Search

Tae Jun Kim

Examiner (ID: 3368, Phone: (571)272-4829 , Office: P/3741 )

Most Active Art Unit
3746
Art Unit(s)
2899, 3746, 3403, 3799, 3741
Total Applications
2146
Issued Applications
1499
Pending Applications
168
Abandoned Applications
492

Applications

Application numberTitle of the applicationFiling DateStatus
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 Abandoned
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] => 20337188 [patent_doc_number] => 20250341308 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2025-11-06 [patent_title] => FUEL INJECTOR FOR A TURBINE ENGINE [patent_app_type] => utility [patent_app_number] => 18/642095 [patent_app_country] => US [patent_app_date] => 2024-04-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 10016 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -18 [patent_words_short_claim] => 96 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18642095 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/642095
FUEL INJECTOR FOR A TURBINE ENGINE Apr 21, 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] => 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] => 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 Abandoned
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] => 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] => 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
Array ( [id] => 20164813 [patent_doc_number] => 20250256859 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2025-08-14 [patent_title] => ACOUSTICALLY TREATED THRUST REVERSER BULLNOSE FAIRING AND TORQUE BOX [patent_app_type] => utility [patent_app_number] => 18/436855 [patent_app_country] => US [patent_app_date] => 2024-02-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 1076 [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] => 18436855 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/436855
ACOUSTICALLY TREATED THRUST REVERSER BULLNOSE FAIRING AND TORQUE BOX Feb 7, 2024 Pending
Array ( [id] => 20136739 [patent_doc_number] => 20250243783 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2025-07-31 [patent_title] => INTERMEDIATE CASE FOR AIRCRAFT PROPULSION SYSTEM HOUSING [patent_app_type] => utility [patent_app_number] => 18/422343 [patent_app_country] => US [patent_app_date] => 2024-01-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 2231 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 101 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18422343 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/422343
INTERMEDIATE CASE FOR AIRCRAFT PROPULSION SYSTEM HOUSING Jan 24, 2024 Pending
Array ( [id] => 20896835 [patent_doc_number] => 12704093 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2026-08-11 [patent_title] => PTMS thermal bus vapor cycle architecture [patent_app_type] => utility [patent_app_number] => 18/420957 [patent_app_country] => US [patent_app_date] => 2024-01-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 5 [patent_no_of_words] => 0 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 155 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18420957 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/420957
PTMS THERMAL BUS VAPOR CYCLE ARCHITECTURE Jan 23, 2024 Pending
Array ( [id] => 19128120 [patent_doc_number] => 20240133473 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2024-04-25 [patent_title] => ANTI-BACK-TRANSFER INTAKE STRUCTURE FOR ROTATING DETONATION COMBUSTION CHAMBER [patent_app_type] => utility [patent_app_number] => 18/400324 [patent_app_country] => US [patent_app_date] => 2023-12-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 7286 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -10 [patent_words_short_claim] => 201 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18400324 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/400324
ANTI-BACK-TRANSFER INTAKE STRUCTURE FOR ROTATING DETONATION COMBUSTION CHAMBER Dec 28, 2023 Abandoned
Array ( [id] => 20085904 [patent_doc_number] => 20250215840 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2025-07-03 [patent_title] => AIRCRAFT PROPULSION SYSTEM WITH ASYMMETRIC EXHAUST ASSEMBLY [patent_app_type] => utility [patent_app_number] => 18/400441 [patent_app_country] => US [patent_app_date] => 2023-12-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 1120 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 123 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18400441 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/400441
AIRCRAFT PROPULSION SYSTEM WITH ASYMMETRIC EXHAUST ASSEMBLY Dec 28, 2023 Pending
Array ( [id] => 19128120 [patent_doc_number] => 20240133473 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2024-04-25 [patent_title] => ANTI-BACK-TRANSFER INTAKE STRUCTURE FOR ROTATING DETONATION COMBUSTION CHAMBER [patent_app_type] => utility [patent_app_number] => 18/400324 [patent_app_country] => US [patent_app_date] => 2023-12-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 7286 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -10 [patent_words_short_claim] => 201 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18400324 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/400324
ANTI-BACK-TRANSFER INTAKE STRUCTURE FOR ROTATING DETONATION COMBUSTION CHAMBER Dec 28, 2023 Abandoned
Array ( [id] => 18923835 [patent_doc_number] => 20240026839 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2024-01-25 [patent_title] => Pulse Detonation Wave Generator [patent_app_type] => utility [patent_app_number] => 18/377032 [patent_app_country] => US [patent_app_date] => 2023-10-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 4605 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -22 [patent_words_short_claim] => 292 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18377032 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/377032
Pulse Detonation Wave Generator Oct 4, 2023 Abandoned
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