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] => 8985724 [patent_doc_number] => 20130213005 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-08-22 [patent_title] => 'SYSTEM AND METHOD FOR ZERO REACTION TIME COMBUSTION' [patent_app_type] => utility [patent_app_number] => 13/763297 [patent_app_country] => US [patent_app_date] => 2013-02-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 4447 [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] => 13763297 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/763297
SYSTEM AND METHOD FOR ZERO REACTION TIME COMBUSTION Feb 7, 2013 Abandoned
Array ( [id] => 10970474 [patent_doc_number] => 20140373507 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-12-25 [patent_title] => 'ROCKET ENGINE WITH OPTIMIZED FUEL SUPPLY' [patent_app_type] => utility [patent_app_number] => 14/372883 [patent_app_country] => US [patent_app_date] => 2013-01-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 4278 [patent_no_of_claims] => 9 [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] => 14372883 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/372883
ROCKET ENGINE WITH OPTIMIZED FUEL SUPPLY Jan 15, 2013 Abandoned
Array ( [id] => 9599754 [patent_doc_number] => 20140196435 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-07-17 [patent_title] => 'Space Impulse Drive' [patent_app_type] => utility [patent_app_number] => 13/740209 [patent_app_country] => US [patent_app_date] => 2013-01-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 1901 [patent_no_of_claims] => 6 [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] => 13740209 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/740209
Space Impulse Drive Jan 12, 2013 Abandoned
Array ( [id] => 9564595 [patent_doc_number] => 20140182308 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-07-03 [patent_title] => 'GAS TURBINE ENGINE WITH V-BAND CLAMP CONNECTION FOR COLLECTOR BOX' [patent_app_type] => utility [patent_app_number] => 13/729477 [patent_app_country] => US [patent_app_date] => 2012-12-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 3316 [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] => 13729477 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/729477
GAS TURBINE ENGINE WITH V-BAND CLAMP CONNECTION FOR COLLECTOR BOX Dec 27, 2012 Abandoned
Array ( [id] => 8828438 [patent_doc_number] => 20130129483 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-05-23 [patent_title] => 'CRACK AND DELAMINATION STOPPERS FOR AIRCRAFT PROPULSION SYSTEM COMPONENTS' [patent_app_type] => utility [patent_app_number] => 13/723095 [patent_app_country] => US [patent_app_date] => 2012-12-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 15 [patent_figures_cnt] => 15 [patent_no_of_words] => 7330 [patent_no_of_claims] => 13 [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] => 13723095 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/723095
CRACK AND DELAMINATION STOPPERS FOR AIRCRAFT PROPULSION SYSTEM COMPONENTS Dec 19, 2012 Abandoned
Array ( [id] => 10935327 [patent_doc_number] => 20140338348 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-11-20 [patent_title] => 'ROTARY PULSE DETONATION ENGINE' [patent_app_type] => utility [patent_app_number] => 14/365626 [patent_app_country] => US [patent_app_date] => 2012-12-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 3812 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 4 [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] => 14365626 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/365626
ROTARY PULSE DETONATION ENGINE Dec 16, 2012 Abandoned
Array ( [id] => 10949273 [patent_doc_number] => 20140352294 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-12-04 [patent_title] => 'COLD WIND GENERATION FROM SLAG HEAT' [patent_app_type] => utility [patent_app_number] => 14/365669 [patent_app_country] => US [patent_app_date] => 2012-12-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 2996 [patent_no_of_claims] => 10 [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] => 14365669 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/365669
COLD WIND GENERATION FROM SLAG HEAT Dec 13, 2012 Abandoned
Array ( [id] => 9540928 [patent_doc_number] => 20140165575 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-06-19 [patent_title] => 'NOZZLE SECTION FOR A GAS TURBINE ENGINE' [patent_app_type] => utility [patent_app_number] => 13/713819 [patent_app_country] => US [patent_app_date] => 2012-12-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 2698 [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] => 13713819 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/713819
NOZZLE SECTION FOR A GAS TURBINE ENGINE Dec 12, 2012 Abandoned
Array ( [id] => 10636453 [patent_doc_number] => 09353950 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2016-05-31 [patent_title] => 'System for reducing combustion dynamics and NOx in a combustor' [patent_app_type] => utility [patent_app_number] => 13/709320 [patent_app_country] => US [patent_app_date] => 2012-12-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 10 [patent_no_of_words] => 4802 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 275 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13709320 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/709320
System for reducing combustion dynamics and NOx in a combustor Dec 9, 2012 Issued
Array ( [id] => 10842344 [patent_doc_number] => 08869506 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-10-28 [patent_title] => 'Turbojet engine nacelle including a device for absorbing circumferential stresses' [patent_app_type] => utility [patent_app_number] => 13/692227 [patent_app_country] => US [patent_app_date] => 2012-12-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 28 [patent_no_of_words] => 10061 [patent_no_of_claims] => 7 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 431 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13692227 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/692227
Turbojet engine nacelle including a device for absorbing circumferential stresses Dec 2, 2012 Issued
Array ( [id] => 9507630 [patent_doc_number] => 20140144122 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-05-29 [patent_title] => 'CROSSFIRE TUBE ASSEMBLY BETWEEN ADJACENT COMBUSTORS' [patent_app_type] => utility [patent_app_number] => 13/688625 [patent_app_country] => US [patent_app_date] => 2012-11-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 3047 [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] => 13688625 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/688625
Crossfire tube assembly with tube bias between adjacent combustors Nov 28, 2012 Issued
Array ( [id] => 8849846 [patent_doc_number] => 20130139521 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-06-06 [patent_title] => 'ON BOARD INERT GAS GENERATION SYSTEM' [patent_app_type] => utility [patent_app_number] => 13/687063 [patent_app_country] => US [patent_app_date] => 2012-11-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 3704 [patent_no_of_claims] => 10 [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] => 13687063 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/687063
ON BOARD INERT GAS GENERATION SYSTEM Nov 27, 2012 Abandoned
Array ( [id] => 10923115 [patent_doc_number] => 20140326135 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-11-06 [patent_title] => 'ON BOARD INERT GAS GENERATION SYSTEM' [patent_app_type] => utility [patent_app_number] => 14/360666 [patent_app_country] => US [patent_app_date] => 2012-11-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 4239 [patent_no_of_claims] => 16 [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] => 14360666 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/360666
ON BOARD INERT GAS GENERATION SYSTEM Nov 26, 2012 Abandoned
Array ( [id] => 10928837 [patent_doc_number] => 20140331857 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-11-13 [patent_title] => 'ON BOARD INERT GAS GENERATION SYSTEM' [patent_app_type] => utility [patent_app_number] => 14/360655 [patent_app_country] => US [patent_app_date] => 2012-11-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 5599 [patent_no_of_claims] => 19 [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] => 14360655 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/360655
ON BOARD INERT GAS GENERATION SYSTEM Nov 26, 2012 Abandoned
Array ( [id] => 9078044 [patent_doc_number] => 20130263573 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-10-10 [patent_title] => 'Rocket Stage Having Engine Thrust Frame Integrated With Tank' [patent_app_type] => utility [patent_app_number] => 13/684729 [patent_app_country] => US [patent_app_date] => 2012-11-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 3476 [patent_no_of_claims] => 19 [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] => 13684729 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/684729
Rocket stage having engine thrust frame integrated with tank Nov 25, 2012 Issued
Array ( [id] => 9487130 [patent_doc_number] => 20140137536 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-05-22 [patent_title] => 'SUPER TELESCOPING CROSS-FIRE TUBE AND METHOD OF ASSEMBLING A COMBUSTOR STRUCTURE' [patent_app_type] => utility [patent_app_number] => 13/682965 [patent_app_country] => US [patent_app_date] => 2012-11-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 3036 [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] => 13682965 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/682965
SUPER TELESCOPING CROSS-FIRE TUBE AND METHOD OF ASSEMBLING A COMBUSTOR STRUCTURE Nov 20, 2012 Abandoned
Array ( [id] => 10915126 [patent_doc_number] => 20140318144 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-10-30 [patent_title] => 'DEVICE AND METHOD FOR SLOW TURNING OF AN AERODERIVATIVE GAS TURBINE' [patent_app_type] => utility [patent_app_number] => 14/358181 [patent_app_country] => US [patent_app_date] => 2012-11-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 6757 [patent_no_of_claims] => 29 [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] => 14358181 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/358181
DEVICE AND METHOD FOR SLOW TURNING OF AN AERODERIVATIVE GAS TURBINE Nov 12, 2012 Abandoned
Array ( [id] => 11773981 [patent_doc_number] => 09382847 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2016-07-05 [patent_title] => 'Rotor resonance disturbance rejection controller' [patent_app_type] => utility [patent_app_number] => 13/667705 [patent_app_country] => US [patent_app_date] => 2012-11-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 14 [patent_no_of_words] => 10885 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 178 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13667705 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/667705
Rotor resonance disturbance rejection controller Nov 1, 2012 Issued
Array ( [id] => 16843732 [patent_doc_number] => 11015808 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2021-05-25 [patent_title] => Aerodynamically enhanced premixer with purge slots for reduced emissions [patent_app_type] => utility [patent_app_number] => 13/657924 [patent_app_country] => US [patent_app_date] => 2012-10-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 21 [patent_figures_cnt] => 35 [patent_no_of_words] => 4512 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 357 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13657924 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/657924
Aerodynamically enhanced premixer with purge slots for reduced emissions Oct 22, 2012 Issued
Array ( [id] => 8728945 [patent_doc_number] => 20130074514 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-03-28 [patent_title] => 'SYSTEMS AND METHODS INVOLVING IMPROVED FUEL ATOMIZATION IN AIR BLAST FUEL NOZZLES OF GAS TURBINE ENGINES' [patent_app_type] => utility [patent_app_number] => 13/657088 [patent_app_country] => US [patent_app_date] => 2012-10-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 2385 [patent_no_of_claims] => 4 [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] => 13657088 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/657088
SYSTEMS AND METHODS INVOLVING IMPROVED FUEL ATOMIZATION IN AIR BLAST FUEL NOZZLES OF GAS TURBINE ENGINES Oct 21, 2012 Abandoned
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