
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] => 5424801
[patent_doc_number] => 20090084111
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-04-02
[patent_title] => 'TURBOMACHINE NOZZLE COWL HAVING JET NOISE REDUCTION PATTERNS'
[patent_app_type] => utility
[patent_app_number] => 12/210533
[patent_app_country] => US
[patent_app_date] => 2008-09-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 3526
[patent_no_of_claims] => 12
[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/A1/0084/20090084111.pdf
[firstpage_image] =>[orig_patent_app_number] => 12210533
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/210533 | TURBOMACHINE NOZZLE COWL HAVING JET NOISE REDUCTION PATTERNS | Sep 14, 2008 | Abandoned |
Array
(
[id] => 10078053
[patent_doc_number] => 09115897
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-08-25
[patent_title] => 'Gas turbine engine systems and methods involving enhanced fuel dispersion'
[patent_app_type] => utility
[patent_app_number] => 12/204272
[patent_app_country] => US
[patent_app_date] => 2008-09-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 4
[patent_no_of_words] => 1750
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 96
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12204272
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/204272 | Gas turbine engine systems and methods involving enhanced fuel dispersion | Sep 3, 2008 | Issued |
Array
(
[id] => 6217223
[patent_doc_number] => 20100052836
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-03-04
[patent_title] => 'Air Cooled Core Mounted Ignition System'
[patent_app_type] => utility
[patent_app_number] => 12/203712
[patent_app_country] => US
[patent_app_date] => 2008-09-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 11
[patent_no_of_words] => 5990
[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/A1/0052/20100052836.pdf
[firstpage_image] =>[orig_patent_app_number] => 12203712
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/203712 | Air cooled core mounted ignition system | Sep 2, 2008 | Issued |
Array
(
[id] => 6213710
[patent_doc_number] => 20100050646
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-03-04
[patent_title] => 'Systems and Methods Involving Improved Fuel Atomization in Air-Blast Fuel Nozzles of Gas Turbine Engines'
[patent_app_type] => utility
[patent_app_number] => 12/203383
[patent_app_country] => US
[patent_app_date] => 2008-09-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2364
[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] => publications/A1/0050/20100050646.pdf
[firstpage_image] =>[orig_patent_app_number] => 12203383
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/203383 | Air-blast fuel-injector with shield-cone upstream of fuel orifices | Sep 2, 2008 | Issued |
Array
(
[id] => 5400326
[patent_doc_number] => 20090235639
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-09-24
[patent_title] => 'ROCKET NOZZLE AND CONTROL METHOD FOR COMBUSTION GAS FLOW IN ROCKET ENGINE'
[patent_app_type] => utility
[patent_app_number] => 12/200265
[patent_app_country] => US
[patent_app_date] => 2008-08-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 6305
[patent_no_of_claims] => 18
[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/A1/0235/20090235639.pdf
[firstpage_image] =>[orig_patent_app_number] => 12200265
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/200265 | Rocket nozzle and control method for combustion gas flow in rocket engine | Aug 27, 2008 | Issued |
Array
(
[id] => 6213709
[patent_doc_number] => 20100050645
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-03-04
[patent_title] => 'Fuel distribution manifold system for gas turbine engines'
[patent_app_type] => utility
[patent_app_number] => 12/229935
[patent_app_country] => US
[patent_app_date] => 2008-08-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 17
[patent_figures_cnt] => 17
[patent_no_of_words] => 6010
[patent_no_of_claims] => 25
[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/A1/0050/20100050645.pdf
[firstpage_image] =>[orig_patent_app_number] => 12229935
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/229935 | Fuel distribution manifold system for gas turbine engines | Aug 27, 2008 | Issued |
Array
(
[id] => 5322733
[patent_doc_number] => 20090060723
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-03-05
[patent_title] => ' SEPARATOR FOR FEEDING COOLING AIR TO A TURBINE'
[patent_app_type] => utility
[patent_app_number] => 12/199182
[patent_app_country] => US
[patent_app_date] => 2008-08-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 3627
[patent_no_of_claims] => 12
[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/A1/0060/20090060723.pdf
[firstpage_image] =>[orig_patent_app_number] => 12199182
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/199182 | Separator for feeding cooling air to a turbine | Aug 26, 2008 | Issued |
Array
(
[id] => 5498050
[patent_doc_number] => 20090158738
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-06-25
[patent_title] => 'METHODS AND APPARATUS FOR STARTING UP COMBINED CYCLE POWER SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 12/197712
[patent_app_country] => US
[patent_app_date] => 2008-08-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2841
[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] => publications/A1/0158/20090158738.pdf
[firstpage_image] =>[orig_patent_app_number] => 12197712
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/197712 | METHODS AND APPARATUS FOR STARTING UP COMBINED CYCLE POWER SYSTEM | Aug 24, 2008 | Abandoned |
Array
(
[id] => 9821772
[patent_doc_number] => 08931253
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-01-13
[patent_title] => 'Double-acting telescopic linear actuator with single-motor drive system'
[patent_app_type] => utility
[patent_app_number] => 12/681416
[patent_app_country] => US
[patent_app_date] => 2008-08-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 5
[patent_no_of_words] => 3363
[patent_no_of_claims] => 2
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 427
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12681416
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/681416 | Double-acting telescopic linear actuator with single-motor drive system | Aug 19, 2008 | Issued |
Array
(
[id] => 6437144
[patent_doc_number] => 20100037590
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-02-18
[patent_title] => 'LOW VELOCITY INJECTOR MANIFOLD FOR HYPERGOLIC ROCKET ENGINE'
[patent_app_type] => utility
[patent_app_number] => 12/193679
[patent_app_country] => US
[patent_app_date] => 2008-08-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 1984
[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] => publications/A1/0037/20100037590.pdf
[firstpage_image] =>[orig_patent_app_number] => 12193679
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/193679 | Low velocity injector manifold for hypergolic rocket engine | Aug 17, 2008 | Issued |
Array
(
[id] => 6437375
[patent_doc_number] => 20100037622
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-02-18
[patent_title] => 'Contoured Impingement Sleeve Holes'
[patent_app_type] => utility
[patent_app_number] => 12/193239
[patent_app_country] => US
[patent_app_date] => 2008-08-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 1527
[patent_no_of_claims] => 16
[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/A1/0037/20100037622.pdf
[firstpage_image] =>[orig_patent_app_number] => 12193239
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/193239 | Contoured Impingement Sleeve Holes | Aug 17, 2008 | Abandoned |
Array
(
[id] => 6496999
[patent_doc_number] => 20100218479
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-09-02
[patent_title] => 'LINEAR TELESCOPIC ACTUATOR FOR MOVING A FIRST AND A SECOND ELEMENT RELATIVE TO A STATIONARY ELEMENT'
[patent_app_type] => utility
[patent_app_number] => 12/681219
[patent_app_country] => US
[patent_app_date] => 2008-07-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2745
[patent_no_of_claims] => 8
[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/A1/0218/20100218479.pdf
[firstpage_image] =>[orig_patent_app_number] => 12681219
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/681219 | Linear telescopic actuator for moving a first and a second element relative to a stationary element | Jul 3, 2008 | Issued |
Array
(
[id] => 6614473
[patent_doc_number] => 20100003123
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-01-07
[patent_title] => 'INLET AIR HEATING SYSTEM FOR A GAS TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 12/165800
[patent_app_country] => US
[patent_app_date] => 2008-07-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 1003
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 3
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[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0003/20100003123.pdf
[firstpage_image] =>[orig_patent_app_number] => 12165800
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/165800 | INLET AIR HEATING SYSTEM FOR A GAS TURBINE ENGINE | Jun 30, 2008 | Abandoned |
Array
(
[id] => 9164615
[patent_doc_number] => 08590285
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-11-26
[patent_title] => 'Three-point fixing arrangement of ignition electrodes of a burner'
[patent_app_type] => utility
[patent_app_number] => 12/665389
[patent_app_country] => US
[patent_app_date] => 2008-06-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 6
[patent_no_of_words] => 3392
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 91
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12665389
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/665389 | Three-point fixing arrangement of ignition electrodes of a burner | Jun 29, 2008 | Issued |
Array
(
[id] => 5977887
[patent_doc_number] => 20110094204
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-04-28
[patent_title] => 'COUPLING SYSTEM CONNECTING AN INTERNAL STRUCTURE AND AN EXTERNAL STUCTURE OF A JET ENGINE NACELLE'
[patent_app_type] => utility
[patent_app_number] => 12/673259
[patent_app_country] => US
[patent_app_date] => 2008-06-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[patent_no_of_words] => 2392
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0094/20110094204.pdf
[firstpage_image] =>[orig_patent_app_number] => 12673259
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/673259 | COUPLING SYSTEM CONNECTING AN INTERNAL STRUCTURE AND AN EXTERNAL STUCTURE OF A JET ENGINE NACELLE | Jun 19, 2008 | Abandoned |
Array
(
[id] => 7737506
[patent_doc_number] => 20120018005
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-01-26
[patent_title] => 'COUPLING DEVICE FOR CONNECTING THE TWO HALF-SHELLS OF AN AIRCRAFT ENGINE NACELLE, AND NACELLE EQUIPPED WITH SUCH A DEVICE'
[patent_app_type] => utility
[patent_app_number] => 12/674181
[patent_app_country] => US
[patent_app_date] => 2008-06-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2176
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 1
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[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0018/20120018005.pdf
[firstpage_image] =>[orig_patent_app_number] => 12674181
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/674181 | COUPLING DEVICE FOR CONNECTING THE TWO HALF-SHELLS OF AN AIRCRAFT ENGINE NACELLE, AND NACELLE EQUIPPED WITH SUCH A DEVICE | Jun 19, 2008 | Abandoned |
Array
(
[id] => 6017983
[patent_doc_number] => 20110048027
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-03-03
[patent_title] => 'Turbine Driven By Predetermined Deflagration Of Anaerobic Fuel And Method Thereof'
[patent_app_type] => utility
[patent_app_number] => 12/990710
[patent_app_country] => US
[patent_app_date] => 2008-05-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 45
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[pdf_file] => publications/A1/0048/20110048027.pdf
[firstpage_image] =>[orig_patent_app_number] => 12990710
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/990710 | Turbine Driven By Predetermined Deflagration Of Anaerobic Fuel And Method Thereof | May 4, 2008 | Abandoned |
Array
(
[id] => 5510956
[patent_doc_number] => 20090211260
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-08-27
[patent_title] => 'Multi-Spool Intercooled Recuperated Gas Turbine'
[patent_app_type] => utility
[patent_app_number] => 12/115134
[patent_app_country] => US
[patent_app_date] => 2008-05-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0211/20090211260.pdf
[firstpage_image] =>[orig_patent_app_number] => 12115134
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/115134 | Multi-Spool Intercooled Recuperated Gas Turbine | May 4, 2008 | Abandoned |
Array
(
[id] => 5569220
[patent_doc_number] => 20090252598
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-10-08
[patent_title] => 'Gas turbine inlet temperature suppression during under frequency events and related method'
[patent_app_type] => utility
[patent_app_number] => 12/078612
[patent_app_country] => US
[patent_app_date] => 2008-04-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
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[patent_no_of_words] => 1024
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0252/20090252598.pdf
[firstpage_image] =>[orig_patent_app_number] => 12078612
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/078612 | Gas turbine inlet temperature suppression during under frequency events and related method | Apr 1, 2008 | Abandoned |
Array
(
[id] => 9237007
[patent_doc_number] => 08601790
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-12-10
[patent_title] => 'Buried radial flow rapid prototyping rocket motors'
[patent_app_type] => utility
[patent_app_number] => 12/074001
[patent_app_country] => US
[patent_app_date] => 2008-02-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 4868
[patent_no_of_claims] => 12
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12074001
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/074001 | Buried radial flow rapid prototyping rocket motors | Feb 27, 2008 | Issued |