
Frederick C. Nicolas
Examiner (ID: 17365, Phone: (571)272-4931 , Office: P/3754 )
| Most Active Art Unit | 3754 |
| Art Unit(s) | 3754 |
| Total Applications | 2465 |
| Issued Applications | 1847 |
| Pending Applications | 211 |
| Abandoned Applications | 435 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 9379595
[patent_doc_number] => 20140083076
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-03-27
[patent_title] => 'Gas Turbine Engine With Geared Turbofan and Oil Thermal Management System'
[patent_app_type] => utility
[patent_app_number] => 13/794976
[patent_app_country] => US
[patent_app_date] => 2013-03-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 3473
[patent_no_of_claims] => 27
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[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13794976
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/794976 | Gas turbine engine with geared turbofan and oil thermal management system | Mar 11, 2013 | Issued |
Array
(
[id] => 9756054
[patent_doc_number] => 20140286754
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-09-25
[patent_title] => 'Elongated Geared Turbofan With High Bypass Ratio'
[patent_app_type] => utility
[patent_app_number] => 13/792303
[patent_app_country] => US
[patent_app_date] => 2013-03-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_no_of_words] => 3485
[patent_no_of_claims] => 20
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13792303
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/792303 | Exhaust nozzle for an elongated gear turbofan with high bypass ratio | Mar 10, 2013 | Issued |
Array
(
[id] => 13257835
[patent_doc_number] => 10141617
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2018-11-27
[patent_title] => Gas turbine-heated high-temperature battery
[patent_app_type] => utility
[patent_app_number] => 14/380712
[patent_app_country] => US
[patent_app_date] => 2013-03-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
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[patent_no_of_words] => 4783
[patent_no_of_claims] => 14
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[patent_words_short_claim] => 231
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14380712
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/380712 | Gas turbine-heated high-temperature battery | Mar 5, 2013 | Issued |
Array
(
[id] => 9379627
[patent_doc_number] => 20140083108
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-03-27
[patent_title] => 'METHOD FOR CONTROLLING COOLING SYSTEM OF GAS TURBINE, CONTROL DEVICE PERFORMING THE SAME, AND GAS TURBINE PLANT COMPRISING THE CONTROL DEVICE'
[patent_app_type] => utility
[patent_app_number] => 13/774409
[patent_app_country] => US
[patent_app_date] => 2013-02-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 9784
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 2
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[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13774409
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/774409 | Method for controlling cooling system of gas turbine, control device performing the same, and gas turbine plant comprising the control device | Feb 21, 2013 | Issued |
Array
(
[id] => 10367723
[patent_doc_number] => 20150252728
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-09-10
[patent_title] => 'GAS TURBINE ENGINE HAVING SUPPORT STRUCTURE WITH SWEPT LEADING EDGE'
[patent_app_type] => utility
[patent_app_number] => 14/430798
[patent_app_country] => US
[patent_app_date] => 2013-02-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[patent_no_of_claims] => 17
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14430798
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/430798 | Gas turbine engine having support structure with swept leading edge | Feb 12, 2013 | Issued |
Array
(
[id] => 9333223
[patent_doc_number] => 20140060005
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-03-06
[patent_title] => 'MAGNETIC ADVANCED GENERATION JET ELECTRIC TURBINE'
[patent_app_type] => utility
[patent_app_number] => 13/756140
[patent_app_country] => US
[patent_app_date] => 2013-01-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 28
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[patent_no_of_words] => 17539
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13756140
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/756140 | MAGNETIC ADVANCED GENERATION JET ELECTRIC TURBINE | Jan 30, 2013 | Abandoned |
Array
(
[id] => 8837703
[patent_doc_number] => 20130133331
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-05-30
[patent_title] => 'SYSTEM AND METHOD FOR REDUCING COMBUSTION DYNAMICS IN A TURBOMACHINE'
[patent_app_type] => utility
[patent_app_number] => 13/751301
[patent_app_country] => US
[patent_app_date] => 2013-01-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 2656
[patent_no_of_claims] => 20
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13751301
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/751301 | SYSTEM AND METHOD FOR REDUCING COMBUSTION DYNAMICS IN A TURBOMACHINE | Jan 27, 2013 | Abandoned |
Array
(
[id] => 9613700
[patent_doc_number] => 20140203557
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-07-24
[patent_title] => 'System and Method for Extending Minimum Turn Down Load of Combined Cycle Power Plant'
[patent_app_type] => utility
[patent_app_number] => 13/749656
[patent_app_country] => US
[patent_app_date] => 2013-01-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 3989
[patent_no_of_claims] => 20
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13749656
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/749656 | System and Method for Extending Minimum Turn Down Load of Combined Cycle Power Plant | Jan 23, 2013 | Abandoned |
Array
(
[id] => 10896467
[patent_doc_number] => 08919668
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-12-30
[patent_title] => 'Thrust reverser having a lockable variable nozzle section'
[patent_app_type] => utility
[patent_app_number] => 13/741868
[patent_app_country] => US
[patent_app_date] => 2013-01-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
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[patent_no_of_words] => 3943
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13741868
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/741868 | Thrust reverser having a lockable variable nozzle section | Jan 14, 2013 | Issued |
Array
(
[id] => 8924468
[patent_doc_number] => 20130180228
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-07-18
[patent_title] => 'SUPERCRITICAL HEAT RECOVERY STEAM GENERATOR REHEATER AND SUPERCRITICAL EVAPORATOR ARRANGEMENT'
[patent_app_type] => utility
[patent_app_number] => 13/739568
[patent_app_country] => US
[patent_app_date] => 2013-01-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 4590
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
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[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13739568
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/739568 | Supercritical heat recovery steam generator reheater and supercritical evaporator arrangement | Jan 10, 2013 | Issued |
Array
(
[id] => 9326791
[patent_doc_number] => 20140053573
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-02-27
[patent_title] => 'HOT GAS EXPANDER INLET CASING ASSEMBLY AND METHOD'
[patent_app_type] => utility
[patent_app_number] => 13/982552
[patent_app_country] => US
[patent_app_date] => 2012-12-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 6268
[patent_no_of_claims] => 20
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13982552
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/982552 | Hot gas expander inlet casing assembly and method | Dec 26, 2012 | Issued |
Array
(
[id] => 9556540
[patent_doc_number] => 20140174252
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-06-26
[patent_title] => 'MOUNT WITH AN AXIAL UPSTREAM LINKAGE FOR CONNETING A GEARBOX TO A TURBINE ENGINE CASE'
[patent_app_type] => utility
[patent_app_number] => 13/726131
[patent_app_country] => US
[patent_app_date] => 2012-12-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13726131
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/726131 | Mount with an axial upstream linkage for connecting a gearbox to a turbine engine case | Dec 22, 2012 | Issued |
Array
(
[id] => 9788358
[patent_doc_number] => 20150000302
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-01-01
[patent_title] => 'POWER PLANT COMPRISING A CONDENSED WATER RECOVERY DEVICE'
[patent_app_type] => utility
[patent_app_number] => 14/368058
[patent_app_country] => US
[patent_app_date] => 2012-12-19
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/368058 | POWER PLANT COMPRISING A CONDENSED WATER RECOVERY DEVICE | Dec 18, 2012 | Abandoned |
Array
(
[id] => 10935339
[patent_doc_number] => 20140338360
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-11-20
[patent_title] => 'BLEED PORT RIBS FOR TURBOMACHINE CASE'
[patent_app_type] => utility
[patent_app_number] => 13/712113
[patent_app_country] => US
[patent_app_date] => 2012-12-12
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[patent_drawing_sheets_cnt] => 6
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13712113
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/712113 | BLEED PORT RIBS FOR TURBOMACHINE CASE | Dec 11, 2012 | Abandoned |
Array
(
[id] => 9533139
[patent_doc_number] => 20140157785
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-06-12
[patent_title] => 'FUEL SUPPLY SYSTEM FOR GAS TURBINE'
[patent_app_type] => utility
[patent_app_number] => 13/707516
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/707516 | FUEL SUPPLY SYSTEM FOR GAS TURBINE | Dec 5, 2012 | Abandoned |
Array
(
[id] => 9513948
[patent_doc_number] => 20140150440
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-06-05
[patent_title] => 'GAS TURBINE ENGINE WITH A LOW SPEED SPOOL DRIVEN PUMP ARRANGEMENT'
[patent_app_type] => utility
[patent_app_number] => 13/705462
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13705462
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/705462 | GAS TURBINE ENGINE WITH A LOW SPEED SPOOL DRIVEN PUMP ARRANGEMENT | Dec 4, 2012 | Abandoned |
Array
(
[id] => 10949300
[patent_doc_number] => 20140352321
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-12-04
[patent_title] => 'GAS TURBINE ENGINE SYSTEM AND AN ASSOCIATED METHOD THEREOF'
[patent_app_type] => utility
[patent_app_number] => 13/691017
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/691017 | Gas turbine engine system and an associated method thereof | Nov 29, 2012 | Issued |
Array
(
[id] => 9782000
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[patent_title] => 'TURBINE ENGINE COMPRISING AN ELECTRICALLY ACTIVATED FUEL SUPPLY PUMP, AND TURBINE ENGINE FUEL SUPPLY METHOD'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/354343 | Turbine engine comprising an electrically activated fuel supply pump, and turbine engine fuel supply method | Nov 27, 2012 | Issued |
Array
(
[id] => 11481295
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[patent_title] => 'Cooled combustor seal'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/686303 | Cooled combustor seal | Nov 26, 2012 | Issued |
Array
(
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/686303 | Cooled combustor seal | Nov 26, 2012 | Issued |