Inventor

Christopher Charles Glynn

Inventor

Hamilton, OH, US

Overview

1992–2021

Patent span

Mechanical engineering

Primary field (CPC F)

Patents· 78 as inventor

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

F01Dprimary

F01DNon-positive displacement machines or engines, e.g. steam turbines27%

Y02TClimate change mitigation technologies related to transportation13%

F05DIndexing scheme for aspects relating to non-positive-displacement machines or engines, gas-turbines or jet-propulsion plants13%

F02CGas-turbine plants11%

F04DNon-positive-displacement pumps4%

F23RGenerating combustion products of high pressure or high velocity, e.g. gas-turbine combustion chambers4%

F02KJet-propulsion plants3%

F16JPistons3%

Y10STechnical subjects covered by former uspc cross-reference art collections [xracs] and digests3%

F05BIndexing scheme relating to wind, spring, weight, inertia or like motors, to machines or engines for liquids covered by subclasses f03b, f03d and f03g2%

PatentTitleYear

11,098,592Turbomachine with alternatingly spaced turbine rotor blades2021 11,092,023Ceramic matrix composite nozzle mounted with a strut and concepts thereof2021 D0907732Curved ski2021 10,823,000Turbomachine with alternatingly spaced turbine rotor blades2020 10,823,001Turbomachine with alternatingly spaced turbine rotor blades2020 10,781,717Turbomachine with alternatingly spaced turbine rotor blades2020 10,738,617Turbomachine with alternatingly spaced turbine rotor blades2020 10,704,425Assembly for a gas turbine engine2020 10,508,546Turbomachine with alternatingly spaced turbine rotor blades2019 10,480,322Turbine engine with annular cavity2019 10,428,692Turbine center frame fairing assembly2019 10,415,897Monolithic tube-in matrix heat exchanger2019 10,227,928Engine architecture with reverse rotation integral drive and vaneless turbine2019 9,915,159'Ceramic matrix composite nozzle mounted with a strut and concepts thereof'2018 8,876,042'Integrated nacelle assembly'2014 8,726,787'Rotary hydraulic actuator with hydraulically controlled position limits'2014 8,371,105'Hydraulic system for fan pitch change actuation of counter-rotating propellers'2013 8,336,290'Pitch change apparatus for counter-rotating propellers'2012 7,788,927'Turbine engine fuel nozzles and methods of assembling the same'2010 7,514,810'Electric power generation using power turbine aft of LPT'2009 7,367,776'Turbine engine stator including shape memory alloy and clearance control method'2008 7,363,762'Gas turbine engines seal assembly and methods of assembling the same'2008 7,341,429'Methods and apparatuses for cooling gas turbine engine rotor assemblies'2008 7,269,955'Methods and apparatus for maintaining rotor assembly tip clearances'2007 7,048,496'Turbine cooling, purge, and sealing system'2006 7,018,168'Method and apparatus for fabricating gas turbine engines'2006 6,920,762'Mounting assembly for igniter in a gas turbine engine combustor having a ceramic matrix composite liner'2005 6,904,757'Mounting assembly for the forward end of a ceramic matrix composite liner in a gas turbine engine combustor'2005 6,895,757'Sealing assembly for the aft end of a ceramic matrix composite liner in a gas turbine engine combustor'2005 6,895,761'Mounting assembly for the aft end of a ceramic matrix composite liner in a gas turbine engine combustor'2005 6,884,026'Turbine engine shroud assembly including axially floating shroud segment'2005 6,775,985'Support assembly for a gas turbine engine combustor'2004 6,719,296'Seal for a rotating member'2004 6,702,550'Turbine shroud segment and shroud assembly'2004 6,676,369'Aspirating face seal with axially extending seal teeth'2004 6,666,017'Counterrotatable booster compressor assembly for a gas turbine engine'2003 6,540,477'Turbine cooling circuit'2003 6,491,497'Method and apparatus for supporting rotor assemblies during unbalances'2002 6,464,461'Steam cooling system for a gas turbine'2002 6,402,469'Fan decoupling fuse'2002 6,398,500'Retention system and method for the blades of a rotary machine'2002 6,398,487'Methods and apparatus for supplying cooling airflow in turbine engines'2002 6,357,237'Fuel injection assembly for gas turbine engine combustor'2002 6,298,667'Modular combustor dome'2001 6,268,668'Gas cooled generator stator structure and method for impingement cooling of generator stator coil'2001 6,240,719'Fan decoupler system for a gas turbine engine'2001 6,206,638'Low cost airfoil cooling circuit with sidewall impingement cooling chambers'2001 5,971,706'Inter-rotor bearing assembly'1999 5,853,285'Cooling air tube vibration damper'1998 5,725,355'Adhesive bonded fan blade'1998 5,713,721'Retention system for the blades of a rotary machine'1998 5,685,158'Compressor rotor cooling system for a gas turbine'1997 5,568,931'Brush seal'1996 5,486,086'Blade containment system'1996 5,431,532'Blade containment system'1995 5,357,744'Segmented turbine flowpath assembly'1994 5,335,920'Brush seal'1994 5,333,993'Stator seal assembly providing improved clearance control'1994 5,320,486'Apparatus for positioning compressor liner segments'1994 5,320,484'Turbomachine stator having a double skin casing including means for preventing gas flow longitudinally therethrough'1994 5,320,487'Spring clip made of a directionally solidified material for use in a gas turbine engine'1994 5,318,309'Brush seal'1994 5,292,138'Rotor to rotor split ring seal'1994 5,292,227'Turbine frame'1994 5,281,098'Single ring blade retaining assembly'1994 5,263,312'Tube fitting for a gas turbine engine'1993 5,257,909'Dovetail sealing device for axial dovetail rotor blades'1993 5,236,302'Turbine disk interstage seal system'1993 5,232,337'Slip joint for maintaining concentricity'1993 5,226,784'Blade damper'1993 5,211,407'Compressor rotor cross shank leak seal for axial dovetails'1993 5,211,533'Flow diverter for turbomachinery seals'1993 5,205,713'Fan blade damper'1993 5,197,857'Multiple rotor disk assembly'1993 5,167,734'Process for identification evaluation and removal of microshrinkage'1992 5,160,241'Multi-port air channeling assembly'1992 5,143,383'Stepped tooth rotating labyrinth seal'1992 5,131,814'Turbine blade inner end attachment structure'1992

Career & activity timeline

Assembled from patent assignee/location history and declaration credentials.

1992–2021Patents assigned to GEN ELECTRIC (76)· patent assignee history

1992–2010Based in Hamilton, OH, US· patent location history

2012–2014Patents assigned to GLYNN CHRISTOPHER CHARLES (4)· patent assignee history

2012–2014Patents assigned to DINSMORE NICHOLAS ROWE (3)· patent assignee history

2012–2014Patents assigned to MILLER BRANDON WAYNE (3)· patent assignee history

2012–2013Patents assigned to MENARD JEFFREY RAYMOND (2)· patent assignee history

2012–2021Based in Lawrenceburg, IN, US· patent location history

2019–2020Based in Clearwater Beach, FL, US· patent location history

2021Based in Clearwater, FL, US· patent location history

2021Based in Blue River, CO, US· patent location history

Inventor activity

Assignee and location history derived from the patent record.

Assignees

Assignee	Patents	Span
GEN ELECTRIC	76	1992–2021
GLYNN CHRISTOPHER CHARLESself	4	2012–2014
DINSMORE NICHOLAS ROWE	3	2012–2014
MILLER BRANDON WAYNE	3	2012–2014
MENARD JEFFREY RAYMOND	2	2012–2013

Locations

Location	Patents	Span
Hamilton, OH, US	60	1992–2010
Lawrenceburg, IN, US	9	2012–2021
Clearwater Beach, Florida, US	6	2019–2020
Clearwater, Florida, US	1	2021
Blue River, CO, US	1	2021