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] => 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 [patent_figures_cnt] => 9 [patent_no_of_words] => 4611 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 242 [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 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [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 [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] => 15359948 [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 [patent_figures_cnt] => 0 [patent_no_of_words] => 5291 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 86 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [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 [patent_figures_cnt] => 0 [patent_no_of_words] => 562 [patent_no_of_claims] => 2 [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] => 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 [patent_words_short_claim] => 2 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [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 [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] => 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 [patent_figures_cnt] => 0 [patent_no_of_words] => 3792 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -10 [patent_words_short_claim] => 198 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [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 [patent_words_short_claim] => 241 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [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 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 2849 [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] => 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 [patent_app_number] => 15/229094 [patent_app_country] => US [patent_app_date] => 2016-08-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 1642 [patent_no_of_claims] => 9 [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] => 15229094 [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' [patent_app_type] => utility [patent_app_number] => 15/227031 [patent_app_country] => US [patent_app_date] => 2016-08-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 3295 [patent_no_of_claims] => 12 [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] => 15227031 [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' [patent_app_type] => utility [patent_app_number] => 15/227599 [patent_app_country] => US [patent_app_date] => 2016-08-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 3472 [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] => 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 [patent_issue_date] => 2018-02-08 [patent_title] => 'LIQUID-FUELED ROCKET ENGINE ASSEMBLIES, AND RELATED METHODS OF USING LIQUID-FUELED ROCKET ENGINE ASSEMBLIES' [patent_app_type] => utility [patent_app_number] => 15/226765 [patent_app_country] => US [patent_app_date] => 2016-08-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 8779 [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] => 15226765 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/226765
LIQUID-FUELED ROCKET ENGINE ASSEMBLIES, AND RELATED METHODS OF USING LIQUID-FUELED ROCKET ENGINE ASSEMBLIES Aug 1, 2016 Abandoned
Array ( [id] => 12138934 [patent_doc_number] => 20180017017 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2018-01-18 [patent_title] => 'RAMBURNING ENGINE WITH INLET TURBINE' [patent_app_type] => utility [patent_app_number] => 15/208141 [patent_app_country] => US [patent_app_date] => 2016-07-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 8490 [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] => 15208141 [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 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2017-04-06 [patent_title] => 'THROAT AREA CONTROL SYSTEM' [patent_app_type] => utility [patent_app_number] => 15/204205 [patent_app_country] => US [patent_app_date] => 2016-07-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 2507 [patent_no_of_claims] => 16 [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] => 15204205 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/204205
THROAT AREA CONTROL SYSTEM Jul 6, 2016 Abandoned
Array ( [id] => 11108694 [patent_doc_number] => 20160305664 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2016-10-20 [patent_title] => '3D NON-AXISYMMETRIC COMBUSTOR LINER' [patent_app_type] => utility [patent_app_number] => 15/195383 [patent_app_country] => US [patent_app_date] => 2016-06-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 4013 [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] => 15195383 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/195383
3D non-axisymmetric combustor liner Jun 27, 2016 Issued
Array ( [id] => 17785258 [patent_doc_number] => 11408373 [patent_country] => US [patent_kind] => B1 [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 [patent_app_number] => 15/192251 [patent_app_country] => US [patent_app_date] => 2016-06-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 13 [patent_figures_cnt] => 18 [patent_no_of_words] => 11305 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 417 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15192251 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/192251
Jettisonable battery systems for powering electrical turbopumps for launch vehicle rocket engine systems Jun 23, 2016 Issued
Array ( [id] => 12887368 [patent_doc_number] => 20180187631 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2018-07-05 [patent_title] => RETRACTABLE ROCKET MOTOR IGNITER [patent_app_type] => utility [patent_app_number] => 15/738916 [patent_app_country] => US [patent_app_date] => 2016-06-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 4191 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -9 [patent_words_short_claim] => 93 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15738916 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/738916
RETRACTABLE ROCKET MOTOR IGNITER Jun 20, 2016 Abandoned
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