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] => 18375618 [patent_doc_number] => 20230150698 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2023-05-18 [patent_title] => PROPULSION SYSTEM FOR SPACECRAFT [patent_app_type] => utility [patent_app_number] => 17/918293 [patent_app_country] => US [patent_app_date] => 2020-10-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 5209 [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] => 17918293 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/918293
PROPULSION SYSTEM FOR SPACECRAFT Oct 8, 2020 Abandoned
Array ( [id] => 17705430 [patent_doc_number] => 20220205436 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-06-30 [patent_title] => INTELLIGENT CONTROL GAS SUCTION-TYPE ELECTRIC PROPULSION SYSTEM APPLICABLE TO MULTI-FLOW REGIMES [patent_app_type] => utility [patent_app_number] => 17/605568 [patent_app_country] => US [patent_app_date] => 2020-09-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 3823 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -9 [patent_words_short_claim] => 623 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17605568 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/605568
Intelligent control gas suction-type electric propulsion system applicable to multi-flow regimes Sep 29, 2020 Issued
Array ( [id] => 17876121 [patent_doc_number] => 11448125 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2022-09-20 [patent_title] => Multistage gas turbine engine with differential drive of compressor [patent_app_type] => utility [patent_app_number] => 16/999408 [patent_app_country] => US [patent_app_date] => 2020-08-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 9129 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 84 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16999408 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/999408
Multistage gas turbine engine with differential drive of compressor Aug 20, 2020 Issued
Array ( [id] => 16484740 [patent_doc_number] => 20200378341 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2020-12-03 [patent_title] => PROPULSION UNIT INCLUDING LIFTING POINTS DISPOSED ON THRUST REVERSER CYLINDER SUPPORTS [patent_app_type] => utility [patent_app_number] => 16/998720 [patent_app_country] => US [patent_app_date] => 2020-08-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 2901 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -9 [patent_words_short_claim] => 136 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16998720 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/998720
Propulsion unit including lifting points disposed on thrust reverser cylinder supports Aug 19, 2020 Issued
Array ( [id] => 16762089 [patent_doc_number] => 20210107670 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2021-04-15 [patent_title] => ANTERIOR PART OF A NACELLE OF AN AIRCRAFT PROPULSION ASSEMBLY HAVING A THERMAL TRANSITION REGION [patent_app_type] => utility [patent_app_number] => 16/990298 [patent_app_country] => US [patent_app_date] => 2020-08-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 5114 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -8 [patent_words_short_claim] => 338 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16990298 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/990298
Anterior part of a nacelle of an aircraft propulsion assembly having a thermal transition region Aug 10, 2020 Issued
Array ( [id] => 17830908 [patent_doc_number] => 20220268212 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-08-25 [patent_title] => INTERNAL STRUCTURE FOR A TURBOMACHINE NACELLE [patent_app_type] => utility [patent_app_number] => 17/629523 [patent_app_country] => US [patent_app_date] => 2020-08-06 [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] => -8 [patent_words_short_claim] => 127 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17629523 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/629523
Internal structure for a turbomachine nacelle Aug 5, 2020 Issued
Array ( [id] => 17357515 [patent_doc_number] => 20220018311 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-01-20 [patent_title] => GEARED TURBOFAN WITH OVER-SPEED PROTECTION [patent_app_type] => utility [patent_app_number] => 16/931685 [patent_app_country] => US [patent_app_date] => 2020-07-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 3759 [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] => 16931685 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/931685
Geared turbofan with over-speed protection Jul 16, 2020 Issued
Array ( [id] => 17251713 [patent_doc_number] => 11187190 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2021-11-30 [patent_title] => Turbofan comprising a cam actuating a set of rotatable blades for blocking off the bypass flow duct [patent_app_type] => utility [patent_app_number] => 16/926973 [patent_app_country] => US [patent_app_date] => 2020-07-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 6 [patent_no_of_words] => 3817 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 468 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16926973 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/926973
Turbofan comprising a cam actuating a set of rotatable blades for blocking off the bypass flow duct Jul 12, 2020 Issued
Array ( [id] => 18029676 [patent_doc_number] => 11512853 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2022-11-29 [patent_title] => Fuel circuit for a fuel injector [patent_app_type] => utility [patent_app_number] => 16/916446 [patent_app_country] => US [patent_app_date] => 2020-06-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 12 [patent_no_of_words] => 8288 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 173 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16916446 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/916446
Fuel circuit for a fuel injector Jun 29, 2020 Issued
Array ( [id] => 18029492 [patent_doc_number] => 11512669 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2022-11-29 [patent_title] => Distributed airfoil aerospike rocket nozzle [patent_app_type] => utility [patent_app_number] => 16/910342 [patent_app_country] => US [patent_app_date] => 2020-06-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 3 [patent_no_of_words] => 2907 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 161 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16910342 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/910342
Distributed airfoil aerospike rocket nozzle Jun 23, 2020 Issued
Array ( [id] => 16863337 [patent_doc_number] => 11022073 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2021-06-01 [patent_title] => Rocket engine turbopump with coolant passage in impeller central hub [patent_app_type] => utility [patent_app_number] => 16/946341 [patent_app_country] => US [patent_app_date] => 2020-06-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 18 [patent_figures_cnt] => 26 [patent_no_of_words] => 16324 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 286 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16946341 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/946341
Rocket engine turbopump with coolant passage in impeller central hub Jun 16, 2020 Issued
Array ( [id] => 16312009 [patent_doc_number] => 20200290747 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2020-09-17 [patent_title] => AIRCRAFT NACELLE [patent_app_type] => utility [patent_app_number] => 16/889197 [patent_app_country] => US [patent_app_date] => 2020-06-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 2232 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -9 [patent_words_short_claim] => 57 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16889197 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/889197
AIRCRAFT NACELLE May 31, 2020 Abandoned
Array ( [id] => 18461988 [patent_doc_number] => 11686274 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2023-06-27 [patent_title] => Confluence structure of a primary stream and a secondary stream in a bypass turbine engine [patent_app_type] => utility [patent_app_number] => 17/616456 [patent_app_country] => US [patent_app_date] => 2020-05-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 10 [patent_no_of_words] => 4184 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 233 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17616456 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/616456
Confluence structure of a primary stream and a secondary stream in a bypass turbine engine May 27, 2020 Issued
Array ( [id] => 16484701 [patent_doc_number] => 20200378302 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2020-12-03 [patent_title] => Advanced 2-spool turboprop engine [patent_app_type] => utility [patent_app_number] => 16/873610 [patent_app_country] => US [patent_app_date] => 2020-05-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 10504 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -16 [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] => 16873610 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/873610
Advanced 2-spool turboprop engine May 21, 2020 Issued
Array ( [id] => 17200813 [patent_doc_number] => 20210340908 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2021-11-04 [patent_title] => GAS TURBINE ENGINES HAVING CRYOGENIC FUEL SYSTEMS [patent_app_type] => utility [patent_app_number] => 16/864844 [patent_app_country] => US [patent_app_date] => 2020-05-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 6481 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -19 [patent_words_short_claim] => 122 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16864844 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/864844
GAS TURBINE ENGINES HAVING CRYOGENIC FUEL SYSTEMS Apr 30, 2020 Abandoned
Array ( [id] => 17185874 [patent_doc_number] => 20210332759 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2021-10-28 [patent_title] => ENGINE USING HEATED AND TURBO-EXPANDED AMMONIA FUEL [patent_app_type] => utility [patent_app_number] => 16/858858 [patent_app_country] => US [patent_app_date] => 2020-04-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 3119 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -18 [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] => 16858858 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/858858
ENGINE USING HEATED AND TURBO-EXPANDED AMMONIA FUEL Apr 26, 2020 Abandoned
Array ( [id] => 16254260 [patent_doc_number] => 20200263634 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2020-08-20 [patent_title] => THRUST REVERSER WITH A SYSTEM FOR LOCKING AND UNLOCKING UNDER LOAD [patent_app_type] => utility [patent_app_number] => 16/859028 [patent_app_country] => US [patent_app_date] => 2020-04-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 2180 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -6 [patent_words_short_claim] => 147 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16859028 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/859028
THRUST REVERSER WITH A SYSTEM FOR LOCKING AND UNLOCKING UNDER LOAD Apr 26, 2020 Abandoned
Array ( [id] => 18275115 [patent_doc_number] => 11614051 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2023-03-28 [patent_title] => Air intake of a turbojet engine nacelle comprising guide vanes [patent_app_type] => utility [patent_app_number] => 17/600539 [patent_app_country] => US [patent_app_date] => 2020-04-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 20 [patent_no_of_words] => 4750 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 283 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17600539 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/600539
Air intake of a turbojet engine nacelle comprising guide vanes Apr 7, 2020 Issued
Array ( [id] => 17642679 [patent_doc_number] => 20220170417 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-06-02 [patent_title] => TURBOJET COMPRISING A NACELLE WITH AN AIR INTAKE FOR PROMOTING A REVERSE THRUST PHASE [patent_app_type] => utility [patent_app_number] => 17/600550 [patent_app_country] => US [patent_app_date] => 2020-04-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 6457 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -7 [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] => 17600550 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/600550
Turbojet comprising a nacelle with an air intake for promoting a reverse thrust phase Apr 7, 2020 Issued
Array ( [id] => 16361823 [patent_doc_number] => 20200318574 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2020-10-08 [patent_title] => TURBOFAN COMPRISING A NACELLE EQUIPPED WITH A REVERSER SYSTEM AND A MOBILE CASCADE GRILL [patent_app_type] => utility [patent_app_number] => 16/832344 [patent_app_country] => US [patent_app_date] => 2020-03-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 3581 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -4 [patent_words_short_claim] => 408 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16832344 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/832344
Turbofan comprising a nacelle equipped with a reverser system and a mobile cascade grill Mar 26, 2020 Issued
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