Branon C Painter
Examiner (ID: 12107)
Most Active Art Unit | 3635 |
Art Unit(s) | 3635, 3633 |
Total Applications | 434 |
Issued Applications | 192 |
Pending Applications | 4 |
Abandoned Applications | 237 |
Applications
Application number | Title of the application | Filing Date | Status |
---|---|---|---|
Array
(
[id] => 17193682
[patent_doc_number] => 11162428
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2021-11-02
[patent_title] => Method of starting a gas turbine engine
[patent_app_type] => utility
[patent_app_number] => 15/845082
[patent_app_country] => US
[patent_app_date] => 2017-12-18
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15845082
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/845082 | Method of starting a gas turbine engine | Dec 17, 2017 | Issued |
Array
(
[id] => 12608160
[patent_doc_number] => 20180094550
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2018-04-05
[patent_title] => PART LOAD OPERATION OF LIQUID AIR POWER AND STORAGE SYSTEM
[patent_app_type] => utility
[patent_app_number] => 15/820292
[patent_app_country] => US
[patent_app_date] => 2017-11-21
[patent_effective_date] => 0000-00-00
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/820292 | Part load operation of liquid air power and storage system | Nov 20, 2017 | Issued |
Array
(
[id] => 12608139
[patent_doc_number] => 20180094543
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2018-04-05
[patent_title] => INSERT APPARATUS AND SYSTEM FOR OIL NOZZLE BOUNDARY LAYER INJECTION
[patent_app_type] => utility
[patent_app_number] => 15/721986
[patent_app_country] => US
[patent_app_date] => 2017-10-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/721986 | INSERT APPARATUS AND SYSTEM FOR OIL NOZZLE BOUNDARY LAYER INJECTION | Oct 1, 2017 | Abandoned |
Array
(
[id] => 16407664
[patent_doc_number] => 10816210
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2020-10-27
[patent_title] => Premixed fuel nozzle
[patent_app_type] => utility
[patent_app_number] => 15/718077
[patent_app_country] => US
[patent_app_date] => 2017-09-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15718077
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/718077 | Premixed fuel nozzle | Sep 27, 2017 | Issued |
Array
(
[id] => 12261458
[patent_doc_number] => 20180080653
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2018-03-22
[patent_title] => 'BURNER ASSEMBLY FOR A BURNER OF A GAS TURBINE'
[patent_app_type] => utility
[patent_app_number] => 15/710093
[patent_app_country] => US
[patent_app_date] => 2017-09-20
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15710093
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/710093 | Burner assembly for a burner of a gas turbine | Sep 19, 2017 | Issued |
Array
(
[id] => 17453590
[patent_doc_number] => 11268438
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2022-03-08
[patent_title] => Combustor liner dilution opening
[patent_app_type] => utility
[patent_app_number] => 15/705314
[patent_app_country] => US
[patent_app_date] => 2017-09-15
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15705314
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/705314 | Combustor liner dilution opening | Sep 14, 2017 | Issued |
Array
(
[id] => 16407665
[patent_doc_number] => 10816211
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2020-10-27
[patent_title] => Axially staged rich quench lean combustion system
[patent_app_type] => utility
[patent_app_number] => 15/686533
[patent_app_country] => US
[patent_app_date] => 2017-08-25
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15686533
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/686533 | Axially staged rich quench lean combustion system | Aug 24, 2017 | Issued |
Array
(
[id] => 13989183
[patent_doc_number] => 20190063749
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2019-02-28
[patent_title] => COMBUSTOR PANEL COOLING ARRANGEMENTS
[patent_app_type] => utility
[patent_app_number] => 15/683965
[patent_app_country] => US
[patent_app_date] => 2017-08-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
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[patent_no_of_words] => 7688
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15683965
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/683965 | Combustor panel cooling arrangements | Aug 22, 2017 | Issued |
Array
(
[id] => 18135349
[patent_doc_number] => 11561008
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2023-01-24
[patent_title] => Fuel nozzle assembly for high fuel/air ratio and reduced combustion dynamics
[patent_app_type] => utility
[patent_app_number] => 15/684083
[patent_app_country] => US
[patent_app_date] => 2017-08-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15684083
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/684083 | Fuel nozzle assembly for high fuel/air ratio and reduced combustion dynamics | Aug 22, 2017 | Issued |
Array
(
[id] => 16445451
[patent_doc_number] => 10837369
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2020-11-17
[patent_title] => Igniter assembly for a gas turbine combustor
[patent_app_type] => utility
[patent_app_number] => 15/684546
[patent_app_country] => US
[patent_app_date] => 2017-08-23
[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] => 15684546
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/684546 | Igniter assembly for a gas turbine combustor | Aug 22, 2017 | Issued |
Array
(
[id] => 13988329
[patent_doc_number] => 20190063322
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2019-02-28
[patent_title] => HYBRID FLOATWALL COOLING FEATURE
[patent_app_type] => utility
[patent_app_number] => 15/682887
[patent_app_country] => US
[patent_app_date] => 2017-08-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15682887
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/682887 | HYBRID FLOATWALL COOLING FEATURE | Aug 21, 2017 | Abandoned |
Array
(
[id] => 13959529
[patent_doc_number] => 20190056108
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2019-02-21
[patent_title] => NON-UNIFORM MIXER FOR COMBUSTION DYNAMICS ATTENUATION
[patent_app_type] => utility
[patent_app_number] => 15/681851
[patent_app_country] => US
[patent_app_date] => 2017-08-21
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15681851
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/681851 | NON-UNIFORM MIXER FOR COMBUSTION DYNAMICS ATTENUATION | Aug 20, 2017 | Abandoned |
Array
(
[id] => 16336971
[patent_doc_number] => 10787918
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2020-09-29
[patent_title] => Gas turbine transition duct
[patent_app_type] => utility
[patent_app_number] => 15/680378
[patent_app_country] => US
[patent_app_date] => 2017-08-18
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15680378
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/680378 | Gas turbine transition duct | Aug 17, 2017 | Issued |
Array
(
[id] => 13959091
[patent_doc_number] => 20190055889
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2019-02-21
[patent_title] => DUCTED ENGINE COMPRESSOR BLEED VALVE ARCHITECTURE
[patent_app_type] => utility
[patent_app_number] => 15/679808
[patent_app_country] => US
[patent_app_date] => 2017-08-17
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15679808
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/679808 | DUCTED ENGINE COMPRESSOR BLEED VALVE ARCHITECTURE | Aug 16, 2017 | Abandoned |
Array
(
[id] => 18052203
[patent_doc_number] => 11525578
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2022-12-13
[patent_title] => Dynamics-mitigating adapter for bundled tube fuel nozzle
[patent_app_type] => utility
[patent_app_number] => 15/678263
[patent_app_country] => US
[patent_app_date] => 2017-08-16
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/678263 | Dynamics-mitigating adapter for bundled tube fuel nozzle | Aug 15, 2017 | Issued |
Array
(
[id] => 13931195
[patent_doc_number] => 20190049113
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2019-02-14
[patent_title] => PURGE COOLING STRUCTURE FOR COMBUSTOR ASSEMBLY
[patent_app_type] => utility
[patent_app_number] => 15/673882
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/673882 | Purge cooling structure for combustor assembly | Aug 9, 2017 | Issued |
Array
(
[id] => 16043823
[patent_doc_number] => 10683775
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2020-06-16
[patent_title] => Gas shielding arrangements for gas turbine engines
[patent_app_type] => utility
[patent_app_number] => 15/671813
[patent_app_country] => US
[patent_app_date] => 2017-08-08
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/671813 | Gas shielding arrangements for gas turbine engines | Aug 7, 2017 | Issued |
Array
(
[id] => 12179345
[patent_doc_number] => 20180038280
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2018-02-08
[patent_title] => 'TURBOMACHINE COMPRISING A HEAT MANAGEMENT SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 15/667873
[patent_app_country] => US
[patent_app_date] => 2017-08-03
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/667873 | TURBOMACHINE COMPRISING A HEAT MANAGEMENT SYSTEM | Aug 2, 2017 | Abandoned |
Array
(
[id] => 13903111
[patent_doc_number] => 20190040760
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2019-02-07
[patent_title] => REINFORCED OXIDE-OXIDE CERAMIC MATRIX COMPOSITE (CMC) COMPONENT AND METHOD OF MAKING A REINFORCED OXIDE-OXIDE CMC COMPONENT
[patent_app_type] => utility
[patent_app_number] => 15/667995
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/667995 | Reinforced oxide-oxide ceramic matrix composite (CMC) component and method of making a reinforced oxide-oxide CMC component | Aug 2, 2017 | Issued |
Array
(
[id] => 13903183
[patent_doc_number] => 20190040796
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2019-02-07
[patent_title] => GAS TURBINE ENGINE COOLING ARRANGEMENT
[patent_app_type] => utility
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/668135 | GAS TURBINE ENGINE COOLING ARRANGEMENT | Aug 2, 2017 | Abandoned |