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] => 10375392
[patent_doc_number] => 20150260399
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-09-17
[patent_title] => 'COMBUSTOR SECTION OF A GAS TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 14/432437
[patent_app_country] => US
[patent_app_date] => 2013-09-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 3887
[patent_no_of_claims] => 18
[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] => 14432437
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/432437 | COMBUSTOR SECTION OF A GAS TURBINE ENGINE | Sep 29, 2013 | Abandoned |
Array
(
[id] => 9900870
[patent_doc_number] => 20150056070
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-02-26
[patent_title] => 'MULTI SURFACE BLOCKER DOOR SYSTEM AND APPARATUS'
[patent_app_type] => utility
[patent_app_number] => 13/975038
[patent_app_country] => US
[patent_app_date] => 2013-08-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2292
[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] =>[firstpage_image] =>[orig_patent_app_number] => 13975038
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/975038 | Multi surface blocker door system and apparatus | Aug 22, 2013 | Issued |
Array
(
[id] => 10935336
[patent_doc_number] => 20140338357
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-11-20
[patent_title] => 'CAVITY SWIRL FUEL INJECTOR FOR AN AUGMENTOR SECTION OF A GAS TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 13/936876
[patent_app_country] => US
[patent_app_date] => 2013-07-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 12
[patent_no_of_words] => 3827
[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] =>[firstpage_image] =>[orig_patent_app_number] => 13936876
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/936876 | Cavity swirl fuel injector for an augmentor section of a gas turbine engine | Jul 7, 2013 | Issued |
Array
(
[id] => 9788357
[patent_doc_number] => 20150000301
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-01-01
[patent_title] => 'SYSTEM AND METHOD FOR MODELING BOTTOMING CYCLE PERFORMANCE OF A COMBINED CYCLE POWER PLANT'
[patent_app_type] => utility
[patent_app_number] => 13/932196
[patent_app_country] => US
[patent_app_date] => 2013-07-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2233
[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] =>[firstpage_image] =>[orig_patent_app_number] => 13932196
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/932196 | SYSTEM AND METHOD FOR MODELING BOTTOMING CYCLE PERFORMANCE OF A COMBINED CYCLE POWER PLANT | Jun 30, 2013 | Abandoned |
Array
(
[id] => 10040071
[patent_doc_number] => 09080772
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-07-14
[patent_title] => 'Continuous ignition'
[patent_app_type] => utility
[patent_app_number] => 13/917053
[patent_app_country] => US
[patent_app_date] => 2013-06-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 7
[patent_no_of_words] => 4242
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 252
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13917053
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/917053 | Continuous ignition | Jun 12, 2013 | Issued |
Array
(
[id] => 9194050
[patent_doc_number] => 20130333365
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-12-19
[patent_title] => 'CONTROLLING METHOD AND SYSTEM FOR COMPRESSED AIR SUPPLY TO A PNEUMATIC NETWORK, IN PARTICULAR IN AN AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 13/911346
[patent_app_country] => US
[patent_app_date] => 2013-06-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 2306
[patent_no_of_claims] => 8
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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] => 13911346
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/911346 | Controlling method and system for compressed air supply to a pneumatic network, in particular in an aircraft | Jun 5, 2013 | Issued |
Array
(
[id] => 10949303
[patent_doc_number] => 20140352324
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-12-04
[patent_title] => 'DUAL PRESSURE REGULATOR SHUT OFF VALVE APPARATUS'
[patent_app_type] => utility
[patent_app_number] => 13/904659
[patent_app_country] => US
[patent_app_date] => 2013-05-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 3142
[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] =>[firstpage_image] =>[orig_patent_app_number] => 13904659
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/904659 | DUAL PRESSURE REGULATOR SHUT OFF VALVE APPARATUS | May 28, 2013 | Abandoned |
Array
(
[id] => 10942230
[patent_doc_number] => 20140345252
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-11-27
[patent_title] => 'SYSTEM, APPARATUS, AND METHOD FOR A VIRTUAL BLOCKER'
[patent_app_type] => utility
[patent_app_number] => 13/888193
[patent_app_country] => US
[patent_app_date] => 2013-05-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 3253
[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] => 13888193
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/888193 | System, apparatus, and method for a virtual blocker | May 5, 2013 | Issued |
Array
(
[id] => 12491895
[patent_doc_number] => 09995245
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2018-06-12
[patent_title] => Variable immersion lobe mixer for turbofan jet engine exhaust and method of fabricating the same
[patent_app_type] => utility
[patent_app_number] => 14/396800
[patent_app_country] => US
[patent_app_date] => 2013-04-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14396800
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/396800 | Variable immersion lobe mixer for turbofan jet engine exhaust and method of fabricating the same | Apr 25, 2013 | Issued |
Array
(
[id] => 9752827
[patent_doc_number] => 20140283527
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-09-25
[patent_title] => 'MULTI-ENGINE PERFORMANCE MARGIN SYNCHRONIZATION ADAPTIVE CONTROL SYSTEM AND METHOD'
[patent_app_type] => utility
[patent_app_number] => 13/870302
[patent_app_country] => US
[patent_app_date] => 2013-04-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 5011
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 2
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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] => 13870302
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/870302 | Multi-engine performance margin synchronization adaptive control system and method | Apr 24, 2013 | Issued |
Array
(
[id] => 9926981
[patent_doc_number] => 20150075173
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-03-19
[patent_title] => 'COMPRESSED-AIR ENERGY-STORAGE SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 14/391493
[patent_app_country] => US
[patent_app_date] => 2013-04-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_no_of_words] => 6282
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14391493
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/391493 | Compressed-air energy-storage system | Apr 7, 2013 | Issued |
Array
(
[id] => 10051343
[patent_doc_number] => 09091212
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-07-28
[patent_title] => 'Fuel and actuation system for gas turbine engine'
[patent_app_type] => utility
[patent_app_number] => 13/851580
[patent_app_country] => US
[patent_app_date] => 2013-03-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13851580
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/851580 | Fuel and actuation system for gas turbine engine | Mar 26, 2013 | Issued |
Array
(
[id] => 8959599
[patent_doc_number] => 20130199201
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-08-08
[patent_title] => 'MAIN ENGINE START BY MEANS OF AN AIRCRAFT AIR CONDITIONING SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 13/788656
[patent_app_country] => US
[patent_app_date] => 2013-03-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13788656
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/788656 | Main engine start by means of an aircraft air conditioning system | Mar 6, 2013 | Issued |
Array
(
[id] => 9853740
[patent_doc_number] => 20150033756
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-02-05
[patent_title] => 'Gas Turbine with Primary and Secondary Lubricating Oil Cooler'
[patent_app_type] => utility
[patent_app_number] => 14/383861
[patent_app_country] => US
[patent_app_date] => 2013-03-06
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14383861
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/383861 | Gas Turbine with Primary and Secondary Lubricating Oil Cooler | Mar 5, 2013 | Abandoned |
Array
(
[id] => 13637547
[patent_doc_number] => 09845730
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2017-12-19
[patent_title] => Device and method for gas turbine unlocking
[patent_app_type] => utility
[patent_app_number] => 14/383231
[patent_app_country] => US
[patent_app_date] => 2013-03-06
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/383231 | Device and method for gas turbine unlocking | Mar 5, 2013 | Issued |
Array
(
[id] => 9696057
[patent_doc_number] => 20140245742
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-09-04
[patent_title] => 'AIR SWIRLERS'
[patent_app_type] => utility
[patent_app_number] => 13/783832
[patent_app_country] => US
[patent_app_date] => 2013-03-04
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13783832
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/783832 | Air swirlers | Mar 3, 2013 | Issued |
Array
(
[id] => 9795628
[patent_doc_number] => 20150007572
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-01-08
[patent_title] => 'FUEL INJECTOR FOR A TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 14/378797
[patent_app_country] => US
[patent_app_date] => 2013-02-12
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14378797
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/378797 | Turbine engine fuel injector with permanent leakage flow | Feb 11, 2013 | Issued |
Array
(
[id] => 10407403
[patent_doc_number] => 20150292412
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-10-15
[patent_title] => 'FUEL INJECTOR FOR A TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 14/378816
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/378816 | Turbine engine fuel injector with leakage flow controlled by position of metering valve | Feb 6, 2013 | Issued |
Array
(
[id] => 12166715
[patent_doc_number] => 09885480
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2018-02-06
[patent_title] => 'Combustion chamber of a combustor for a gas turbine'
[patent_app_type] => utility
[patent_app_number] => 14/369687
[patent_app_country] => US
[patent_app_date] => 2012-12-21
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/369687 | Combustion chamber of a combustor for a gas turbine | Dec 20, 2012 | Issued |
Array
(
[id] => 9788341
[patent_doc_number] => 20150000285
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-01-01
[patent_title] => 'FUEL NOZZLE FOR TWO FUELS'
[patent_app_type] => utility
[patent_app_number] => 14/364277
[patent_app_country] => US
[patent_app_date] => 2012-11-09
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14364277
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/364277 | Fuel nozzle having an inner tube and an outer tube engaged with the inner tube | Nov 8, 2012 | Issued |