
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 number | Title of the application | Filing Date | Status |
|---|---|---|---|
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
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[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
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[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
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[patent_no_of_words] => 4123
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[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
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[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
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[patent_no_of_words] => 4452
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[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
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[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
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[patent_no_of_words] => 3482
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[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
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[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
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[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
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[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
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[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 |