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] => 17777335 [patent_doc_number] => 20220243684 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-08-04 [patent_title] => PROPULSION CONCEPT COMBINING CONVENTIONAL ROCKET ENGINES AND AIR-BREATHING ENGINES (HEBER CONCEPT) [patent_app_type] => utility [patent_app_number] => 17/492587 [patent_app_country] => US [patent_app_date] => 2022-04-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 16048 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -8 [patent_words_short_claim] => 31 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17492587 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/492587
PROPULSION CONCEPT COMBINING CONVENTIONAL ROCKET ENGINES AND AIR-BREATHING ENGINES (HEBER CONCEPT) Apr 19, 2022 Abandoned
Array ( [id] => 18667215 [patent_doc_number] => 11774103 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2023-10-03 [patent_title] => Engine with rotating detonation combustion system [patent_app_type] => utility [patent_app_number] => 17/658750 [patent_app_country] => US [patent_app_date] => 2022-04-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 21 [patent_no_of_words] => 9135 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 307 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17658750 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/658750
Engine with rotating detonation combustion system Apr 10, 2022 Issued
Array ( [id] => 19249484 [patent_doc_number] => 20240200472 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2024-06-20 [patent_title] => GENERATING ELECTRICAL ENERGY FROM HYDROGEN AND OXYGEN [patent_app_type] => utility [patent_app_number] => 18/286126 [patent_app_country] => US [patent_app_date] => 2022-04-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 4585 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -12 [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] => 18286126 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/286126
GENERATING ELECTRICAL ENERGY FROM HYDROGEN AND OXYGEN Apr 7, 2022 Pending
Array ( [id] => 17930554 [patent_doc_number] => 20220325679 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-10-13 [patent_title] => THRUST REVERSER SYSTEM FOR AN AIRCRAFT PROPULSION SYSTEM [patent_app_type] => utility [patent_app_number] => 17/716477 [patent_app_country] => US [patent_app_date] => 2022-04-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 8678 [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] => 17716477 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/716477
Thrust reverser system for an aircraft propulsion system Apr 7, 2022 Issued
Array ( [id] => 18005749 [patent_doc_number] => 20220364515 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-11-17 [patent_title] => ADAPTED PROCESS CONCEPT AND PERFORMANCE CONCEPT FOR ENGINES (E.G. ROCKETS), AIR-BREATHING PROPULSION SYSTEMS (E.G. SUBSONIC RAMJETS, RAMJETS, ROCKET RAMJETS), TURBOPUMPS OR NOZZLES (E.G. BELL NOZZLES, AEROSPIKES) [patent_app_type] => utility [patent_app_number] => 17/656459 [patent_app_country] => US [patent_app_date] => 2022-03-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 6526 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -12 [patent_words_short_claim] => 132 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17656459 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/656459
ADAPTED PROCESS CONCEPT AND PERFORMANCE CONCEPT FOR ENGINES (E.G. ROCKETS), AIR-BREATHING PROPULSION SYSTEMS (E.G. SUBSONIC RAMJETS, RAMJETS, ROCKET RAMJETS), TURBOPUMPS OR NOZZLES (E.G. BELL NOZZLES, AEROSPIKES) Mar 24, 2022 Abandoned
Array ( [id] => 18583551 [patent_doc_number] => 20230265812 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2023-08-24 [patent_title] => Variable Area Fan Nozzle Actuation System [patent_app_type] => utility [patent_app_number] => 17/694479 [patent_app_country] => US [patent_app_date] => 2022-03-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 5921 [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] => 17694479 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/694479
Variable area fan nozzle actuation system Mar 13, 2022 Issued
Array ( [id] => 18583551 [patent_doc_number] => 20230265812 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2023-08-24 [patent_title] => Variable Area Fan Nozzle Actuation System [patent_app_type] => utility [patent_app_number] => 17/694479 [patent_app_country] => US [patent_app_date] => 2022-03-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 5921 [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] => 17694479 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/694479
Variable area fan nozzle actuation system Mar 13, 2022 Issued
Array ( [id] => 18613299 [patent_doc_number] => 20230280035 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2023-09-07 [patent_title] => BIMODAL COMBUSTION SYSTEM [patent_app_type] => utility [patent_app_number] => 17/687873 [patent_app_country] => US [patent_app_date] => 2022-03-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 22616 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -19 [patent_words_short_claim] => 114 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17687873 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/687873
BIMODAL COMBUSTION SYSTEM Mar 6, 2022 Abandoned
Array ( [id] => 17930768 [patent_doc_number] => 20220325893 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-10-13 [patent_title] => CHAMBER FOR ROTATING DETONATION ENGINE AND WALL OBSTACLES FOR SAME [patent_app_type] => utility [patent_app_number] => 17/670575 [patent_app_country] => US [patent_app_date] => 2022-02-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 3673 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 98 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17670575 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/670575
CHAMBER FOR ROTATING DETONATION ENGINE AND WALL OBSTACLES FOR SAME Feb 13, 2022 Abandoned
Array ( [id] => 17946532 [patent_doc_number] => 20220333550 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-10-20 [patent_title] => POSITION SENSOR FOR AIRCRAFT NACELLE THRUST REVERSER DOOR [patent_app_type] => utility [patent_app_number] => 17/666244 [patent_app_country] => US [patent_app_date] => 2022-02-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 3646 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -19 [patent_words_short_claim] => 79 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17666244 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/666244
Position sensor for aircraft nacelle thrust reverser door Feb 6, 2022 Issued
Array ( [id] => 17762115 [patent_doc_number] => 20220235727 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-07-28 [patent_title] => ROTATING DETONATION ENGINE [patent_app_type] => utility [patent_app_number] => 17/582408 [patent_app_country] => US [patent_app_date] => 2022-01-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 3962 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -26 [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] => 17582408 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/582408
ROTATING DETONATION ENGINE Jan 23, 2022 Abandoned
Array ( [id] => 17750336 [patent_doc_number] => 20220228541 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-07-21 [patent_title] => TURBOFAN ENGINE COMPRISING A SYSTEM FOR BLOCKING THE FLOW PATH OF THE BYPASS STREAM COMPRISING VEILS [patent_app_type] => utility [patent_app_number] => 17/580110 [patent_app_country] => US [patent_app_date] => 2022-01-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 5744 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -8 [patent_words_short_claim] => 411 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17580110 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/580110
Turbofan engine comprising a system for blocking the flow path of the bypass stream comprising veils Jan 19, 2022 Issued
Array ( [id] => 17483285 [patent_doc_number] => 20220090789 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-03-24 [patent_title] => ISOLATION SECTION SUPPRESSING SHOCK WAVE FORWARD TRANSMISSION STRUCTURE FOR WAVE ROTOR COMBUSTOR AND WAVE ROTOR COMBUSTOR [patent_app_type] => utility [patent_app_number] => 17/544315 [patent_app_country] => US [patent_app_date] => 2021-12-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 3557 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -8 [patent_words_short_claim] => 150 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17544315 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/544315
Isolation section suppressing shock wave forward transmission structure for wave rotor combustor and wave rotor combustor Dec 6, 2021 Issued
Array ( [id] => 18420996 [patent_doc_number] => 20230175459 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2023-06-08 [patent_title] => PLURALITY OF AIRBREATHING AND NON-AIRBREATHING ENGINES [patent_app_type] => utility [patent_app_number] => 17/457653 [patent_app_country] => US [patent_app_date] => 2021-12-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 3002 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -5 [patent_words_short_claim] => 62 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17457653 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/457653
PLURALITY OF AIRBREATHING AND NON-AIRBREATHING ENGINES Dec 3, 2021 Abandoned
Array ( [id] => 17474560 [patent_doc_number] => 20220082064 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-03-17 [patent_title] => AIRCRAFT PROPULSION UNIT [patent_app_type] => utility [patent_app_number] => 17/536480 [patent_app_country] => US [patent_app_date] => 2021-11-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 4003 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -14 [patent_words_short_claim] => 113 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17536480 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/536480
Aircraft propulsion unit Nov 28, 2021 Issued
Array ( [id] => 17474560 [patent_doc_number] => 20220082064 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-03-17 [patent_title] => AIRCRAFT PROPULSION UNIT [patent_app_type] => utility [patent_app_number] => 17/536480 [patent_app_country] => US [patent_app_date] => 2021-11-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 4003 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -14 [patent_words_short_claim] => 113 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17536480 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/536480
Aircraft propulsion unit Nov 28, 2021 Issued
Array ( [id] => 19970169 [patent_doc_number] => 12338767 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2025-06-24 [patent_title] => Gas turbine inlet cooling for constant power output [patent_app_type] => utility [patent_app_number] => 18/037161 [patent_app_country] => US [patent_app_date] => 2021-10-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 2243 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 658 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18037161 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/037161
Gas turbine inlet cooling for constant power output Oct 12, 2021 Issued
Array ( [id] => 18785771 [patent_doc_number] => 20230373645 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2023-11-23 [patent_title] => COOLING SYSTEM OF A COMPARTMENT OF PIECES OF EQUIPMENT IN A NACELLE OF AN AIRCRAFT PROPELLING ASSEMBLY [patent_app_type] => utility [patent_app_number] => 18/044958 [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] => 7634 [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] => 18044958 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/044958
Cooling system of a compartment of pieces of equipment in a nacelle of an aircraft propelling assembly Sep 30, 2021 Issued
Array ( [id] => 18692189 [patent_doc_number] => 20230322418 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2023-10-12 [patent_title] => PLANAR ELECTRIC MOTOR FOR AEROSPACE USE [patent_app_type] => utility [patent_app_number] => 18/043583 [patent_app_country] => US [patent_app_date] => 2021-09-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 4632 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -7 [patent_words_short_claim] => 205 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18043583 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/043583
PLANAR ELECTRIC MOTOR FOR AEROSPACE USE Sep 1, 2021 Pending
Array ( [id] => 18862718 [patent_doc_number] => 20230417154 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2023-12-28 [patent_title] => METHOD FOR CREATING MAXIMUM OUTPUT IN GAS TURBINE, METHOD FOR CREATING OUTPUT FOR CONTROLLING GAS TURBINE, METHOD FOR CONTROLLING GAS TURBINE, DEVICE FOR EXECUTING SAID METHODS, AND PROGRAM FOR CAUSING COMPUTER TO EXECUTE SAID METHODS [patent_app_type] => utility [patent_app_number] => 18/033700 [patent_app_country] => US [patent_app_date] => 2021-07-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 26772 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -24 [patent_words_short_claim] => 215 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18033700 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/033700
Method for creating maximum output in gas turbine, method for creating output for controlling gas turbine, method for controlling gas turbine, device for executing said methods, and program for causing computer to execute said methods Jul 25, 2021 Issued
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