Search

Lorne Edward Meade

Examiner (ID: 989, Phone: (571)270-7570 , Office: P/3741 )

Most Active Art Unit
3741
Art Unit(s)
3741
Total Applications
695
Issued Applications
353
Pending Applications
87
Abandoned Applications
285

Applications

Application numberTitle of the applicationFiling DateStatus
Array ( [id] => 11515049 [patent_doc_number] => 20170082124 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2017-03-23 [patent_title] => 'Directed Energy Deposition to Facilitate High Speed Applications' [patent_app_type] => utility [patent_app_number] => 15/186337 [patent_app_country] => US [patent_app_date] => 2016-06-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 25 [patent_figures_cnt] => 25 [patent_no_of_words] => 32057 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 4 [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] => 15186337 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/186337
Directed Energy Deposition to Facilitate High Speed Applications Jun 16, 2016 Abandoned
Array ( [id] => 11084645 [patent_doc_number] => 20160281610 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2016-09-29 [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] => 15/181102 [patent_app_country] => US [patent_app_date] => 2016-06-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 3639 [patent_no_of_claims] => 30 [patent_no_of_ind_claims] => 4 [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] => 15181102 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/181102
METHOD FOR SETTING A GEAR RATIO OF A FAN DRIVE GEAR SYSTEM OF A GAS TURBINE ENGINE Jun 12, 2016 Abandoned
Array ( [id] => 15817965 [patent_doc_number] => 10634153 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2020-04-28 [patent_title] => Apparatus and process for manufacturing a centrifugal pump with a rotor within a single piece housing [patent_app_type] => utility [patent_app_number] => 15/173773 [patent_app_country] => US [patent_app_date] => 2016-06-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 1595 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 121 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15173773 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/173773
Apparatus and process for manufacturing a centrifugal pump with a rotor within a single piece housing Jun 5, 2016 Issued
Array ( [id] => 15229417 [patent_doc_number] => 10502425 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2019-12-10 [patent_title] => Contoured shroud swirling pre-mix fuel injector assembly [patent_app_type] => utility [patent_app_number] => 15/172590 [patent_app_country] => US [patent_app_date] => 2016-06-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 5571 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 166 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15172590 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/172590
Contoured shroud swirling pre-mix fuel injector assembly Jun 2, 2016 Issued
Array ( [id] => 11312423 [patent_doc_number] => 20160348533 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2016-12-01 [patent_title] => 'ROTOR RESONANCE DISTURBANCE REJECTION CONTROLLER' [patent_app_type] => utility [patent_app_number] => 15/170024 [patent_app_country] => US [patent_app_date] => 2016-06-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 10907 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 6 [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] => 15170024 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/170024
ROTOR RESONANCE DISTURBANCE REJECTION CONTROLLER May 31, 2016 Abandoned
Array ( [id] => 11312502 [patent_doc_number] => 20160348612 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2016-12-01 [patent_title] => 'MOTOR PROPELLANT LIQUID' [patent_app_type] => utility [patent_app_number] => 15/165592 [patent_app_country] => US [patent_app_date] => 2016-05-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2043 [patent_no_of_claims] => 5 [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] => 15165592 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/165592
MOTOR PROPELLANT LIQUID May 25, 2016 Abandoned
Array ( [id] => 16215755 [patent_doc_number] => 10731556 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2020-08-04 [patent_title] => Isentropic compression inlet for supersonic aircraft [patent_app_type] => utility [patent_app_number] => 15/164557 [patent_app_country] => US [patent_app_date] => 2016-05-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 18 [patent_figures_cnt] => 31 [patent_no_of_words] => 15224 [patent_no_of_claims] => 2 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 190 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15164557 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/164557
Isentropic compression inlet for supersonic aircraft May 24, 2016 Issued
Array ( [id] => 11039835 [patent_doc_number] => 20160236792 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2016-08-18 [patent_title] => 'ON BOARD INERT GAS GENERATION SYSTEM WITH ROTARY POSITIVE DISPLACEMENT COMPRESSOR' [patent_app_type] => utility [patent_app_number] => 15/139351 [patent_app_country] => US [patent_app_date] => 2016-04-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 3826 [patent_no_of_claims] => 13 [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] => 15139351 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/139351
ON BOARD INERT GAS GENERATION SYSTEM WITH ROTARY POSITIVE DISPLACEMENT COMPRESSOR Apr 26, 2016 Abandoned
Array ( [id] => 15356793 [patent_doc_number] => 10527003 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2020-01-07 [patent_title] => Rocket engine thrust chamber, injector, and turbopump [patent_app_type] => utility [patent_app_number] => 15/094809 [patent_app_country] => US [patent_app_date] => 2016-04-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 18 [patent_figures_cnt] => 26 [patent_no_of_words] => 16333 [patent_no_of_claims] => 26 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 439 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15094809 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/094809
Rocket engine thrust chamber, injector, and turbopump Apr 7, 2016 Issued
Array ( [id] => 12947134 [patent_doc_number] => 09835113 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2017-12-05 [patent_title] => Thrust reverser for a turbojet engine nacelle comprising an end-of-travel stop on the primary guide rail [patent_app_type] => utility [patent_app_number] => 15/076907 [patent_app_country] => US [patent_app_date] => 2016-03-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 15 [patent_no_of_words] => 3316 [patent_no_of_claims] => 5 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 176 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15076907 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/076907
Thrust reverser for a turbojet engine nacelle comprising an end-of-travel stop on the primary guide rail Mar 21, 2016 Issued
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
Menu