Willis Little
Examiner (ID: 16938)
Most Active Art Unit | 3203 |
Art Unit(s) | 3203, 3643, 2107, 2103, 2406, 3616, 2401, 2899, 2403 |
Total Applications | 2327 |
Issued Applications | 2182 |
Pending Applications | 48 |
Abandoned Applications | 97 |
Applications
Application number | Title of the application | Filing Date | Status |
---|---|---|---|
Array
(
[id] => 8679341
[patent_doc_number] => 20130047625
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-02-28
[patent_title] => 'ENHANCED PULSE DETONATION ENGINE SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 13/591393
[patent_app_country] => US
[patent_app_date] => 2012-08-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 15
[patent_figures_cnt] => 15
[patent_no_of_words] => 4872
[patent_no_of_claims] => 21
[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] => 13591393
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/591393 | ENHANCED PULSE DETONATION ENGINE SYSTEM | Aug 21, 2012 | Abandoned |
Array
(
[id] => 9326785
[patent_doc_number] => 20140053567
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-02-27
[patent_title] => 'SYSTEM AND METHOD FOR CONTROLLING A GAS TURBINE ENGINE GENERATOR SET'
[patent_app_type] => utility
[patent_app_number] => 13/592253
[patent_app_country] => US
[patent_app_date] => 2012-08-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 4481
[patent_no_of_claims] => 20
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13592253
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/592253 | SYSTEM AND METHOD FOR CONTROLLING A GAS TURBINE ENGINE GENERATOR SET | Aug 21, 2012 | Abandoned |
Array
(
[id] => 9326751
[patent_doc_number] => 20140053533
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-02-27
[patent_title] => 'REVERSE FLOW GAS TURBINE ENGINE WITH THRUST REVERSER'
[patent_app_type] => utility
[patent_app_number] => 13/590223
[patent_app_country] => US
[patent_app_date] => 2012-08-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2003
[patent_no_of_claims] => 25
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13590223
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/590223 | REVERSE FLOW GAS TURBINE ENGINE WITH THRUST REVERSER | Aug 20, 2012 | Abandoned |
Array
(
[id] => 9674575
[patent_doc_number] => 08813473
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-08-26
[patent_title] => 'Steam injected gas turbine engine'
[patent_app_type] => utility
[patent_app_number] => 13/588646
[patent_app_country] => US
[patent_app_date] => 2012-08-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 14
[patent_no_of_words] => 5256
[patent_no_of_claims] => 10
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13588646
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/588646 | Steam injected gas turbine engine | Aug 16, 2012 | Issued |
Array
(
[id] => 8668090
[patent_doc_number] => 20130042627
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-02-21
[patent_title] => 'COMBUSTION CHAMBER HEAD OF A GAS TURBINE WITH COOLING AND DAMPING FUNCTIONS'
[patent_app_type] => utility
[patent_app_number] => 13/587663
[patent_app_country] => US
[patent_app_date] => 2012-08-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
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[patent_no_of_words] => 4373
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13587663
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/587663 | COMBUSTION CHAMBER HEAD OF A GAS TURBINE WITH COOLING AND DAMPING FUNCTIONS | Aug 15, 2012 | Abandoned |
Array
(
[id] => 9315510
[patent_doc_number] => 20140047848
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-02-20
[patent_title] => 'ADJUSTABLE CABLE FOR EXHAUST DUCT LINER HANGER'
[patent_app_type] => utility
[patent_app_number] => 13/586623
[patent_app_country] => US
[patent_app_date] => 2012-08-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_no_of_words] => 4859
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13586623
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/586623 | Adjustable cable for exhaust duct liner hanger | Aug 14, 2012 | Issued |
Array
(
[id] => 9315508
[patent_doc_number] => 20140047846
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-02-20
[patent_title] => 'TURBINE COMPONENT COOLING ARRANGEMENT AND METHOD OF COOLING A TURBINE COMPONENT'
[patent_app_type] => utility
[patent_app_number] => 13/585568
[patent_app_country] => US
[patent_app_date] => 2012-08-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2625
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13585568
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/585568 | TURBINE COMPONENT COOLING ARRANGEMENT AND METHOD OF COOLING A TURBINE COMPONENT | Aug 13, 2012 | Abandoned |
Array
(
[id] => 9302717
[patent_doc_number] => 20140041391
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-02-13
[patent_title] => 'APPARATUS INCLUDING A FLOW CONDITIONER COUPLED TO A TRANSITION PIECE FORWARD END'
[patent_app_type] => utility
[patent_app_number] => 13/568842
[patent_app_country] => US
[patent_app_date] => 2012-08-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2285
[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] => 13568842
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/568842 | APPARATUS INCLUDING A FLOW CONDITIONER COUPLED TO A TRANSITION PIECE FORWARD END | Aug 6, 2012 | Abandoned |
Array
(
[id] => 9387219
[patent_doc_number] => 08683805
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-04-01
[patent_title] => 'Injector seal for a gas turbomachine'
[patent_app_type] => utility
[patent_app_number] => 13/567415
[patent_app_country] => US
[patent_app_date] => 2012-08-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13567415
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/567415 | Injector seal for a gas turbomachine | Aug 5, 2012 | Issued |
Array
(
[id] => 9290090
[patent_doc_number] => 20140033724
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-02-06
[patent_title] => 'FUEL NOZZLE ASSEMBLY AND METHODS OF ASSEMBLING SAME'
[patent_app_type] => utility
[patent_app_number] => 13/566506
[patent_app_country] => US
[patent_app_date] => 2012-08-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 6260
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13566506
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/566506 | FUEL NOZZLE ASSEMBLY AND METHODS OF ASSEMBLING SAME | Aug 2, 2012 | Abandoned |
Array
(
[id] => 9955621
[patent_doc_number] => 09003803
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-04-14
[patent_title] => 'Combustor cap assembly'
[patent_app_type] => utility
[patent_app_number] => 13/566286
[patent_app_country] => US
[patent_app_date] => 2012-08-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13566286
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/566286 | Combustor cap assembly | Aug 2, 2012 | Issued |
Array
(
[id] => 9290085
[patent_doc_number] => 20140033719
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-02-06
[patent_title] => 'MULTI-STEP COMBUSTOR'
[patent_app_type] => utility
[patent_app_number] => 13/564808
[patent_app_country] => US
[patent_app_date] => 2012-08-02
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13564808
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/564808 | MULTI-STEP COMBUSTOR | Aug 1, 2012 | Abandoned |
Array
(
[id] => 10090743
[patent_doc_number] => 09127558
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-09-08
[patent_title] => 'Turbomachine including horizontal joint heating and method of controlling tip clearance in a gas turbomachine'
[patent_app_type] => utility
[patent_app_number] => 13/564175
[patent_app_country] => US
[patent_app_date] => 2012-08-01
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13564175
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/564175 | Turbomachine including horizontal joint heating and method of controlling tip clearance in a gas turbomachine | Jul 31, 2012 | Issued |
Array
(
[id] => 9981658
[patent_doc_number] => 09027354
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-05-12
[patent_title] => 'System and method for recirculating and recovering energy from compressor discharge bleed air'
[patent_app_type] => utility
[patent_app_number] => 13/562252
[patent_app_country] => US
[patent_app_date] => 2012-07-30
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13562252
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/562252 | System and method for recirculating and recovering energy from compressor discharge bleed air | Jul 29, 2012 | Issued |
Array
(
[id] => 8633453
[patent_doc_number] => 20130025256
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-01-31
[patent_title] => 'Pulsed Detonation Engine'
[patent_app_type] => utility
[patent_app_number] => 13/561074
[patent_app_country] => US
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13561074
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/561074 | Pulsed detonation engine | Jul 28, 2012 | Issued |
Array
(
[id] => 10187955
[patent_doc_number] => 09217367
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-12-22
[patent_title] => 'Method for operating a gas turbine power plant with flue gas recirculation'
[patent_app_type] => utility
[patent_app_number] => 13/560551
[patent_app_country] => US
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13560551
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/560551 | Method for operating a gas turbine power plant with flue gas recirculation | Jul 26, 2012 | Issued |
Array
(
[id] => 9276613
[patent_doc_number] => 20140026581
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-01-30
[patent_title] => 'LINER STOP FOR TURBINE SYSTEM COMBUSTOR'
[patent_app_type] => utility
[patent_app_number] => 13/558470
[patent_app_country] => US
[patent_app_date] => 2012-07-26
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/558470 | Liner stop for turbine system combustor | Jul 25, 2012 | Issued |
Array
(
[id] => 12247925
[patent_doc_number] => 09920696
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2018-03-20
[patent_title] => 'Method for operating a gas turbine and gas turbine unit useful for carrying out the method'
[patent_app_type] => utility
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/555331 | Method for operating a gas turbine and gas turbine unit useful for carrying out the method | Jul 22, 2012 | Issued |
Array
(
[id] => 9265484
[patent_doc_number] => 20140020400
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-01-23
[patent_title] => 'SYSTEM AND METHOD FOR AUTO-TUNING A COMBUSTION SYSTEM OF A GAS TURBINE'
[patent_app_type] => utility
[patent_app_number] => 13/551702
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/551702 | SYSTEM AND METHOD FOR AUTO-TUNING A COMBUSTION SYSTEM OF A GAS TURBINE | Jul 17, 2012 | Abandoned |
Array
(
[id] => 8614296
[patent_doc_number] => 20130019608
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-01-24
[patent_title] => 'METHOD OF INHIBITING ICE ACCRETION WITHIN A TURBINE ENGINE AND CONTROL SYSTEM THEREFOR'
[patent_app_type] => utility
[patent_app_number] => 13/546514
[patent_app_country] => US
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13546514
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/546514 | Method of inhibiting ice accretion within a turbine engine and control system therefor | Jul 10, 2012 | Issued |