Search

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 numberTitle of the applicationFiling DateStatus
Array ( [id] => 18323492 [patent_doc_number] => 20230121620 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2023-04-20 [patent_title] => BLEED PLENUM FOR COMPRESSOR SECTION [patent_app_type] => utility [patent_app_number] => 17/451340 [patent_app_country] => US [patent_app_date] => 2021-10-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 6792 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 115 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17451340 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/451340
Bleed plenum for compressor section Oct 18, 2021 Issued
Array ( [id] => 17579547 [patent_doc_number] => 20220136402 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-05-05 [patent_title] => ELECTRIC MACHINE ASSEMBLY FOR A TURBINE ENGINE [patent_app_type] => utility [patent_app_number] => 17/498090 [patent_app_country] => US [patent_app_date] => 2021-10-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 11982 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -19 [patent_words_short_claim] => 66 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17498090 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/498090
ELECTRIC MACHINE ASSEMBLY FOR A TURBINE ENGINE Oct 10, 2021 Pending
Array ( [id] => 17579547 [patent_doc_number] => 20220136402 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-05-05 [patent_title] => ELECTRIC MACHINE ASSEMBLY FOR A TURBINE ENGINE [patent_app_type] => utility [patent_app_number] => 17/498090 [patent_app_country] => US [patent_app_date] => 2021-10-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 11982 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -19 [patent_words_short_claim] => 66 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17498090 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/498090
ELECTRIC MACHINE ASSEMBLY FOR A TURBINE ENGINE Oct 10, 2021 Pending
Array ( [id] => 18045397 [patent_doc_number] => 11519339 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2022-12-06 [patent_title] => System and methods for controlling surge margin in the compressor section of a gas turbine engine [patent_app_type] => utility [patent_app_number] => 17/494339 [patent_app_country] => US [patent_app_date] => 2021-10-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 6122 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 312 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17494339 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/494339
System and methods for controlling surge margin in the compressor section of a gas turbine engine Oct 4, 2021 Issued
Array ( [id] => 17705382 [patent_doc_number] => 20220205388 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-06-30 [patent_title] => AIRCRAFT [patent_app_type] => utility [patent_app_number] => 17/494537 [patent_app_country] => US [patent_app_date] => 2021-10-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 9829 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -5 [patent_words_short_claim] => 143 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17494537 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/494537
AIRCRAFT Oct 4, 2021 Pending
Array ( [id] => 18710147 [patent_doc_number] => 20230332771 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2023-10-19 [patent_title] => GAS TURBINE COMBUSTOR AND GAS TURBINE [patent_app_type] => utility [patent_app_number] => 18/027182 [patent_app_country] => US [patent_app_date] => 2021-10-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 6985 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -6 [patent_words_short_claim] => 112 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18027182 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/027182
GAS TURBINE COMBUSTOR AND GAS TURBINE Oct 4, 2021 Pending
Array ( [id] => 18676132 [patent_doc_number] => 20230313757 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2023-10-05 [patent_title] => PULSE DETONATION JET ENGINE [patent_app_type] => utility [patent_app_number] => 17/794196 [patent_app_country] => US [patent_app_date] => 2021-10-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 6070 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -19 [patent_words_short_claim] => 184 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17794196 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/794196
PULSE DETONATION JET ENGINE Sep 30, 2021 Pending
Array ( [id] => 18862746 [patent_doc_number] => 20230417182 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2023-12-28 [patent_title] => AIR INLET OF A TURBOMACHINE NACELLE INCLUDING A CIRCULATION CONDUIT OF A HOT AIR FLOW BETWEEN A MOVABLE UPSTREAM PART AND A FIXED DOWNSTREAM PART [patent_app_type] => utility [patent_app_number] => 18/247852 [patent_app_country] => US [patent_app_date] => 2021-10-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 3561 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -10 [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] => 18247852 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/247852
AIR INLET OF A TURBOMACHINE NACELLE INCLUDING A CIRCULATION CONDUIT OF A HOT AIR FLOW BETWEEN A MOVABLE UPSTREAM PART AND A FIXED DOWNSTREAM PART Sep 30, 2021 Pending
Array ( [id] => 18280251 [patent_doc_number] => 20230095723 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2023-03-30 [patent_title] => TURBINE ENGINE WITH VARIABLE PITCH FAN [patent_app_type] => utility [patent_app_number] => 17/484416 [patent_app_country] => US [patent_app_date] => 2021-09-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 6675 [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] => 17484416 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/484416
TURBINE ENGINE WITH VARIABLE PITCH FAN Sep 23, 2021 Abandoned
Array ( [id] => 18029429 [patent_doc_number] => 11512606 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2022-11-29 [patent_title] => Micro-turbine generator multi-stage turbine with interstage catalytic converter [patent_app_type] => utility [patent_app_number] => 17/472258 [patent_app_country] => US [patent_app_date] => 2021-09-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 7206 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 173 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17472258 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/472258
Micro-turbine generator multi-stage turbine with interstage catalytic converter Sep 9, 2021 Issued
Array ( [id] => 18629188 [patent_doc_number] => 20230288068 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2023-09-14 [patent_title] => PERFORATED PLATE FOR GAS TURBINE COMBUSTOR, GAS TURBINE COMBUSTOR, AND GAS TURBINE [patent_app_type] => utility [patent_app_number] => 18/020155 [patent_app_country] => US [patent_app_date] => 2021-08-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 9736 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -12 [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] => 18020155 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/020155
PERFORATED PLATE FOR GAS TURBINE COMBUSTOR, GAS TURBINE COMBUSTOR, AND GAS TURBINE Aug 30, 2021 Pending
Array ( [id] => 18230674 [patent_doc_number] => 20230069668 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2023-03-02 [patent_title] => SYSTEM AND METHOD FOR CONTROLLING FUEL FLOW TO AN AIRCRAFT ENGINE DURING START [patent_app_type] => utility [patent_app_number] => 17/461557 [patent_app_country] => US [patent_app_date] => 2021-08-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 7351 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -18 [patent_words_short_claim] => 246 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17461557 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/461557
System and method for controlling fuel flow to an aircraft engine during start Aug 29, 2021 Issued
Array ( [id] => 17845473 [patent_doc_number] => 11434832 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2022-09-06 [patent_title] => Geared gas turbine engine [patent_app_type] => utility [patent_app_number] => 17/411617 [patent_app_country] => US [patent_app_date] => 2021-08-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 6 [patent_no_of_words] => 7742 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 281 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17411617 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/411617
Geared gas turbine engine Aug 24, 2021 Issued
Array ( [id] => 18620993 [patent_doc_number] => 11754021 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2023-09-12 [patent_title] => Propulsion systems for aircraft [patent_app_type] => utility [patent_app_number] => 17/407880 [patent_app_country] => US [patent_app_date] => 2021-08-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 6474 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 209 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17407880 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/407880
Propulsion systems for aircraft Aug 19, 2021 Issued
Array ( [id] => 18429184 [patent_doc_number] => 11674396 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2023-06-13 [patent_title] => Cooling air delivery assembly [patent_app_type] => utility [patent_app_number] => 17/389503 [patent_app_country] => US [patent_app_date] => 2021-07-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 8 [patent_no_of_words] => 9104 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 170 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17389503 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/389503
Cooling air delivery assembly Jul 29, 2021 Issued
Array ( [id] => 18148080 [patent_doc_number] => 20230021937 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2023-01-26 [patent_title] => ELECTRIC MACHINE POWER ASSIST OF TURBINE ENGINE DURING IDLE OPERATION [patent_app_type] => utility [patent_app_number] => 17/380524 [patent_app_country] => US [patent_app_date] => 2021-07-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 16038 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 85 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17380524 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/380524
ELECTRIC MACHINE POWER ASSIST OF TURBINE ENGINE DURING IDLE OPERATION Jul 19, 2021 Pending
Array ( [id] => 18142086 [patent_doc_number] => 20230015930 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2023-01-19 [patent_title] => MULTI-FUEL ENGINE FOR AN AIRCRAFT [patent_app_type] => utility [patent_app_number] => 17/379532 [patent_app_country] => US [patent_app_date] => 2021-07-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 6438 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 64 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17379532 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/379532
MULTI-FUEL ENGINE FOR AN AIRCRAFT Jul 18, 2021 Pending
Array ( [id] => 18764579 [patent_doc_number] => 11814968 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2023-11-14 [patent_title] => Gas turbine engine with idle thrust ratio [patent_app_type] => utility [patent_app_number] => 17/379202 [patent_app_country] => US [patent_app_date] => 2021-07-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 6467 [patent_no_of_claims] => 22 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 324 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17379202 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/379202
Gas turbine engine with idle thrust ratio Jul 18, 2021 Issued
Array ( [id] => 18948614 [patent_doc_number] => 11891899 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2024-02-06 [patent_title] => Dual engine system [patent_app_type] => utility [patent_app_number] => 17/371989 [patent_app_country] => US [patent_app_date] => 2021-07-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 4820 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 174 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17371989 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/371989
Dual engine system Jul 8, 2021 Issued
Array ( [id] => 18552951 [patent_doc_number] => 20230250962 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2023-08-10 [patent_title] => ANNULAR COMBUSTION CHAMBER FOR AN AIRCRAFT TURBOMACHINE [patent_app_type] => utility [patent_app_number] => 18/014326 [patent_app_country] => US [patent_app_date] => 2021-07-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 4406 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -5 [patent_words_short_claim] => 237 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18014326 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/014326
ANNULAR COMBUSTION CHAMBER FOR AN AIRCRAFT TURBOMACHINE Jul 1, 2021 Pending
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