
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] => 6384404
[patent_doc_number] => 20100162703
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-07-01
[patent_title] => 'PROCESS FOR REDUCING CARBON DIOXIDE EMISSION IN A POWER PLANT'
[patent_app_type] => utility
[patent_app_number] => 12/524177
[patent_app_country] => US
[patent_app_date] => 2008-01-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 3471
[patent_no_of_claims] => 10
[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/A1/0162/20100162703.pdf
[firstpage_image] =>[orig_patent_app_number] => 12524177
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/524177 | PROCESS FOR REDUCING CARBON DIOXIDE EMISSION IN A POWER PLANT | Jan 22, 2008 | Abandoned |
Array
(
[id] => 8537010
[patent_doc_number] => 08312726
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-11-20
[patent_title] => 'Gas turbine engine systems involving I-beam struts'
[patent_app_type] => utility
[patent_app_number] => 11/962653
[patent_app_country] => US
[patent_app_date] => 2007-12-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 5
[patent_no_of_words] => 2026
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 67
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 11962653
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/962653 | Gas turbine engine systems involving I-beam struts | Dec 20, 2007 | Issued |
Array
(
[id] => 5418678
[patent_doc_number] => 20090145132
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-06-11
[patent_title] => 'METHODS AND SYSTEM FOR REDUCING PRESSURE LOSSES IN GAS TURBINE ENGINES'
[patent_app_type] => utility
[patent_app_number] => 11/952165
[patent_app_country] => US
[patent_app_date] => 2007-12-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 3563
[patent_no_of_claims] => 23
[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/A1/0145/20090145132.pdf
[firstpage_image] =>[orig_patent_app_number] => 11952165
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/952165 | METHODS AND SYSTEM FOR REDUCING PRESSURE LOSSES IN GAS TURBINE ENGINES | Dec 6, 2007 | Abandoned |
| 11/948348 | Rotary Mechanically Reciprocated Sliding Metal Vane Air Pump and Boundary Layer Gas Turbines Integrated with a Pulse Gas Turbine Engine System | Nov 29, 2007 | Abandoned |
Array
(
[id] => 4895887
[patent_doc_number] => 20080115500
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-05-22
[patent_title] => 'Combustion of water borne fuels in an oxy-combustion gas generator'
[patent_app_type] => utility
[patent_app_number] => 11/985399
[patent_app_country] => US
[patent_app_date] => 2007-11-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 5638
[patent_no_of_claims] => 24
[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/A1/0115/20080115500.pdf
[firstpage_image] =>[orig_patent_app_number] => 11985399
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/985399 | Combustion of water borne fuels in an oxy-combustion gas generator | Nov 13, 2007 | Abandoned |
Array
(
[id] => 8569682
[patent_doc_number] => 08336314
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-12-25
[patent_title] => 'Method of manufacturing a nozzle arrangement and method for in-situ repairing a nozzle arrangement'
[patent_app_type] => utility
[patent_app_number] => 12/439749
[patent_app_country] => US
[patent_app_date] => 2007-09-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 19
[patent_no_of_words] => 6278
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 113
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12439749
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/439749 | Method of manufacturing a nozzle arrangement and method for in-situ repairing a nozzle arrangement | Sep 3, 2007 | Issued |
Array
(
[id] => 6482749
[patent_doc_number] => 20100199632
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-08-12
[patent_title] => 'SOLUTE ION COULOMB FORCE ACCELARATION AND ELECTRIC FIELD MONOPOLE PASSIVE VOLTAGE SOURCE'
[patent_app_type] => utility
[patent_app_number] => 12/733322
[patent_app_country] => US
[patent_app_date] => 2007-08-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 73
[patent_figures_cnt] => 73
[patent_no_of_words] => 83637
[patent_no_of_claims] => 106
[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/A1/0199/20100199632.pdf
[firstpage_image] =>[orig_patent_app_number] => 12733322
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/733322 | Solute ion coulomb force accelaration and electric field monopole passive voltage source | Aug 22, 2007 | Issued |
Array
(
[id] => 4694326
[patent_doc_number] => 20080216510
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-09-11
[patent_title] => 'Combined Cycle System For Gas Turbines and Reciprocating Engines and a Method for the Use of Air as Working Fluid in Combined Cycle Power Plants'
[patent_app_type] => utility
[patent_app_number] => 11/843309
[patent_app_country] => US
[patent_app_date] => 2007-08-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 6383
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0216/20080216510.pdf
[firstpage_image] =>[orig_patent_app_number] => 11843309
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/843309 | Combined Cycle System For Gas Turbines and Reciprocating Engines and a Method for the Use of Air as Working Fluid in Combined Cycle Power Plants | Aug 21, 2007 | Abandoned |
Array
(
[id] => 5370490
[patent_doc_number] => 20090308049
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-12-17
[patent_title] => 'ELECTRIC PROPULSION SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 12/374117
[patent_app_country] => US
[patent_app_date] => 2007-07-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2610
[patent_no_of_claims] => 15
[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/A1/0308/20090308049.pdf
[firstpage_image] =>[orig_patent_app_number] => 12374117
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/374117 | ELECTRIC PROPULSION SYSTEM | Jul 17, 2007 | Abandoned |
Array
(
[id] => 6578160
[patent_doc_number] => 20100000227
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-01-07
[patent_title] => 'AIR INTAKE FOR AN AIRCRAFT TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 12/307881
[patent_app_country] => US
[patent_app_date] => 2007-07-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 1421
[patent_no_of_claims] => 7
[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/A1/0000/20100000227.pdf
[firstpage_image] =>[orig_patent_app_number] => 12307881
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/307881 | AIR INTAKE FOR AN AIRCRAFT TURBINE ENGINE | Jul 3, 2007 | Abandoned |
Array
(
[id] => 5348636
[patent_doc_number] => 20090003997
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-01-01
[patent_title] => 'VARIABLE SHAPE INLET SECTION FOR A NACELLE ASSEMBLY OF A GAS TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 11/769749
[patent_app_country] => US
[patent_app_date] => 2007-06-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 3903
[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] => publications/A1/0003/20090003997.pdf
[firstpage_image] =>[orig_patent_app_number] => 11769749
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/769749 | Variable shape inlet section for a nacelle assembly of a gas turbine engine | Jun 27, 2007 | Issued |
Array
(
[id] => 5363540
[patent_doc_number] => 20090301099
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-12-10
[patent_title] => 'Power Generation'
[patent_app_type] => utility
[patent_app_number] => 12/306076
[patent_app_country] => US
[patent_app_date] => 2007-06-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 3271
[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] => publications/A1/0301/20090301099.pdf
[firstpage_image] =>[orig_patent_app_number] => 12306076
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/306076 | Power Generation | Jun 21, 2007 | Abandoned |
Array
(
[id] => 6275776
[patent_doc_number] => 20100154423
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-06-24
[patent_title] => ' SYSTEM FOR MIXING GAS FLOWS IN A GAS TURBINE ENGINE, GAS TURBINE ENGINE AND AN AIRCRAFT ENGINE'
[patent_app_type] => utility
[patent_app_number] => 12/600261
[patent_app_country] => US
[patent_app_date] => 2007-06-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 5656
[patent_no_of_claims] => 23
[patent_no_of_ind_claims] => 4
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0154/20100154423.pdf
[firstpage_image] =>[orig_patent_app_number] => 12600261
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/600261 | SYSTEM FOR MIXING GAS FLOWS IN A GAS TURBINE ENGINE, GAS TURBINE ENGINE AND AN AIRCRAFT ENGINE | Jun 3, 2007 | Abandoned |
Array
(
[id] => 10855345
[patent_doc_number] => 08881529
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-11-11
[patent_title] => 'Modular fuel supply device for a gas turbine including a fuel supply device having an integrated control device'
[patent_app_type] => utility
[patent_app_number] => 12/297935
[patent_app_country] => US
[patent_app_date] => 2007-05-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 1
[patent_no_of_words] => 1369
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 198
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12297935
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/297935 | Modular fuel supply device for a gas turbine including a fuel supply device having an integrated control device | May 8, 2007 | Issued |
Array
(
[id] => 6400414
[patent_doc_number] => 20100139286
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-06-10
[patent_title] => 'BURNER AND FUEL SUPPLY FOR A GAS TURBINE'
[patent_app_type] => utility
[patent_app_number] => 12/521930
[patent_app_country] => US
[patent_app_date] => 2007-04-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 4596
[patent_no_of_claims] => 21
[patent_no_of_ind_claims] => 4
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0139/20100139286.pdf
[firstpage_image] =>[orig_patent_app_number] => 12521930
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/521930 | BURNER AND FUEL SUPPLY FOR A GAS TURBINE | Apr 19, 2007 | Abandoned |
Array
(
[id] => 5326631
[patent_doc_number] => 20090107108
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-04-30
[patent_title] => 'NACELL FOR BYPASS ENGINE WITH HIGH BYPASS RATIO'
[patent_app_type] => utility
[patent_app_number] => 12/297485
[patent_app_country] => US
[patent_app_date] => 2007-04-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 4157
[patent_no_of_claims] => 9
[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/A1/0107/20090107108.pdf
[firstpage_image] =>[orig_patent_app_number] => 12297485
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/297485 | NACELL FOR BYPASS ENGINE WITH HIGH BYPASS RATIO | Apr 11, 2007 | Abandoned |
Array
(
[id] => 9579969
[patent_doc_number] => 08769963
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-07-08
[patent_title] => 'Low leakage spring clip/ring combinations for gas turbine engine'
[patent_app_type] => utility
[patent_app_number] => 11/699958
[patent_app_country] => US
[patent_app_date] => 2007-01-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 13
[patent_no_of_words] => 3926
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 196
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 11699958
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/699958 | Low leakage spring clip/ring combinations for gas turbine engine | Jan 29, 2007 | Issued |
Array
(
[id] => 8361789
[patent_doc_number] => 08250852
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-08-28
[patent_title] => 'Dual flow turbine engine equipped with a precooler'
[patent_app_type] => utility
[patent_app_number] => 12/160190
[patent_app_country] => US
[patent_app_date] => 2007-01-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 11
[patent_no_of_words] => 2495
[patent_no_of_claims] => 10
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12160190
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/160190 | Dual flow turbine engine equipped with a precooler | Jan 17, 2007 | Issued |
Array
(
[id] => 4924264
[patent_doc_number] => 20080163627
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-07-10
[patent_title] => 'FUEL-FLEXIBLE TRIPLE-COUNTER-ROTATING SWIRLER AND METHOD OF USE'
[patent_app_type] => utility
[patent_app_number] => 11/621705
[patent_app_country] => US
[patent_app_date] => 2007-01-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 8144
[patent_no_of_claims] => 20
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0163/20080163627.pdf
[firstpage_image] =>[orig_patent_app_number] => 11621705
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/621705 | FUEL-FLEXIBLE TRIPLE-COUNTER-ROTATING SWIRLER AND METHOD OF USE | Jan 9, 2007 | Abandoned |
Array
(
[id] => 5571845
[patent_doc_number] => 20090139204
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-06-04
[patent_title] => 'Hybrid Rocket System'
[patent_app_type] => utility
[patent_app_number] => 12/086191
[patent_app_country] => US
[patent_app_date] => 2006-12-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 3645
[patent_no_of_claims] => 33
[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/A1/0139/20090139204.pdf
[firstpage_image] =>[orig_patent_app_number] => 12086191
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/086191 | Hybrid rocket system with moveable combustion control member | Dec 6, 2006 | Issued |