
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 number | Title of the application | Filing Date | Status |
|---|---|---|---|
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
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[patent_no_of_words] => 2888
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[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
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[patent_no_of_words] => 2910
[patent_no_of_claims] => 22
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[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
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[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
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[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
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[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
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[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
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[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
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[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
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[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 |