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] => 9258506 [patent_doc_number] => 20130340435 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-12-26 [patent_title] => 'GAS TURBINE ENGINE AFT SPOOL BEARING ARRANGEMENT AND HUB WALL CONFIGURATION' [patent_app_type] => utility [patent_app_number] => 13/364502 [patent_app_country] => US [patent_app_date] => 2012-02-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 2948 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 6 [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] => 13364502 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/364502
GAS TURBINE ENGINE AFT SPOOL BEARING ARRANGEMENT AND HUB WALL CONFIGURATION Feb 1, 2012 Abandoned
Array ( [id] => 8946455 [patent_doc_number] => 20130192235 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-08-01 [patent_title] => 'INTERNAL MANIFOLD FOR TURNING MID-TURBINE FRAME FLOW DISTRIBUTION' [patent_app_type] => utility [patent_app_number] => 13/360988 [patent_app_country] => US [patent_app_date] => 2012-01-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 3459 [patent_no_of_claims] => 30 [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] => 13360988 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/360988
Internal manifold for turning mid-turbine frame flow distribution Jan 29, 2012 Issued
Array ( [id] => 8286257 [patent_doc_number] => 20120174586 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-07-12 [patent_title] => 'DUCT WITH TRANSITION SECTION FOR TURBINE EXHAUST' [patent_app_type] => utility [patent_app_number] => 13/358346 [patent_app_country] => US [patent_app_date] => 2012-01-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 4677 [patent_no_of_claims] => 6 [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] => 13358346 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/358346
DUCT WITH TRANSITION SECTION FOR TURBINE EXHAUST Jan 24, 2012 Abandoned
Array ( [id] => 10116371 [patent_doc_number] => 09151244 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2015-10-06 [patent_title] => 'Aircraft jet engine comprising a system for reducing the noise generated by the ejection of the gases' [patent_app_type] => utility [patent_app_number] => 13/357065 [patent_app_country] => US [patent_app_date] => 2012-01-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 4068 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 173 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13357065 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/357065
Aircraft jet engine comprising a system for reducing the noise generated by the ejection of the gases Jan 23, 2012 Issued
Array ( [id] => 8924488 [patent_doc_number] => 20130180248 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-07-18 [patent_title] => 'Combustor Nozzle/Premixer with Curved Sections' [patent_app_type] => utility [patent_app_number] => 13/352814 [patent_app_country] => US [patent_app_date] => 2012-01-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 1683 [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] => 13352814 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/352814
Combustor Nozzle/Premixer with Curved Sections Jan 17, 2012 Abandoned
Array ( [id] => 8924496 [patent_doc_number] => 20130180256 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-07-18 [patent_title] => 'TURBINE FUEL NOZZLE ASSEMBLY AND METHOD FOR OPERATING A TURBINE' [patent_app_type] => utility [patent_app_number] => 13/351815 [patent_app_country] => US [patent_app_date] => 2012-01-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 2222 [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] => 13351815 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/351815
TURBINE FUEL NOZZLE ASSEMBLY AND METHOD FOR OPERATING A TURBINE Jan 16, 2012 Abandoned
Array ( [id] => 8924494 [patent_doc_number] => 20130180254 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-07-18 [patent_title] => 'SYSTEM AND METHOD FOR SUPPLYING A WORKING FLUID TO A COMBUSTOR' [patent_app_type] => utility [patent_app_number] => 13/349906 [patent_app_country] => US [patent_app_date] => 2012-01-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 3333 [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] => 13349906 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/349906
System and method for supplying a working fluid to a combustor via a non-uniform distribution manifold Jan 12, 2012 Issued
Array ( [id] => 8924493 [patent_doc_number] => 20130180253 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-07-18 [patent_title] => 'SYSTEM AND METHOD FOR SUPPLYING A WORKING FLUID TO A COMBUSTOR' [patent_app_type] => utility [patent_app_number] => 13/349886 [patent_app_country] => US [patent_app_date] => 2012-01-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2701 [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] => 13349886 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/349886
SYSTEM AND METHOD FOR SUPPLYING A WORKING FLUID TO A COMBUSTOR Jan 12, 2012 Abandoned
Array ( [id] => 8378769 [patent_doc_number] => 20120222398 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-09-06 [patent_title] => 'GAS TURBINE ENGINE WITH GEARED ARCHITECTURE' [patent_app_type] => utility [patent_app_number] => 13/346100 [patent_app_country] => US [patent_app_date] => 2012-01-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 3198 [patent_no_of_claims] => 18 [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] => 13346100 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/346100
GAS TURBINE ENGINE WITH GEARED ARCHITECTURE Jan 8, 2012 Abandoned
Array ( [id] => 8912909 [patent_doc_number] => 20130174534 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-07-11 [patent_title] => 'SYSTEM AND DEVICE FOR CONTROLLING FLUID FLOW THROUGH A GAS TURBINE EXHAUST' [patent_app_type] => utility [patent_app_number] => 13/344422 [patent_app_country] => US [patent_app_date] => 2012-01-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 4879 [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] => 13344422 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/344422
SYSTEM AND DEVICE FOR CONTROLLING FLUID FLOW THROUGH A GAS TURBINE EXHAUST Jan 4, 2012 Abandoned
Array ( [id] => 8163544 [patent_doc_number] => 20120102915 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-05-03 [patent_title] => 'GAS TURBINE ENGINE BIFURCATION LOCATED FAN VARIABLE AREA NOZZLE' [patent_app_type] => utility [patent_app_number] => 13/343964 [patent_app_country] => US [patent_app_date] => 2012-01-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2935 [patent_no_of_claims] => 29 [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] => publications/A1/0102/20120102915.pdf [firstpage_image] =>[orig_patent_app_number] => 13343964 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/343964
Gas turbine engine bifurcation located fan variable area nozzle Jan 4, 2012 Issued
Array ( [id] => 10516465 [patent_doc_number] => 09243506 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2016-01-26 [patent_title] => 'Methods and systems for cooling a transition nozzle' [patent_app_type] => utility [patent_app_number] => 13/342475 [patent_app_country] => US [patent_app_date] => 2012-01-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 2888 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 194 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13342475 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/342475
Methods and systems for cooling a transition nozzle Jan 2, 2012 Issued
Array ( [id] => 8900328 [patent_doc_number] => 20130167831 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-07-04 [patent_title] => 'THERMAL INSULATOR HAVING INFRARED-REFLECTIVE COATING' [patent_app_type] => utility [patent_app_number] => 13/342538 [patent_app_country] => US [patent_app_date] => 2012-01-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 2910 [patent_no_of_claims] => 22 [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] => 13342538 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/342538
THERMAL INSULATOR HAVING INFRARED-REFLECTIVE COATING Jan 2, 2012 Abandoned
Array ( [id] => 8273671 [patent_doc_number] => 20120167550 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-07-05 [patent_title] => 'THRUST AUGMENTED GAS TURBINE ENGINE' [patent_app_type] => utility [patent_app_number] => 13/337993 [patent_app_country] => US [patent_app_date] => 2011-12-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 3430 [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] => 13337993 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/337993
THRUST AUGMENTED GAS TURBINE ENGINE Dec 26, 2011 Abandoned
Array ( [id] => 8838228 [patent_doc_number] => 20130133857 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-05-30 [patent_title] => 'Exhaust impingement cooling' [patent_app_type] => utility [patent_app_number] => 13/307741 [patent_app_country] => US [patent_app_date] => 2011-11-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 2268 [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] => 13307741 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/307741
Exhaust impingement cooling Nov 29, 2011 Issued
Array ( [id] => 9134236 [patent_doc_number] => 20130294950 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-11-07 [patent_title] => 'ON BOARD INERT GAS GENERATION SYSTEM' [patent_app_type] => utility [patent_app_number] => 13/991930 [patent_app_country] => US [patent_app_date] => 2011-11-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 3704 [patent_no_of_claims] => 18 [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] => 13991930 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/991930
On board inert gas generation system with rotary positive displacement compressor Nov 28, 2011 Issued
Array ( [id] => 9176957 [patent_doc_number] => 20130318943 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-12-05 [patent_title] => 'ROCKET MOTOR COMBUSTION CHAMBER INJECTION HEAD' [patent_app_type] => utility [patent_app_number] => 13/989081 [patent_app_country] => US [patent_app_date] => 2011-11-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2198 [patent_no_of_claims] => 15 [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] => 13989081 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/989081
Rocket motor combustion chamber injection head Nov 13, 2011 Issued
Array ( [id] => 9157409 [patent_doc_number] => 20130305686 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-11-21 [patent_title] => 'COMBINED TURBOJET AND RAMJET ENGINE' [patent_app_type] => utility [patent_app_number] => 13/989070 [patent_app_country] => US [patent_app_date] => 2011-11-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 4255 [patent_no_of_claims] => 8 [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] => 13989070 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/989070
Combined turbojet and ramjet engine Nov 13, 2011 Issued
Array ( [id] => 7771233 [patent_doc_number] => 20120036828 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-02-16 [patent_title] => 'Combined Cycle Power Plant Including a Heat Recovery Steam Generator' [patent_app_type] => utility [patent_app_number] => 13/283045 [patent_app_country] => US [patent_app_date] => 2011-10-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [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] => publications/A1/0036/20120036828.pdf [firstpage_image] =>[orig_patent_app_number] => 13283045 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/283045
Combined cycle power plant including a heat recovery steam generator Oct 26, 2011 Issued
Array ( [id] => 8946466 [patent_doc_number] => 20130192246 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-08-01 [patent_title] => 'DUAL FUEL AIRCRAFT ENGINE CONTROL SYSTEM AND METHOD FOR OPERATING SAME' [patent_app_type] => utility [patent_app_number] => 13/876750 [patent_app_country] => US [patent_app_date] => 2011-09-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 9925 [patent_no_of_claims] => 25 [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] => 13876750 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/876750
DUAL FUEL AIRCRAFT ENGINE CONTROL SYSTEM AND METHOD FOR OPERATING SAME Sep 29, 2011 Abandoned
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