Inventor

Anthony John Dean

Inventor

Scotia, NY, US

Overview

1997–2020

Patent span

Mechanical engineering

Primary field (CPC F)

Patents· 58 as inventor

Public. Assignee & technology derived from the patent record. Each patent links to its LexDana page.

F23Rprimary

F23RGenerating combustion products of high pressure or high velocity, e.g. gas-turbine combustion chambers25%

F02CGas-turbine plants15%

F02KJet-propulsion plants12%

F23CMethods or apparatus for combustion using fluid fuel or solid fuel suspended in a carrier gas or air8%

F23DBurners8%

Y02TClimate change mitigation technologies related to transportation8%

F05DIndexing scheme for aspects relating to non-positive-displacement machines or engines, gas-turbines or jet-propulsion plants6%

F01DNon-positive displacement machines or engines, e.g. steam turbines4%

G01NInvestigating or analysing materials by determining their chemical or physical properties2%

B08BCleaning in general1%

PatentTitleYear

10,724,741Combustors and methods of assembling the same2020 10,415,833Premixer for gas turbine combustor2019 10,352,567Fuel-air premixer for a gas turbine2019 10,221,763Combustor for rotating detonation engine and method of operating same2019 8,726,630'System and method for passive valving for pulse detonation combustors'2014 8,448,611'Detonation combustor cleaning device and method of cleaning a vessel with a detonation combustor cleaning device'2013 7,987,821'Detonation combustor cleaning device and method of cleaning a vessel with a detonation combustor cleaning device'2011 7,980,056'Methods and apparatus for controlling air flow within a pulse detonation engine'2011 7,966,803'Pulse detonation combustor with folded flow path'2011 7,950,219'Dual mode combustion operation of a pulse detonation combustor in a hybrid engine'2011 7,891,164'Inlet airflow management system for a pulse detonation engine for supersonic applications'2011 7,841,167'Pulse detonation engine bypass and cooling flow with downstream mixing volume'2010 7,836,682'Methods and apparatus for operating a pulse detonation engine'2010 7,828,546'Naturally aspirated fluidic control for diverting strong pressure waves'2010 7,818,956'Pulse detonation assembly and hybrid engine'2010 7,784,287'Pulse detonation firing detuning and frequency modulated firing'2010 7,784,265'Multiple tube pulse detonation engine turbine apparatus and system'2010 7,739,867'Compact, low pressure-drop shock-driven combustor'2010 7,721,523'Ground based pulse detonation combustor for power generation'2010 7,690,191'Fuel preconditioning for detonation combustion'2010 7,669,406'Compact, low pressure-drop shock-driven combustor and rocket booster, pulse detonation based supersonic propulsion system employing the same'2010 7,669,405'Shaped walls for enhancement of deflagration-to-detonation transition'2010 7,634,904'Methods and apparatus to facilitate generating power from a turbine engine'2009 7,614,211'Swirling flows and swirler to enhance pulse detonation engine operation'2009 7,526,912'Pulse detonation engines and components thereof'2009 7,260,935'Method and apparatus for reducing gas turbine engine emissions'2007 7,200,987'Off-axis pulse detonation configuration for gas turbine engine'2007 7,150,143'Hybrid fuel cell-pulse detonation power system'2006 7,131,260'Multiple detonation initiator for frequency multiplied pulsed detonation combustion'2006 7,093,794'Aircraft and detonative engine incorporating pulse detonation engines'2006 7,055,308'Detonation damper for pulse detonation engines'2006 6,983,586'Two-stage pulse detonation system'2006 6,968,693'Method and apparatus for reducing gas turbine engine emissions'2005 6,910,853'Structures for attaching or sealing a space between components having different coefficients or rates of thermal expansion'2005 6,726,448'Ceramic turbine shroud'2004 6,710,878'In-line particulate detector'2004 6,629,674'Method and apparatus for modulating airfoil lift'2003 6,438,959'Combustion cap with integral air diffuser and related method'2002 6,434,926'Combustion chamber for gas turbines'2002 6,363,725'Pre-mixing chamber for gas turbines'2002 6,334,309'Liquid fuel injector for burners in gas turbines'2002 6,315,519'Turbine inner shroud and turbine assembly containing such inner shroud'2001 6,311,471'Steam cooled fuel injector for gas turbine'2001 6,301,899'Mixer having intervane fuel injection'2001 6,272,842'Combustor tuning'2001 6,173,563'Modified bottoming cycle for cooling inlet air to a gas turbine combined cycle plant'2001 6,155,098'Dewpoint sensor'2000 6,123,273'Dual-fuel nozzle for inhibiting carbon deposition onto combustor surfaces in a gas turbine'2000 6,113,349'Turbine assembly containing an inner shroud'2000 6,073,479'Dewpoint sensor'2000 6,070,410'Low emissions combustor premixer'2000 5,899,075'Turbine engine combustor with fuel-air mixer'1999 5,833,141'Anti-coking dual-fuel nozzle for a gas turbine combustor'1998 5,822,992'Low emissions combustor premixer'1998 5,778,676'Dual fuel mixer for gas turbine combustor'1998 5,680,766'Dual fuel mixer for gas turbine combustor'1997 5,675,971'Dual fuel mixer for gas turbine combustor'1997 5,644,918'Dynamics free low emissions gas turbine combustor'1997

Career & activity timeline

Assembled from patent assignee/location history and declaration credentials.

1997–2020Patents assigned to GEN ELECTRIC (55)· patent assignee history

1997–2020Based in Scotia, NY, US· patent location history

2002Patents assigned to NUOVO PIGNONE SPA (2)· patent assignee history

2013–2014Patents assigned to CHAPIN DAVID MICHAEL (2)· patent assignee history

2013–2014Patents assigned to DEAN ANTHONY JOHN (2)· patent assignee history

2013Patents assigned to CREAR DONNELL EUGENE (1)· patent assignee history

Inventor activity

Assignee and location history derived from the patent record.

Assignees

Assignee	Patents	Span
GEN ELECTRIC	55	1997–2020
CHAPIN DAVID MICHAEL	2	2013–2014
DEAN ANTHONY JOHNself	2	2013–2014
NUOVO PIGNONE SPA	2	2002
CREAR DONNELL EUGENE	1	2013

Locations

Location	Patents	Span
Scotia, New York, US	58	1997–2020