
Thomas P. Burke
Examiner (ID: 12894, Phone: (571)270-5407 , Office: P/3741 )
| Most Active Art Unit | 3741 |
| Art Unit(s) | 3741 |
| Total Applications | 448 |
| Issued Applications | 159 |
| Pending Applications | 79 |
| Abandoned Applications | 221 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 20407821
[patent_doc_number] => 20250376930
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2025-12-11
[patent_title] => Turbine Engine Centerbody Generator
[patent_app_type] => utility
[patent_app_number] => 19/297470
[patent_app_country] => US
[patent_app_date] => 2025-08-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 0
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -17
[patent_words_short_claim] => 65
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 19297470
[rel_patent_id] =>[rel_patent_doc_number] =>) 19/297470 | Turbine Engine Centerbody Generator | Aug 11, 2025 | Pending |
Array
(
[id] => 20348894
[patent_doc_number] => 20250345746
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2025-11-13
[patent_title] => EXHAUST GAS PROCESSING EQUIPMENT AND GAS TURBINE PLANT
[patent_app_type] => utility
[patent_app_number] => 19/275231
[patent_app_country] => US
[patent_app_date] => 2025-07-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 3591
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -34
[patent_words_short_claim] => 110
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 19275231
[rel_patent_id] =>[rel_patent_doc_number] =>) 19/275231 | EXHAUST GAS PROCESSING EQUIPMENT AND GAS TURBINE PLANT | Jul 20, 2025 | Pending |
Array
(
[id] => 20100995
[patent_doc_number] => 20250230931
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2025-07-17
[patent_title] => COMBUSTOR ASSEMBLY FOR A GAS TURBINE ENGINE
[patent_app_type] => utility
[patent_app_number] => 19/061269
[patent_app_country] => US
[patent_app_date] => 2025-02-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 2207
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -18
[patent_words_short_claim] => 221
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 19061269
[rel_patent_id] =>[rel_patent_doc_number] =>) 19/061269 | Combustor assembly for a gas turbine engine | Feb 23, 2025 | Issued |
Array
(
[id] => 20033869
[patent_doc_number] => 20250172091
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2025-05-29
[patent_title] => SYSTEM FOR PURGING A FUEL HAVING REACTIVE GAS
[patent_app_type] => utility
[patent_app_number] => 19/036602
[patent_app_country] => US
[patent_app_date] => 2025-01-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 0
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -8
[patent_words_short_claim] => 2
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 19036602
[rel_patent_id] =>[rel_patent_doc_number] =>) 19/036602 | SYSTEM FOR PURGING A FUEL HAVING REACTIVE GAS | Jan 23, 2025 | Pending |
Array
(
[id] => 20025601
[patent_doc_number] => 20250163823
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2025-05-22
[patent_title] => HYBRID GAS TURBOFAN POWERED SUB-IDLE DESCENT MODE
[patent_app_type] => utility
[patent_app_number] => 19/033023
[patent_app_country] => US
[patent_app_date] => 2025-01-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 0
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -15
[patent_words_short_claim] => 93
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 19033023
[rel_patent_id] =>[rel_patent_doc_number] =>) 19/033023 | HYBRID GAS TURBOFAN POWERED SUB-IDLE DESCENT MODE | Jan 20, 2025 | Pending |
Array
(
[id] => 20284486
[patent_doc_number] => 20250309728
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2025-10-02
[patent_title] => METHOD AND SYSTEM FOR RAPID STARTING OF A COMBUSTION ENGINE IN A MULTI-ENGINE AIRCRAFT
[patent_app_type] => utility
[patent_app_number] => 19/002420
[patent_app_country] => US
[patent_app_date] => 2024-12-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 3118
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -13
[patent_words_short_claim] => 305
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 19002420
[rel_patent_id] =>[rel_patent_doc_number] =>) 19/002420 | METHOD AND SYSTEM FOR RAPID STARTING OF A COMBUSTION ENGINE IN A MULTI-ENGINE AIRCRAFT | Dec 25, 2024 | Issued |
Array
(
[id] => 20069320
[patent_doc_number] => 20250207542
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2025-06-26
[patent_title] => ACOUSTIC ENGINE EXHAUST CENTER BODY WITH TAPERED INNER SKIN
[patent_app_type] => utility
[patent_app_number] => 18/999974
[patent_app_country] => US
[patent_app_date] => 2024-12-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 1077
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -17
[patent_words_short_claim] => 149
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18999974
[rel_patent_id] =>[rel_patent_doc_number] =>) 18/999974 | ACOUSTIC ENGINE EXHAUST CENTER BODY WITH TAPERED INNER SKIN | Dec 22, 2024 | Pending |
Array
(
[id] => 20337192
[patent_doc_number] => 20250341312
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2025-11-06
[patent_title] => DESIGN METHOD FOR AXIAL MULTI-STAGE COMBUSTOR AND AXIAL MULTI-STAGE COMBUSTOR APPLYING THE SAME METHOD
[patent_app_type] => utility
[patent_app_number] => 18/965510
[patent_app_country] => US
[patent_app_date] => 2024-12-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 0
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -8
[patent_words_short_claim] => 107
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18965510
[rel_patent_id] =>[rel_patent_doc_number] =>) 18/965510 | DESIGN METHOD FOR AXIAL MULTI-STAGE COMBUSTOR AND AXIAL MULTI-STAGE COMBUSTOR APPLYING THE SAME METHOD | Dec 1, 2024 | Abandoned |
Array
(
[id] => 20652153
[patent_doc_number] => 20260104167
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2026-04-16
[patent_title] => GAS TURBINE ENGINE
[patent_app_type] => utility
[patent_app_number] => 18/907952
[patent_app_country] => US
[patent_app_date] => 2024-10-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 2409
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -6
[patent_words_short_claim] => 183
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18907952
[rel_patent_id] =>[rel_patent_doc_number] =>) 18/907952 | GAS TURBINE ENGINE | Oct 6, 2024 | Pending |
Array
(
[id] => 20640124
[patent_doc_number] => 20260098477
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2026-04-09
[patent_title] => Improved Gas Turbine Engine
[patent_app_type] => utility
[patent_app_number] => 18/907918
[patent_app_country] => US
[patent_app_date] => 2024-10-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 3841
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -9
[patent_words_short_claim] => 231
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18907918
[rel_patent_id] =>[rel_patent_doc_number] =>) 18/907918 | Improved Gas Turbine Engine | Oct 6, 2024 | Pending |
Array
(
[id] => 20628294
[patent_doc_number] => 20260092578
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2026-04-02
[patent_title] => AIRCRAFT POWERPLANT EXHAUST SECTION WITH FLOW DIVERTER
[patent_app_type] => utility
[patent_app_number] => 18/899904
[patent_app_country] => US
[patent_app_date] => 2024-09-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 3264
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -18
[patent_words_short_claim] => 2
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18899904
[rel_patent_id] =>[rel_patent_doc_number] =>) 18/899904 | AIRCRAFT POWERPLANT EXHAUST SECTION WITH FLOW DIVERTER | Sep 26, 2024 | Pending |
Array
(
[id] => 20585973
[patent_doc_number] => 20260071565
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2026-03-12
[patent_title] => HOT SCR TEMPERING AIR SYSTEM FOR GAS TURBINE PART LOAD EFFICIENCY AND EXTENDED TURNDOWN
[patent_app_type] => utility
[patent_app_number] => 18/826523
[patent_app_country] => US
[patent_app_date] => 2024-09-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 0
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -17
[patent_words_short_claim] => 75
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18826523
[rel_patent_id] =>[rel_patent_doc_number] =>) 18/826523 | HOT SCR TEMPERING AIR SYSTEM FOR GAS TURBINE PART LOAD EFFICIENCY AND EXTENDED TURNDOWN | Sep 5, 2024 | Pending |
Array
(
[id] => 20486471
[patent_doc_number] => 20260022669
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2026-01-22
[patent_title] => Accessory Gearbox with Accessories with a Stacked Configuration
[patent_app_type] => utility
[patent_app_number] => 18/779286
[patent_app_country] => US
[patent_app_date] => 2024-07-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 0
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -17
[patent_words_short_claim] => 78
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18779286
[rel_patent_id] =>[rel_patent_doc_number] =>) 18/779286 | Accessory Gearbox with Accessories with a Stacked Configuration | Jul 21, 2024 | Pending |
Array
(
[id] => 19557433
[patent_doc_number] => 20240369225
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2024-11-07
[patent_title] => INJECTION NOZZLE AND COMBUSTION DEVICE
[patent_app_type] => utility
[patent_app_number] => 18/776600
[patent_app_country] => US
[patent_app_date] => 2024-07-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 6153
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -5
[patent_words_short_claim] => 65
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18776600
[rel_patent_id] =>[rel_patent_doc_number] =>) 18/776600 | INJECTION NOZZLE AND COMBUSTION DEVICE | Jul 17, 2024 | Abandoned |
Array
(
[id] => 19724898
[patent_doc_number] => 20250027649
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2025-01-23
[patent_title] => STAGED BLADE INJECTOR
[patent_app_type] => utility
[patent_app_number] => 18/774437
[patent_app_country] => US
[patent_app_date] => 2024-07-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 4951
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -18
[patent_words_short_claim] => 67
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18774437
[rel_patent_id] =>[rel_patent_doc_number] =>) 18/774437 | STAGED BLADE INJECTOR | Jul 15, 2024 | Pending |
Array
(
[id] => 19977739
[patent_doc_number] => 12345206
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2025-07-01
[patent_title] => Propulsion assembly for an aircraft
[patent_app_type] => utility
[patent_app_number] => 18/772636
[patent_app_country] => US
[patent_app_date] => 2024-07-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 3
[patent_no_of_words] => 0
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 201
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18772636
[rel_patent_id] =>[rel_patent_doc_number] =>) 18/772636 | Propulsion assembly for an aircraft | Jul 14, 2024 | Issued |
Array
(
[id] => 20453762
[patent_doc_number] => 12516814
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2026-01-06
[patent_title] => Combustor assembly with fastened combustor liner and head
[patent_app_type] => utility
[patent_app_number] => 18/772375
[patent_app_country] => US
[patent_app_date] => 2024-07-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 9
[patent_no_of_words] => 4530
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 190
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18772375
[rel_patent_id] =>[rel_patent_doc_number] =>) 18/772375 | Combustor assembly with fastened combustor liner and head | Jul 14, 2024 | Issued |
Array
(
[id] => 20473750
[patent_doc_number] => 20260015969
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2026-01-15
[patent_title] => FUEL CELL EXHAUST CONDENSATION WITH TURBOMACHINERY WATER AUGMENTATION USING CRYOGENIC BOTTOMING CYCLE
[patent_app_type] => utility
[patent_app_number] => 18/770950
[patent_app_country] => US
[patent_app_date] => 2024-07-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 0
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -12
[patent_words_short_claim] => 2
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18770950
[rel_patent_id] =>[rel_patent_doc_number] =>) 18/770950 | FUEL CELL EXHAUST CONDENSATION WITH TURBOMACHINERY WATER AUGMENTATION USING CRYOGENIC BOTTOMING CYCLE | Jul 11, 2024 | Pending |
Array
(
[id] => 19955701
[patent_doc_number] => 12326110
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2025-06-10
[patent_title] => Systems and methods of generating power using a hydrogen fuel system
[patent_app_type] => utility
[patent_app_number] => 18/738326
[patent_app_country] => US
[patent_app_date] => 2024-06-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2298
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 348
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18738326
[rel_patent_id] =>[rel_patent_doc_number] =>) 18/738326 | Systems and methods of generating power using a hydrogen fuel system | Jun 9, 2024 | Issued |
Array
(
[id] => 20407847
[patent_doc_number] => 20250376956
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2025-12-11
[patent_title] => SYSTEM AND METHOD FOR BLENDING MULTIPLE FUELS
[patent_app_type] => utility
[patent_app_number] => 18/734378
[patent_app_country] => US
[patent_app_date] => 2024-06-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 6847
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -16
[patent_words_short_claim] => 2
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18734378
[rel_patent_id] =>[rel_patent_doc_number] =>) 18/734378 | SYSTEM AND METHOD FOR BLENDING MULTIPLE FUELS | Jun 4, 2024 | Abandoned |