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] => 12186478 [patent_doc_number] => 20180045414 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2018-02-15 [patent_title] => 'SWIRLER, BURNER AND COMBUSTOR FOR A GAS TURBINE ENGINE' [patent_app_type] => utility [patent_app_number] => 15/559557 [patent_app_country] => US [patent_app_date] => 2016-03-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 4044 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15559557 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/559557
SWIRLER, BURNER AND COMBUSTOR FOR A GAS TURBINE ENGINE Mar 16, 2016 Abandoned
Array ( [id] => 11048153 [patent_doc_number] => 20160245111 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2016-08-25 [patent_title] => 'WAVE ROTOR WITH PISTON ASSEMBLY' [patent_app_type] => utility [patent_app_number] => 15/044674 [patent_app_country] => US [patent_app_date] => 2016-02-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 7056 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15044674 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/044674
Wave rotor with piston assembly Feb 15, 2016 Issued
Array ( [id] => 11642711 [patent_doc_number] => 09664070 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2017-05-30 [patent_title] => 'Bowed rotor prevention system' [patent_app_type] => utility [patent_app_number] => 15/042331 [patent_app_country] => US [patent_app_date] => 2016-02-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 6 [patent_no_of_words] => 4261 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 114 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15042331 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/042331
Bowed rotor prevention system Feb 11, 2016 Issued
Array ( [id] => 15009553 [patent_doc_number] => 10450899 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2019-10-22 [patent_title] => Gas turbine exhaust diverter system duct guide rails [patent_app_type] => utility [patent_app_number] => 15/018879 [patent_app_country] => US [patent_app_date] => 2016-02-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 13 [patent_no_of_words] => 3081 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 272 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15018879 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/018879
Gas turbine exhaust diverter system duct guide rails Feb 8, 2016 Issued
Array ( [id] => 12159662 [patent_doc_number] => 20180030928 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2018-02-01 [patent_title] => 'CAPACITIVE SYSTEM FOR CORRECTING THE POGO EFFECT WITH SEMI-CENTERED DISCHARGE TUBE CAPABLE OF BEING POSITIONED IN A BEND' [patent_app_type] => utility [patent_app_number] => 15/547384 [patent_app_country] => US [patent_app_date] => 2016-01-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 7588 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15547384 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/547384
Capacitive system for correcting the pogo effect with semi-centered discharge tube capable of being positioned in a bend Jan 28, 2016 Issued
Array ( [id] => 11436759 [patent_doc_number] => 20170037779 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2017-02-09 [patent_title] => 'AIRCRAFT BOUNDARY LAYER REMOVAL WITH AUXILLIARY POWER UNIT SUCTION' [patent_app_type] => utility [patent_app_number] => 14/967240 [patent_app_country] => US [patent_app_date] => 2015-12-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 2451 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14967240 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/967240
AIRCRAFT BOUNDARY LAYER REMOVAL WITH AUXILLIARY POWER UNIT SUCTION Dec 10, 2015 Abandoned
Array ( [id] => 10751153 [patent_doc_number] => 20160097304 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2016-04-07 [patent_title] => 'GAS TURBINE ENGINE WITH LOW STAGE COUNT LOW PRESSURE TURBINE' [patent_app_type] => utility [patent_app_number] => 14/966538 [patent_app_country] => US [patent_app_date] => 2015-12-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 12 [patent_no_of_words] => 4667 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14966538 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/966538
GAS TURBINE ENGINE WITH LOW STAGE COUNT LOW PRESSURE TURBINE Dec 10, 2015 Abandoned
Array ( [id] => 11130011 [patent_doc_number] => 20160326986 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2016-11-10 [patent_title] => 'SELECTABLE MODE RAMJET/ROCKET JET ENGINE' [patent_app_type] => utility [patent_app_number] => 14/965718 [patent_app_country] => US [patent_app_date] => 2015-12-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 11 [patent_no_of_words] => 2957 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14965718 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/965718
SELECTABLE MODE RAMJET/ROCKET JET ENGINE Dec 9, 2015 Abandoned
Array ( [id] => 10737954 [patent_doc_number] => 20160084106 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2016-03-24 [patent_title] => 'ANTI-ICING CORE INLET STATOR ASSEMBLY FOR A GAS TURBINE ENGINE' [patent_app_type] => utility [patent_app_number] => 14/959542 [patent_app_country] => US [patent_app_date] => 2015-12-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2556 [patent_no_of_claims] => 22 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14959542 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/959542
Anti-icing core inlet stator assembly for a gas turbine engine Dec 3, 2015 Issued
Array ( [id] => 11650054 [patent_doc_number] => 20170145955 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2017-05-25 [patent_title] => 'HYBRID EXHAUST NOZZLE' [patent_app_type] => utility [patent_app_number] => 14/949315 [patent_app_country] => US [patent_app_date] => 2015-11-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 10105 [patent_no_of_claims] => 24 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14949315 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/949315
Hybrid exhaust nozzle Nov 22, 2015 Issued
Array ( [id] => 10714904 [patent_doc_number] => 20160061051 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2016-03-03 [patent_title] => 'GEARED TURBOFAN WITH THREE TURBINES WITH HIGH SPEED FAN DRIVE TURBINE' [patent_app_type] => utility [patent_app_number] => 14/934228 [patent_app_country] => US [patent_app_date] => 2015-11-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 3385 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14934228 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/934228
GEARED TURBOFAN WITH THREE TURBINES WITH HIGH SPEED FAN DRIVE TURBINE Nov 5, 2015 Abandoned
Array ( [id] => 10777070 [patent_doc_number] => 20160123226 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2016-05-05 [patent_title] => 'GAS TURBINE USING A CRYOGENIC FUEL AND EXTRACTING WORK THEREFROM' [patent_app_type] => utility [patent_app_number] => 14/879833 [patent_app_country] => US [patent_app_date] => 2015-10-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 4123 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14879833 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/879833
GAS TURBINE USING A CRYOGENIC FUEL AND EXTRACTING WORK THEREFROM Oct 8, 2015 Abandoned
Array ( [id] => 15667813 [patent_doc_number] => 10598128 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2020-03-24 [patent_title] => Attitude control system [patent_app_type] => utility [patent_app_number] => 14/875424 [patent_app_country] => US [patent_app_date] => 2015-10-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 30 [patent_figures_cnt] => 31 [patent_no_of_words] => 17766 [patent_no_of_claims] => 31 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 80 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14875424 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/875424
Attitude control system Oct 4, 2015 Issued
Array ( [id] => 10678812 [patent_doc_number] => 20160024957 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2016-01-28 [patent_title] => 'GAS TURBINE ENGINE WITH LOW STAGE COUNT LOW PRESSURE TURBINE' [patent_app_type] => utility [patent_app_number] => 14/872405 [patent_app_country] => US [patent_app_date] => 2015-10-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 12 [patent_no_of_words] => 4452 [patent_no_of_claims] => 22 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14872405 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/872405
GAS TURBINE ENGINE WITH LOW STAGE COUNT LOW PRESSURE TURBINE Sep 30, 2015 Abandoned
Array ( [id] => 10678813 [patent_doc_number] => 20160024958 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2016-01-28 [patent_title] => 'GAS TURBINE ENGINE WITH LOW STAGE COUNT LOW PRESSURE TURBINE' [patent_app_type] => utility [patent_app_number] => 14/872508 [patent_app_country] => US [patent_app_date] => 2015-10-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 12 [patent_no_of_words] => 4578 [patent_no_of_claims] => 24 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14872508 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/872508
GAS TURBINE ENGINE WITH LOW STAGE COUNT LOW PRESSURE TURBINE Sep 30, 2015 Abandoned
Array ( [id] => 15228857 [patent_doc_number] => 10502143 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2019-12-10 [patent_title] => Compressor of axial turbine engine with contra-rotating rotor [patent_app_type] => utility [patent_app_number] => 14/865202 [patent_app_country] => US [patent_app_date] => 2015-09-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 3 [patent_no_of_words] => 3482 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 203 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14865202 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/865202
Compressor of axial turbine engine with contra-rotating rotor Sep 24, 2015 Issued
Array ( [id] => 11513946 [patent_doc_number] => 20170081020 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2017-03-23 [patent_title] => 'ACTIVE LAMINAR FLOW CONTROL SYSTEM WITH DRAINAGE' [patent_app_type] => utility [patent_app_number] => 14/861767 [patent_app_country] => US [patent_app_date] => 2015-09-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 13 [patent_figures_cnt] => 13 [patent_no_of_words] => 4672 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14861767 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/861767
ACTIVE LAMINAR FLOW CONTROL SYSTEM WITH DRAINAGE Sep 21, 2015 Abandoned
Array ( [id] => 11852473 [patent_doc_number] => 20170226965 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2017-08-10 [patent_title] => 'METHOD FOR SUPPRESSING THE POGO EFFECT' [patent_app_type] => utility [patent_app_number] => 15/515423 [patent_app_country] => US [patent_app_date] => 2015-09-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 7246 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15515423 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/515423
Method for suppressing the pogo effect Sep 20, 2015 Issued
Array ( [id] => 10628421 [patent_doc_number] => 09346565 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2016-05-24 [patent_title] => 'Nuclear thermal propulsion rocket engine' [patent_app_type] => utility [patent_app_number] => 14/851665 [patent_app_country] => US [patent_app_date] => 2015-09-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 7386 [patent_no_of_claims] => 41 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 226 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14851665 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/851665
Nuclear thermal propulsion rocket engine Sep 10, 2015 Issued
Array ( [id] => 11500026 [patent_doc_number] => 20170074211 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2017-03-16 [patent_title] => 'SYSTEM AND METHOD FOR REDUCING IDLE THRUST IN A TRANSLATING COWL THRUST REVERSER' [patent_app_type] => utility [patent_app_number] => 14/850348 [patent_app_country] => US [patent_app_date] => 2015-09-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 5087 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14850348 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/850348
System and method for reducing idle thrust in a translating cowl thrust reverser Sep 9, 2015 Issued
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