Co-generator utilizing micro gas turbine engine

• US 6,679,433 B2
• Filed: 12/18/2000
• Issued: 01/20/2004
• Est. Priority Date: 09/14/1998
• Status: Expired due to Term

• Current Assignee: JetHeat LLC
• Original Assignee: JetHeat, Inc.
• Inventors: Gordon, Richard W., Chute, Richard
• Primary Examiner(s): Boles, Derek
• Application Number:
  US09/740,090
• Publication Number:
  US 20020095939A1
• Time in Patent Office: 1,128 Days
• Field of Search: 237/13, 237/12.1, 60/393.6, 606/48, 165/48.1
• US Class Current: 237/12.1
• CPC Class Codes: F02C 3/14 characterised by the arrangement of the combustion chamber in the plant combustion chambers per se F23R; F02C3/205 takes precedence
• CPC Class Codes: F02C 6/18 using the waste heat of gas-turbine plants outside the plants themselves, e.g. gas-turbine power heat plants using waste heat as source of energy for refrigeration plants F25B27/02; using the waste heat of a gasturbine for steam generation or in a steam cycle see F01K23/10
• CPC Class Codes: F05D 2250/82 Micromachines
• CPC Class Codes: F24H 2240/02 with combustion engines
• CPC Class Codes: Y02E 20/14 Combined heat and power generation [CHP]

Abstract

The present invention provides a turbo heater which utilizes a gas turbine engine and a heat exchanger assembly. The gas turbine engine is adapted to efficiently operate over a prolonged period of time and at varying power outputs without adverse or detrimental effects to the components thereof. For example, the gas turbine engine includes bearing assemblies and a fuel delivery systems which are uniquely designed for the demands of repeated cycling (i.e. starting and stopping), as well as operation at various power outputs without damage to the gas turbine engine. In addition, the use of exhaust gas from the gas turbine engine eliminates direct impingement of combustion on the heat exchanger element, thereby significantly increasing the durability and life span of the turbo heater.

Claims

1. A co-generator comprising:

a micro gas turbine engine including an engine housing, a compressor rotatably supported in said engine housing for drawing air into said gas turbine engine and generating compressed air, a combustor disposed in said engine housing and in fluid communication with said compressor such that said compressed air is directed from said compressor into said combustor, a fuel system for injecting a fuel into said combustor such that said fuel is ignited and burned in said combustor to generate an exhaust gas, and a turbine rotatably supported in said engine housing and in fluid communication with said combustor such that said exhaust gas is expanded in said turbine; and

a heat exchanger assembly including a heat exchanger housing surrounding said micro gas turbine engine and a heat exchanger element providing fluid communication between said micro gas turbine engine and ambient air such that said exhaust gas interacts with said ambient air to generate a heated ambient air which is discharged from said heat exchanger housing.

2. The co-generator of claim 1 wherein said heat exchanger comprises a fan operably coupled to said micro gas turbine for propelling an ambient air into said heat exchanger housing such that said exhaust gas interacts with said ambient air to generate said heated ambient air.

3. The co-generator of claim 2 wherein said heat exchanger further comprises a tube bundle disposed in said heat exchanger housing to define a fresh air volume in fluid communication with said fan for propelling said ambient air therethrough, and an exhaust gas volume in fluid communication with said gas turbine engine for passing said exhaust gas therethrough, said tube bundle operable to transfer heat from said exhaust gas to said ambient air for generating said heated ambient air.

4. The co-generator of claim 3 wherein said tube bundle is generally annularly configured such that said gas turbine engine is at least partially disposed within said annular tube bundle.

5. The co-generator of claim 1 wherein said heat exchanger comprises a liquid coil disposed within said heat exchanger housing to define a liquid volume in fluid communication with a liquid pump for pumping a liquid therethrough and an exhaust gas volume in fluid communication with said gas turbine engine for passing said exhaust gas therethrough, whereby said liquid coil transfers heat from said exhaust gas to said liquid for generating a heated liquid.

6. The turbo heater of claim 1 wherein said heat exchanger comprises a catalytic converter disposed within said heat exchanger housing and in fluid communication with said gas turbine engine for passing said exhaust gas therethrough to generate a catalytically-treated exhaust gas which is exhausted into said heat exchanger housing for mixing with said ambient air.

7. A co-generator comprising:

a co-generator housing having a shell and a inlet plenum and an exhaust diffuser formed in said shell;

a micro gas turbine engine supported within said shell and including;

an engine housing having a compressor chamber with an intake in fluid communication with said inlet plenum, a turbine chamber with an exhaust in fluid communication with said exhaust diffuser and a combustion chamber interposed between said compressor chamber and said turbine chamber to provide fluid communication therebetween;

a compressor rotatably supported in said compressor chamber;

a fuel system for injecting a fuel into said combustor; and

a turbine rotatably supported in said turbine housing; and

a heat exchanger assembly supported within said shell and including;

a first fluid circuit in fluid communication with said exhaust diffuser; and

a second fluid loop in heat transfer relationship with said first fluid circuit such that an exhaust gas flowing in said first fluid circuit heats an ambient fluid flowing in said second fluid circuit to generate a heated ambient fluid.

8. The co-generator of claim 7 wherein said heat exchanger assembly further comprises a fan rotatably supported in said shell for propelling an ambient air into said plenum, said second fluid loop being in fluid communication with said plenum such that a portion of said ambient air flows through said second fluid loop to generate a heated ambient air.

9. The co-generator of claim 8 wherein said fan is rotatably driven by said micro gas turbine engine.

10. The co-generator of claim 8 wherein said second fluid circuit comprises a tube bundle disposed in said shell fluid communication with said plenum.

11. The co-generator of claim 10 wherein said tube bundle is generally annularly configured such that said gas turbine engine is at least partially disposed within said tube bundle.

12. The co-generator of claim 11 wherein said exhaust gas and said ambient air flow through said heat exchanger assembly in opposite directions.

13. The co-generator of claim 7 wherein said second fluid circuit comprises a liquid fluid coil in fluid communication with a liquid pump for pumping a liquid therethrough such that said liquid coil transfers heat from said exhaust gas to said liquid for generating a heated liquid fluid.