
Lorne Edward Meade
Examiner (ID: 6709, Phone: (571)270-7570 , Office: P/3741 )
| Most Active Art Unit | 3741 |
| Art Unit(s) | 3741 |
| Total Applications | 713 |
| Issued Applications | 362 |
| Pending Applications | 77 |
| Abandoned Applications | 288 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 8581491
[patent_doc_number] => 20130000312
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-01-03
[patent_title] => 'TURBOMACHINE COMBUSTOR ASSEMBLY INCLUDING A VORTEX MODIFICATION SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 13/173951
[patent_app_country] => US
[patent_app_date] => 2011-06-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 2726
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13173951
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/173951 | Turbomachine combustor assembly including a vortex modification system | Jun 29, 2011 | Issued |
Array
(
[id] => 9848468
[patent_doc_number] => 08950189
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-02-10
[patent_title] => 'Gas turbine engine staged fuel injection using adjacent bluff body and swirler fuel injectors'
[patent_app_type] => utility
[patent_app_number] => 13/170406
[patent_app_country] => US
[patent_app_date] => 2011-06-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[patent_no_of_words] => 1450
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13170406
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/170406 | Gas turbine engine staged fuel injection using adjacent bluff body and swirler fuel injectors | Jun 27, 2011 | Issued |
Array
(
[id] => 8562327
[patent_doc_number] => 20120324898
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-12-27
[patent_title] => 'COMBUSTOR ASSEMBLY FOR USE IN A TURBINE ENGINE AND METHODS OF ASSEMBLING SAME'
[patent_app_type] => utility
[patent_app_number] => 13/164948
[patent_app_country] => US
[patent_app_date] => 2011-06-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13164948
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/164948 | COMBUSTOR ASSEMBLY FOR USE IN A TURBINE ENGINE AND METHODS OF ASSEMBLING SAME | Jun 20, 2011 | Abandoned |
Array
(
[id] => 7665562
[patent_doc_number] => 20110314831
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-12-29
[patent_title] => 'SECONDARY WATER INJECTION FOR DIFFUSION COMBUSTION SYSTEMS'
[patent_app_type] => utility
[patent_app_number] => 13/163826
[patent_app_country] => US
[patent_app_date] => 2011-06-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[patent_no_of_words] => 1382
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13163826
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/163826 | SECONDARY WATER INJECTION FOR DIFFUSION COMBUSTION SYSTEMS | Jun 19, 2011 | Abandoned |
Array
(
[id] => 8518584
[patent_doc_number] => 20120317992
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-12-20
[patent_title] => 'FEED INJECTOR FOR GASIFICATION SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 13/162623
[patent_app_country] => US
[patent_app_date] => 2011-06-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/162623 | FEED INJECTOR FOR GASIFICATION SYSTEM | Jun 16, 2011 | Abandoned |
Array
(
[id] => 10643114
[patent_doc_number] => 09359973
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-06-07
[patent_title] => 'Multitube valveless pulse detonation engine'
[patent_app_type] => utility
[patent_app_number] => 13/160840
[patent_app_country] => US
[patent_app_date] => 2011-06-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[patent_no_of_words] => 3675
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13160840
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/160840 | Multitube valveless pulse detonation engine | Jun 14, 2011 | Issued |
Array
(
[id] => 8498372
[patent_doc_number] => 20120297780
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-11-29
[patent_title] => 'ACTIVE FUEL TEMPERATURE CONTROL'
[patent_app_type] => utility
[patent_app_number] => 13/113347
[patent_app_country] => US
[patent_app_date] => 2011-05-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_no_of_words] => 2928
[patent_no_of_claims] => 21
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13113347
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/113347 | ACTIVE FUEL TEMPERATURE CONTROL | May 22, 2011 | Abandoned |
Array
(
[id] => 8693709
[patent_doc_number] => 20130055718
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-03-07
[patent_title] => 'DEVICE FOR REDUCING THE NOISE EMITTED BY THE JET OF AN AIRCRAFT PROPULSION ENGINE'
[patent_app_type] => utility
[patent_app_number] => 13/696821
[patent_app_country] => US
[patent_app_date] => 2011-05-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2238
[patent_no_of_claims] => 7
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13696821
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/696821 | Device for reducing the noise emitted by the jet of an aircraft propulsion engine | May 10, 2011 | Issued |
Array
(
[id] => 9941901
[patent_doc_number] => 08991185
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-03-31
[patent_title] => 'Combustion device for a gas turbine configured to suppress thermo-acoustical pulsations'
[patent_app_type] => utility
[patent_app_number] => 13/097221
[patent_app_country] => US
[patent_app_date] => 2011-04-29
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13097221
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/097221 | Combustion device for a gas turbine configured to suppress thermo-acoustical pulsations | Apr 28, 2011 | Issued |
Array
(
[id] => 9387226
[patent_doc_number] => 08683812
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-04-01
[patent_title] => 'Arrangement for controlling fluid jets injected into a fluid stream of a bleed air discharge nozzle'
[patent_app_type] => utility
[patent_app_number] => 13/094881
[patent_app_country] => US
[patent_app_date] => 2011-04-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 8
[patent_no_of_words] => 4105
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13094881
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/094881 | Arrangement for controlling fluid jets injected into a fluid stream of a bleed air discharge nozzle | Apr 26, 2011 | Issued |
Array
(
[id] => 8763814
[patent_doc_number] => 20130091851
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-04-18
[patent_title] => 'METHOD AND A DEVICE FOR PRODUCING A SETPOINT SIGNAL'
[patent_app_type] => utility
[patent_app_number] => 13/640819
[patent_app_country] => US
[patent_app_date] => 2011-04-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13640819
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/640819 | Method and a device for producing a setpoint signal | Apr 11, 2011 | Issued |
Array
(
[id] => 9815551
[patent_doc_number] => 08925325
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-01-06
[patent_title] => 'Recirculating product injection nozzle'
[patent_app_type] => utility
[patent_app_number] => 13/083298
[patent_app_country] => US
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/083298 | Recirculating product injection nozzle | Apr 7, 2011 | Issued |
Array
(
[id] => 9848449
[patent_doc_number] => 08950170
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-02-10
[patent_title] => 'Aircraft fuel system cooling flow device'
[patent_app_type] => utility
[patent_app_number] => 13/042538
[patent_app_country] => US
[patent_app_date] => 2011-03-08
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/042538 | Aircraft fuel system cooling flow device | Mar 7, 2011 | Issued |
Array
(
[id] => 8849839
[patent_doc_number] => 20130139514
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-06-06
[patent_title] => 'COMBUSTOR LINER SUPPORT AND SEAL ASSEMBLY'
[patent_app_type] => utility
[patent_app_number] => 13/042393
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13042393
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/042393 | COMBUSTOR LINER SUPPORT AND SEAL ASSEMBLY | Mar 6, 2011 | Abandoned |
Array
(
[id] => 13015525
[patent_doc_number] => 10030872
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2018-07-24
[patent_title] => Combustor mixing joint with flow disruption surface
[patent_app_type] => utility
[patent_app_number] => 13/036084
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/036084 | Combustor mixing joint with flow disruption surface | Feb 27, 2011 | Issued |
Array
(
[id] => 6041173
[patent_doc_number] => 20110203250
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-08-25
[patent_title] => 'COMBUSTION DEVICE FOR A GAS TURBINE'
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[pdf_file] => publications/A1/0203/20110203250.pdf
[firstpage_image] =>[orig_patent_app_number] => 13031654
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/031654 | Combustion device with a layered wall structure for a gas turbine | Feb 21, 2011 | Issued |
Array
(
[id] => 6056952
[patent_doc_number] => 20110197591
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-08-18
[patent_title] => 'AXIALLY STAGED PREMIXED COMBUSTION CHAMBER'
[patent_app_type] => utility
[patent_app_number] => 13/025307
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[pdf_file] => publications/A1/0197/20110197591.pdf
[firstpage_image] =>[orig_patent_app_number] => 13025307
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/025307 | AXIALLY STAGED PREMIXED COMBUSTION CHAMBER | Feb 10, 2011 | Abandoned |
Array
(
[id] => 8537008
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[patent_issue_date] => 2012-11-20
[patent_title] => 'Mixer assembly for a gas turbine engine having a pilot mixer with a corner flame stabilizing recirculation zone'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/014434 | Mixer assembly for a gas turbine engine having a pilot mixer with a corner flame stabilizing recirculation zone | Jan 25, 2011 | Issued |
Array
(
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[patent_title] => 'SYSTEM AND METHOD FOR A GAS TURBINE EXHAUST DIFFUSER'
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Array
(
[id] => 12712177
[patent_doc_number] => 20180129225
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[patent_kind] => A1
[patent_issue_date] => 2018-05-10
[patent_title] => MONOLITHIC ATTITUDE CONTROL MOTOR FRAME AND SYSTEM
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15564942
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/564942 | Monolithic attitude control motor frame and system | Jan 13, 2011 | Issued |