
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 number | Title of the application | Filing Date | Status |
|---|---|---|---|
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
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[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
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[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
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[patent_no_of_words] => 7056
[patent_no_of_claims] => 20
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[patent_maintenance] => 1
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[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
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[patent_no_of_words] => 4261
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[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
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[patent_no_of_words] => 3081
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[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
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[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
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[patent_no_of_words] => 2451
[patent_no_of_claims] => 19
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[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
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[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
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[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
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[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
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[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 |