
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] => 10058075
[patent_doc_number] => 09097425
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-08-04
[patent_title] => 'Fuel mixing device for turbine engine combustion chamber comprising improved air feed means'
[patent_app_type] => utility
[patent_app_number] => 13/503737
[patent_app_country] => US
[patent_app_date] => 2010-11-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 3
[patent_no_of_words] => 2585
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 263
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13503737
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/503737 | Fuel mixing device for turbine engine combustion chamber comprising improved air feed means | Nov 2, 2010 | Issued |
Array
(
[id] => 6166475
[patent_doc_number] => 20110173984
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-07-21
[patent_title] => 'GAS TURBINE TRANSITION PIECE AIR BYPASS BAND ASSEMBLY'
[patent_app_type] => utility
[patent_app_number] => 12/917561
[patent_app_country] => US
[patent_app_date] => 2010-11-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 2635
[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/A1/0173/20110173984.pdf
[firstpage_image] =>[orig_patent_app_number] => 12917561
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/917561 | GAS TURBINE TRANSITION PIECE AIR BYPASS BAND ASSEMBLY | Nov 1, 2010 | Abandoned |
Array
(
[id] => 8163617
[patent_doc_number] => 20120102964
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-05-03
[patent_title] => 'TURBOMACHINE INCLUDING A CARBON DIOXIDE (CO2) CONCENTRATION CONTROL SYSTEM AND METHOD'
[patent_app_type] => utility
[patent_app_number] => 12/915341
[patent_app_country] => US
[patent_app_date] => 2010-10-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 1948
[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/A1/0102/20120102964.pdf
[firstpage_image] =>[orig_patent_app_number] => 12915341
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/915341 | TURBOMACHINE INCLUDING A CARBON DIOXIDE (CO2) CONCENTRATION CONTROL SYSTEM AND METHOD | Oct 28, 2010 | Abandoned |
Array
(
[id] => 8163611
[patent_doc_number] => 20120102958
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-05-03
[patent_title] => 'LATE LEAN INJECTION MANIFOLD'
[patent_app_type] => utility
[patent_app_number] => 12/914537
[patent_app_country] => US
[patent_app_date] => 2010-10-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 3269
[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/A1/0102/20120102958.pdf
[firstpage_image] =>[orig_patent_app_number] => 12914537
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/914537 | Late lean injection manifold | Oct 27, 2010 | Issued |
Array
(
[id] => 8163613
[patent_doc_number] => 20120102967
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-05-03
[patent_title] => 'Method and system for preventing combustion instabilities during transient operations'
[patent_app_type] => utility
[patent_app_number] => 12/926121
[patent_app_country] => US
[patent_app_date] => 2010-10-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2162
[patent_no_of_claims] => 24
[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/A1/0102/20120102967.pdf
[firstpage_image] =>[orig_patent_app_number] => 12926121
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/926121 | Method and system for preventing combustion instabilities during transient operations | Oct 26, 2010 | Abandoned |
Array
(
[id] => 8158104
[patent_doc_number] => 20120099976
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-04-26
[patent_title] => 'FAN CONTAINMENT SYSTEMS WITH IMPROVED IMPACT STRUCTURES'
[patent_app_type] => utility
[patent_app_number] => 12/912268
[patent_app_country] => US
[patent_app_date] => 2010-10-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 3468
[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/A1/0099/20120099976.pdf
[firstpage_image] =>[orig_patent_app_number] => 12912268
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/912268 | FAN CONTAINMENT SYSTEMS WITH IMPROVED IMPACT STRUCTURES | Oct 25, 2010 | Abandoned |
Array
(
[id] => 8196886
[patent_doc_number] => 08186169
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-05-29
[patent_title] => 'Nitrogen cooled gas turbine with combustor nitrogen injection and partial nitrogen recycling'
[patent_app_type] => utility
[patent_app_number] => 12/910033
[patent_app_country] => US
[patent_app_date] => 2010-10-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 2215
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 106
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/186/08186169.pdf
[firstpage_image] =>[orig_patent_app_number] => 12910033
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/910033 | Nitrogen cooled gas turbine with combustor nitrogen injection and partial nitrogen recycling | Oct 21, 2010 | Issued |
Array
(
[id] => 8121107
[patent_doc_number] => 20120085103
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-04-12
[patent_title] => 'SHIM FOR SEALING TRANSITION PIECES'
[patent_app_type] => utility
[patent_app_number] => 12/900072
[patent_app_country] => US
[patent_app_date] => 2010-10-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 2658
[patent_no_of_claims] => 19
[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/A1/0085/20120085103.pdf
[firstpage_image] =>[orig_patent_app_number] => 12900072
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/900072 | Shim for sealing transition pieces | Oct 6, 2010 | Issued |
Array
(
[id] => 10643094
[patent_doc_number] => 09359953
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-06-07
[patent_title] => 'Combined cycle power plant with solar assisted cooling of compressor inlet air'
[patent_app_type] => utility
[patent_app_number] => 13/818377
[patent_app_country] => US
[patent_app_date] => 2010-09-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 5533
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 402
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13818377
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/818377 | Combined cycle power plant with solar assisted cooling of compressor inlet air | Sep 29, 2010 | Issued |
Array
(
[id] => 8389566
[patent_doc_number] => 20120227407
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-09-13
[patent_title] => 'BURNER FOR A TURBINE'
[patent_app_type] => utility
[patent_app_number] => 13/509329
[patent_app_country] => US
[patent_app_date] => 2010-09-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 3797
[patent_no_of_claims] => 20
[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] =>[firstpage_image] =>[orig_patent_app_number] => 13509329
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/509329 | BURNER FOR A TURBINE | Sep 27, 2010 | Abandoned |
Array
(
[id] => 10136491
[patent_doc_number] => 09169807
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-10-27
[patent_title] => 'Convex thermal shield for rocket engine with extendable divergent nozzle'
[patent_app_type] => utility
[patent_app_number] => 13/395344
[patent_app_country] => US
[patent_app_date] => 2010-09-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 6
[patent_no_of_words] => 2175
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 161
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13395344
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/395344 | Convex thermal shield for rocket engine with extendable divergent nozzle | Sep 5, 2010 | Issued |
Array
(
[id] => 9748161
[patent_doc_number] => 08839624
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-09-23
[patent_title] => 'Combustion device of a gas turbine including a plurality of passages and chambers defining helmholtz resonators'
[patent_app_type] => utility
[patent_app_number] => 12/871310
[patent_app_country] => US
[patent_app_date] => 2010-08-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 6
[patent_no_of_words] => 3273
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 130
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12871310
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/871310 | Combustion device of a gas turbine including a plurality of passages and chambers defining helmholtz resonators | Aug 29, 2010 | Issued |
Array
(
[id] => 8849842
[patent_doc_number] => 20130139517
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-06-06
[patent_title] => 'Solar Assisted Gas Turbine System'
[patent_app_type] => utility
[patent_app_number] => 13/816295
[patent_app_country] => US
[patent_app_date] => 2010-08-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 12
[patent_no_of_words] => 12159
[patent_no_of_claims] => 12
[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] => 13816295
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/816295 | Solar Assisted Gas Turbine System | Aug 26, 2010 | Abandoned |
Array
(
[id] => 8408829
[patent_doc_number] => 08272220
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-09-25
[patent_title] => 'Impingement cooling plate for a hot gas duct of a thermal machine'
[patent_app_type] => utility
[patent_app_number] => 12/860620
[patent_app_country] => US
[patent_app_date] => 2010-08-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 7
[patent_no_of_words] => 3102
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 300
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12860620
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/860620 | Impingement cooling plate for a hot gas duct of a thermal machine | Aug 19, 2010 | Issued |
Array
(
[id] => 7771301
[patent_doc_number] => 20120036866
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-02-16
[patent_title] => 'AUXILIARY POWER UNIT WITH MULTIPLE FUEL SOURCES'
[patent_app_type] => utility
[patent_app_number] => 12/854230
[patent_app_country] => US
[patent_app_date] => 2010-08-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 3594
[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/A1/0036/20120036866.pdf
[firstpage_image] =>[orig_patent_app_number] => 12854230
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/854230 | AUXILIARY POWER UNIT WITH MULTIPLE FUEL SOURCES | Aug 10, 2010 | Abandoned |
Array
(
[id] => 8223489
[patent_doc_number] => 20120137697
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-06-07
[patent_title] => 'COMBUSTION CHAMBER FOR A TURBOMACHINE INCLUDING IMPROVED AIR INLETS'
[patent_app_type] => utility
[patent_app_number] => 13/388345
[patent_app_country] => US
[patent_app_date] => 2010-08-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 3407
[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] =>[firstpage_image] =>[orig_patent_app_number] => 13388345
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/388345 | Combustion chamber for a turbomachine including improved air inlets | Aug 1, 2010 | Issued |
Array
(
[id] => 7748018
[patent_doc_number] => 20120023896
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-02-02
[patent_title] => 'AUXILIARY POWER UNIT FIRE ENCLOSURE DRAIN'
[patent_app_type] => utility
[patent_app_number] => 12/847343
[patent_app_country] => US
[patent_app_date] => 2010-07-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 3669
[patent_no_of_claims] => 16
[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/A1/0023/20120023896.pdf
[firstpage_image] =>[orig_patent_app_number] => 12847343
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/847343 | AUXILIARY POWER UNIT FIRE ENCLOSURE DRAIN | Jul 29, 2010 | Abandoned |
Array
(
[id] => 9689467
[patent_doc_number] => 08820045
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-09-02
[patent_title] => 'Auxiliary power unit fire enclosure drain seal'
[patent_app_type] => utility
[patent_app_number] => 12/847359
[patent_app_country] => US
[patent_app_date] => 2010-07-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 4359
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 183
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12847359
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/847359 | Auxiliary power unit fire enclosure drain seal | Jul 29, 2010 | Issued |
Array
(
[id] => 7748120
[patent_doc_number] => 20120023953
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-02-02
[patent_title] => 'METHODS FOR CONTROLLING FUEL SPLITS TO A GAS TURBINE COMBUSTOR'
[patent_app_type] => utility
[patent_app_number] => 12/844280
[patent_app_country] => US
[patent_app_date] => 2010-07-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 5606
[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/A1/0023/20120023953.pdf
[firstpage_image] =>[orig_patent_app_number] => 12844280
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/844280 | METHODS FOR CONTROLLING FUEL SPLITS TO A GAS TURBINE COMBUSTOR | Jul 26, 2010 | Abandoned |
Array
(
[id] => 8190900
[patent_doc_number] => 20120118249
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-05-17
[patent_title] => 'AXIAL-PISTON ENGINE, METHOD FOR OPERATING AN AXIAL-PISTON ENGINE, AND METHOD FOR PRODUCING A HEAT EXCHANGER OF AN AXIAL-PISTON ENGINE'
[patent_app_type] => utility
[patent_app_number] => 13/386569
[patent_app_country] => US
[patent_app_date] => 2010-07-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 20382
[patent_no_of_claims] => 17
[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/A1/0118/20120118249.pdf
[firstpage_image] =>[orig_patent_app_number] => 13386569
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/386569 | AXIAL-PISTON ENGINE, METHOD FOR OPERATING AN AXIAL-PISTON ENGINE, AND METHOD FOR PRODUCING A HEAT EXCHANGER OF AN AXIAL-PISTON ENGINE | Jul 25, 2010 | Abandoned |