
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] => 13676591
[patent_doc_number] => 20160377029
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-12-29
[patent_title] => HELICON YIELD PLASMA ELECTROMAGNETIC RAM-SCRAMJET DRIVE ROCKET ION VECTOR ENGINE
[patent_app_type] => utility
[patent_app_number] => 14/209858
[patent_app_country] => US
[patent_app_date] => 2014-03-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 6338
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -6
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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] => 14209858
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/209858 | HELICON YIELD PLASMA ELECTROMAGNETIC RAM-SCRAMJET DRIVE ROCKET ION VECTOR ENGINE | Mar 12, 2014 | Abandoned |
Array
(
[id] => 10375120
[patent_doc_number] => 20150260127
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-09-17
[patent_title] => 'Aircraft Turbofan Engine with Multiple High-Pressure Core Modules Not Concentric with the Engine Centerline'
[patent_app_type] => utility
[patent_app_number] => 14/209679
[patent_app_country] => US
[patent_app_date] => 2014-03-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 1645
[patent_no_of_claims] => 3
[patent_no_of_ind_claims] => 1
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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] => 14209679
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/209679 | Aircraft Turbofan Engine with Multiple High-Pressure Core Modules Not Concentric with the Engine Centerline | Mar 12, 2014 | Abandoned |
Array
(
[id] => 10679194
[patent_doc_number] => 20160025339
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-01-28
[patent_title] => 'ENERGY-EFFICIENT AND CONTROLLED VAPORIZATION OF CRYOFUELS FOR AIRCRAFT ENGINES'
[patent_app_type] => utility
[patent_app_number] => 14/774917
[patent_app_country] => US
[patent_app_date] => 2014-03-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 11
[patent_no_of_words] => 11530
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 2
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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] => 14774917
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/774917 | ENERGY-EFFICIENT AND CONTROLLED VAPORIZATION OF CRYOFUELS FOR AIRCRAFT ENGINES | Mar 11, 2014 | Abandoned |
Array
(
[id] => 9593498
[patent_doc_number] => 20140190175
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-07-10
[patent_title] => '3D NON-AXISYMMETRIC COMBUSTOR LINER'
[patent_app_type] => utility
[patent_app_number] => 14/202969
[patent_app_country] => US
[patent_app_date] => 2014-03-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 3954
[patent_no_of_claims] => 20
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/202969 | 3D NON-AXISYMMETRIC COMBUSTOR LINER | Mar 9, 2014 | Abandoned |
Array
(
[id] => 10367748
[patent_doc_number] => 20150252753
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-09-10
[patent_title] => 'ANTIVORTEX DEVICE AND METHOD OF ASSEMBLING THEREOF'
[patent_app_type] => utility
[patent_app_number] => 14/199093
[patent_app_country] => US
[patent_app_date] => 2014-03-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 3302
[patent_no_of_claims] => 20
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14199093
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/199093 | Antivortex device and method of assembling thereof | Mar 5, 2014 | Issued |
Array
(
[id] => 11613145
[patent_doc_number] => 09650997
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2017-05-16
[patent_title] => 'Rotary turbo rocket'
[patent_app_type] => utility
[patent_app_number] => 14/191926
[patent_app_country] => US
[patent_app_date] => 2014-02-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 6535
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 282
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14191926
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/191926 | Rotary turbo rocket | Feb 26, 2014 | Issued |
| 14/188938 | Liquid rocket engine with Mondaloy and glass coating | Feb 24, 2014 | Abandoned |
Array
(
[id] => 10469488
[patent_doc_number] => 20150354504
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-12-10
[patent_title] => 'ROCKET ENGINE, ROCKET AND START METHOD OF ROCKET ENGINE'
[patent_app_type] => utility
[patent_app_number] => 14/760526
[patent_app_country] => US
[patent_app_date] => 2014-02-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 6335
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 5
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14760526
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/760526 | ROCKET ENGINE, ROCKET AND START METHOD OF ROCKET ENGINE | Feb 16, 2014 | Abandoned |
Array
(
[id] => 13038631
[patent_doc_number] => 10041445
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2018-08-07
[patent_title] => Nozzle having a movable divergent section with a thermal protection system
[patent_app_type] => utility
[patent_app_number] => 14/767934
[patent_app_country] => US
[patent_app_date] => 2014-02-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 1
[patent_no_of_words] => 2156
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 185
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14767934
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/767934 | Nozzle having a movable divergent section with a thermal protection system | Feb 12, 2014 | Issued |
Array
(
[id] => 10469436
[patent_doc_number] => 20150354452
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-12-10
[patent_title] => 'STARTER DEVICE FOR ROCKET MOTOR TURBOPUMP'
[patent_app_type] => utility
[patent_app_number] => 14/761401
[patent_app_country] => US
[patent_app_date] => 2014-01-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_no_of_claims] => 12
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14761401
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/761401 | STARTER DEVICE FOR ROCKET MOTOR TURBOPUMP | Jan 15, 2014 | Abandoned |
Array
(
[id] => 9599755
[patent_doc_number] => 20140196436
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-07-17
[patent_title] => 'OPERATION STABILIZATION METHOD AND OPERATION STABILIZATION APPARATUS FOR SUPERSONIC INTAKE'
[patent_app_type] => utility
[patent_app_number] => 14/155472
[patent_app_country] => US
[patent_app_date] => 2014-01-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 4024
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14155472
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/155472 | OPERATION STABILIZATION METHOD AND OPERATION STABILIZATION APPARATUS FOR SUPERSONIC INTAKE | Jan 14, 2014 | Abandoned |
Array
(
[id] => 10469487
[patent_doc_number] => 20150354503
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-12-10
[patent_title] => 'SYSTEM AND A METHOD FOR FEEDING A ROCKET ENGINE'
[patent_app_type] => utility
[patent_app_number] => 14/760186
[patent_app_country] => US
[patent_app_date] => 2014-01-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14760186
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/760186 | SYSTEM AND A METHOD FOR FEEDING A ROCKET ENGINE | Jan 7, 2014 | Abandoned |
Array
(
[id] => 10701157
[patent_doc_number] => 20160047304
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-02-18
[patent_title] => 'ULTRA HIGH OVERALL PRESSURE RATIO GAS TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 14/146758
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[patent_app_date] => 2014-01-03
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/146758 | ULTRA HIGH OVERALL PRESSURE RATIO GAS TURBINE ENGINE | Jan 2, 2014 | Abandoned |
Array
(
[id] => 9724481
[patent_doc_number] => 20140260182
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-09-18
[patent_title] => 'FREE STREAM INTAKE FOR REVERSE CORE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 14/142968
[patent_app_country] => US
[patent_app_date] => 2013-12-30
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14142968
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/142968 | Free stream intake with particle separator for reverse core engine | Dec 29, 2013 | Issued |
Array
(
[id] => 9724482
[patent_doc_number] => 20140260183
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-09-18
[patent_title] => 'VARIABLE CYCLE INTAKE FOR REVERSE CORE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 14/142966
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[patent_app_date] => 2013-12-30
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/142966 | Variable cycle intake for reverse core engine | Dec 29, 2013 | Issued |
Array
(
[id] => 9724589
[patent_doc_number] => 20140260290
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-09-18
[patent_title] => 'POWER-GENERATING APPARATUS AND METHOD'
[patent_app_type] => utility
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/143356 | POWER-GENERATING APPARATUS AND METHOD | Dec 29, 2013 | Abandoned |
Array
(
[id] => 10291531
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[patent_title] => 'ULTRA HIGH OVERALL PESSURE RATIO GAS TURBINE ENGINE'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/134281 | ULTRA HIGH OVERALL PESSURE RATIO GAS TURBINE ENGINE | Dec 18, 2013 | Abandoned |
Array
(
[id] => 10657050
[patent_doc_number] => 20160003194
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-01-07
[patent_title] => 'Asymmetric Fan Nozzle in High-BPR Separate-Flow Nacelle'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/768830 | Asymmetric fan nozzle in high-BPR separate-flow nacelle | Dec 17, 2013 | Issued |
Array
(
[id] => 10282552
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Array
(
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