An atomizing injector includes a metering set having a swirl chamber, a spray orifice and one or more feed slots etched in a thin plate. The swirl chamber is etched in a first side of the plate and the spray orifice is etched through a second side to the center of the swirl chamber. Fuel feed slots extend non-radially to the swirl chamber. The injector also includes integral swirler structure. The swirler structure includes a cylindrical air swirler passage, also shaped by etching, through at least one other thin plate. The cylindrical air swirler passage is located in co-axial relation to the spray orifice of the plate of the fuel metering set such that fuel directed through the spray orifice passes through the air swirler passage and swirling air is imparted to the fuel such that the fuel has a swirling component of motion. At least one air feed slot is provided in fluid communication with the air swirler passage and extends in non-radial relation thereto. Air supply passages extend through the plates of the metering set and the swirler structure to feed the air feed slot in each plate of the swirler structure.
Integrated Fuel Injection And Mixing System With Impingement Cooling Face
Adel B. Mansour - Mentor OH 44060 Rex J. Harvey - Mentor OH 44060 Robert R. Tacina - Brunswick OH 44212 Peter Laing - Geneva OH 44041
International Classification:
B05B 710
US Classification:
239399, 239402, 239403, 239404
Abstract:
An atomizing injector includes a metering set having a swirl chamber, a spray orifice and one or more feed slots etched in a thin plate. The swirl chamber is etched in a first side of the plate and the spray orifice is etched through a second side to the center of the swirl chamber. Fuel feed slots extend non-radially to the swirl chamber. The injector also includes integral swirler structure. The swirler structure includes a cylindrical air swirler passage, also shaped by etching, through at least one other thin plate. The cylindrical air swirler passage is located in co-axial relation to the spray orifice of the plate of the fuel metering set such that fuel directed through the spray orifice passes through the air swirler passage and swirling air is imparted to the fuel such that the fuel has a swirling component of motion. At least one air feed slot is provided in fluid communication with the air swirler passage and extends in non-radial relation thereto. Air supply passages extend through the plates of the metering set and the swirler structure to feed the air feed slot in each plate of the swirler structure.
Michael P. Wrubel - Westlake OH Rex J. Harvey - Mentor OH Peter Laing - Geneva OH Robert T. Mains - Euclid OH Barry W. Savel - Andover OH Alfred A. Mancini - Cincinnati OH James Neil Cooper - Hamilton OH
Assignee:
Parker-Hannifin Corporation - Cleveland OH
International Classification:
F02G 100
US Classification:
60740, 60 39281, 60742, 60746, 60772
Abstract:
A fuel injector nozzle for dispensing fuel in the combustion chamber of a gas turbine engine, includes an elongated, multi-layered, convoluted nozzle feed strip having an internal passage for directing fuel through the length of the strip from the inlet end to an outlet end; and a cylindrical, multi-layered fuel dispensing nozzle unitary with the feed strip and fluidly connected to the outlet end of the feed strip for dispensing the fuel. The multi-layered feed strip and nozzle allows complex porting of fuel circuits through the injector. The internal fluid passages through the feed strip and nozzle are formed by etching.
Fuel Manifold Block And Ring With Macrolaminate Layers
Peter Laing - Willow Park TX Dale L. Arnold - Concord Township OH Charles R. Bovard - Austinburg OH Jeffrey R. Lehtinen - Concord Township OH
Assignee:
Parker-Hannifin Corporation - Cleveland OH
International Classification:
F02C 100
US Classification:
60740, 60739
Abstract:
A fuel injector assembly for dispensing fuel in the combustion chamber of a gas turbine engine, includes in one embodiment an elongated, multi-layered, convoluted nozzle feed strip having an internal passage for directing fuel through the length of the strip from the inlet end to an outlet end; and a cylindrical, multi-layered fuel dispensing nozzle unitary with the feed strip and fluidly connected to the outlet end of the feed strip for dispensing the fuel. The multi-layered feed strip and nozzle allow complex porting of fuel circuits through the injector. The internal fluid passages through the feed strip and nozzle are formed by etching. In another embodiment, the feed strip can be used for directing fuel from the manifold to one or more fuel injectors.
Peter Laing - Willow Park TX Michael Peter Wrubel - Westlake OH Barry Walford Savel - Summerville SC Rex Jay Harvey - Mentor OH Alfred Albert Mancini - Cincinnati OH James Neil Cooper - Hamilton OH Robert Thane Mains - Euclid OH
Assignee:
General Electric Company - Schenectady NY
International Classification:
F02C 100
US Classification:
60740, 60742, 60747, 239548
Abstract:
A gas turbine engine fuel injector conduit includes a single feed strip having a single bonded together pair of lengthwise extending plates. Each of the plates has a single row of widthwise spaced apart and lengthwise extending parallel grooves. Opposing grooves in each of the plates are aligned forming internal fuel flow passages through the strip from an inlet end to an outlet end. The feed strip includes a substantially straight middle portion between the inlet end and the outlet end. In one alternative, the middle portion has a radius of curvature greater than a length of the middle portion. The feed strip has at least one acute bend between the inlet end and the middle portion and a bend between the outlet end and the middle portion. The feed strip has fuel inlet holes in the inlet end connected to the internal fuel flow passages.
Adel B. Mansour - Mentor OH, US Rex J. Harvey - Mentor OH, US Peter Laing - Willow Park TX, US
Assignee:
Parker-Hannifin Corporation - Cleveland OH
International Classification:
B05B 7/10 B05B 1/30 B05B 1/00
US Classification:
239399, 239403, 239404, 23953314, 239596
Abstract:
An atomizing injector includes a metering set having a swirl chamber, a spray orifice and one or more feed slots etched in a thin plate. The swirl chamber is etched in a first side of the plate and the spray orifice is etched through a second side to the center of the swirl chamber. Fuel feed slots extend non-radially to the swirl chamber. The injector also includes integral swirler structure. The swirler structure includes a cylindrical air swirler passage, also shaped by etching, through at least one other thin plate. The cylindrical air swirler passage is located in co-axial relation to the spray orifice of the plate of the fuel metering set such that fuel directed through the spray orifice passes through the air swirler passage and swirling air is imparted to the fuel such that the fuel has a swirling component of motion. At least one air feed slot is provided in fluid communication with the air swirler passage and extends in non-radial relation thereto. Air supply passages extend through the plates of the metering set and the swirler structure to feed the air feed slot in each plate of the swirler structure.
Michael Wrubel - Westlake OH, US Rex Harvey - Mentor OH, US Peter Laing - Geneva OH, US Robert Mains - Euclid OH, US Barry Savel - Andover OH, US
International Classification:
F02C007/22
US Classification:
060/740000, 060/746000
Abstract:
A fuel injector nozzle for dispensing fuel in the combustion chamber of a gas turbine engine, includes an elongated, multi-layered, convoluted nozzle feed strip having an internal passage for directing fuel through the length of the strip from the inlet end to an outlet end; and a cylindrical, multi-layered fuel dispensing nozzle unitary with the feed strip and fluidly connected to the outlet end of the feed strip for dispensing the fuel. The multi-layered feed strip and nozzle allows complex porting of fuel circuits through the injector. The internal fluid passages through the feed strip and nozzle are formed by etching.
Michael P. Wrubel - Westlake OH Rex J. Harvey - Mentor OH Peter Laing - Geneva OH Robert T. Mains - Euclid OH Barry W. Savel - Andover OH
Assignee:
Parker-Hannifin Corporation - Cleveland OH
International Classification:
F02G 100
US Classification:
60740
Abstract:
A fuel injector nozzle for dispensing fuel in the combustion chamber of a gas turbine engine, includes an elongated, multi-layered, convoluted nozzle feed strip having an internal passage for directing fuel through the length of the strip from the inlet end to an outlet end; and a cylindrical, multi-layered fuel dispensing nozzle unitary with the feed strip and fluidly connected to the outlet end of the feed strip for dispensing the fuel. The multi-layered feed strip and nozzle allows complex porting of fuel circuits through the injector. The internal fluid passages through the feed strip and nozzle are formed by etching.
Raytheon
Senior Principal Mechanical Engineer
Lockheed Martin Feb 2002 - Jan 2018
Systems Engineer, Senior Staff
Parker Hannifin Oct 1, 1997 - Feb 1, 2002
Senior Design Engineer
Ge Jan 1, 1994 - Oct 1, 1997
Project Engineer
Education:
Purdue University 1991 - 1993
Master of Science, Masters
University of the Witwatersrand 1988 - 1990
Bachelors, Bachelor of Science, Engineering
University of Kwazulu - Natal 1987 - 1987
Bachelors, Bachelor of Science, Mechanical Engineering
Durban High School 1982 - 1986
Skills:
Aircraft Propulsion Aerospace Systems Engineering Testing Cfd Engineering Aerospace Engineering Earned Value Management Finite Element Analysis Aerodynamics Flight Test Dod Aircraft Design Analysis Catia Manufacturing Gas Turbine Combustion Gas Turbine Fuel Injection Propulsion Integration Low Nox Combstor Fuel Injection
Languages:
English Afrikaans
Certifications:
Faa Private Pilot License, Sel Instrument Rating, Sel Federal Aviation Administration - Faa
Berala public, Birrong boys high, Granville Tech - Chemistry
About:
Retired..well trying to. Live at Dunbogan, like fishing,paragliding,motorbike riding,bowls,guitar and spending time with family and friends ...not necessarily in that order.
Bragging Rights:
Have 3 great kids,2 beautiful grandchildren and a wonderful wife.
Peter Laing
Work:
L Mawby - Operations Manager (11)
Education:
University of Michigan - Industrial & Operations Engineering