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] => 17105230
[patent_doc_number] => 11125435
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[patent_kind] => B2
[patent_issue_date] => 2021-09-21
[patent_title] => Bent combustion chamber from a turbine engine
[patent_app_type] => utility
[patent_app_number] => 15/742447
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Array
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[patent_kind] => A1
[patent_issue_date] => 2016-10-20
[patent_title] => 'AFTERBURNER AND AIRCRAFT ENGINE'
[patent_app_type] => utility
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Array
(
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[patent_issue_date] => 2019-02-05
[patent_title] => Afterburner and aircraft engine
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Array
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[patent_issue_date] => 2020-07-21
[patent_title] => Fuel injection locations based on combustor flow path
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Array
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[patent_kind] => A1
[patent_issue_date] => 2017-12-28
[patent_title] => SYSTEM AND METHOD OF COOLING A TURBINE ENGINE
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Array
(
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[patent_doc_number] => 20170363295
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[patent_issue_date] => 2017-12-21
[patent_title] => SMALL EXIT DUCT FOR A REVERSE FLOW COMBUSTOR WITH INTEGRATED COOLING ELEMENTS
[patent_app_type] => utility
[patent_app_number] => 15/185317
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Array
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[patent_doc_number] => 20180195723
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[patent_issue_date] => 2018-07-12
[patent_title] => BURNER FOR A GAS TURBINE
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/742151 | Burner for a gas turbine | Jun 9, 2016 | Issued |
Array
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[id] => 11743629
[patent_doc_number] => 20170197701
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[patent_issue_date] => 2017-07-13
[patent_title] => 'COOLING OF AEROSPACE FLIGHT SYSTEMS'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/168812 | COOLING OF AEROSPACE FLIGHT SYSTEMS | May 30, 2016 | Abandoned |
Array
(
[id] => 12981952
[patent_doc_number] => 20170342903
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[patent_kind] => A1
[patent_issue_date] => 2017-11-30
[patent_title] => SYSTEM AND METHOD OF COMPRESSOR INLET TEMPERATURE CONTROL WITH MIXING CHAMBER
[patent_app_type] => utility
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/167328 | System and method of compressor inlet temperature control with mixing chamber | May 26, 2016 | Issued |
Array
(
[id] => 14007241
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[patent_title] => Ducting arrangement with injector assemblies arranged in an expanding cross-sectional area of a downstream combustion stage in a gas turbine engine
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[patent_app_number] => 15/165195
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/165195 | Ducting arrangement with injector assemblies arranged in an expanding cross-sectional area of a downstream combustion stage in a gas turbine engine | May 25, 2016 | Issued |
Array
(
[id] => 12981784
[patent_doc_number] => 20170342839
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[patent_title] => SYSTEM FOR A LOW SWIRL LOW PRESSURE TURBINE
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/164648 | SYSTEM FOR A LOW SWIRL LOW PRESSURE TURBINE | May 24, 2016 | Abandoned |
Array
(
[id] => 14666219
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[patent_issue_date] => 2019-08-06
[patent_title] => Aircraft vapour trail control system
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Array
(
[id] => 16941906
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[patent_title] => Gas turbine fuel nozzle with integrated flame ionization sensor and gas turbine engine
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Array
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[patent_title] => Shaped cooling passages for turbine blade outer air seal
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Array
(
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[patent_title] => System and method for an integral drive engine with a forward main gearbox
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Array
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[patent_title] => 'METHOD AND APPARATUS FOR OPERATING A COMBUSTION DEVICE'
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Array
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Array
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