
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 number | Title of the application | Filing Date | Status |
|---|---|---|---|
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 |