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] => 11773976
[patent_doc_number] => 09382841
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-07-05
[patent_title] => 'Aircraft environmental control system selectively powered by three bleed ports'
[patent_app_type] => utility
[patent_app_number] => 14/088557
[patent_app_country] => US
[patent_app_date] => 2013-11-25
[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] => 14088557
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/088557 | Aircraft environmental control system selectively powered by three bleed ports | Nov 24, 2013 | Issued |
Array
(
[id] => 12451098
[patent_doc_number] => 09982890
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2018-05-29
[patent_title] => Combustor dome heat shield
[patent_app_type] => utility
[patent_app_number] => 14/085011
[patent_app_country] => US
[patent_app_date] => 2013-11-20
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14085011
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/085011 | Combustor dome heat shield | Nov 19, 2013 | Issued |
Array
(
[id] => 10492463
[patent_doc_number] => 20150377485
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-12-31
[patent_title] => 'COMBUSTION INSTABILITY CONTROL DEVICE AND CONTROL METHOD FOR SAME'
[patent_app_type] => utility
[patent_app_number] => 14/772288
[patent_app_country] => US
[patent_app_date] => 2013-11-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/772288 | Combustion instability control method | Nov 19, 2013 | Issued |
Array
(
[id] => 14949713
[patent_doc_number] => 10436117
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2019-10-08
[patent_title] => Carbureted fuel injection system for a gas turbine engine
[patent_app_type] => utility
[patent_app_number] => 14/083040
[patent_app_country] => US
[patent_app_date] => 2013-11-18
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14083040
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/083040 | Carbureted fuel injection system for a gas turbine engine | Nov 17, 2013 | Issued |
Array
(
[id] => 11613110
[patent_doc_number] => 09650961
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2017-05-16
[patent_title] => 'Gas turbine combustor including burner having plural gaseous fuel manifolds'
[patent_app_type] => utility
[patent_app_number] => 14/081609
[patent_app_country] => US
[patent_app_date] => 2013-11-15
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14081609
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/081609 | Gas turbine combustor including burner having plural gaseous fuel manifolds | Nov 14, 2013 | Issued |
Array
(
[id] => 12247869
[patent_doc_number] => 09920639
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2018-03-20
[patent_title] => 'Gas turbine combustion chamber having a flow sleeve with a plurality of integrated segments'
[patent_app_type] => utility
[patent_app_number] => 14/079920
[patent_app_country] => US
[patent_app_date] => 2013-11-14
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14079920
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/079920 | Gas turbine combustion chamber having a flow sleeve with a plurality of integrated segments | Nov 13, 2013 | Issued |
Array
(
[id] => 9474018
[patent_doc_number] => 20140131481
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-05-15
[patent_title] => 'THREADED ROD FOR SYSTEM FOR DEPLOYING A DEPLOYABLE DIVERGENT SEGMENT OF A THRUSTER'
[patent_app_type] => utility
[patent_app_number] => 14/080009
[patent_app_country] => US
[patent_app_date] => 2013-11-14
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14080009
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/080009 | Threaded rod for system for deploying a deployable divergent segment of a thruster | Nov 13, 2013 | Issued |
Array
(
[id] => 9459245
[patent_doc_number] => 20140123670
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-05-08
[patent_title] => 'GAS TURBINE BURNER'
[patent_app_type] => utility
[patent_app_number] => 14/074292
[patent_app_country] => US
[patent_app_date] => 2013-11-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14074292
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/074292 | Method for operating a gas turbine burner with a swirl generator | Nov 6, 2013 | Issued |
Array
(
[id] => 10469805
[patent_doc_number] => 20150354821
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-12-10
[patent_title] => 'Cumbustor Liners with U-Shaped Cooling Channels'
[patent_app_type] => utility
[patent_app_number] => 14/647035
[patent_app_country] => US
[patent_app_date] => 2013-11-06
[patent_effective_date] => 0000-00-00
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/647035 | Combustor liners with U-shaped cooling channels | Nov 5, 2013 | Issued |
Array
(
[id] => 9473038
[patent_doc_number] => 20140130501
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-05-15
[patent_title] => 'COMBUSTION CHAMBER TILE OF A GAS TURBINE'
[patent_app_type] => utility
[patent_app_number] => 14/072452
[patent_app_country] => US
[patent_app_date] => 2013-11-05
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14072452
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/072452 | Combustion chamber tile of a gas turbine | Nov 4, 2013 | Issued |
Array
(
[id] => 10229011
[patent_doc_number] => 20150114004
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-04-30
[patent_title] => 'GAS TURBINE ENCLOSURE'
[patent_app_type] => utility
[patent_app_number] => 14/068577
[patent_app_country] => US
[patent_app_date] => 2013-10-31
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/068577 | GAS TURBINE ENCLOSURE | Oct 30, 2013 | Abandoned |
Array
(
[id] => 9459244
[patent_doc_number] => 20140123669
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-05-08
[patent_title] => 'SYSTEM AND METHOD FOR DIFFUSION COMBUSTION WITH OXIDANT-DILUENT MIXING IN A STOICHIOMETRIC EXHAUST GAS RECIRCULATION GAS TURBINE SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 14/067552
[patent_app_country] => US
[patent_app_date] => 2013-10-30
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14067552
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/067552 | System and method for diffusion combustion with oxidant-diluent mixing in a stoichiometric exhaust gas recirculation gas turbine system | Oct 29, 2013 | Issued |
Array
(
[id] => 9459199
[patent_doc_number] => 20140123624
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-05-08
[patent_title] => 'GAS TURBINE COMBUSTOR CONTROL SYSTEM'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/066551 | Gas turbine combustor control system for stoichiometric combustion in the presence of a diluent | Oct 28, 2013 | Issued |
Array
(
[id] => 9459240
[patent_doc_number] => 20140123665
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-05-08
[patent_title] => 'REHEAT BURNER ARRANGEMENT'
[patent_app_type] => utility
[patent_app_number] => 14/063065
[patent_app_country] => US
[patent_app_date] => 2013-10-25
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14063065
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/063065 | Reheat burner arrangement having an increasing flow path cross-section | Oct 24, 2013 | Issued |
Array
(
[id] => 11231509
[patent_doc_number] => 09458732
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-10-04
[patent_title] => 'Transition duct assembly with modified trailing edge in turbine system'
[patent_app_type] => utility
[patent_app_number] => 14/063358
[patent_app_country] => US
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/063358 | Transition duct assembly with modified trailing edge in turbine system | Oct 24, 2013 | Issued |
Array
(
[id] => 9431682
[patent_doc_number] => 20140109588
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-04-24
[patent_title] => 'BURNER FOR A CAN COMBUSTOR'
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14060931
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/060931 | Burner for a combustion chamber of a gas turbine having a mixing and injection device | Oct 22, 2013 | Issued |
Array
(
[id] => 10223255
[patent_doc_number] => 20150108248
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-04-23
[patent_title] => 'THRUST REVERSER FAN RAMP WITH NOISE SUPPRESSION'
[patent_app_type] => utility
[patent_app_number] => 14/060194
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[patent_app_date] => 2013-10-22
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/060194 | THRUST REVERSER FAN RAMP WITH NOISE SUPPRESSION | Oct 21, 2013 | Abandoned |
Array
(
[id] => 10390759
[patent_doc_number] => 20150275766
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-10-01
[patent_title] => 'GEARED TURBINE ENGINE WITH A D-DUCT AND A THRUST REVERSER'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/435077 | GEARED TURBINE ENGINE WITH A D-DUCT AND A THRUST REVERSER | Oct 9, 2013 | Abandoned |
Array
(
[id] => 9290099
[patent_doc_number] => 20140033733
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-02-06
[patent_title] => 'FLOW DISCHARGE DEVICE'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/048575 | FLOW DISCHARGE DEVICE | Oct 7, 2013 | Abandoned |
Array
(
[id] => 9405281
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[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-04-10
[patent_title] => 'Bearing chamber venting system for an aircraft engine and method for providing a required pressure ratio at bearing chamber seals of an air-sealed bearing chamber'
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14043507
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/043507 | Bearing chamber venting system for an aircraft engine and method for providing a required pressure ratio at bearing chamber seals of an air-sealed bearing chamber | Sep 30, 2013 | Abandoned |