
Thomas P. Burke
Examiner (ID: 12894, Phone: (571)270-5407 , Office: P/3741 )
| Most Active Art Unit | 3741 |
| Art Unit(s) | 3741 |
| Total Applications | 448 |
| Issued Applications | 159 |
| Pending Applications | 79 |
| Abandoned Applications | 221 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 9724563
[patent_doc_number] => 20140260264
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-09-18
[patent_title] => 'SYSTEM FOR CONTROLLING A FLOW RATE OF A COMPRESSED WORKING FLUID TO A COMBUSTOR FUEL INJECTOR'
[patent_app_type] => utility
[patent_app_number] => 13/845397
[patent_app_country] => US
[patent_app_date] => 2013-03-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 4793
[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] => 13845397
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/845397 | System for controlling a flow rate of a compressed working fluid to a combustor fuel injector | Mar 17, 2013 | Issued |
Array
(
[id] => 9724576
[patent_doc_number] => 20140260277
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-09-18
[patent_title] => 'FLOW SLEEVE FOR A COMBUSTION MODULE OF A GAS TURBINE'
[patent_app_type] => utility
[patent_app_number] => 13/845485
[patent_app_country] => US
[patent_app_date] => 2013-03-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 4920
[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] => 13845485
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/845485 | Flow sleeve for a combustion module of a gas turbine | Mar 17, 2013 | Issued |
Array
(
[id] => 9724616
[patent_doc_number] => 20140260318
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-09-18
[patent_title] => 'SIDE SEAL SLOT FOR A COMBUSTION LINER'
[patent_app_type] => utility
[patent_app_number] => 13/845617
[patent_app_country] => US
[patent_app_date] => 2013-03-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 4757
[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] => 13845617
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/845617 | SIDE SEAL SLOT FOR A COMBUSTION LINER | Mar 17, 2013 | Abandoned |
Array
(
[id] => 9724579
[patent_doc_number] => 20140260280
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-09-18
[patent_title] => 'ASSEMBLY FOR CONTROLLING CLEARANCE BETWEEN A LINER AND STATIONARY NOZZLE WITHIN A GAS TURBINE'
[patent_app_type] => utility
[patent_app_number] => 13/845565
[patent_app_country] => US
[patent_app_date] => 2013-03-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 4393
[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] => 13845565
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/845565 | Assembly for controlling clearance between a liner and stationary nozzle within a gas turbine | Mar 17, 2013 | Issued |
Array
(
[id] => 10957171
[patent_doc_number] => 20140360193
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-12-11
[patent_title] => 'SUPPORT FRAME AND METHOD FOR ASSEMBLY OF A COMBUSTION MODULE OF A GAS TURBINE'
[patent_app_type] => utility
[patent_app_number] => 13/845661
[patent_app_country] => US
[patent_app_date] => 2013-03-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
[patent_figures_cnt] => 13
[patent_no_of_words] => 7807
[patent_no_of_claims] => 20
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13845661
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/845661 | Support frame and method for assembly of a combustion module of a gas turbine | Mar 17, 2013 | Issued |
Array
(
[id] => 9835048
[patent_doc_number] => 20150027128
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-01-29
[patent_title] => 'HEAT-SHIELD ELEMENT FOR A COMPRESSOR-AIR BYPASS AROUND THE COMBUSTION CHAMBER'
[patent_app_type] => utility
[patent_app_number] => 14/384257
[patent_app_country] => US
[patent_app_date] => 2013-03-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2151
[patent_no_of_claims] => 10
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14384257
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/384257 | HEAT-SHIELD ELEMENT FOR A COMPRESSOR-AIR BYPASS AROUND THE COMBUSTION CHAMBER | Mar 11, 2013 | Abandoned |
Array
(
[id] => 9459196
[patent_doc_number] => 20140123621
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-05-08
[patent_title] => 'ACTUATED BYPASS HOOD FOR GAS TURBINE AIR INLET SYSTEM AND METHODS'
[patent_app_type] => utility
[patent_app_number] => 13/776095
[patent_app_country] => US
[patent_app_date] => 2013-02-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
[patent_figures_cnt] => 13
[patent_no_of_words] => 3764
[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] => 13776095
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/776095 | ACTUATED BYPASS HOOD FOR GAS TURBINE AIR INLET SYSTEM AND METHODS | Feb 24, 2013 | Abandoned |
Array
(
[id] => 10970471
[patent_doc_number] => 20140373504
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-12-25
[patent_title] => 'GAS TURBINE HAVING AN EXHAUST GAS DIFFUSER AND SUPPORTING FINS'
[patent_app_type] => utility
[patent_app_number] => 14/376429
[patent_app_country] => US
[patent_app_date] => 2013-01-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 2396
[patent_no_of_claims] => 5
[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] => 14376429
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/376429 | GAS TURBINE HAVING AN EXHAUST GAS DIFFUSER AND SUPPORTING FINS | Jan 14, 2013 | Abandoned |
Array
(
[id] => 10629519
[patent_doc_number] => 09347666
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-05-24
[patent_title] => 'Combustor with fuel injector pegs for reducing combustion pressure oscillations'
[patent_app_type] => utility
[patent_app_number] => 13/727283
[patent_app_country] => US
[patent_app_date] => 2012-12-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 4244
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 255
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13727283
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/727283 | Combustor with fuel injector pegs for reducing combustion pressure oscillations | Dec 25, 2012 | Issued |
Array
(
[id] => 10935330
[patent_doc_number] => 20140338351
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-11-20
[patent_title] => 'GAS TURBINE ENGINE COMBUSTOR WITH TAILORED TEMPERATURE PROFILE'
[patent_app_type] => utility
[patent_app_number] => 13/725137
[patent_app_country] => US
[patent_app_date] => 2012-12-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 15
[patent_figures_cnt] => 15
[patent_no_of_words] => 4554
[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] => 13725137
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/725137 | Gas turbine engine combustor with tailored temperature profile | Dec 20, 2012 | Issued |
Array
(
[id] => 9379629
[patent_doc_number] => 20140083110
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-03-27
[patent_title] => 'SEAL FOR FUEL DISTRIBUTION PLATE'
[patent_app_type] => utility
[patent_app_number] => 13/720118
[patent_app_country] => US
[patent_app_date] => 2012-12-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 27
[patent_figures_cnt] => 27
[patent_no_of_words] => 3625
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13720118
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/720118 | Seal for fuel distribution plate | Dec 18, 2012 | Issued |
Array
(
[id] => 9637935
[patent_doc_number] => 20140216044
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-08-07
[patent_title] => 'GAS TURBINE ENGINE COMBUSTOR HEAT SHIELD WITH INCREASED FILM COOLING EFFECTIVENESS'
[patent_app_type] => utility
[patent_app_number] => 13/716774
[patent_app_country] => US
[patent_app_date] => 2012-12-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
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[patent_no_of_words] => 3666
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13716774
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/716774 | GAS TURBINE ENGINE COMBUSTOR HEAT SHIELD WITH INCREASED FILM COOLING EFFECTIVENESS | Dec 16, 2012 | Abandoned |
Array
(
[id] => 8887277
[patent_doc_number] => 20130160461
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-06-27
[patent_title] => 'ELECTRONIC UNIT MOUNTING'
[patent_app_type] => utility
[patent_app_number] => 13/716439
[patent_app_country] => US
[patent_app_date] => 2012-12-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
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[patent_no_of_words] => 13224
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13716439
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/716439 | Electronic unit mounting | Dec 16, 2012 | Issued |
Array
(
[id] => 9405257
[patent_doc_number] => 20140096509
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-04-10
[patent_title] => 'Geared Turbofan Engine With Increased Bypass Ratio and Compressor Ratio ...'
[patent_app_type] => utility
[patent_app_number] => 13/716253
[patent_app_country] => US
[patent_app_date] => 2012-12-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_no_of_words] => 2354
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13716253
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/716253 | Geared Turbofan Engine With Increased Bypass Ratio and Compressor Ratio ... | Dec 16, 2012 | Abandoned |
Array
(
[id] => 8887274
[patent_doc_number] => 20130160458
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-06-27
[patent_title] => 'ELECTRICAL RAFT ASSEMBLY'
[patent_app_type] => utility
[patent_app_number] => 13/716808
[patent_app_country] => US
[patent_app_date] => 2012-12-17
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13716808
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/716808 | Electrical raft assembly | Dec 16, 2012 | Issued |
Array
(
[id] => 8879360
[patent_doc_number] => 20130152544
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-06-20
[patent_title] => 'JET ENGINE'
[patent_app_type] => utility
[patent_app_number] => 13/714133
[patent_app_country] => US
[patent_app_date] => 2012-12-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13714133
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/714133 | JET ENGINE | Dec 12, 2012 | Abandoned |
Array
(
[id] => 9533140
[patent_doc_number] => 20140157786
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-06-12
[patent_title] => 'CONTROLLING COMBUSTION SYSTEM WITH FUEL CHEMICAL INDUCTION TIME'
[patent_app_type] => utility
[patent_app_number] => 13/708365
[patent_app_country] => US
[patent_app_date] => 2012-12-07
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13708365
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/708365 | CONTROLLING COMBUSTION SYSTEM WITH FUEL CHEMICAL INDUCTION TIME | Dec 6, 2012 | Abandoned |
Array
(
[id] => 10516520
[patent_doc_number] => 09243561
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-01-26
[patent_title] => 'Combustor head arrangement'
[patent_app_type] => utility
[patent_app_number] => 13/693863
[patent_app_country] => US
[patent_app_date] => 2012-12-04
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13693863
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/693863 | Combustor head arrangement | Dec 3, 2012 | Issued |
Array
(
[id] => 10922971
[patent_doc_number] => 20140325991
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-11-06
[patent_title] => 'Aircraft having an Engine, a Fuel Tank, and a Fuel Cell'
[patent_app_type] => utility
[patent_app_number] => 14/365293
[patent_app_country] => US
[patent_app_date] => 2012-12-03
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14365293
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/365293 | Aircraft having an Engine, a Fuel Tank, and a Fuel Cell | Dec 2, 2012 | Abandoned |
Array
(
[id] => 9513911
[patent_doc_number] => 20140150403
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-06-05
[patent_title] => 'THRUST REVERSER SYSTEM WITH TRANSLATING-ROTATING CASCADE AND METHOD OF OPERATION'
[patent_app_type] => utility
[patent_app_number] => 13/690065
[patent_app_country] => US
[patent_app_date] => 2012-11-30
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13690065
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/690065 | Thrust reverser system with translating-rotating cascade and method of operation | Nov 29, 2012 | Issued |