Search

Lorne Edward Meade

Examiner (ID: 481, Phone: (571)270-7570 , Office: P/3741 )

Most Active Art Unit
3741
Art Unit(s)
3741
Total Applications
713
Issued Applications
362
Pending Applications
77
Abandoned Applications
288

Applications

Application numberTitle of the applicationFiling DateStatus
Array ( [id] => 19126255 [patent_doc_number] => 20240131608 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2024-04-25 [patent_title] => METHOD FOR PREPARING LAMINATION PLAN [patent_app_type] => utility [patent_app_number] => 18/547142 [patent_app_country] => US [patent_app_date] => 2022-01-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 10091 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -11 [patent_words_short_claim] => 306 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18547142 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/547142
METHOD FOR PREPARING LAMINATION PLAN Jan 27, 2022 Pending
Array ( [id] => 20214113 [patent_doc_number] => 12410758 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2025-09-09 [patent_title] => Three-stream gas turbine engine control [patent_app_type] => utility [patent_app_number] => 17/571642 [patent_app_country] => US [patent_app_date] => 2022-01-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 17 [patent_figures_cnt] => 17 [patent_no_of_words] => 18592 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 244 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17571642 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/571642
Three-stream gas turbine engine control Jan 9, 2022 Issued
Array ( [id] => 17954038 [patent_doc_number] => 11480136 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2022-10-25 [patent_title] => Monopropellant continuous detonation engines [patent_app_type] => utility [patent_app_number] => 17/564743 [patent_app_country] => US [patent_app_date] => 2021-12-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 27 [patent_figures_cnt] => 32 [patent_no_of_words] => 15762 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 1 [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] => 17564743 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/564743
Monopropellant continuous detonation engines Dec 28, 2021 Issued
Array ( [id] => 19166356 [patent_doc_number] => 11982250 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2024-05-14 [patent_title] => Tripropellant rotating detonation rocket engine systems [patent_app_type] => utility [patent_app_number] => 17/561623 [patent_app_country] => US [patent_app_date] => 2021-12-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 1371 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 128 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17561623 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/561623
Tripropellant rotating detonation rocket engine systems Dec 22, 2021 Issued
Array ( [id] => 17656839 [patent_doc_number] => 20220177304 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-06-09 [patent_title] => DESALINATION METHODS AND DEVICES USING GEOTHERMAL ENERGY [patent_app_type] => utility [patent_app_number] => 17/555279 [patent_app_country] => US [patent_app_date] => 2021-12-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 3199 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [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] => 17555279 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/555279
DESALINATION METHODS AND DEVICES USING GEOTHERMAL ENERGY Dec 16, 2021 Abandoned
Array ( [id] => 19809249 [patent_doc_number] => 12240618 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2025-03-04 [patent_title] => Turbojet engine fan casing [patent_app_type] => utility [patent_app_number] => 17/549291 [patent_app_country] => US [patent_app_date] => 2021-12-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 4 [patent_no_of_words] => 3266 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 253 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17549291 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/549291
Turbojet engine fan casing Dec 12, 2021 Issued
Array ( [id] => 18110298 [patent_doc_number] => 20230003178 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2023-01-05 [patent_title] => COMBUSTOR OF LIQUID ROCKET ENGINE [patent_app_type] => utility [patent_app_number] => 17/539846 [patent_app_country] => US [patent_app_date] => 2021-12-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 2476 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -6 [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] => 17539846 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/539846
Combustor of liquid rocket engine Nov 30, 2021 Issued
Array ( [id] => 18862748 [patent_doc_number] => 20230417184 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2023-12-28 [patent_title] => ENGINES [patent_app_type] => utility [patent_app_number] => 18/038819 [patent_app_country] => US [patent_app_date] => 2021-11-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 23086 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -50 [patent_words_short_claim] => 35 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18038819 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/038819
ENGINES Nov 25, 2021 Abandoned
Array ( [id] => 17761154 [patent_doc_number] => 20220234766 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-07-28 [patent_title] => ENGINE MODULAR DESIGN AND CONSTRUCTION FOR REDUCED COST AND ACCELERATED DEVELOPMENT, APPLYING A USER-SPECIFIED DESIGN PROCESS [patent_app_type] => utility [patent_app_number] => 17/524401 [patent_app_country] => US [patent_app_date] => 2021-11-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 9521 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [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] => 17524401 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/524401
ENGINE MODULAR DESIGN AND CONSTRUCTION FOR REDUCED COST AND ACCELERATED DEVELOPMENT, APPLYING A USER-SPECIFIED DESIGN PROCESS Nov 10, 2021 Pending
Array ( [id] => 18845447 [patent_doc_number] => 20230407851 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2023-12-21 [patent_title] => PROPULSION UNIT FOR SPACECRAFT [patent_app_type] => utility [patent_app_number] => 18/035193 [patent_app_country] => US [patent_app_date] => 2021-11-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 4222 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -6 [patent_words_short_claim] => 72 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18035193 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/035193
PROPULSION UNIT FOR SPACECRAFT Nov 2, 2021 Pending
Array ( [id] => 18895968 [patent_doc_number] => 20240011453 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2024-01-11 [patent_title] => FASTENING OF AN EXHAUST CONE IN A TURBOMACHINE NOZZLE [patent_app_type] => utility [patent_app_number] => 18/035574 [patent_app_country] => US [patent_app_date] => 2021-11-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 3679 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -15 [patent_words_short_claim] => 155 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18035574 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/035574
Fastening of an exhaust cone in a turbomachine nozzle Nov 2, 2021 Issued
Array ( [id] => 19210452 [patent_doc_number] => 11999500 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2024-06-04 [patent_title] => Deployable inlet assembly for aerial vehicle [patent_app_type] => utility [patent_app_number] => 17/506107 [patent_app_country] => US [patent_app_date] => 2021-10-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 13 [patent_figures_cnt] => 17 [patent_no_of_words] => 6207 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 189 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17506107 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/506107
Deployable inlet assembly for aerial vehicle Oct 19, 2021 Issued
Array ( [id] => 18323811 [patent_doc_number] => 20230121939 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2023-04-20 [patent_title] => STRADDLE MOUNTED LOW PRESSURE COMPRESSOR [patent_app_type] => utility [patent_app_number] => 17/504869 [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] => 3710 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -18 [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] => 17504869 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/504869
STRADDLE MOUNTED LOW PRESSURE COMPRESSOR Oct 18, 2021 Pending
Array ( [id] => 17578379 [patent_doc_number] => 20220135234 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-05-05 [patent_title] => GAS TURBINE ENGINE WITH CABIN BLOWER SYSTEM [patent_app_type] => utility [patent_app_number] => 17/502203 [patent_app_country] => US [patent_app_date] => 2021-10-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 6770 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -19 [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] => 17502203 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/502203
GAS TURBINE ENGINE WITH CABIN BLOWER SYSTEM Oct 14, 2021 Abandoned
Array ( [id] => 17548901 [patent_doc_number] => 20220120242 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-04-21 [patent_title] => THRUST CHAMBER INTEGRATED WITH IGNITER OF ROCKET ENGINE USING CRYOGENIC FUEL AND LIQUID OXYGEN AND ROCKET INCLUDING THE SAME [patent_app_type] => utility [patent_app_number] => 17/501370 [patent_app_country] => US [patent_app_date] => 2021-10-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 6376 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -18 [patent_words_short_claim] => 164 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17501370 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/501370
Thrust chamber integrated with igniter of rocket engine using cryogenic fuel and liquid oxygen and rocket including the same Oct 13, 2021 Issued
Array ( [id] => 17521078 [patent_doc_number] => 20220106927 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-04-07 [patent_title] => AIRCRAFT TURBOFAN HAVING A COWL ARTICULATED IN ROTATION AND A SYSTEM FOR DEPLOYING SAID COWL [patent_app_type] => utility [patent_app_number] => 17/488725 [patent_app_country] => US [patent_app_date] => 2021-09-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 3275 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -7 [patent_words_short_claim] => 204 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17488725 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/488725
Aircraft turbofan having a cowl articulated in rotation and a system for deploying said cowl Sep 28, 2021 Issued
Array ( [id] => 18643067 [patent_doc_number] => 11767124 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2023-09-26 [patent_title] => Aircraft propulsion system with variable area inlet [patent_app_type] => utility [patent_app_number] => 17/472120 [patent_app_country] => US [patent_app_date] => 2021-09-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 15 [patent_no_of_words] => 6004 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 304 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17472120 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/472120
Aircraft propulsion system with variable area inlet Sep 9, 2021 Issued
Array ( [id] => 18241236 [patent_doc_number] => 20230073547 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2023-03-09 [patent_title] => PROPULSION SYSTEM WITH SINGLE INITIATOR FOR MULTIPLE ROCKET MOTORS [patent_app_type] => utility [patent_app_number] => 17/466245 [patent_app_country] => US [patent_app_date] => 2021-09-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 3142 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 38 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17466245 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/466245
Propulsion system with single initiator for multiple rocket motors Sep 2, 2021 Issued
Array ( [id] => 18545850 [patent_doc_number] => 11719194 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2023-08-08 [patent_title] => Combustion chamber with vibration damping inner wall shape and method for manufacturing a combustion chamber [patent_app_type] => utility [patent_app_number] => 17/463609 [patent_app_country] => US [patent_app_date] => 2021-09-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 4876 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 282 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17463609 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/463609
Combustion chamber with vibration damping inner wall shape and method for manufacturing a combustion chamber Aug 31, 2021 Issued
Array ( [id] => 17292867 [patent_doc_number] => 20210388706 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2021-12-16 [patent_title] => DRIVE EQUIPMENT AND METHODS FOR MOBILE FRACTURING TRANSPORTATION PLATFORMS [patent_app_type] => utility [patent_app_number] => 17/460754 [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] => 10021 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -10 [patent_words_short_claim] => 162 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17460754 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/460754
DRIVE EQUIPMENT AND METHODS FOR MOBILE FRACTURING TRANSPORTATION PLATFORMS Aug 29, 2021 Pending
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