Search

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 numberTitle of the applicationFiling DateStatus
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 [patent_words_short_claim] => 89 [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 [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] => 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 [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] => 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 [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] => 14202969 [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 [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] => 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 [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] => 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 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_figures_cnt] => 5 [patent_no_of_words] => 2654 [patent_no_of_claims] => 12 [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] => 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 [patent_no_of_claims] => 5 [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] => 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 [patent_figures_cnt] => 9 [patent_no_of_words] => 4310 [patent_no_of_claims] => 14 [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] => 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 [patent_app_country] => US [patent_app_date] => 2014-01-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 3211 [patent_no_of_claims] => 21 [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] => 14146758 [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 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 1939 [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] => 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 [patent_app_country] => US [patent_app_date] => 2013-12-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 3238 [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] => 14142966 [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 [patent_app_number] => 14/143356 [patent_app_country] => US [patent_app_date] => 2013-12-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 3846 [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] => 14143356 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/143356
POWER-GENERATING APPARATUS AND METHOD Dec 29, 2013 Abandoned
Array ( [id] => 10291531 [patent_doc_number] => 20150176530 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-06-25 [patent_title] => 'ULTRA HIGH OVERALL PESSURE RATIO GAS TURBINE ENGINE' [patent_app_type] => utility [patent_app_number] => 14/134281 [patent_app_country] => US [patent_app_date] => 2013-12-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 2768 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 5 [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] => 14134281 [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' [patent_app_type] => utility [patent_app_number] => 14/768830 [patent_app_country] => US [patent_app_date] => 2013-12-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 4364 [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] => 14768830 [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 [patent_doc_number] => 20150167550 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-06-18 [patent_title] => 'SYSTEM AND METHOD FOR PROCESSING GAS STREAMS' [patent_app_type] => utility [patent_app_number] => 14/132198 [patent_app_country] => US [patent_app_date] => 2013-12-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 4610 [patent_no_of_claims] => 27 [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] => 14132198 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/132198
SYSTEM AND METHOD FOR PROCESSING GAS STREAMS Dec 17, 2013 Abandoned
Array ( [id] => 10282982 [patent_doc_number] => 20150167980 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-06-18 [patent_title] => 'AXIAL STAGE INJECTION DUAL FREQUENCY RESONATOR FOR A COMBUSTOR OF A GAS TURBINE ENGINE' [patent_app_type] => utility [patent_app_number] => 14/132007 [patent_app_country] => US [patent_app_date] => 2013-12-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 3213 [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] => 14132007 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/132007
AXIAL STAGE INJECTION DUAL FREQUENCY RESONATOR FOR A COMBUSTOR OF A GAS TURBINE ENGINE Dec 17, 2013 Abandoned
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