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] => 18498076 [patent_doc_number] => 20230220779 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2023-07-13 [patent_title] => RECOVERED-CYCLE AIRCRAFT TURBOMACHINE [patent_app_type] => utility [patent_app_number] => 18/001677 [patent_app_country] => US [patent_app_date] => 2021-06-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 3601 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -9 [patent_words_short_claim] => 147 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18001677 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/001677
RECOVERED-CYCLE AIRCRAFT TURBOMACHINE Jun 14, 2021 Pending
Array ( [id] => 18568002 [patent_doc_number] => 20230258337 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2023-08-17 [patent_title] => PRODUCTION BY ADDITIVE MANUFACTURING OF COMPLEX PARTS [patent_app_type] => utility [patent_app_number] => 18/002011 [patent_app_country] => US [patent_app_date] => 2021-06-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 3570 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -7 [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] => 18002011 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/002011
PRODUCTION BY ADDITIVE MANUFACTURING OF COMPLEX PARTS Jun 8, 2021 Pending
Array ( [id] => 17444691 [patent_doc_number] => 20220065196 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-03-03 [patent_title] => AIRCRAFT ENGINE WITH IMPROVED HANDLING OF VIBRATIONAL MODES [patent_app_type] => utility [patent_app_number] => 17/331384 [patent_app_country] => US [patent_app_date] => 2021-05-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 18368 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -18 [patent_words_short_claim] => 259 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17331384 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/331384
AIRCRAFT ENGINE WITH IMPROVED HANDLING OF VIBRATIONAL MODES May 25, 2021 Abandoned
Array ( [id] => 17891234 [patent_doc_number] => 11454193 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2022-09-27 [patent_title] => Gas turbine engine with axial movable fan variable area nozzle [patent_app_type] => utility [patent_app_number] => 17/326904 [patent_app_country] => US [patent_app_date] => 2021-05-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 12 [patent_no_of_words] => 3984 [patent_no_of_claims] => 25 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 299 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17326904 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/326904
Gas turbine engine with axial movable fan variable area nozzle May 20, 2021 Issued
Array ( [id] => 18021421 [patent_doc_number] => 20220372920 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-11-24 [patent_title] => METHOD AND SYSTEM FOR OPERATING AN ENGINE TO PREVENT HIGH POWER ENGINE SURGES [patent_app_type] => utility [patent_app_number] => 17/324404 [patent_app_country] => US [patent_app_date] => 2021-05-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 4478 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -18 [patent_words_short_claim] => 104 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17324404 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/324404
METHOD AND SYSTEM FOR OPERATING AN ENGINE TO PREVENT HIGH POWER ENGINE SURGES May 18, 2021 Pending
Array ( [id] => 17571618 [patent_doc_number] => 11319878 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2022-05-03 [patent_title] => Direct drive unit removal system and associated methods [patent_app_type] => utility [patent_app_number] => 17/204338 [patent_app_country] => US [patent_app_date] => 2021-03-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 19 [patent_figures_cnt] => 19 [patent_no_of_words] => 6904 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 191 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17204338 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/204338
Direct drive unit removal system and associated methods Mar 16, 2021 Issued
Array ( [id] => 17126910 [patent_doc_number] => 20210301679 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2021-09-30 [patent_title] => IN-FLIGHT MONITORING OF AERO ENGINE HEALTH [patent_app_type] => utility [patent_app_number] => 17/201695 [patent_app_country] => US [patent_app_date] => 2021-03-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 5879 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -13 [patent_words_short_claim] => 181 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17201695 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/201695
In-flight monitoring of aero engine health Mar 14, 2021 Issued
Array ( [id] => 17867879 [patent_doc_number] => 20220290615 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-09-15 [patent_title] => MOUNT ASSEMBLY FOR ACCESSORY GEARBOX OF AIRCRAFT ENGINE AND ASSOCIATED METHOD OF ASSEMBLY [patent_app_type] => utility [patent_app_number] => 17/200292 [patent_app_country] => US [patent_app_date] => 2021-03-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 5168 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -11 [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] => 17200292 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/200292
Mount assembly for accessory gearbox of aircraft engine and associated method of assembly Mar 11, 2021 Issued
Array ( [id] => 16932087 [patent_doc_number] => 20210197976 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2021-07-01 [patent_title] => PYLON SHAPE WITH GEARED TURBOFAN FOR STRUCTURAL STIFFNESS [patent_app_type] => utility [patent_app_number] => 17/198610 [patent_app_country] => US [patent_app_date] => 2021-03-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 2676 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -13 [patent_words_short_claim] => 60 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17198610 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/198610
PYLON SHAPE WITH GEARED TURBOFAN FOR STRUCTURAL STIFFNESS Mar 10, 2021 Abandoned
Array ( [id] => 17215217 [patent_doc_number] => 20210348555 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2021-11-11 [patent_title] => HIGH PRESSURE RATIO GAS TURBINE ENGINE [patent_app_type] => utility [patent_app_number] => 17/196345 [patent_app_country] => US [patent_app_date] => 2021-03-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 8059 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -13 [patent_words_short_claim] => 103 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17196345 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/196345
HIGH PRESSURE RATIO GAS TURBINE ENGINE Mar 8, 2021 Abandoned
Array ( [id] => 17126995 [patent_doc_number] => 20210301764 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2021-09-30 [patent_title] => GAS TURBINE ENGINE [patent_app_type] => utility [patent_app_number] => 17/196460 [patent_app_country] => US [patent_app_date] => 2021-03-09 [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] => -18 [patent_words_short_claim] => 102 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17196460 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/196460
GAS TURBINE ENGINE Mar 8, 2021 Abandoned
Array ( [id] => 16886128 [patent_doc_number] => 20210172323 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2021-06-10 [patent_title] => GAS TURBINE ENGINE WITH OPTIMIZED FAN BLADE GEOMETRY [patent_app_type] => utility [patent_app_number] => 17/181594 [patent_app_country] => US [patent_app_date] => 2021-02-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 8309 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -18 [patent_words_short_claim] => 366 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17181594 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/181594
Gas turbine engine with optimized fan blade geometry Feb 21, 2021 Issued
Array ( [id] => 18361791 [patent_doc_number] => 20230143382 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2023-05-11 [patent_title] => BYPASS TURBINE ENGINE COMPRISING AT LEAST ONE ACCESSORY OR EQUIPMENT [patent_app_type] => utility [patent_app_number] => 17/905077 [patent_app_country] => US [patent_app_date] => 2021-02-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 10236 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -14 [patent_words_short_claim] => 347 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17905077 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/905077
BYPASS TURBINE ENGINE COMPRISING AT LEAST ONE ACCESSORY OR EQUIPMENT Feb 17, 2021 Pending
Array ( [id] => 18267056 [patent_doc_number] => 20230088298 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2023-03-23 [patent_title] => FRONT FRAME AND CASCADE OF A THRUST REVERSER OF AN AIRCRAFT NACELLE [patent_app_type] => utility [patent_app_number] => 17/904572 [patent_app_country] => US [patent_app_date] => 2021-02-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 3604 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -10 [patent_words_short_claim] => 117 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17904572 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/904572
FRONT FRAME AND CASCADE OF A THRUST REVERSER OF AN AIRCRAFT NACELLE Feb 15, 2021 Pending
Array ( [id] => 16870950 [patent_doc_number] => 20210164417 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2021-06-03 [patent_title] => FAN ARRANGEMENT FOR A GAS TURBINE ENGINE [patent_app_type] => utility [patent_app_number] => 17/175092 [patent_app_country] => US [patent_app_date] => 2021-02-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 44098 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -19 [patent_words_short_claim] => 222 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17175092 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/175092
FAN ARRANGEMENT FOR A GAS TURBINE ENGINE Feb 11, 2021 Pending
Array ( [id] => 17022964 [patent_doc_number] => 20210246835 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2021-08-12 [patent_title] => HYBRID TRANSMISSION ON PROPELLER GEARBOX [patent_app_type] => utility [patent_app_number] => 17/173523 [patent_app_country] => US [patent_app_date] => 2021-02-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 9243 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -13 [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] => 17173523 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/173523
Hybrid transmission on propeller gearbox Feb 10, 2021 Issued
Array ( [id] => 17791663 [patent_doc_number] => 20220250754 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-08-11 [patent_title] => PROPULSION APPARATUS, FLYING BODY AND PROPULSION METHOD [patent_app_type] => utility [patent_app_number] => 17/628301 [patent_app_country] => US [patent_app_date] => 2021-02-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 6776 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -14 [patent_words_short_claim] => 45 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17628301 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/628301
PROPULSION APPARATUS, FLYING BODY AND PROPULSION METHOD Feb 2, 2021 Pending
Array ( [id] => 17845465 [patent_doc_number] => 11434824 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2022-09-06 [patent_title] => Fuel heater and energy conversion system [patent_app_type] => utility [patent_app_number] => 17/166245 [patent_app_country] => US [patent_app_date] => 2021-02-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 7071 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 372 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17166245 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/166245
Fuel heater and energy conversion system Feb 2, 2021 Issued
Array ( [id] => 16840269 [patent_doc_number] => 20210148281 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2021-05-20 [patent_title] => MULTILOOP GAS TURBINE, SYSTEM, AND METHOD OF OPERATION THEREOF [patent_app_type] => utility [patent_app_number] => 17/161565 [patent_app_country] => US [patent_app_date] => 2021-01-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 9472 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -20 [patent_words_short_claim] => 104 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17161565 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/161565
Multiloop gas turbine, system, and method of operation thereof Jan 27, 2021 Issued
Array ( [id] => 16825077 [patent_doc_number] => 20210140370 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2021-05-13 [patent_title] => DIRECT DRIVE UNIT REMOVAL SYSTEM AND ASSOCIATED METHODS [patent_app_type] => utility [patent_app_number] => 17/154601 [patent_app_country] => US [patent_app_date] => 2021-01-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 6748 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -10 [patent_words_short_claim] => 159 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17154601 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/154601
Direct drive unit removal system and associated methods Jan 20, 2021 Issued
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