Dual turbogenerator auxiliary power system

• US 5,799,484 A
• Filed: 04/15/1997
• Issued: 09/01/1998
• Est. Priority Date: 04/15/1997
• Status: Expired due to Fees

• Current Assignee: Hybrid Power Generation Systems, LLC
• Original Assignee: Alliedsignal Inc.
• Inventors: Nims, Robert A.
• Primary Examiner(s): Casaregola, Louis J.
• Application Number:
  US08/839,746
• Time in Patent Office: 504 Days
• Field of Search: 60/39.142, 60/39.15, 60/39.33, 60/39.511, 290/4 R, 290/4 A, 290/4 D
• US Class Current: 60/39.15
• CPC Class Codes: F01D 15/10 Adaptations for driving, or combinations with, electric generators
• CPC Class Codes: F01D 21/02 Shutting-down responsive to overspeed
• CPC Class Codes: F02C 6/02 Plural gas-turbine plants having a common power output
• CPC Class Codes: F02C 7/08 Heating air supply before combustion, e.g. by exhaust gases
• CPC Class Codes: F02C 9/42 specially adapted for the control of two or more plants simultaneously
• CPC Class Codes: F05D 2220/50 for auxiliary power units (APU's)
• CPC Class Codes: Y02E 20/14 Combined heat and power generation [CHP]

Abstract

An auxiliary power system comprises two turbogenerators sharing a single combustor for delivery of elevated pressure and temperature gas to both the turbogenerators, a single fuel system for supplying elevated pressure fuel to the single combustor, and a single electronic unit for conditioning the electrical power input and output. The auxiliary power system also comprises first and second recuperator means operating in association with the dual turbogenerators for transferring heat from turbine exhaust to air entering the single combustor. The entire recuperator volume is used in both the single and dual turbogenerator operating modes.

Claims

1. An auxiliary power system comprising:

a first turbogenerator having an associated first turbine, first compressor and first generator mounted on a first high-speed shaft;

a second turbogenerator having an associated second turbine, second compressor and second generator mounted on a second high-speed shaft;

a single electronic unit for conditioning externally supplied electrical power for startup/motoring of the first and second turbogenerators;

a single combustor for delivery of elevated pressure and temperature gas to both the first and second turbogenerators;

a single fuel system for safely supplying elevated pressure fuel to the single combustor; and

first and second recuperator means operating in association with the first and second turbogenerators for transferring heat from turbine exhaust to air entering the single combustor.

2. An auxiliary power system as claimed in claim 1 wherein the first and second turbogenerators comprise essentially identical one-half rated power turbogenerators.

3. An auxiliary power system as claimed in claim 1 wherein the first turbogenerator comprises a first partial rated power turbogenerator and the second turbogenerator comprises a second partial rated power turbogenerator.

4. An auxiliary power system as claimed in claim 3 wherein the first partial rated power and the second partial rated power total a full rated power value.

5. An auxiliary power system as claimed in claim 1 further comprising means for operating the system in a single or a dual turbogenerator operating mode.

6. An auxiliary power system as claimed in claim 5 wherein the entire recuperator volume is used in both single and dual turbogenerator operating modes.

7. An auxiliary power system as claimed in claim 1 wherein the single electronic unit further comprises means for supervising, controlling and monitoring critical parameters and operation of the auxiliary power system.

8. An auxiliary power system as claimed in claim 1 wherein the system has high thermal cycle efficiency throughout its operating range.

9. An auxiliary power system as claimed in claim 8 wherein the operating range is from about 10% to about 100% of rated power.

10. An auxiliary power system as claimed in claim 1 wherein the first and second generators are configured to rotate at the same speed as the respective associated shaft, compressor and turbine.

11. An auxiliary power system as claimed in claim 1 wherein the single electronic unit further comprises means for conditioning electrical power input for turbogenerator startup and electrical power output of the system.