Search

Thomas P. Burke

Examiner (ID: 9758, Phone: (571)270-5407 , Office: P/3741 )

Most Active Art Unit
3741
Art Unit(s)
3741
Total Applications
418
Issued Applications
146
Pending Applications
82
Abandoned Applications
215

Applications

Application numberTitle of the applicationFiling DateStatus
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 Pending
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] => 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 Pending
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] => 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] => 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 Pending
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] => 19770999 [patent_doc_number] => 20250052425 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2025-02-13 [patent_title] => COMBUSTOR ASSEMBLY [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] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 11012 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -15 [patent_words_short_claim] => 71 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18772375 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/772375
COMBUSTOR ASSEMBLY Jul 14, 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] => 19632132 [patent_doc_number] => 20240410581 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2024-12-12 [patent_title] => COMBUSTOR ASSEMBLY FOR A GAS TURBINE ENGINE [patent_app_type] => utility [patent_app_number] => 18/669683 [patent_app_country] => US [patent_app_date] => 2024-05-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 7085 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -18 [patent_words_short_claim] => 228 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18669683 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/669683
COMBUSTOR ASSEMBLY FOR A GAS TURBINE ENGINE May 20, 2024 Pending
Array ( [id] => 19433322 [patent_doc_number] => 20240301820 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2024-09-12 [patent_title] => MICRO GAS TURBINE DESIGNED TO LIMIT HEAT LOSSES THEREFROM [patent_app_type] => utility [patent_app_number] => 18/665680 [patent_app_country] => US [patent_app_date] => 2024-05-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 8399 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -16 [patent_words_short_claim] => 122 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18665680 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/665680
MICRO GAS TURBINE DESIGNED TO LIMIT HEAT LOSSES THEREFROM May 15, 2024 Pending
Array ( [id] => 19433322 [patent_doc_number] => 20240301820 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2024-09-12 [patent_title] => MICRO GAS TURBINE DESIGNED TO LIMIT HEAT LOSSES THEREFROM [patent_app_type] => utility [patent_app_number] => 18/665680 [patent_app_country] => US [patent_app_date] => 2024-05-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 8399 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -16 [patent_words_short_claim] => 122 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18665680 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/665680
MICRO GAS TURBINE DESIGNED TO LIMIT HEAT LOSSES THEREFROM May 15, 2024 Pending
Array ( [id] => 19657267 [patent_doc_number] => 20240424332 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2024-12-26 [patent_title] => METHOD FOR SUPPRESSION OF BATTERY HAZARDS [patent_app_type] => utility [patent_app_number] => 18/655019 [patent_app_country] => US [patent_app_date] => 2024-05-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 3495 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 38 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18655019 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/655019
METHOD FOR SUPPRESSION OF BATTERY HAZARDS May 2, 2024 Pending
Array ( [id] => 20337191 [patent_doc_number] => 20250341311 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2025-11-06 [patent_title] => FUEL NOZZLE [patent_app_type] => utility [patent_app_number] => 18/652153 [patent_app_country] => US [patent_app_date] => 2024-05-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 7473 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -15 [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] => 18652153 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/652153
FUEL NOZZLE Apr 30, 2024 Pending
Array ( [id] => 19602090 [patent_doc_number] => 20240392970 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2024-11-28 [patent_title] => COMBUSTOR APPARATUS [patent_app_type] => utility [patent_app_number] => 18/652125 [patent_app_country] => US [patent_app_date] => 2024-05-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 12700 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -7 [patent_words_short_claim] => 55 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18652125 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/652125
COMBUSTOR APPARATUS Apr 30, 2024 Pending
Array ( [id] => 19537269 [patent_doc_number] => 12129813 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2024-10-29 [patent_title] => Power plant cycle using renewable energy facilitated by a supersonic shock wave compressor apparatus [patent_app_type] => utility [patent_app_number] => 18/633815 [patent_app_country] => US [patent_app_date] => 2024-04-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 9 [patent_no_of_words] => 9488 [patent_no_of_claims] => 26 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 285 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18633815 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/633815
Power plant cycle using renewable energy facilitated by a supersonic shock wave compressor apparatus Apr 11, 2024 Issued
Array ( [id] => 20248710 [patent_doc_number] => 20250297579 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2025-09-25 [patent_title] => OPEN PUSHER ROTOR WITH REMOTE EXHAUST [patent_app_type] => utility [patent_app_number] => 18/614971 [patent_app_country] => US [patent_app_date] => 2024-03-25 [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] => -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] => 18614971 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/614971
OPEN PUSHER ROTOR WITH REMOTE EXHAUST Mar 24, 2024 Pending
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