
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] => 13509141
[patent_doc_number] => 20180306113
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2018-10-25
[patent_title] => COMBUSTOR LINER PANEL END RAIL MATCHING HEAT TRANSFER FEATURES
[patent_app_type] => utility
[patent_app_number] => 15/491047
[patent_app_country] => US
[patent_app_date] => 2017-04-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 3782
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -15
[patent_words_short_claim] => 61
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15491047
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/491047 | COMBUSTOR LINER PANEL END RAIL MATCHING HEAT TRANSFER FEATURES | Apr 18, 2017 | Abandoned |
Array
(
[id] => 16573305
[patent_doc_number] => 10895221
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2021-01-19
[patent_title] => Continuous detonation wave engine and aircraft provided with such an engine
[patent_app_type] => utility
[patent_app_number] => 15/445271
[patent_app_country] => US
[patent_app_date] => 2017-02-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_no_of_words] => 4611
[patent_no_of_claims] => 20
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15445271
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/445271 | Continuous detonation wave engine and aircraft provided with such an engine | Feb 27, 2017 | Issued |
Array
(
[id] => 13779769
[patent_doc_number] => 20190003423
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2019-01-03
[patent_title] => DUAL-EXPANDER SHORT-LENGTH AEROSPIKE ENGINE
[patent_app_type] => utility
[patent_app_number] => 15/412548
[patent_app_country] => US
[patent_app_date] => 2017-01-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 4563
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -15
[patent_words_short_claim] => 256
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15412548
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/412548 | DUAL-EXPANDER SHORT-LENGTH AEROSPIKE ENGINE | Jan 22, 2017 | Abandoned |
Array
(
[id] => 11500023
[patent_doc_number] => 20170074208
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-03-16
[patent_title] => 'GAS TURBINE ENGINE WITH AXIAL MOVABLE FAN VARIABLE AREA NOZZLE'
[patent_app_type] => utility
[patent_app_number] => 15/359948
[patent_app_country] => US
[patent_app_date] => 2016-11-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 4022
[patent_no_of_claims] => 30
[patent_no_of_ind_claims] => 2
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/359948 | GAS TURBINE ENGINE WITH AXIAL MOVABLE FAN VARIABLE AREA NOZZLE | Nov 22, 2016 | Abandoned |
Array
(
[id] => 12709063
[patent_doc_number] => 20180128187
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2018-05-10
[patent_title] => COOLED COOLING AIR SAFETY THROUGH A TEMPERATURE-MONITORING LINE REPLACEABLE UNIT
[patent_app_type] => utility
[patent_app_number] => 15/346187
[patent_app_country] => US
[patent_app_date] => 2016-11-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15346187
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/346187 | COOLED COOLING AIR SAFETY THROUGH A TEMPERATURE-MONITORING LINE REPLACEABLE UNIT | Nov 7, 2016 | Abandoned |
Array
(
[id] => 11619440
[patent_doc_number] => 20170129628
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-05-11
[patent_title] => 'Thermal-nucleak powered rocket using non-cryogenic propellant'
[patent_app_type] => utility
[patent_app_number] => 15/330757
[patent_app_country] => US
[patent_app_date] => 2016-11-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
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[patent_no_of_words] => 562
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15330757
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/330757 | Thermal-nucleak powered rocket using non-cryogenic propellant | Nov 2, 2016 | Abandoned |
Array
(
[id] => 12643086
[patent_doc_number] => 20180106193
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2018-04-19
[patent_title] => HIGH OVERALL PRESSURE RATIO GAS TURBINE ENGINE
[patent_app_type] => utility
[patent_app_number] => 15/292203
[patent_app_country] => US
[patent_app_date] => 2016-10-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 3006
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -15
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15292203
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/292203 | HIGH OVERALL PRESSURE RATIO GAS TURBINE ENGINE | Oct 12, 2016 | Abandoned |
Array
(
[id] => 11543142
[patent_doc_number] => 20170096967
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-04-06
[patent_title] => 'ENHANCED LIQUID OXYGEN-PROPYLENE ROCKET ENGINE'
[patent_app_type] => utility
[patent_app_number] => 15/285324
[patent_app_country] => US
[patent_app_date] => 2016-10-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 7575
[patent_no_of_claims] => 20
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15285324
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/285324 | Enhanced liquid oxygen-propylene rocket engine | Oct 3, 2016 | Issued |
Array
(
[id] => 13358815
[patent_doc_number] => 20180230947
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2018-08-16
[patent_title] => LIQUID ROCKET ENGINE USING PUMP DRIVEN BY ELECTRIC MOTOR
[patent_app_type] => utility
[patent_app_number] => 15/750776
[patent_app_country] => US
[patent_app_date] => 2016-09-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
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[patent_no_of_words] => 3792
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[patent_no_of_ind_claims] => -10
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15750776
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/750776 | LIQUID ROCKET ENGINE USING PUMP DRIVEN BY ELECTRIC MOTOR | Sep 12, 2016 | Abandoned |
Array
(
[id] => 13358817
[patent_doc_number] => 20180230948
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2018-08-16
[patent_title] => LIQUID ROCKET ENGINE USING BOOSTER PUMP DRIVEN BY ELECTRIC MOTOR
[patent_app_type] => utility
[patent_app_number] => 15/750757
[patent_app_country] => US
[patent_app_date] => 2016-09-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 4865
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -13
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[patent_no_of_assignments] => 0
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15750757
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/750757 | Liquid rocket engine using booster pump driven by electric motor | Sep 12, 2016 | Issued |
Array
(
[id] => 12206401
[patent_doc_number] => 20180051627
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2018-02-22
[patent_title] => 'GAS GENERATOR BIFURCATING EXHAUST DUCT TO FREE TURBINE'
[patent_app_type] => utility
[patent_app_number] => 15/239086
[patent_app_country] => US
[patent_app_date] => 2016-08-17
[patent_effective_date] => 0000-00-00
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[patent_no_of_claims] => 20
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15239086
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/239086 | GAS GENERATOR BIFURCATING EXHAUST DUCT TO FREE TURBINE | Aug 16, 2016 | Abandoned |
Array
(
[id] => 12179341
[patent_doc_number] => 20180038277
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2018-02-08
[patent_title] => 'CLOSED-LOOP GAS TURBINE GENERATOR'
[patent_app_type] => utility
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[patent_app_date] => 2016-08-04
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/229094 | CLOSED-LOOP GAS TURBINE GENERATOR | Aug 3, 2016 | Abandoned |
Array
(
[id] => 11514995
[patent_doc_number] => 20170082070
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-03-23
[patent_title] => 'Turbopump with a single piece housing and a smooth enamel glass surface'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/227031 | Turbopump with a single piece housing and a smooth enamel glass surface | Aug 2, 2016 | Abandoned |
Array
(
[id] => 11471917
[patent_doc_number] => 20170058700
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-03-02
[patent_title] => 'EXHAUST MIXER WITH OUTER LOBE CONSTRAINT BAND'
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[patent_app_number] => 15/227599
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[patent_app_date] => 2016-08-03
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15227599
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/227599 | EXHAUST MIXER WITH OUTER LOBE CONSTRAINT BAND | Aug 2, 2016 | Abandoned |
Array
(
[id] => 12179380
[patent_doc_number] => 20180038316
[patent_country] => US
[patent_kind] => A1
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[patent_title] => 'LIQUID-FUELED ROCKET ENGINE ASSEMBLIES, AND RELATED METHODS OF USING LIQUID-FUELED ROCKET ENGINE ASSEMBLIES'
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Array
(
[id] => 12138934
[patent_doc_number] => 20180017017
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[patent_issue_date] => 2018-01-18
[patent_title] => 'RAMBURNING ENGINE WITH INLET TURBINE'
[patent_app_type] => utility
[patent_app_number] => 15/208141
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/208141 | RAMBURNING ENGINE WITH INLET TURBINE | Jul 11, 2016 | Abandoned |
Array
(
[id] => 11543136
[patent_doc_number] => 20170096962
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[patent_issue_date] => 2017-04-06
[patent_title] => 'THROAT AREA CONTROL SYSTEM'
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Array
(
[id] => 11108694
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/195383 | 3D non-axisymmetric combustor liner | Jun 27, 2016 | Issued |
Array
(
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[patent_issue_date] => 2022-08-09
[patent_title] => Jettisonable battery systems for powering electrical turbopumps for launch vehicle rocket engine systems
[patent_app_type] => utility
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Array
(
[id] => 12887368
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[patent_title] => RETRACTABLE ROCKET MOTOR IGNITER
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/738916 | RETRACTABLE ROCKET MOTOR IGNITER | Jun 20, 2016 | Abandoned |