Search

Lorne Edward Meade

Examiner (ID: 2272, Phone: (571)270-7570 , Office: P/3741 )

Most Active Art Unit
3741
Art Unit(s)
3741
Total Applications
732
Issued Applications
369
Pending Applications
82
Abandoned Applications
292

Applications

Application numberTitle of the applicationFiling DateStatus
Array ( [id] => 20466349 [patent_doc_number] => 12522381 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2026-01-13 [patent_title] => Miniaturized green end-burning hybrid propulsion system for cubesats [patent_app_type] => utility [patent_app_number] => 17/391843 [patent_app_country] => US [patent_app_date] => 2021-08-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 18 [patent_figures_cnt] => 27 [patent_no_of_words] => 4581 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 147 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17391843 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/391843
Miniaturized green end-burning hybrid propulsion system for cubesats Aug 1, 2021 Issued
Array ( [id] => 17946534 [patent_doc_number] => 20220333553 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-10-20 [patent_title] => THREE-STREAM GAS TURBINE ENGINE WITH EMBEDDED ELECTRIC MACHINE [patent_app_type] => utility [patent_app_number] => 17/378026 [patent_app_country] => US [patent_app_date] => 2021-07-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 33850 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -26 [patent_words_short_claim] => 84 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17378026 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/378026
Three-stream gas turbine engine with embedded electric machine Jul 15, 2021 Issued
Array ( [id] => 19738829 [patent_doc_number] => 12215654 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2025-02-04 [patent_title] => Cascade element for a thrust reverser system of an engine [patent_app_type] => utility [patent_app_number] => 18/005344 [patent_app_country] => US [patent_app_date] => 2021-07-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 17 [patent_figures_cnt] => 36 [patent_no_of_words] => 6538 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 89 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18005344 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/005344
Cascade element for a thrust reverser system of an engine Jul 12, 2021 Issued
Array ( [id] => 17483056 [patent_doc_number] => 20220090560 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-03-24 [patent_title] => HELICON YIELD PLASMA ELECTROMAGNETIC RAM-SCRAMJET DRIVE ROCKET ION VECTOR ENGINE [patent_app_type] => utility [patent_app_number] => 17/368589 [patent_app_country] => US [patent_app_date] => 2021-07-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 6651 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -6 [patent_words_short_claim] => 89 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17368589 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/368589
HELICON YIELD PLASMA ELECTROMAGNETIC RAM-SCRAMJET DRIVE ROCKET ION VECTOR ENGINE Jul 5, 2021 Pending
Array ( [id] => 18093915 [patent_doc_number] => 20220412256 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-12-29 [patent_title] => AIRCRAFT PROPULSION SYSTEM WITH VARIABLE AREA INLET [patent_app_type] => utility [patent_app_number] => 17/358957 [patent_app_country] => US [patent_app_date] => 2021-06-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 7119 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [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] => 17358957 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/358957
Aircraft propulsion system with variable area inlet Jun 24, 2021 Issued
Array ( [id] => 18065975 [patent_doc_number] => 20220397062 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-12-15 [patent_title] => GAS TURBINE ENGINE WITH ELECTRICALLY DRIVEN COMPRESSOR [patent_app_type] => utility [patent_app_number] => 17/345205 [patent_app_country] => US [patent_app_date] => 2021-06-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 3287 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -18 [patent_words_short_claim] => 73 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17345205 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/345205
Gas turbine engine with electrically driven compressor Jun 10, 2021 Issued
Array ( [id] => 17785260 [patent_doc_number] => 11408375 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2022-08-09 [patent_title] => Rocket engine turbopump with coolant passage in impeller central hub [patent_app_type] => utility [patent_app_number] => 17/303893 [patent_app_country] => US [patent_app_date] => 2021-06-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 19 [patent_figures_cnt] => 27 [patent_no_of_words] => 16391 [patent_no_of_claims] => 30 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 110 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17303893 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/303893
Rocket engine turbopump with coolant passage in impeller central hub Jun 8, 2021 Issued
17/343679 LINEAR CONTINUOUS DETONATION ROCKET ENGINES Jun 8, 2021 Abandoned
Array ( [id] => 17800792 [patent_doc_number] => 11415082 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2022-08-16 [patent_title] => Turbopump, thrust chamber, and injector with distribution system and a circular array of support columns to flow liquid from the distribution system into a combustion chamber [patent_app_type] => utility [patent_app_number] => 17/303894 [patent_app_country] => US [patent_app_date] => 2021-06-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 18 [patent_figures_cnt] => 26 [patent_no_of_words] => 16356 [patent_no_of_claims] => 29 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 216 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17303894 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/303894
Turbopump, thrust chamber, and injector with distribution system and a circular array of support columns to flow liquid from the distribution system into a combustion chamber Jun 8, 2021 Issued
Array ( [id] => 18519087 [patent_doc_number] => 11708972 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2023-07-25 [patent_title] => Gas/air mixing device of a gas burner [patent_app_type] => utility [patent_app_number] => 17/323607 [patent_app_country] => US [patent_app_date] => 2021-05-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 7 [patent_no_of_words] => 3300 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 338 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17323607 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/323607
Gas/air mixing device of a gas burner May 17, 2021 Issued
Array ( [id] => 17315342 [patent_doc_number] => 20210404390 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2021-12-30 [patent_title] => GEARED GAS TURBINE ENGINE [patent_app_type] => utility [patent_app_number] => 17/244091 [patent_app_country] => US [patent_app_date] => 2021-04-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 41451 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 220 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17244091 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/244091
GEARED GAS TURBINE ENGINE Apr 28, 2021 Abandoned
Array ( [id] => 17946760 [patent_doc_number] => 20220333779 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-10-20 [patent_title] => COMBUSTOR SWIRL VANE APPARATUS [patent_app_type] => utility [patent_app_number] => 17/232638 [patent_app_country] => US [patent_app_date] => 2021-04-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 4923 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -18 [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] => 17232638 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/232638
Combustor swirl vane apparatus Apr 15, 2021 Issued
Array ( [id] => 18733969 [patent_doc_number] => 11802693 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2023-10-31 [patent_title] => Combustor swirl vane apparatus [patent_app_type] => utility [patent_app_number] => 17/232653 [patent_app_country] => US [patent_app_date] => 2021-04-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 10 [patent_no_of_words] => 5143 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 215 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17232653 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/232653
Combustor swirl vane apparatus Apr 15, 2021 Issued
Array ( [id] => 17816282 [patent_doc_number] => 11421885 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2022-08-23 [patent_title] => System for aerodynamically enhanced premixer for reduced emissions [patent_app_type] => utility [patent_app_number] => 17/231771 [patent_app_country] => US [patent_app_date] => 2021-04-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 21 [patent_figures_cnt] => 35 [patent_no_of_words] => 4528 [patent_no_of_claims] => 4 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 335 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17231771 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/231771
System for aerodynamically enhanced premixer for reduced emissions Apr 14, 2021 Issued
Array ( [id] => 17097851 [patent_doc_number] => 20210285642 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2021-09-16 [patent_title] => SYSTEM FOR AERODYNAMICALLY ENHANCED PREMIXER FOR REDUCED EMISSIONS [patent_app_type] => utility [patent_app_number] => 17/231750 [patent_app_country] => US [patent_app_date] => 2021-04-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 4527 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -4 [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] => 17231750 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/231750
System for aerodynamically enhanced premixer for reduced emissions Apr 14, 2021 Issued
Array ( [id] => 17229315 [patent_doc_number] => 20210355871 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2021-11-18 [patent_title] => INTAKE CENTRE FAIRING FOR A GAS TURBINE ENGINE [patent_app_type] => utility [patent_app_number] => 17/231275 [patent_app_country] => US [patent_app_date] => 2021-04-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 7095 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -12 [patent_words_short_claim] => 129 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17231275 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/231275
Intake centre fairing for a gas turbine engine Apr 14, 2021 Issued
Array ( [id] => 17946516 [patent_doc_number] => 20220333534 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-10-20 [patent_title] => MULTI-FUEL, FUEL INJECTION SYSTEM FOR A TURBINE ENGINE [patent_app_type] => utility [patent_app_number] => 17/231742 [patent_app_country] => US [patent_app_date] => 2021-04-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 11449 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 77 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17231742 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/231742
Multi-fuel, fuel injection system for a turbine engine Apr 14, 2021 Issued
Array ( [id] => 18176671 [patent_doc_number] => 20230037400 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2023-02-09 [patent_title] => THRUSTER ASSEMBLY [patent_app_type] => utility [patent_app_number] => 17/916456 [patent_app_country] => US [patent_app_date] => 2021-04-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 3262 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -12 [patent_words_short_claim] => 154 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17916456 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/916456
Thruster assembly Mar 31, 2021 Issued
Array ( [id] => 16963602 [patent_doc_number] => 20210215101 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2021-07-15 [patent_title] => METHOD FOR SETTING A GEAR RATIO OF A FAN DRIVE GEAR SYSTEM OF A GAS TURBINE ENGINE [patent_app_type] => utility [patent_app_number] => 17/217754 [patent_app_country] => US [patent_app_date] => 2021-03-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 4618 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -26 [patent_words_short_claim] => 328 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17217754 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/217754
METHOD FOR SETTING A GEAR RATIO OF A FAN DRIVE GEAR SYSTEM OF A GAS TURBINE ENGINE Mar 29, 2021 Abandoned
Array ( [id] => 17743181 [patent_doc_number] => 11391240 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2022-07-19 [patent_title] => Gas turbine engine bifurcation located fan variable area nozzle [patent_app_type] => utility [patent_app_number] => 17/217048 [patent_app_country] => US [patent_app_date] => 2021-03-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 2909 [patent_no_of_claims] => 30 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 268 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17217048 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/217048
Gas turbine engine bifurcation located fan variable area nozzle Mar 29, 2021 Issued
Menu