• Time in Patent Office: 1,469 Days
• CPC Class Codes: F01D 15/10 Adaptations for driving, or combinations with, electric generators
• CPC Class Codes: F01D 25/16 Arrangement of bearings; Supporting or mounting bearings in casings bearings per se F16C
• CPC Class Codes: F02C 3/05 the compressor and the turbine being of the radial flow type
• CPC Class Codes: F02C 6/12 Turbochargers, i.e. plants for augmenting mechanical power output of internal-combustion piston engines by increase of charge pressure
• CPC Class Codes: F02C 7/08 Heating air supply before combustion, e.g. by exhaust gases
• CPC Class Codes: F16C 2360/23 Gas turbine engines in general F02C

Abstract

A radial flow gas turbine generator (10) where the gas turbine generator (10) includes a shaft (30) having a rotor (20) of the generator (10), a compressor wheel (16) and a turbine wheel (18) fixed thereto. The shaft (30) is supported for rotation by a single bearing arrangement (38 provided at an axial position on the shaft (30) that is between the rotor (20) and the compressor wheel (16).

Claims

1. A radial flow gas turbine generator, the radial flow gas turbine generator including:

a radial flow gas turbine section and an electrical generation section;

a shaft having a rotor of the electrical generation section, with a compressor wheel and a turbine wheel of the gas turbine section fixed to the shaft; and

a single bearing arrangement supporting the shaft for rotation, wherein said single bearing arrangement is at an axial position on the shaft between the rotor of the electrical generation section and the compressor and turbine wheel of the gas turbine section, wherein the rotor of the electrical generation section and the compressor of the gas turbine section are overhung on opposing sides of the single bearing arrangement.

2. The gas turbine generator as claimed in claim 1 wherein the single bearing arrangement includes two or more mechanical contact bearings.

3. The gas turbine generator as claim 2 wherein the mechanical contact bearings are rolling element bearings.

4. The gas turbine generator as claimed in claim 2 wherein the bearing arrangement includes bearings in a module that maintains a predetermined relationship between the bearings.

5. The gas turbine generator as claimed in claim 4 wherein the bearings are mounted within a sleeve.

6. The gas turbine generator as claimed in claim 5 wherein the bearings are mounted in a spaced apart relationship to one another within the sleeve.

7. The gas turbine generator as claimed in claim 6 wherein a resilient member is located between the bearings in the sleeve.

8. The gas turbine generator as claimed in claim 7 wherein the resilient member is a coil spring.

9. The gas turbine generator as claimed in claim 8 wherein the coil spring is located within the sleeve such that a first end of the coil spring abuts one of the bearings and an opposite end of the coil spring abuts a seat provided on the sleeve.

10. The gas turbine generator as claimed in claim 1 wherein the bearing arrangement is air cooled.

11. The gas turbine generator as claimed in claim 1 wherein the bearing arrangement is self-lubricating.

12. The gas turbine generator as claimed in claim 1, further comprising an oil wick system configured to lubricate the bearing arrangement.

13. The gas turbine generator as claimed in claim 1, further comprising a recirculating lubrication system configured to cool and lubricate the bearing arrangement.

14. A method of operating a radial flow gas turbine generator as claimed in claim 1, wherein the operating speed of the radial flow gas turbine generator is greater than the first resonant speed.

15. A vehicle comprising:

battery cells; and

a gas turbine generator in electrical communication with the battery cells, the gas turbine generator including a radial flow gas turbine section and an electrical generation section, a shaft, a compressor wheel and a turbine wheel of the gas turbine section, and a single bearing arrangement, the shaft having a rotor of the electrical generation section, the compressor wheel fixed to the shaft, the turbine wheel fixed to the shaft, and the single bearing arrangement supporting the shaft for rotation, the single bearing arrangement at an axial position on the shaft between the rotor of the electrical generation section and the compressor and turbine wheel of the gas turbine section, wherein rotation of the shaft produces electrical power to recharge the battery cells, wherein the rotor of the electrical generation section and the compressor wheel of the gas turbine section are overhung on opposing sides of the single bearing arrangement.