Search

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 numberTitle of the applicationFiling DateStatus
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 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_figures_cnt] => 7 [patent_no_of_words] => 2392 [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/A1/0094/20110094204.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 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_figures_cnt] => 45 [patent_no_of_words] => 15966 [patent_no_of_claims] => 21 [patent_no_of_ind_claims] => 6 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [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 [patent_figures_cnt] => 8 [patent_no_of_words] => 2058 [patent_no_of_claims] => 22 [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/A1/0211/20090211260.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 [patent_figures_cnt] => 2 [patent_no_of_words] => 1024 [patent_no_of_claims] => 11 [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/A1/0252/20090252598.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 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 237 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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
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