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] => 11298423
[patent_doc_number] => 09506423
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-11-29
[patent_title] => 'Flow control device for a three stream turbofan engine'
[patent_app_type] => utility
[patent_app_number] => 14/206232
[patent_app_country] => US
[patent_app_date] => 2014-03-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 1924
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 166
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14206232
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/206232 | Flow control device for a three stream turbofan engine | Mar 11, 2014 | Issued |
Array
(
[id] => 13038569
[patent_doc_number] => 10041411
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2018-08-07
[patent_title] => Compact dosing device for an injector with two fuel circuits for an aircraft turbomachine
[patent_app_type] => utility
[patent_app_number] => 14/772924
[patent_app_country] => US
[patent_app_date] => 2014-03-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 7
[patent_no_of_words] => 3989
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 408
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14772924
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/772924 | Compact dosing device for an injector with two fuel circuits for an aircraft turbomachine | Mar 4, 2014 | Issued |
Array
(
[id] => 11025860
[patent_doc_number] => 20160222815
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-08-04
[patent_title] => 'High Efficiency Geared Turbofan'
[patent_app_type] => utility
[patent_app_number] => 15/021046
[patent_app_country] => US
[patent_app_date] => 2014-03-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 3000
[patent_no_of_claims] => 21
[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] =>[firstpage_image] =>[orig_patent_app_number] => 15021046
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/021046 | High Efficiency Geared Turbofan | Mar 4, 2014 | Abandoned |
Array
(
[id] => 16142805
[patent_doc_number] => 10704468
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2020-07-07
[patent_title] => Method and apparatus for handling pre-diffuser airflow for cooling high pressure turbine components
[patent_app_type] => utility
[patent_app_number] => 14/771069
[patent_app_country] => US
[patent_app_date] => 2014-02-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 23
[patent_figures_cnt] => 23
[patent_no_of_words] => 5942
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 186
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14771069
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/771069 | Method and apparatus for handling pre-diffuser airflow for cooling high pressure turbine components | Feb 27, 2014 | Issued |
Array
(
[id] => 10236902
[patent_doc_number] => 20150121896
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-05-07
[patent_title] => 'REVERSE CORE FLOW ENGINE MOUNTING ARRANGEMENT'
[patent_app_type] => utility
[patent_app_number] => 14/190162
[patent_app_country] => US
[patent_app_date] => 2014-02-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 2657
[patent_no_of_claims] => 16
[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] => 14190162
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/190162 | REVERSE CORE FLOW ENGINE MOUNTING ARRANGEMENT | Feb 25, 2014 | Abandoned |
Array
(
[id] => 10678799
[patent_doc_number] => 20160024944
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-01-28
[patent_title] => 'TRANSIENT LIQUID PAHSE BONDED TURBINE ROTOR ASSEMBLY'
[patent_app_type] => utility
[patent_app_number] => 14/775730
[patent_app_country] => US
[patent_app_date] => 2014-02-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 4287
[patent_no_of_claims] => 24
[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] =>[firstpage_image] =>[orig_patent_app_number] => 14775730
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/775730 | TRANSIENT LIQUID PAHSE BONDED TURBINE ROTOR ASSEMBLY | Feb 25, 2014 | Abandoned |
Array
(
[id] => 11205674
[patent_doc_number] => 09435293
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-09-06
[patent_title] => 'Full ring sliding nacelle with thrust reverser'
[patent_app_type] => utility
[patent_app_number] => 14/187027
[patent_app_country] => US
[patent_app_date] => 2014-02-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 22
[patent_figures_cnt] => 33
[patent_no_of_words] => 17347
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 335
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14187027
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/187027 | Full ring sliding nacelle with thrust reverser | Feb 20, 2014 | Issued |
Array
(
[id] => 14089277
[patent_doc_number] => 10240535
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2019-03-26
[patent_title] => Gas turbine silencer, and gas turbine provided with same
[patent_app_type] => utility
[patent_app_number] => 14/771357
[patent_app_country] => US
[patent_app_date] => 2014-02-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
[patent_figures_cnt] => 13
[patent_no_of_words] => 9212
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 809
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14771357
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/771357 | Gas turbine silencer, and gas turbine provided with same | Feb 9, 2014 | Issued |
Array
(
[id] => 10492010
[patent_doc_number] => 20150377032
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-12-31
[patent_title] => 'GAS TURBINE ENGINE COMPONENT WITH COMBINED MATE FACE AND PLATFORM COOLING'
[patent_app_type] => utility
[patent_app_number] => 14/766190
[patent_app_country] => US
[patent_app_date] => 2014-02-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 4795
[patent_no_of_claims] => 20
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14766190
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/766190 | Gas turbine engine component with combined mate face and platform cooling | Feb 6, 2014 | Issued |
Array
(
[id] => 14032359
[patent_doc_number] => 10227923
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2019-03-12
[patent_title] => System for preventing icing on an aircraft surface using a plasma actuator
[patent_app_type] => utility
[patent_app_number] => 14/765744
[patent_app_country] => US
[patent_app_date] => 2014-02-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 5
[patent_no_of_words] => 3144
[patent_no_of_claims] => 5
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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] => 14765744
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/765744 | System for preventing icing on an aircraft surface using a plasma actuator | Feb 2, 2014 | Issued |
Array
(
[id] => 11549371
[patent_doc_number] => 09618208
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2017-04-11
[patent_title] => 'Lean azimuthal flame combustor'
[patent_app_type] => utility
[patent_app_number] => 14/143589
[patent_app_country] => US
[patent_app_date] => 2013-12-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_no_of_words] => 3275
[patent_no_of_claims] => 19
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[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14143589
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/143589 | Lean azimuthal flame combustor | Dec 29, 2013 | Issued |
Array
(
[id] => 9698436
[patent_doc_number] => 20140248121
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-09-04
[patent_title] => 'AIRCRAFT POWER SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 14/140959
[patent_app_country] => US
[patent_app_date] => 2013-12-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14140959
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/140959 | Aircraft power system | Dec 25, 2013 | Issued |
Array
(
[id] => 10957182
[patent_doc_number] => 20140360205
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-12-11
[patent_title] => 'GAS TURBINE ENGINE AND ELECTRICAL SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 14/135567
[patent_app_country] => US
[patent_app_date] => 2013-12-19
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14135567
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/135567 | Gas turbine engine and electrical system | Dec 18, 2013 | Issued |
Array
(
[id] => 10949296
[patent_doc_number] => 20140352317
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-12-04
[patent_title] => 'INTERCOOLED GAS TURBINE WITH CLOSED COMBINED POWER CYCLE'
[patent_app_type] => utility
[patent_app_number] => 14/134427
[patent_app_country] => US
[patent_app_date] => 2013-12-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14134427
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/134427 | Intercooled gas turbine with closed combined power cycle | Dec 18, 2013 | Issued |
Array
(
[id] => 10282981
[patent_doc_number] => 20150167979
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-06-18
[patent_title] => 'FIRST STAGE NOZZLE OR TRANSITION NOZZLE CONFIGURED TO PROMOTE MIXING OF RESPECTIVE COMBUSTION STREAMS DOWNSTREAM THEREOF BEFORE ENTRY INTO A FIRST STAGE BUCKET OF A TURBINE'
[patent_app_type] => utility
[patent_app_number] => 14/109418
[patent_app_country] => US
[patent_app_date] => 2013-12-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14109418
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/109418 | FIRST STAGE NOZZLE OR TRANSITION NOZZLE CONFIGURED TO PROMOTE MIXING OF RESPECTIVE COMBUSTION STREAMS DOWNSTREAM THEREOF BEFORE ENTRY INTO A FIRST STAGE BUCKET OF A TURBINE | Dec 16, 2013 | Abandoned |
Array
(
[id] => 9788346
[patent_doc_number] => 20150000291
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-01-01
[patent_title] => 'GAS TURBINE ENGINE COMBUSTOR HEAT EXCHANGER'
[patent_app_type] => utility
[patent_app_number] => 14/109685
[patent_app_country] => US
[patent_app_date] => 2013-12-17
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14109685
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/109685 | GAS TURBINE ENGINE COMBUSTOR HEAT EXCHANGER | Dec 16, 2013 | Abandoned |
Array
(
[id] => 13118669
[patent_doc_number] => 10077681
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2018-09-18
[patent_title] => Compliant heat shield liner hanger assembly for gas turbine engines
[patent_app_type] => utility
[patent_app_number] => 14/759623
[patent_app_country] => US
[patent_app_date] => 2013-12-13
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14759623
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/759623 | Compliant heat shield liner hanger assembly for gas turbine engines | Dec 12, 2013 | Issued |
Array
(
[id] => 14058973
[patent_doc_number] => 10233771
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2019-03-19
[patent_title] => System and method for preventing an emergency over-speed condition in a rotating machine
[patent_app_type] => utility
[patent_app_number] => 14/097958
[patent_app_country] => US
[patent_app_date] => 2013-12-05
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14097958
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/097958 | System and method for preventing an emergency over-speed condition in a rotating machine | Dec 4, 2013 | Issued |
Array
(
[id] => 11320003
[patent_doc_number] => 09518742
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-12-13
[patent_title] => 'Premixer assembly for mixing air and fuel for combustion'
[patent_app_type] => utility
[patent_app_number] => 14/094098
[patent_app_country] => US
[patent_app_date] => 2013-12-02
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14094098
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/094098 | Premixer assembly for mixing air and fuel for combustion | Dec 1, 2013 | Issued |
Array
(
[id] => 9513944
[patent_doc_number] => 20140150436
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-06-05
[patent_title] => 'GAS TURBINE PART COMPRISING A NEAR WALL COOLING ARRANGEMENT'
[patent_app_type] => utility
[patent_app_number] => 14/091621
[patent_app_country] => US
[patent_app_date] => 2013-11-27
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14091621
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/091621 | Gas turbine part comprising a near wall cooling arrangement | Nov 26, 2013 | Issued |