EDWARD E MOORE
Engineers in Hummelstown, PA

License number
Pennsylvania PE039659R
Category
Engineers
Type
Professional Engineer
Address
Address
Hummelstown, PA 17036

Professional information

Edward Moore Photo 1

Compact Combination Burner With Adjustable Spin Section

US Patent:
6488496, Dec 3, 2002
Filed:
Sep 6, 2001
Appl. No.:
09/946598
Inventors:
James J. Feese - Elizabethtown PA
Raymond F. Baum - Lebanon PA
Edward E. Moore - Hummelstown PA
Bruce C. Irwin - Chattanooga TN
Assignee:
Hauck Manufacturing Co. - Lebanon PA
International Classification:
F23Q 900
US Classification:
431285, 431115, 431182, 431188, 431284
Abstract:
A combination burner for selectively firing oil, natural gas and liquid propane. A modular first section has primary and secondary air tubes coaxially arranged therein and communicates with the main combustion air supply fan. A modular section is joined by bolts or the like to the first section and into which the primary and secondary air tubes extend. A center air spin vane rack is upstream of the secondary air tube in the first section. An adjustable spin vane rack is located radially outwardly of the secondary air tube for selectively spinning the main combustion air for flame adjustability. An air diverter is provided at a downstream end of the primary air tube. A compressed air atomizer is also at the downstream end of the primary air tube.


Edward Moore Photo 2

Combination Burner With Boost Gas Injection

US Patent:
5259755, Nov 9, 1993
Filed:
Jul 31, 1992
Appl. No.:
7/922765
Inventors:
Bruce C. Irwin - Palmyra PA
Edward E. Moore - Hummelstown PA
Raymond F. Baum - Lebanon PA
Assignee:
Hauck Manufacturing Company - Lebanon PA
International Classification:
F23C 1700, F23C 900, F23C 506
US Classification:
431 9
Abstract:
A burning method promotes rapid mixing and a stable flame in a burner to reduce NO. sub. x and CO emissions and to provide a smoother, quieter operation. The burner includes a primary fuel supply, a combustion air supply arranged to supply combustion air at low pressure, and a swirler for swirling the combustion air. When the primary fuel supply is gaseous fuel, the gaseous fuel is introduced radially into the swirling combustion air. A bluff body cone is arranged near the exit of the burner so as to be encountered by at least the swirling combustion air. An atomizer is arranged within the bluff body cone for atomizing liquid fuel when the primary fuel supply is a liquid fuel. Boost gas nozzles are arranged toroidily at the exit of the burner to supply and mix swirling boost gas for combustion with the combustion air when the gaseous fuel is the primary fuel supply, and mixer tabs are disposed around the periphery of the exit.


Edward Moore Photo 3

High Velocity Burner, System And Method

US Patent:
5263849, Nov 23, 1993
Filed:
Dec 20, 1991
Appl. No.:
7/810847
Inventors:
Bruce C. Irwin - Palmyra PA
Edward E. Moore - Hummelstown PA
Richard A. Carpenter - Cornwall PA
Assignee:
Hauck Manufacturing Company - Lebanon PA
International Classification:
F23C 700
US Classification:
431 6
Abstract:
A burner and burner firing method and system for a furnace combustion chamber in which a burner, having an ignition chamber for discharging an ignited combustible mixture of primary air and fuel into the furnace combustion chamber, and a plurality of nozzle ports for directing a high velocity stream of secondary air into the furnace combustion chamber in a direction generally parallel to the direction of flow from said ignition chamber, is operated in a first mode at furnace combustion chamber temperatures up to a transitional temperature by accelerating a burning mixture of fuel and air to moderately high velocities into the furnace combustion chamber, and in a second mode at furnace combustion temperatures above said transitional temperature by introducing a relatively low velocity stream of fuel mixed with a minor amount of air needed for stoichiometric combustion and accelerating a separate stream of air to high velocities into the furnace combustion chamber for mixture with said low velocity stream downstream from the burner in the furnace combustion chamber, said separate stream of air comprising the remainder of air required for stoichiometric combustion of the fuel. The system includes fuel supply and separately controlled primary and secondary air supply flow lines in which the fuel/air ratio in the respective modes of operation is dependent on air flow rates.


Edward Moore Photo 4

Method And Apparatus For Reducing Nitrous Oxides And Co Emissions In A Gas-Fired Recuperated Radiant Tube Burner

US Patent:
6190159, Feb 20, 2001
Filed:
Mar 3, 1999
Appl. No.:
9/261235
Inventors:
Edward E. Moore - Hummelstown PA
Raymond F. Baum - Lebanon PA
Brian K. Kelly - Harrisburg PA
Assignee:
Hauck Manufacturing Company - Lebanon PA
International Classification:
F23D 2100, F23C 900, F23C 1100
US Classification:
431 11
Abstract:
A radiant tube burner assembly and method is provided to reduce nitrous oxides and carbon monoxide emissions in the combustion of hydrocarbon fuels. The burner assembly comprises a burner section, exhaust section, radiant tube, plenum and a jet pump assembly. A volume of exhaust gas drawn from the stream of exhaust gases into the jet pump assembly by way of a motive gas is flowed into a stream of combustion air so as to vitiate the oxygen content of the combustion mixture. When the combustion mixture is combusted with fuel in the burner section, the production of nitrous oxides and other harmful emission is mitigated.


Edward Moore Photo 5

Combination Burner With Primary And Secondary Fuel Injection

US Patent:
5700143, Dec 23, 1997
Filed:
May 12, 1995
Appl. No.:
8/439944
Inventors:
Bruce C. Irwin - Palmyra PA
Edward E. Moore - Hummelstown PA
Raymond F. Baum - Lebanon PA
Assignee:
Hauck Manufacturing Company - Lebanon PA
International Classification:
F23D 1700
US Classification:
431284
Abstract:
A combination burner which uses primary and secondary fuel injection and improves liquid propane combustion. The burner supplies primary air, while secondary air is swirled to shape and mix the flame when the burner is firing "on oil". When the burner is firing "on gas", primary air enters the burner through an annulus at the atomizing air pipe or conduit so as to have the primary gas enter that pipe; secondary gas is injected radially into the air stream at a downstream location relative to an atomizing nozzle. In using liquid propane (butane) to fire the burner, two stage fuel injection is used, with a stream of fuel being injected upstream and toward the burner centerline and another stream of fuel being injected downstream and outwardly away from the burner centerline.


Edward Moore Photo 6

Combination Burner With Primary And Secondary Fuel Injection

US Patent:
5511970, Apr 30, 1996
Filed:
Jan 24, 1994
Appl. No.:
8/188406
Inventors:
Bruce C. Irwin - Palmyra PA
Edward E. Moore - Hummelstown PA
Raymond F. Baum - Lebanon PA
Assignee:
Hauck Manufacturing Company - Lebanon PA
International Classification:
F23D 1700
US Classification:
431 9
Abstract:
A burning method provides a versatile burner by promoting rapid mixing and a stable flame to reduce NO. sub. x and CO emissions over a wide operating range. The burner includes a primary fuel supply, a combustion air supply arranged to supply combustion air at low pressure, and a swirler for swirling the combustion air. When the primary fuel supply is gaseous fuel, the gaseous fuel is introduced axially into the swirling combustion air. Secondary gas nozzles are arranged at the exit of the burner to supply and mix boost gas for combustion with the combustion air when the gaseous fuel is the primary fuel supply. An atomizer is arranged for atomizing liquid fuel when the primary fuel supply is a liquid fuel.


Edward Moore Photo 7

Variable Exit High Velocity Burner

US Patent:
6220852, Apr 24, 2001
Filed:
Jun 1, 2000
Appl. No.:
9/583531
Inventors:
Edward E. Moore - Hummelstown PA
Assignee:
Hauck Manufacturing Company - Lebanon PA
International Classification:
F23C 112, F23C 700
US Classification:
431 8
Abstract:
A method and apparatus for adjusting the flame exit velocity of a high velocity burner. The burner includes burner combustor chamber having a fluid accelerating nozzle and a burner combustor exhaust port. Fuel is delivered to the burner combustor through a fuel inlet. An ignitor is provided to initiate combustion of the fuel which is mixed with air from an air inlet. An adjusting device is provided to vary the flame exit area of the burner. The adjusting device includes an adjusting rod connected to an extension rod which preferably extends through the burner ignition chamber to the burner combustion exit port. For example, a tapered plug is attached to the end of the extension rod. The tapered plug is tapered in a direction decreasing toward the burner combustion exit port and can include fins attached around a periphery of the plug.