
Marc J. Amar
Examiner (ID: 17142, Phone: (571)272-9948 , Office: P/3741 )
| Most Active Art Unit | 3741 |
| Art Unit(s) | 3741 |
| Total Applications | 488 |
| Issued Applications | 346 |
| Pending Applications | 52 |
| Abandoned Applications | 95 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 8505211
[patent_doc_number] => 20120304619
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-12-06
[patent_title] => 'ENGINE FOR THRUST OR SHAFT OUTPUT AND CORRESPONDING OPERATING METHOD'
[patent_app_type] => utility
[patent_app_number] => 13/579448
[patent_app_country] => US
[patent_app_date] => 2010-11-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 3377
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13579448
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/579448 | ENGINE FOR THRUST OR SHAFT OUTPUT AND CORRESPONDING OPERATING METHOD | Nov 18, 2010 | Abandoned |
Array
(
[id] => 10026617
[patent_doc_number] => 09068509
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-06-30
[patent_title] => 'Gas turbine engine fuel control thrust control override system'
[patent_app_type] => utility
[patent_app_number] => 12/947411
[patent_app_country] => US
[patent_app_date] => 2010-11-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 4653
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 343
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12947411
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/947411 | Gas turbine engine fuel control thrust control override system | Nov 15, 2010 | Issued |
Array
(
[id] => 5994018
[patent_doc_number] => 20110113748
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-05-19
[patent_title] => 'GUIDING AN IGNITION SPARK PLUG IN A TURBOMACHINE COMBUSTION CHAMBER'
[patent_app_type] => utility
[patent_app_number] => 12/946253
[patent_app_country] => US
[patent_app_date] => 2010-11-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 2147
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0113/20110113748.pdf
[firstpage_image] =>[orig_patent_app_number] => 12946253
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/946253 | GUIDING AN IGNITION SPARK PLUG IN A TURBOMACHINE COMBUSTION CHAMBER | Nov 14, 2010 | Abandoned |
Array
(
[id] => 6181593
[patent_doc_number] => 20110167829
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-07-14
[patent_title] => 'FUEL CONTROL ARRANGEMENTS'
[patent_app_type] => utility
[patent_app_number] => 12/945149
[patent_app_country] => US
[patent_app_date] => 2010-11-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2692
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0167/20110167829.pdf
[firstpage_image] =>[orig_patent_app_number] => 12945149
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/945149 | FUEL CONTROL ARRANGEMENTS | Nov 11, 2010 | Abandoned |
Array
(
[id] => 10130010
[patent_doc_number] => 09163838
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-10-20
[patent_title] => 'Gas turbine combustion burner'
[patent_app_type] => utility
[patent_app_number] => 13/395763
[patent_app_country] => US
[patent_app_date] => 2010-11-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 12
[patent_no_of_words] => 3664
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 129
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13395763
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/395763 | Gas turbine combustion burner | Nov 7, 2010 | Issued |
Array
(
[id] => 6081126
[patent_doc_number] => 20110214428
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-09-08
[patent_title] => 'HYBRID VENTURI COOLING SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 12/917784
[patent_app_country] => US
[patent_app_date] => 2010-11-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 1771
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0214/20110214428.pdf
[firstpage_image] =>[orig_patent_app_number] => 12917784
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/917784 | HYBRID VENTURI COOLING SYSTEM | Nov 1, 2010 | Abandoned |
Array
(
[id] => 8175462
[patent_doc_number] => 20120109593
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-05-03
[patent_title] => 'GAS TURBINE ENGINE WITH VARIABLE AREA FAN NOZZLE'
[patent_app_type] => utility
[patent_app_number] => 12/915208
[patent_app_country] => US
[patent_app_date] => 2010-10-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 3087
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0109/20120109593.pdf
[firstpage_image] =>[orig_patent_app_number] => 12915208
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/915208 | Gas turbine engine with variable area fan nozzle | Oct 28, 2010 | Issued |
Array
(
[id] => 9981660
[patent_doc_number] => 09027355
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-05-12
[patent_title] => 'Mechanical drive device for driving the high pressure sub assembly of an airplane engine'
[patent_app_type] => utility
[patent_app_number] => 12/913409
[patent_app_country] => US
[patent_app_date] => 2010-10-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 6
[patent_no_of_words] => 2196
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 93
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12913409
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/913409 | Mechanical drive device for driving the high pressure sub assembly of an airplane engine | Oct 26, 2010 | Issued |
Array
(
[id] => 8131605
[patent_doc_number] => 20120090352
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-04-19
[patent_title] => 'Methods And Apparatus For An Oxy-Fuel Based Power Cycle'
[patent_app_type] => utility
[patent_app_number] => 12/903979
[patent_app_country] => US
[patent_app_date] => 2010-10-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 3883
[patent_no_of_claims] => 32
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0090/20120090352.pdf
[firstpage_image] =>[orig_patent_app_number] => 12903979
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/903979 | Methods and apparatus for an oxy-fuel based power cycle | Oct 12, 2010 | Issued |
Array
(
[id] => 6542445
[patent_doc_number] => 20100287940
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-11-18
[patent_title] => 'Burner of a gas turbine'
[patent_app_type] => utility
[patent_app_number] => 12/720192
[patent_app_country] => US
[patent_app_date] => 2010-03-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2327
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0287/20100287940.pdf
[firstpage_image] =>[orig_patent_app_number] => 12720192
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/720192 | Burner of a gas turbine | Mar 8, 2010 | Issued |
Array
(
[id] => 6368911
[patent_doc_number] => 20100300063
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-12-02
[patent_title] => 'Apparatus and Method for Combusting a Fuel at High Pressure and High Temperature, and Associated System and Device'
[patent_app_type] => utility
[patent_app_number] => 12/714074
[patent_app_country] => US
[patent_app_date] => 2010-02-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 12755
[patent_no_of_claims] => 58
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0300/20100300063.pdf
[firstpage_image] =>[orig_patent_app_number] => 12714074
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/714074 | Apparatus and method for combusting a fuel at high pressure and high temperature, and associated system and device | Feb 25, 2010 | Issued |
Array
(
[id] => 10156574
[patent_doc_number] => 09188339
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-11-17
[patent_title] => 'Swirler for mixing fuel and air'
[patent_app_type] => utility
[patent_app_number] => 13/057190
[patent_app_country] => US
[patent_app_date] => 2009-06-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 4
[patent_no_of_words] => 2944
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 110
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13057190
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/057190 | Swirler for mixing fuel and air | Jun 23, 2009 | Issued |
Array
(
[id] => 5977926
[patent_doc_number] => 20110094237
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-04-28
[patent_title] => 'THERMAL POWER PLANT WITH CO2 SEQUESTRATION'
[patent_app_type] => utility
[patent_app_number] => 12/919775
[patent_app_country] => US
[patent_app_date] => 2009-02-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 4284
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0094/20110094237.pdf
[firstpage_image] =>[orig_patent_app_number] => 12919775
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/919775 | THERMAL POWER PLANT WITH CO2 SEQUESTRATION | Feb 25, 2009 | Abandoned |
Array
(
[id] => 11888871
[patent_doc_number] => 09759424
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2017-09-12
[patent_title] => 'Systems and methods involving reduced thermo-acoustic coupling of gas turbine engine augmentors'
[patent_app_type] => utility
[patent_app_number] => 12/260436
[patent_app_country] => US
[patent_app_date] => 2008-10-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 4
[patent_no_of_words] => 3241
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 188
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12260436
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/260436 | Systems and methods involving reduced thermo-acoustic coupling of gas turbine engine augmentors | Oct 28, 2008 | Issued |
Array
(
[id] => 6252739
[patent_doc_number] => 20100293959
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-11-25
[patent_title] => 'Method for Operating a Gas Turbine Engine, Power Supplying Device for Conducting such Method and Aircraft using such Method'
[patent_app_type] => utility
[patent_app_number] => 12/679821
[patent_app_country] => US
[patent_app_date] => 2008-09-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 7364
[patent_no_of_claims] => 41
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0293/20100293959.pdf
[firstpage_image] =>[orig_patent_app_number] => 12679821
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/679821 | Method for operating a gas turbine engine, power supplying device for conducting such method and aircraft using such method | Sep 23, 2008 | Issued |
Array
(
[id] => 6143298
[patent_doc_number] => 20110016846
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-01-27
[patent_title] => 'METHOD AND SYSTEM FOR CONTROLLING AT LEAST ONE ACTUATOR OF THE COWLINGS OF A TURBOJET ENGINE THRUST INVERTER'
[patent_app_type] => utility
[patent_app_number] => 12/673778
[patent_app_country] => US
[patent_app_date] => 2008-07-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2712
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0016/20110016846.pdf
[firstpage_image] =>[orig_patent_app_number] => 12673778
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/673778 | Method and system for controlling at least one actuator of the cowlings of a turbojet engine thrust inverter | Jul 6, 2008 | Issued |
Array
(
[id] => 11371740
[patent_doc_number] => 09541028
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2017-01-10
[patent_title] => 'Managing low pressure turbine maximum speed in a turbofan engine'
[patent_app_type] => utility
[patent_app_number] => 12/442128
[patent_app_country] => US
[patent_app_date] => 2006-10-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2100
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 131
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12442128
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/442128 | Managing low pressure turbine maximum speed in a turbofan engine | Oct 11, 2006 | Issued |