
Thomas P. Burke
Examiner (ID: 8037, Phone: (571)270-5407 , Office: P/3741 )
| Most Active Art Unit | 3741 |
| Art Unit(s) | 3741 |
| Total Applications | 426 |
| Issued Applications | 148 |
| Pending Applications | 81 |
| Abandoned Applications | 216 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 11472375
[patent_doc_number] => 20170059158
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-03-02
[patent_title] => 'WEAR PAD SYSTEM FOR TURBINE COMBUSTION SYSTEMS AND METHOD FOR COUPLING WEAR PAD INTO TURBINE COMBUSTION SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 14/833388
[patent_app_country] => US
[patent_app_date] => 2015-08-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 11
[patent_no_of_words] => 7891
[patent_no_of_claims] => 28
[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] =>[firstpage_image] =>[orig_patent_app_number] => 14833388
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/833388 | Wear pad system for turbine combustion systems and method for coupling wear pad into turbine combustion system | Aug 23, 2015 | Issued |
Array
(
[id] => 11422069
[patent_doc_number] => 20170030213
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-02-02
[patent_title] => 'TURBINE SECTION WITH TIP FLOW VANES'
[patent_app_type] => utility
[patent_app_number] => 14/814927
[patent_app_country] => US
[patent_app_date] => 2015-07-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 2179
[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] =>[firstpage_image] =>[orig_patent_app_number] => 14814927
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/814927 | TURBINE SECTION WITH TIP FLOW VANES | Jul 30, 2015 | Abandoned |
Array
(
[id] => 11383062
[patent_doc_number] => 20170009118
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-01-12
[patent_title] => 'METHOD AND APPARATUS FOR GENERATING LATENT HEAT AT LOW TEMPERATURES USING EXOTHERMIC SALT CRYSTALLIZATION'
[patent_app_type] => utility
[patent_app_number] => 14/796171
[patent_app_country] => US
[patent_app_date] => 2015-07-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 7034
[patent_no_of_claims] => 20
[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] => 14796171
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/796171 | METHOD AND APPARATUS FOR GENERATING LATENT HEAT AT LOW TEMPERATURES USING EXOTHERMIC SALT CRYSTALLIZATION | Jul 9, 2015 | Abandoned |
Array
(
[id] => 11383602
[patent_doc_number] => 20170009658
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-01-12
[patent_title] => 'INSULATION SUPPORT SYSTEM FOR AN EXHAUST GAS SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 14/791540
[patent_app_country] => US
[patent_app_date] => 2015-07-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2811
[patent_no_of_claims] => 20
[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] => 14791540
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/791540 | INSULATION SUPPORT SYSTEM FOR AN EXHAUST GAS SYSTEM | Jul 5, 2015 | Abandoned |
Array
(
[id] => 10980876
[patent_doc_number] => 20160177820
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-06-23
[patent_title] => 'LOW PRESSURE ENVIRONMENTAL CONTROL SYSTEM WITH SAFE PYLON TRANSIT'
[patent_app_type] => utility
[patent_app_number] => 14/751320
[patent_app_country] => US
[patent_app_date] => 2015-06-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 3491
[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] =>[firstpage_image] =>[orig_patent_app_number] => 14751320
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/751320 | LOW PRESSURE ENVIRONMENTAL CONTROL SYSTEM WITH SAFE PYLON TRANSIT | Jun 25, 2015 | Abandoned |
Array
(
[id] => 13128239
[patent_doc_number] => 10082043
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2018-09-25
[patent_title] => Segmented multi-lobe mixer
[patent_app_type] => utility
[patent_app_number] => 14/750094
[patent_app_country] => US
[patent_app_date] => 2015-06-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 8
[patent_no_of_words] => 2079
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 129
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14750094
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/750094 | Segmented multi-lobe mixer | Jun 24, 2015 | Issued |
Array
(
[id] => 11350955
[patent_doc_number] => 20160369695
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-12-22
[patent_title] => 'TEMPERATURE-MODULATED RECUPERATED GAS TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 14/740636
[patent_app_country] => US
[patent_app_date] => 2015-06-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 5233
[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] =>[firstpage_image] =>[orig_patent_app_number] => 14740636
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/740636 | TEMPERATURE-MODULATED RECUPERATED GAS TURBINE ENGINE | Jun 15, 2015 | Abandoned |
Array
(
[id] => 11325609
[patent_doc_number] => 20160356221
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-12-08
[patent_title] => 'SYSTEMS AND METHODS FOR PASSIVELY PROVIDING ONE OR MORE FLOWS OF COOLING FLUID TO A HOT CAVITY WITHIN A COOLING CIRCUIT OF A GAS TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 14/733251
[patent_app_country] => US
[patent_app_date] => 2015-06-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 2707
[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] =>[firstpage_image] =>[orig_patent_app_number] => 14733251
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/733251 | SYSTEMS AND METHODS FOR PASSIVELY PROVIDING ONE OR MORE FLOWS OF COOLING FLUID TO A HOT CAVITY WITHIN A COOLING CIRCUIT OF A GAS TURBINE ENGINE | Jun 7, 2015 | Abandoned |
Array
(
[id] => 10368006
[patent_doc_number] => 20150253011
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-09-10
[patent_title] => 'ANNULAR PREMIXED PILOT IN FUEL NOZZLE'
[patent_app_type] => utility
[patent_app_number] => 14/719356
[patent_app_country] => US
[patent_app_date] => 2015-05-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 7645
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14719356
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/719356 | ANNULAR PREMIXED PILOT IN FUEL NOZZLE | May 21, 2015 | Abandoned |
Array
(
[id] => 11093315
[patent_doc_number] => 20160290283
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-10-06
[patent_title] => 'FLUID-POWERED THRUST REVERSER ACTUATION SYSTEM WITH ELECTROMECHANICAL SPEED CONTROL'
[patent_app_type] => utility
[patent_app_number] => 14/672938
[patent_app_country] => US
[patent_app_date] => 2015-03-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 4214
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14672938
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/672938 | FLUID-POWERED THRUST REVERSER ACTUATION SYSTEM WITH ELECTROMECHANICAL SPEED CONTROL | Mar 29, 2015 | Abandoned |
Array
(
[id] => 15636359
[patent_doc_number] => 10591164
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2020-03-17
[patent_title] => Fuel nozzle for a gas turbine engine
[patent_app_type] => utility
[patent_app_number] => 14/645959
[patent_app_country] => US
[patent_app_date] => 2015-03-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_no_of_words] => 4450
[patent_no_of_claims] => 20
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14645959
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/645959 | Fuel nozzle for a gas turbine engine | Mar 11, 2015 | Issued |
Array
(
[id] => 17378638
[patent_doc_number] => 11236639
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2022-02-01
[patent_title] => Gas turbine engine and an airflow control system
[patent_app_type] => utility
[patent_app_number] => 14/618572
[patent_app_country] => US
[patent_app_date] => 2015-02-10
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14618572
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/618572 | Gas turbine engine and an airflow control system | Feb 9, 2015 | Issued |
Array
(
[id] => 11034037
[patent_doc_number] => 20160230993
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-08-11
[patent_title] => 'COMBUSTOR LINER EFFUSION COOLING HOLES'
[patent_app_type] => utility
[patent_app_number] => 14/618087
[patent_app_country] => US
[patent_app_date] => 2015-02-10
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14618087
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/618087 | COMBUSTOR LINER EFFUSION COOLING HOLES | Feb 9, 2015 | |
Array
(
[id] => 13662205
[patent_doc_number] => 10161256
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2018-12-25
[patent_title] => Seal with backup seal
[patent_app_type] => utility
[patent_app_number] => 14/603033
[patent_app_country] => US
[patent_app_date] => 2015-01-22
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[patent_drawing_sheets_cnt] => 7
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/603033 | Seal with backup seal | Jan 21, 2015 | Issued |
Array
(
[id] => 11011784
[patent_doc_number] => 20160208737
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-07-21
[patent_title] => 'SYSTEM FOR ACTUATING AN EXHAUST COWL'
[patent_app_type] => utility
[patent_app_number] => 14/600824
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[patent_app_date] => 2015-01-20
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14600824
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/600824 | System for actuating an exhaust cowl | Jan 19, 2015 | Issued |
Array
(
[id] => 11012082
[patent_doc_number] => 20160209035
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-07-21
[patent_title] => 'COMBUSTION HOLE INSERT WITH INTEGRATED FILM RESTARTER'
[patent_app_type] => utility
[patent_app_number] => 14/599094
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[patent_app_date] => 2015-01-16
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14599094
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/599094 | COMBUSTION HOLE INSERT WITH INTEGRATED FILM RESTARTER | Jan 15, 2015 | Abandoned |
Array
(
[id] => 10989718
[patent_doc_number] => 20160186663
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-06-30
[patent_title] => 'PILOT NOZZLE IN GAS TURBINE COMBUSTOR'
[patent_app_type] => utility
[patent_app_number] => 14/585837
[patent_app_country] => US
[patent_app_date] => 2014-12-30
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/585837 | PILOT NOZZLE IN GAS TURBINE COMBUSTOR | Dec 29, 2014 | Abandoned |
Array
(
[id] => 12910783
[patent_doc_number] => 20180195437
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[patent_kind] => A1
[patent_issue_date] => 2018-07-12
[patent_title] => TURBOMACHINE AIR STARTER COMPRISING FIRST AND SECOND LUBRICATION COMPARTMENTS
[patent_app_type] => utility
[patent_app_number] => 15/107002
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/107002 | TURBOMACHINE AIR STARTER COMPRISING FIRST AND SECOND LUBRICATION COMPARTMENTS | Dec 18, 2014 | Abandoned |
Array
(
[id] => 11888606
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[patent_kind] => B2
[patent_issue_date] => 2017-09-12
[patent_title] => 'Integrated turbine exhaust struts and mixer of turbofan engine'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/521888 | Integrated turbine exhaust struts and mixer of turbofan engine | Oct 22, 2014 | Issued |
Array
(
[id] => 9795626
[patent_doc_number] => 20150007571
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[patent_title] => 'GAS TURBINE COMBUSTOR'
[patent_app_type] => utility
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/494984 | GAS TURBINE COMBUSTOR | Sep 23, 2014 | Abandoned |