Search

Tae Jun Kim

Examiner (ID: 10360, Phone: (571)272-4829 , Office: P/3741 )

Most Active Art Unit
3746
Art Unit(s)
3799, 3746, 2899, 3403, 3741
Total Applications
2114
Issued Applications
1494
Pending Applications
167
Abandoned Applications
484

Applications

Application numberTitle of the applicationFiling DateStatus
Array ( [id] => 19433326 [patent_doc_number] => 20240301824 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2024-09-12 [patent_title] => SYSTEM FOR GENERATING CAVITATION INCLUDING CANTILEVERED BEARING CONFIGURATION [patent_app_type] => utility [patent_app_number] => 18/667587 [patent_app_country] => US [patent_app_date] => 2024-05-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 6659 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -18 [patent_words_short_claim] => 124 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18667587 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/667587
SYSTEM FOR GENERATING CAVITATION INCLUDING CANTILEVERED BEARING CONFIGURATION May 16, 2024 Pending
Array ( [id] => 20364703 [patent_doc_number] => 20250354515 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2025-11-20 [patent_title] => Turbine Engine Having a Damper [patent_app_type] => utility [patent_app_number] => 18/664933 [patent_app_country] => US [patent_app_date] => 2024-05-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 2163 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -19 [patent_words_short_claim] => 160 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18664933 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/664933
Turbine Engine Having a Damper May 14, 2024 Pending
Array ( [id] => 20364703 [patent_doc_number] => 20250354515 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2025-11-20 [patent_title] => Turbine Engine Having a Damper [patent_app_type] => utility [patent_app_number] => 18/664933 [patent_app_country] => US [patent_app_date] => 2024-05-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 2163 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -19 [patent_words_short_claim] => 160 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18664933 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/664933
Turbine Engine Having a Damper May 14, 2024 Pending
Array ( [id] => 20337070 [patent_doc_number] => 20250341190 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2025-11-06 [patent_title] => PARTIAL-ADMISSION TURBINE ASSEMBLY FOR AN AIRCRAFT AND METHOD FOR CONTROLLING SAME [patent_app_type] => utility [patent_app_number] => 18/654335 [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] => 4463 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 146 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18654335 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/654335
PARTIAL-ADMISSION TURBINE ASSEMBLY FOR AN AIRCRAFT AND METHOD FOR CONTROLLING SAME May 2, 2024 Pending
Array ( [id] => 20337070 [patent_doc_number] => 20250341190 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2025-11-06 [patent_title] => PARTIAL-ADMISSION TURBINE ASSEMBLY FOR AN AIRCRAFT AND METHOD FOR CONTROLLING SAME [patent_app_type] => utility [patent_app_number] => 18/654335 [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] => 4463 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 146 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18654335 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/654335
PARTIAL-ADMISSION TURBINE ASSEMBLY FOR AN AIRCRAFT AND METHOD FOR CONTROLLING SAME May 2, 2024 Pending
Array ( [id] => 19556018 [patent_doc_number] => 20240367810 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2024-11-07 [patent_title] => AIRCRAFT COMPRISING AT LEAST ONE FLUID SUPPLY CIRCUIT EQUIPPED WITH AT LEAST ONE SHUTTER WITH AUTOMATIC CLOSURE [patent_app_type] => utility [patent_app_number] => 18/653407 [patent_app_country] => US [patent_app_date] => 2024-05-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 2877 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -5 [patent_words_short_claim] => 433 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18653407 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/653407
AIRCRAFT COMPRISING AT LEAST ONE FLUID SUPPLY CIRCUIT EQUIPPED WITH AT LEAST ONE SHUTTER WITH AUTOMATIC CLOSURE May 1, 2024 Pending
Array ( [id] => 19404441 [patent_doc_number] => 20240287952 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2024-08-29 [patent_title] => ENGINE WITH ROTATING DETONATION COMBUSTION SYSTEM [patent_app_type] => utility [patent_app_number] => 18/643376 [patent_app_country] => US [patent_app_date] => 2024-04-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 9119 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -19 [patent_words_short_claim] => 317 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18643376 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/643376
ENGINE WITH ROTATING DETONATION COMBUSTION SYSTEM Apr 22, 2024 Pending
Array ( [id] => 20309797 [patent_doc_number] => 20250327426 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2025-10-23 [patent_title] => MONITORING FUEL PHASE IN AIRCRAFT POWERPLANT FUEL SYSTEM [patent_app_type] => utility [patent_app_number] => 18/640938 [patent_app_country] => US [patent_app_date] => 2024-04-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 2286 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 194 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18640938 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/640938
MONITORING FUEL PHASE IN AIRCRAFT POWERPLANT FUEL SYSTEM Apr 18, 2024 Pending
Array ( [id] => 20093988 [patent_doc_number] => 20250223924 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2025-07-10 [patent_title] => CRYOGENIC FUELLED AIRCRAFT PROPULSION SYSTEM [patent_app_type] => utility [patent_app_number] => 18/631539 [patent_app_country] => US [patent_app_date] => 2024-04-10 [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] => 64 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18631539 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/631539
CRYOGENIC FUELLED AIRCRAFT PROPULSION SYSTEM Apr 9, 2024 Pending
Array ( [id] => 20093988 [patent_doc_number] => 20250223924 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2025-07-10 [patent_title] => CRYOGENIC FUELLED AIRCRAFT PROPULSION SYSTEM [patent_app_type] => utility [patent_app_number] => 18/631539 [patent_app_country] => US [patent_app_date] => 2024-04-10 [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] => 64 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18631539 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/631539
CRYOGENIC FUELLED AIRCRAFT PROPULSION SYSTEM Apr 9, 2024 Pending
Array ( [id] => 20288959 [patent_doc_number] => 20250314202 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2025-10-09 [patent_title] => TAILORING AIRCRAFT POWERPLANT FLOW PARAMETERS USING INFLATABLE BLADDER(S) [patent_app_type] => utility [patent_app_number] => 18/628301 [patent_app_country] => US [patent_app_date] => 2024-04-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 2155 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 130 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18628301 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/628301
TAILORING AIRCRAFT POWERPLANT FLOW PARAMETERS USING INFLATABLE BLADDER(S) Apr 4, 2024 Pending
Array ( [id] => 20093995 [patent_doc_number] => 20250223931 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2025-07-10 [patent_title] => HYDROGEN FUEL DELIVERY SYSTEM [patent_app_type] => utility [patent_app_number] => 18/618401 [patent_app_country] => US [patent_app_date] => 2024-03-27 [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] => -13 [patent_words_short_claim] => 97 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18618401 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/618401
HYDROGEN FUEL DELIVERY SYSTEM Mar 26, 2024 Pending
Array ( [id] => 20248704 [patent_doc_number] => 20250297573 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2025-09-25 [patent_title] => GAS TURBINE ENGINE [patent_app_type] => utility [patent_app_number] => 18/615118 [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] => 7848 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -19 [patent_words_short_claim] => 153 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18615118 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/615118
GAS TURBINE ENGINE Mar 24, 2024 Pending
Array ( [id] => 20151292 [patent_doc_number] => 20250251130 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2025-08-07 [patent_title] => Micro Gas Turbine Engine and Related Methods of Manufacture [patent_app_type] => utility [patent_app_number] => 18/616028 [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] => -30 [patent_words_short_claim] => 40 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18616028 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/616028
Micro Gas Turbine Engine and Related Methods of Manufacture Mar 24, 2024 Pending
Array ( [id] => 20248704 [patent_doc_number] => 20250297573 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2025-09-25 [patent_title] => GAS TURBINE ENGINE [patent_app_type] => utility [patent_app_number] => 18/615118 [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] => 7848 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -19 [patent_words_short_claim] => 153 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18615118 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/615118
GAS TURBINE ENGINE Mar 24, 2024 Pending
Array ( [id] => 20151092 [patent_doc_number] => 20250250930 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2025-08-07 [patent_title] => Turbomachine for an Aircraft Engine [patent_app_type] => utility [patent_app_number] => 18/608547 [patent_app_country] => US [patent_app_date] => 2024-03-18 [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] => -9 [patent_words_short_claim] => 116 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18608547 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/608547
Turbomachine for an Aircraft Engine Mar 17, 2024 Pending
Array ( [id] => 20151092 [patent_doc_number] => 20250250930 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2025-08-07 [patent_title] => Turbomachine for an Aircraft Engine [patent_app_type] => utility [patent_app_number] => 18/608547 [patent_app_country] => US [patent_app_date] => 2024-03-18 [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] => -9 [patent_words_short_claim] => 116 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18608547 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/608547
Turbomachine for an Aircraft Engine Mar 17, 2024 Pending
Array ( [id] => 20050667 [patent_doc_number] => 20250188889 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2025-06-12 [patent_title] => THRUST REVERSER WITH BLOCKER DOOR FOLDING LINKAGE [patent_app_type] => utility [patent_app_number] => 18/597518 [patent_app_country] => US [patent_app_date] => 2024-03-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 2138 [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] => 18597518 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/597518
Thrust reverser with blocker door folding linkage Mar 5, 2024 Issued
Array ( [id] => 20050668 [patent_doc_number] => 20250188890 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2025-06-12 [patent_title] => THRUST REVERSER WITH BLOCKER DOOR OPENING CONTROL DEVICE(S) [patent_app_type] => utility [patent_app_number] => 18/597538 [patent_app_country] => US [patent_app_date] => 2024-03-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 3188 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 86 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18597538 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/597538
THRUST REVERSER WITH BLOCKER DOOR OPENING CONTROL DEVICE(S) Mar 5, 2024 Pending
Array ( [id] => 20179215 [patent_doc_number] => 20250263173 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2025-08-21 [patent_title] => EXHAUST DUCT MOUNTING STRUCTURE FOR HYBRID AIRCRAFT POWERPLANT [patent_app_type] => utility [patent_app_number] => 18/582136 [patent_app_country] => US [patent_app_date] => 2024-02-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 1059 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [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] => 18582136 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/582136
EXHAUST DUCT MOUNTING STRUCTURE FOR HYBRID AIRCRAFT POWERPLANT Feb 19, 2024 Pending
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