Career records & work history
Lawyers & Attorneys
Dennis M O'Dea - Lawyer
Address:
The Sfs Law Group
704-7801544 (Office)
704-7801544 (Office)
Licenses:
Dist. of Columbia - Active 1981
Dennis M O'Dea, 838 Courtney Ln, Somerset, NJ 08873
Dennis O'Dea Phones & Addresses
8 Courtney Ln, Somerset, NJ 08873 732-8731709
11 W Goodrich Ave, Beach Haven, NJ 08008
Long Beach Township, NJ
Silver Spring, MD
East Hanover, NJ
Houston, TX
Cockeysville, MD
Ocean, NJ
Social networks
Dennis M O'Dea
Linkedin
Ranks
Licence:
Dist. of Columbia - Active
Date:
1981
Mentions for Dennis M O'Dea
Dennis O'Dea resumes & CV records
Resumes
Dennis O'dea
Publications & IP owners
Us Patents
Combustor Systems And Methods For Using Same
US Patent:
2012013, May 31, 2012
Filed:
Jun 3, 2010
Appl. No.:
13/376277
Inventors:
Franklin F. Mittricker - Jamul CA, US
Dennis M. O'Dea - Somerset NJ, US
Harry W. Deckman - Clinton NJ, US
Chad C. Rasmussen - Houston TX, US
David R. Noble - Marietta GA, US
Jerry M. Seitzman - Atlanta GA, US
Timothy C. Lieuwen - Atlanta GA, US
Sulabh K. Dhanuka - Houston TX, US
Richard Huntington - Houston TX, US
Dennis M. O'Dea - Somerset NJ, US
Harry W. Deckman - Clinton NJ, US
Chad C. Rasmussen - Houston TX, US
David R. Noble - Marietta GA, US
Jerry M. Seitzman - Atlanta GA, US
Timothy C. Lieuwen - Atlanta GA, US
Sulabh K. Dhanuka - Houston TX, US
Richard Huntington - Houston TX, US
Assignee:
EXXONMOBIL UPSTREAM RESEARCH COMPANY - Houston TX
International Classification:
F02C 3/20
F02C 9/00
F23R 3/10
F02C 3/30
F02C 9/00
F23R 3/10
F02C 3/30
US Classification:
60772, 60 39461, 60737, 60754, 60756, 60748, 60 3923
Abstract:
Systems and methods for an oxy-fuel type combustion reaction are provided. In one or more embodiments, a combustion system can include at least two mixing zones, where a first mixing zone at least partially mixes oxygen and carbon dioxide to produce a first mixture and a second mixing zone at least partially mixes the first mixture with a fuel to produce a second mixture. The combustion system can also include a combustion zone configured to combust the second mixture to produce a combustion product. In one or more embodiments, the first mixture can have a spatially varied ratio of oxygen-to-carbon dioxide configured to generate a hot zone in the combustion zone to increase flame stability in the combustion zone.
Low Emission Power Generation And Hydrocarbon Recovery Systems And Methods
US Patent:
2012014, Jun 14, 2012
Filed:
Jul 9, 2010
Appl. No.:
13/387617
Inventors:
Chad Rasmussen - Houston TX, US
Richard A. Huntington - Houston TX, US
Dennis O'Dea - Somerset NJ, US
Franklin F. Mittricker - Jamul CA, US
Frank Hershkowitz - Basking Ridge NJ, US
Richard A. Huntington - Houston TX, US
Dennis O'Dea - Somerset NJ, US
Franklin F. Mittricker - Jamul CA, US
Frank Hershkowitz - Basking Ridge NJ, US
International Classification:
F02C 1/00
US Classification:
60772, 60 3919
Abstract:
Methods and systems for oxyfuel based low emission power generation in hydrocarbon recovery processes are provided. One system includes a plenum and is configured to encourage post-combustor conversion of gaseous components such that a desired chemical state is achieved. Another system includes a steam reformer for reforming a control fuel stream to generate a reformed control fuel stream characterized by an increase in hydrogen, as compared to the control fuel stream.
Systems And Methods For Exhaust Gas Extraction
US Patent:
2013012, May 23, 2013
Filed:
Jun 27, 2011
Appl. No.:
13/704925
Inventors:
Franklin F. Mittricker - Jamul CA, US
Richard A. Huntington - Houston TX, US
Dennis M. O'Dea - Somerset NJ, US
Richard A. Huntington - Houston TX, US
Dennis M. O'Dea - Somerset NJ, US
International Classification:
F02C 3/34
US Classification:
60772, 60 3952
Abstract:
The present techniques are directed to a combustor for a gas turbine. For example, an embodiment provides a spool piece for the combustor. The spool piece includes an oxidant injection port configured for injection of an oxidant proximate to a flame in the combustor and a recycle-gas extraction port configured for an extraction of a recycle gas from the combustor, wherein the recycle gas is isolated from the oxidant prior to the use of the oxidant in a flame.
Systems And Methods For Carbon Dioxide Capture In Low Emission Turbine Systems
US Patent:
2014000, Jan 9, 2014
Filed:
Mar 5, 2012
Appl. No.:
14/005174
Inventors:
Richard A. Huntington - Houston TX, US
Franklin F. Mittricker - Jamul CA, US
Omer Angus Sites - Spring TX, US
Sulabh K. Dhanuka - Houston TX, US
Dennis M. O'Dea - Somerset NJ, US
Russell H. Oelfke - Houston TX, US
Robert D. Denton - Bellaire TX, US
Franklin F. Mittricker - Jamul CA, US
Omer Angus Sites - Spring TX, US
Sulabh K. Dhanuka - Houston TX, US
Dennis M. O'Dea - Somerset NJ, US
Russell H. Oelfke - Houston TX, US
Robert D. Denton - Bellaire TX, US
International Classification:
F02C 3/00
US Classification:
60801
Abstract:
Systems, methods, and apparatus are provided for generating power in low emission turbine systems and capturing and recovering carbon dioxide from the exhaust. In one or more embodiments, the exhaust is cooled, compressed, and separated to yield a carbon dioxide-containing effluent stream and a nitrogen-containing product stream.
Systems And Methods For Carbon Dioxide Captrue And Power Generation In Low Emission Turbine Systems
US Patent:
2014001, Jan 16, 2014
Filed:
Mar 5, 2012
Appl. No.:
14/002625
Inventors:
Franklin F. Mittricker - Jamul CA, US
Sulabh K. Dhanuka - Houston TX, US
Richard A. Huntington - Houston TX, US
Omar Angus Sites - Spring TX, US
Dennis M. O'Dea - Somerset NJ, US
Russell H. Oelfke - Houston TX, US
Sulabh K. Dhanuka - Houston TX, US
Richard A. Huntington - Houston TX, US
Omar Angus Sites - Spring TX, US
Dennis M. O'Dea - Somerset NJ, US
Russell H. Oelfke - Houston TX, US
International Classification:
F02C 7/00
US Classification:
60783, 60784
Abstract:
Systems, methods, and apparatus are provided for generating power in low emission turbine systems and separating the exhaust into rich COand lean COstreams. In one or more embodiments, the exhaust is separated at an elevated pressure, such as between a high-pressure expansion stage and a low-pressure expansion stage.
System And Method For Oxidant Compression In A Stoichiometric Exhaust Gas Recirculation Gas Turbine System
US Patent:
2017018, Jun 29, 2017
Filed:
Mar 13, 2017
Appl. No.:
15/456957
Inventors:
- Schenectady NY, US
- Spring TX, US
Loren K. Starcher - Sugar Land TX, US
Sulabh K. Dhanuka - Houston TX, US
Dennis M. O'Dea - Somerset NJ, US
Samuel D. Draper - Simpsonville SC, US
Christian M. Hansen - Greenville SC, US
Todd Denman - Greenville SC, US
James A. West - Liberty Township OH, US
- Spring TX, US
Loren K. Starcher - Sugar Land TX, US
Sulabh K. Dhanuka - Houston TX, US
Dennis M. O'Dea - Somerset NJ, US
Samuel D. Draper - Simpsonville SC, US
Christian M. Hansen - Greenville SC, US
Todd Denman - Greenville SC, US
James A. West - Liberty Township OH, US
International Classification:
F02C 3/34
F02C 6/18
B01D 53/26
F02C 9/50
F01D 15/10
F01D 15/12
F01K 7/16
F01K 23/10
F02C 3/04
B01D 53/94
F02C 6/18
B01D 53/26
F02C 9/50
F01D 15/10
F01D 15/12
F01K 7/16
F01K 23/10
F02C 3/04
B01D 53/94
Abstract:
A system includes a gas turbine system having a turbine combustor, a turbine driven by combustion products from the turbine combustor, and an exhaust gas compressor driven by the turbine. The exhaust gas compressor is configured to compress and supply an exhaust gas to the turbine combustor. The gas turbine system also has an exhaust gas recirculation (EGR) system. The EGR system is configured to recirculate the exhaust gas along an exhaust recirculation path from the turbine to the exhaust gas compressor. The system further includes a main oxidant compression system having one or more oxidant compressors. The one or more oxidant compressors are separate from the exhaust gas compressor, and the one or more oxidant compressors are configured to supply all compressed oxidant utilized by the turbine combustor in generating the combustion products.
Systems And Methods For Carbon Dioxide Capture And Power Generation In Low Emission Turbine Systems
US Patent:
2017005, Mar 2, 2017
Filed:
Nov 15, 2016
Appl. No.:
15/351918
Inventors:
Franklin F. Mittricker - Jamul CA, US
Sulabh K. Dhanuka - Houston TX, US
Richard A. Huntington - Spring TX, US
Omar Angus Sites - Spring TX, US
Dennis M. O'Dea - Somerset NJ, US
Russell H. Oelfke - Houston TX, US
Sulabh K. Dhanuka - Houston TX, US
Richard A. Huntington - Spring TX, US
Omar Angus Sites - Spring TX, US
Dennis M. O'Dea - Somerset NJ, US
Russell H. Oelfke - Houston TX, US
International Classification:
F01N 3/08
F02C 3/34
H02K 7/18
F01N 5/02
F02C 3/34
H02K 7/18
F01N 5/02
Abstract:
Systems, methods, and apparatus are provided for generating power in low emission turbine systems and separating the exhaust into rich COand lean COstreams. In one or more embodiments, the exhaust is separated at an elevated pressure, such as between a high-pressure expansion stage and a low-pressure expansion stage.
System And Method For Oxidant Compression In A Stoichiometric Exhaust Gas Recirculation Gas Turbine System
US Patent:
2014012, May 8, 2014
Filed:
Oct 29, 2013
Appl. No.:
14/066579
Inventors:
- Houston TX, US
- Schenectady NY, US
Loren K. Starcher - Sugar Land TX, US
Sulabh K. Dhanuka - Houston TX, US
Dennis M. O'Dea - Somerset NJ, US
Samuel D. Draper - Simpsonville SC, US
Christian M. Hansen - Greenville SC, US
Todd Denman - Greenville SC, US
James A. West - Liberty Township OH, US
- Schenectady NY, US
Loren K. Starcher - Sugar Land TX, US
Sulabh K. Dhanuka - Houston TX, US
Dennis M. O'Dea - Somerset NJ, US
Samuel D. Draper - Simpsonville SC, US
Christian M. Hansen - Greenville SC, US
Todd Denman - Greenville SC, US
James A. West - Liberty Township OH, US
Assignee:
ExxonMobil Upstream Research Company - Houston TX
General Electric Company - Schenectady NY
General Electric Company - Schenectady NY
International Classification:
F02M 25/07
US Classification:
60 3952
Abstract:
A system includes a gas turbine system having a turbine combustor, a turbine driven by combustion products from the turbine combustor, and an exhaust gas compressor driven by the turbine. The exhaust gas compressor is configured to compress and supply an exhaust gas to the turbine combustor. The gas turbine system also has an exhaust gas recirculation (EGR) system. The EGR system is configured to recirculate the exhaust gas along an exhaust recirculation path from the turbine to the exhaust gas compressor. The system further includes a main oxidant compression system having one or more oxidant compressors. The one or more oxidant compressors are separate from the exhaust gas compressor, and the one or more oxidant compressors are configured to supply all compressed oxidant utilized by the turbine combustor in generating the combustion products.
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