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] => 9176989
[patent_doc_number] => 20130318974
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-12-05
[patent_title] => 'GAS TURBINE'
[patent_app_type] => utility
[patent_app_number] => 13/985991
[patent_app_country] => US
[patent_app_date] => 2012-02-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 5254
[patent_no_of_claims] => 19
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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] => 13985991
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/985991 | GAS TURBINE | Feb 19, 2012 | Abandoned |
Array
(
[id] => 8985766
[patent_doc_number] => 20130213047
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-08-22
[patent_title] => 'COMBUSTION LINER GUIDE STOP AND METHOD FOR ASSEMBLING A COMBUSTOR'
[patent_app_type] => utility
[patent_app_number] => 13/400264
[patent_app_country] => US
[patent_app_date] => 2012-02-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 4032
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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] => 13400264
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/400264 | Combustion liner guide stop and method for assembling a combustor | Feb 19, 2012 | Issued |
Array
(
[id] => 10629520
[patent_doc_number] => 09347667
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-05-24
[patent_title] => 'Injector for the combustion chamber of a gas turbine having a dual fuel circuit, and combustion chamber provided with at least one such injector'
[patent_app_type] => utility
[patent_app_number] => 13/982608
[patent_app_country] => US
[patent_app_date] => 2012-01-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2554
[patent_no_of_claims] => 11
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[patent_words_short_claim] => 309
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13982608
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/982608 | Injector for the combustion chamber of a gas turbine having a dual fuel circuit, and combustion chamber provided with at least one such injector | Jan 26, 2012 | Issued |
Array
(
[id] => 8936260
[patent_doc_number] => 20130186057
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-07-25
[patent_title] => 'NAPHTHA AND PROCESS GAS/SYNGAS MIXTURE FIRING METHOD FOR GAS TURBINE ENGINES'
[patent_app_type] => utility
[patent_app_number] => 13/357638
[patent_app_country] => US
[patent_app_date] => 2012-01-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 19
[patent_figures_cnt] => 19
[patent_no_of_words] => 4549
[patent_no_of_claims] => 17
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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] => 13357638
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/357638 | NAPHTHA AND PROCESS GAS/SYNGAS MIXTURE FIRING METHOD FOR GAS TURBINE ENGINES | Jan 24, 2012 | Abandoned |
Array
(
[id] => 8609199
[patent_doc_number] => 20130014511
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-01-17
[patent_title] => 'HIGHLY INTEGRATED INSIDE-OUT RAMJET'
[patent_app_type] => utility
[patent_app_number] => 13/342988
[patent_app_country] => US
[patent_app_date] => 2012-01-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 12
[patent_no_of_words] => 6396
[patent_no_of_claims] => 31
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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] => 13342988
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/342988 | HIGHLY INTEGRATED INSIDE-OUT RAMJET | Jan 3, 2012 | Abandoned |
Array
(
[id] => 8562289
[patent_doc_number] => 20120324860
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-12-27
[patent_title] => 'GAS TURBINE ENGINE AND PULSE DETONATION COMBUSTION SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 13/337104
[patent_app_country] => US
[patent_app_date] => 2011-12-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 6150
[patent_no_of_claims] => 16
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13337104
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/337104 | Gas turbine engine and pulse detonation combustion system | Dec 23, 2011 | Issued |
Array
(
[id] => 9049824
[patent_doc_number] => 20130247538
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-09-26
[patent_title] => 'OIL DISCHARGE DEVICE AND TURBOMACHINE COMPRISING SUCH A DEVICE'
[patent_app_type] => utility
[patent_app_number] => 13/988960
[patent_app_country] => US
[patent_app_date] => 2011-11-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 3541
[patent_no_of_claims] => 11
[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] => 13988960
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/988960 | Oil discharge device and turbomachine comprising such a device | Nov 24, 2011 | Issued |
Array
(
[id] => 9586999
[patent_doc_number] => 08776530
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-07-15
[patent_title] => 'Gas turbine engine lockout reduction'
[patent_app_type] => utility
[patent_app_number] => 13/303338
[patent_app_country] => US
[patent_app_date] => 2011-11-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_no_of_words] => 2801
[patent_no_of_claims] => 14
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[patent_words_short_claim] => 179
[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13303338
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/303338 | Gas turbine engine lockout reduction | Nov 22, 2011 | Issued |
Array
(
[id] => 10874231
[patent_doc_number] => 08899012
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2014-12-02
[patent_title] => 'Methods and systems for flux distribution within a heat exchanger'
[patent_app_type] => utility
[patent_app_number] => 13/296909
[patent_app_country] => US
[patent_app_date] => 2011-11-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13296909
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/296909 | Methods and systems for flux distribution within a heat exchanger | Nov 14, 2011 | Issued |
Array
(
[id] => 8646913
[patent_doc_number] => 20130032643
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-02-07
[patent_title] => 'COMBUSTOR LEAF SEAL ARRANGEMENT'
[patent_app_type] => utility
[patent_app_number] => 13/195394
[patent_app_country] => US
[patent_app_date] => 2011-08-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[patent_no_of_words] => 1646
[patent_no_of_claims] => 20
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13195394
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/195394 | Combustor leaf seal arrangement | Jul 31, 2011 | Issued |
Array
(
[id] => 8633484
[patent_doc_number] => 20130025287
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-01-31
[patent_title] => 'DISTRIBUTED COOLING FOR GAS TURBINE ENGINE COMBUSTOR'
[patent_app_type] => utility
[patent_app_number] => 13/193686
[patent_app_country] => US
[patent_app_date] => 2011-07-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
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[patent_no_of_words] => 2820
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13193686
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/193686 | Distributed cooling for gas turbine engine combustor | Jul 28, 2011 | Issued |
Array
(
[id] => 11888610
[patent_doc_number] => 09759163
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2017-09-12
[patent_title] => 'Combustion chamber provided with a tubular element'
[patent_app_type] => utility
[patent_app_number] => 13/812261
[patent_app_country] => US
[patent_app_date] => 2011-07-26
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13812261
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/812261 | Combustion chamber provided with a tubular element | Jul 25, 2011 | Issued |
Array
(
[id] => 11192055
[patent_doc_number] => 09422863
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-08-23
[patent_title] => 'Method and architecture for recombining the power of a turbomachine'
[patent_app_type] => utility
[patent_app_number] => 13/807143
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/807143 | Method and architecture for recombining the power of a turbomachine | Jul 4, 2011 | Issued |
Array
(
[id] => 9249621
[patent_doc_number] => 08613398
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-12-24
[patent_title] => 'Apparatus and methods for linear actuation of flow altering components of jet engine nozzle'
[patent_app_type] => utility
[patent_app_number] => 13/163463
[patent_app_country] => US
[patent_app_date] => 2011-06-17
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/163463 | Apparatus and methods for linear actuation of flow altering components of jet engine nozzle | Jun 16, 2011 | Issued |
Array
(
[id] => 8505248
[patent_doc_number] => 20120304656
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-12-06
[patent_title] => 'COMBUSTION LINER AND TRANSITION PIECE'
[patent_app_type] => utility
[patent_app_number] => 13/153836
[patent_app_country] => US
[patent_app_date] => 2011-06-06
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13153836
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/153836 | COMBUSTION LINER AND TRANSITION PIECE | Jun 5, 2011 | Abandoned |
Array
(
[id] => 8505247
[patent_doc_number] => 20120304655
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-12-06
[patent_title] => 'TURBOMACHINE COMBUSTOR ASSEMBLY INCLUDING A LINER STOP'
[patent_app_type] => utility
[patent_app_number] => 13/150319
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/150319 | TURBOMACHINE COMBUSTOR ASSEMBLY INCLUDING A LINER STOP | May 31, 2011 | Abandoned |
Array
(
[id] => 11198841
[patent_doc_number] => 09429043
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-08-30
[patent_title] => 'Gasification power generation plant'
[patent_app_type] => utility
[patent_app_number] => 13/641771
[patent_app_country] => US
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13641771
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/641771 | Gasification power generation plant | May 18, 2011 | Issued |
Array
(
[id] => 10567940
[patent_doc_number] => 09291099
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-03-22
[patent_title] => 'Structure for extracting compressed air from compressor of gas turbine engine and gas turbine engine with the structure'
[patent_app_type] => utility
[patent_app_number] => 13/696781
[patent_app_country] => US
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/696781 | Structure for extracting compressed air from compressor of gas turbine engine and gas turbine engine with the structure | May 5, 2011 | Issued |
Array
(
[id] => 8633451
[patent_doc_number] => 20130025254
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-01-31
[patent_title] => 'CONTROLLER FOR USE WITH GAS TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 13/641076
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/641076 | CONTROLLER FOR USE WITH GAS TURBINE ENGINE | Apr 10, 2011 | Abandoned |
Array
(
[id] => 11774220
[patent_doc_number] => 09383106
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-07-05
[patent_title] => 'Turbomachine combustion chamber having a perforated chamber end wall and with no deflector'
[patent_app_type] => utility
[patent_app_number] => 13/636873
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13636873
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/636873 | Turbomachine combustion chamber having a perforated chamber end wall and with no deflector | Mar 22, 2011 | Issued |