Teodoro A. Cantu - Mission TX, US Ulric Teodoro Alejandro Cantu - McAllen TX, US Ervin Eliud Torres Gomez - Reynosa, MX
Assignee:
Resource Rex, LLC - McAllen TX
International Classification:
F23N 1/02 F23Q 7/06 F23D 14/64
US Classification:
431 89, 431258, 431354
Abstract:
A high efficiency laminar flow burner system for proving a stream of heat energy including a supply input module for providing fuel and laminar streams of air to a combustion manifold. The combustion manifold includes an air-fuel mixing system, a stoichiometric unit, and a refractory unit each coupled to one another. A first combustion stream is established at the air-fuel mixing chamber system as fuel exits an injector device at direction perpendicular to the laminar air intake stream. A laminar air intake stream traveling from the supply input module and along the staging passageway passes through a stoichiometric unit body at a plurality of air intakes to meet with the first combustion stream within to define a second combustion stream for introduction from the stoichiometric unit to the refractory unit. The refractory unit thus defines a third combustion stream as the second combustion stream travels across a refractory passageway.
Combustion Efficiency Control System For A Laminar Burner System
TEODORO A. CANTU - MISSION TX, US ULRIC TEODORO ALEJANDRO CANTU - MCALLEN TX, US ERVIN ELIUD TORRES GOMEZ - REYNOSA, MX
International Classification:
F23N 1/02 F23Q 9/00 F23L 3/00
US Classification:
431 89, 110297, 431278
Abstract:
A high efficiency laminar flow burner system for proving a stream of heat energy including a supply input module for providing fuel and laminar streams of air to a combustion manifold. The laminar air delivery system includes a damper, a blower, and an air delivery controller. The air delivery controller receives an efficiency signal to control the flow of a laminar air intake stream by adjusting the damper. The combustion manifold includes an air-fuel mixing system, a stoichiometric unit, and a refractory unit each coupled to one another. The laminar air intake stream traveling from the supply input module passes through a stoichiometric unit body to meet with a first combustion stream from an air-fuel mixing chamber within the stoichiometric unit body to define a second combustion stream. The second combustion stream then travels across the refractory passageway to define a third combustion stream.