
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] => 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
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 7
[patent_no_of_words] => 2913
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 181
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[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
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 123
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[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
[patent_figures_cnt] => 4
[patent_no_of_words] => 4292
[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] => 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
[patent_app_date] => 2011-04-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 13
[patent_no_of_words] => 9886
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 310
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13083298
[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
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 3
[patent_no_of_words] => 1407
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 119
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13042538
[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
[patent_app_country] => US
[patent_app_date] => 2011-03-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 3974
[patent_no_of_claims] => 17
[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] => 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
[patent_app_country] => US
[patent_app_date] => 2011-02-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 8
[patent_no_of_words] => 2250
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 144
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13036084
[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'
[patent_app_type] => utility
[patent_app_number] => 13/031654
[patent_app_country] => US
[patent_app_date] => 2011-02-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2523
[patent_no_of_claims] => 15
[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] => 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
[patent_app_country] => US
[patent_app_date] => 2011-02-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2125
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 3
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[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
[patent_doc_number] => 08312724
[patent_country] => US
[patent_kind] => B2
[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'
[patent_app_type] => utility
[patent_app_number] => 13/014434
[patent_app_country] => US
[patent_app_date] => 2011-01-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 3
[patent_no_of_words] => 3696
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 211
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13014434
[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
(
[id] => 8309229
[patent_doc_number] => 20120186261
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-07-26
[patent_title] => 'SYSTEM AND METHOD FOR A GAS TURBINE EXHAUST DIFFUSER'
[patent_app_type] => utility
[patent_app_number] => 13/010272
[patent_app_country] => US
[patent_app_date] => 2011-01-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
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[patent_no_of_words] => 5801
[patent_no_of_claims] => 20
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13010272
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/010272 | SYSTEM AND METHOD FOR A GAS TURBINE EXHAUST DIFFUSER | Jan 19, 2011 | Abandoned |
Array
(
[id] => 12712177
[patent_doc_number] => 20180129225
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2018-05-10
[patent_title] => MONOLITHIC ATTITUDE CONTROL MOTOR FRAME AND SYSTEM
[patent_app_type] => utility
[patent_app_number] => 15/564942
[patent_app_country] => US
[patent_app_date] => 2011-01-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
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[patent_no_of_words] => 3207
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[patent_current_assignee] =>[type] => publication
[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 |
Array
(
[id] => 6096510
[patent_doc_number] => 20110162339
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-07-07
[patent_title] => 'FLOW DISTRIBUTION OF GAS TURBINE EXHAUST USING WALLS SHAPED TO FACILITATE IMPROVED GAS FLOW'
[patent_app_type] => utility
[patent_app_number] => 12/986657
[patent_app_country] => US
[patent_app_date] => 2011-01-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[patent_no_of_words] => 2126
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0162/20110162339.pdf
[firstpage_image] =>[orig_patent_app_number] => 12986657
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/986657 | FLOW DISTRIBUTION OF GAS TURBINE EXHAUST USING WALLS SHAPED TO FACILITATE IMPROVED GAS FLOW | Jan 6, 2011 | Abandoned |
Array
(
[id] => 8247572
[patent_doc_number] => 20120151896
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-06-21
[patent_title] => 'HOT GAS PATH COMPONENT COOLING FOR HYBRID PULSE DETONATION COMBUSTION SYSTEMS'
[patent_app_type] => utility
[patent_app_number] => 12/974085
[patent_app_country] => US
[patent_app_date] => 2010-12-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_no_of_words] => 5373
[patent_no_of_claims] => 26
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0151/20120151896.pdf
[firstpage_image] =>[orig_patent_app_number] => 12974085
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/974085 | Hot gas path component cooling for hybrid pulse detonation combustion systems | Dec 20, 2010 | Issued |
Array
(
[id] => 8247604
[patent_doc_number] => 20120151930
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-06-21
[patent_title] => 'FUEL ATOMIZATION DUAL ORIFICE FUEL NOZZLE'
[patent_app_type] => utility
[patent_app_number] => 12/971597
[patent_app_country] => US
[patent_app_date] => 2010-12-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
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[patent_no_of_words] => 4519
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0151/20120151930.pdf
[firstpage_image] =>[orig_patent_app_number] => 12971597
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/971597 | Fuel atomization dual orifice fuel nozzle | Dec 16, 2010 | Issued |
Array
(
[id] => 6174684
[patent_doc_number] => 20110120137
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-05-26
[patent_title] => 'CARBON CAPTURE WITH POWER GENERATION'
[patent_app_type] => utility
[patent_app_number] => 12/951541
[patent_app_country] => US
[patent_app_date] => 2010-11-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[patent_no_of_words] => 5748
[patent_no_of_claims] => 28
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0120/20110120137.pdf
[firstpage_image] =>[orig_patent_app_number] => 12951541
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/951541 | Carbon capture with power generation | Nov 21, 2010 | Issued |
Array
(
[id] => 8480189
[patent_doc_number] => 20120279596
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-11-08
[patent_title] => 'Arrangement for Influencing an Exhaust Gas Flow'
[patent_app_type] => utility
[patent_app_number] => 13/510765
[patent_app_country] => US
[patent_app_date] => 2010-11-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13510765
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/510765 | Arrangement for influencing an exhaust gas flow | Nov 17, 2010 | Issued |
Array
(
[id] => 5994084
[patent_doc_number] => 20110113784
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-05-19
[patent_title] => 'Swirler Vane, Swirler and Burner Assembly'
[patent_app_type] => utility
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[firstpage_image] =>[orig_patent_app_number] => 12947080
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/947080 | Swirler Vane, Swirler and Burner Assembly | Nov 15, 2010 | Abandoned |
Array
(
[id] => 8389529
[patent_doc_number] => 20120227373
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[patent_kind] => A1
[patent_issue_date] => 2012-09-13
[patent_title] => 'COMBUSTION CHAMBER HAVING A VENTILATED SPARK PLUG'
[patent_app_type] => utility
[patent_app_number] => 13/509815
[patent_app_country] => US
[patent_app_date] => 2010-11-15
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13509815
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/509815 | Combustion chamber having a ventilated spark plug | Nov 14, 2010 | Issued |
Array
(
[id] => 8177759
[patent_doc_number] => 20120111017
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-05-10
[patent_title] => 'PARTICULATE DEFLAGRATION TURBOJET'
[patent_app_type] => utility
[patent_app_number] => 12/943262
[patent_app_country] => US
[patent_app_date] => 2010-11-10
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0111/20120111017.pdf
[firstpage_image] =>[orig_patent_app_number] => 12943262
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/943262 | PARTICULATE DEFLAGRATION TURBOJET | Nov 9, 2010 | Abandoned |