Patent ID: 7625201

Claim:
A burner-based system for producing exhaust that simulates exhaust produced by an internal combustion engine, for delivery of the exhaust to an emissions control device, comprising: a burner system having at least a burner for receiving air and fuel having an air-fuel ratio and for combusting fuel to produce simulated engine exhaust and having a fuel injector for providing fuel to the burner; an exhaust line for carrying the exhaust from the burner to the emissions control device; a heat exchanger for cooling the exhaust gas downstream the burner; a blower for providing pressurized air flow to the burner; a secondary air injector for providing supplemental oxygen into the exhaust line; a computerized control system operable to control the air-fuel ratio to provide a desired stiochiometry of the burner and to provide a number of burner system operating modes, including at least a thermal excursion mode accomplished by providing the burner with a rich air-fuel ratio and by providing supplemental oxygen into the exhaust line between the burner and -the emissions control device via the secondary air injector; wherein the burner has a combustion tube for receiving air-assisted fuel spray from the fuel injector, and at least one igniter extending into the wall of the combustion tube for creating a burner flame; wherein the burner has a swirl plate having a central bore for holding the fuel injector, the swirl plate further having a first set of turbulent jet bores, swirl jet bores, and a second set of turbulent jet bores through which the pressurized air flow passes into the combustion tube; wherein the first set of turbulent jet bores are angled toward the inner wall of the combustion tube to prevent the burner flame from continuously contacting the inner wall of the combustion tube; wherein the swirl jet bores are angled toward the fuel spray from the injector to interact with the fuel spray to create a swirl pattern of the fuel spray within the combustion tube; and wherein the second set of turbulent jet bores are angled toward the fuel injector to converge in front of the fuel injector to prevent the flame from attaching to the fuel injector.