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] => 13676589 [patent_doc_number] => 20160377028 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2016-12-29 [patent_title] => CATALYTIC N2O PILOT IGNITION SYSTEM FOR UPPER STAGE SCRAMJETS [patent_app_type] => utility [patent_app_number] => 14/272273 [patent_app_country] => US [patent_app_date] => 2014-05-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 6047 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -26 [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] => 14272273 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/272273
CATALYTIC N2O PILOT IGNITION SYSTEM FOR UPPER STAGE SCRAMJETS May 6, 2014 Abandoned
Array ( [id] => 9681269 [patent_doc_number] => 20140238031 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-08-28 [patent_title] => 'COMBUSTOR LINER' [patent_app_type] => utility [patent_app_number] => 14/270811 [patent_app_country] => US [patent_app_date] => 2014-05-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 6234 [patent_no_of_claims] => 8 [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] => 14270811 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/270811
COMBUSTOR LINER May 5, 2014 Abandoned
Array ( [id] => 10430954 [patent_doc_number] => 20150315966 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-11-05 [patent_title] => 'Hypersonic Vehicle Base Drag Reduction and Improved Inlet Performance Through Venting Forebody Bleed Air to Base Area Using Open Core Ceramic Composites' [patent_app_type] => utility [patent_app_number] => 14/267716 [patent_app_country] => US [patent_app_date] => 2014-05-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 2492 [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] => 14267716 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/267716
Hypersonic Vehicle Base Drag Reduction and Improved Inlet Performance Through Venting Forebody Bleed Air to Base Area Using Open Core Ceramic Composites Apr 30, 2014 Abandoned
Array ( [id] => 11192322 [patent_doc_number] => 09423130 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2016-08-23 [patent_title] => 'Reverse flow ceramic matrix composite combustor' [patent_app_type] => utility [patent_app_number] => 14/263070 [patent_app_country] => US [patent_app_date] => 2014-04-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 3318 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 2 [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] => 14263070 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/263070
Reverse flow ceramic matrix composite combustor Apr 27, 2014 Issued
Array ( [id] => 15728133 [patent_doc_number] => 10612493 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2020-04-07 [patent_title] => Orientable rocket-motor system [patent_app_type] => utility [patent_app_number] => 14/786143 [patent_app_country] => US [patent_app_date] => 2014-04-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 8 [patent_no_of_words] => 2478 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 148 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14786143 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/786143
Orientable rocket-motor system Apr 21, 2014 Issued
Array ( [id] => 10390816 [patent_doc_number] => 20150275823 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-10-01 [patent_title] => 'PROPULSION SYSTEM AND LAUNCH VEHICLE' [patent_app_type] => utility [patent_app_number] => 14/228306 [patent_app_country] => US [patent_app_date] => 2014-03-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 5858 [patent_no_of_claims] => 21 [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] => 14228306 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/228306
Propulsion system and launch vehicle Mar 27, 2014 Issued
Array ( [id] => 12471291 [patent_doc_number] => 09989014 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2018-06-05 [patent_title] => Premixed liquid propellant propulsion system and method with anti-flashback quenching liquid injector [patent_app_type] => utility [patent_app_number] => 14/229823 [patent_app_country] => US [patent_app_date] => 2014-03-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 14 [patent_no_of_words] => 10792 [patent_no_of_claims] => 23 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 316 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14229823 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/229823
Premixed liquid propellant propulsion system and method with anti-flashback quenching liquid injector Mar 27, 2014 Issued
Array ( [id] => 9835021 [patent_doc_number] => 20150027102 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-01-29 [patent_title] => 'TRI-PROPELLANT ROCKET ENGINE FOR SPACE LAUNCH APPLICATIONS' [patent_app_type] => utility [patent_app_number] => 14/217469 [patent_app_country] => US [patent_app_date] => 2014-03-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 3290 [patent_no_of_claims] => 7 [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] => 14217469 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/217469
TRI-PROPELLANT ROCKET ENGINE FOR SPACE LAUNCH APPLICATIONS Mar 16, 2014 Abandoned
Array ( [id] => 16642872 [patent_doc_number] => 10920714 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2021-02-16 [patent_title] => Stable hybrid rocket technology [patent_app_type] => utility [patent_app_number] => 14/212974 [patent_app_country] => US [patent_app_date] => 2014-03-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 10 [patent_no_of_words] => 2575 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 223 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14212974 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/212974
Stable hybrid rocket technology Mar 13, 2014 Issued
Array ( [id] => 10243604 [patent_doc_number] => 20150128599 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-05-14 [patent_title] => 'CONTINUOUS DETONATION COMBUSTION ENGINE AND SYSTEM' [patent_app_type] => utility [patent_app_number] => 14/213426 [patent_app_country] => US [patent_app_date] => 2014-03-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 17 [patent_figures_cnt] => 17 [patent_no_of_words] => 18588 [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] => 14213426 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/213426
Continuous detonation combustion engine and system Mar 13, 2014 Issued
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] => 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] => 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
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
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
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