
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] => 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
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[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
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[patent_no_of_words] => 4278
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[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
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[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
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[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
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[patent_no_of_words] => 7330
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[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
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[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
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[patent_no_of_words] => 2996
[patent_no_of_claims] => 10
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[patent_current_assignee] =>[type] => publication
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[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
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[patent_no_of_words] => 2698
[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] => 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
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[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
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[patent_no_of_words] => 10061
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[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
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[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
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/687063 | ON BOARD INERT GAS GENERATION SYSTEM | Nov 27, 2012 | Abandoned |
Array
(
[id] => 10923115
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[patent_kind] => A1
[patent_issue_date] => 2014-11-06
[patent_title] => 'ON BOARD INERT GAS GENERATION SYSTEM'
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Array
(
[id] => 10928837
[patent_doc_number] => 20140331857
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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
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[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
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[patent_kind] => A1
[patent_issue_date] => 2014-05-22
[patent_title] => 'SUPER TELESCOPING CROSS-FIRE TUBE AND METHOD OF ASSEMBLING A COMBUSTOR STRUCTURE'
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[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
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[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
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[patent_issue_date] => 2016-07-05
[patent_title] => 'Rotor resonance disturbance rejection controller'
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Array
(
[id] => 16843732
[patent_doc_number] => 11015808
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[patent_issue_date] => 2021-05-25
[patent_title] => Aerodynamically enhanced premixer with purge slots for reduced emissions
[patent_app_type] => utility
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[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
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[patent_issue_date] => 2013-03-28
[patent_title] => 'SYSTEMS AND METHODS INVOLVING IMPROVED FUEL ATOMIZATION IN AIR BLAST FUEL NOZZLES OF GAS TURBINE ENGINES'
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