MICROTURBINE ENGINE SYSTEM

• US 20060066113A1
• Filed: 10/25/2005
• Published: 03/30/2006
• Est. Priority Date: 06/18/2002
• Status: Active Grant

• Current Assignee: Flexenergy Energy Systems, Inc. (FlexEnergy, Inc.)
• Original Assignee: Ingersoll-Rand Energy Systems Incorporated
• Inventors: Oliver, Sunit, Lakov, German, Ebrahim, Mohammed
• Granted Patent: US 7,045,913 B2
• Time in Patent Office: Days
• US Class Current: 290/52
• CPC Class Codes: F05D 2250/82 Micromachines
• CPC Class Codes: H02P 2101/15 for wind-driven turbines
• CPC Class Codes: H02P 9/04 Control effected upon non-electric prime mover and dependent upon electric output value of the generator
• CPC Class Codes: H02P 9/30 using semiconductor devices
• CPC Class Codes: Y02E 20/14 Combined heat and power generation [CHP]

Abstract

A microturbine engine that includes a compressor that is operable to provide a flow of compressed air. The compressed air flows through a recuperator where it is preheated before delivery to a combustor. The preheated compressed air mixes with a fuel and is combusted within the combustor to provide a flow of products of combustion. The flow of products of combustion pass through one or more turbines to drive the compressor and a synchronous generator. The synchronous generator is able to synchronize to a priority load, to the utility grid or to both depending on the mode of operation. A control system monitors various engine parameters as well as load and grid parameters to determine the desired mode of operation.

Claims

1. A microturbine engine system operable to provide electrical power to a load, the microturbine engine system comprising:

a compressor operable to produce a flow of compressed air;

a fuel delivery system operable to deliver a flow of fuel;

a recuperator in fluid communication with the compressor to receive the flow of compressed air, the flow of compressed air being preheated within the recuperator to produce a flow of preheated compressed air;

a combustor receiving the flow of preheated compressed air and the flow of fuel, the combustor combusting the flow of compressed air and the flow of fuel to produce a flow of products of combustion;

a turbine driven by the flow of products of combustion from the combustor;

a synchronous generator coupled to the turbine, the synchronous generator driven by the turbine at a speed, the synchronous generator outputting an electrical power having a frequency;

an energy management system including a variable electric load, the variable electric load absorbing at least a portion of the electrical power, the remainder of the electrical power being delivered to the load; and

a control system operable to vary the flow of fuel and the variable electric load to maintain the portion of the electrical power absorbed by the variable electric load and the frequency of the electrical power within predetermined ranges.

2. The microturbine engine system of claim 1, wherein the variable electrical load includes a plurality of resistors and a plurality of switches, wherein the switches are individually actuatable to apply or remove electrical load.

3. The microturbine engine system of claim 2, wherein the switches include silicon-controlled rectifiers.

4. The microturbine engine system of claim 1, wherein the variable electrical load of the energy management system includes an energy storage device.

5. The microturbine engine system of claim 1 wherein the variable electrical load of the energy management system includes a plurality of energy storage devices each device being one of an ultracapacitor, a resistor, and a battery charger.

6. The microturbine engine system of claim 1, wherein the electrical power is distributed to the load and to the variable electric load, and wherein the energy management system varies the variable electrical load to maintain the electrical power output by the generator, and wherein the control system varies the flow of fuel to maintain the variable electrical load when operating in grid parallel mode.