Search

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 numberTitle of the applicationFiling DateStatus
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] => 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] => 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 [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] => 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 [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] => 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 [patent_figures_cnt] => 13 [patent_no_of_words] => 3666 [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] => 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] => 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 [patent_drawing_sheets_cnt] => 13 [patent_figures_cnt] => 13 [patent_no_of_words] => 10228 [patent_no_of_claims] => 15 [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] => 13716808 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/716808
Electrical raft assembly Dec 16, 2012 Issued
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 [patent_figures_cnt] => 10 [patent_no_of_words] => 13224 [patent_no_of_claims] => 15 [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] => 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 [patent_figures_cnt] => 4 [patent_no_of_words] => 2354 [patent_no_of_claims] => 14 [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] => 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] => 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 [patent_figures_cnt] => 8 [patent_no_of_words] => 3721 [patent_no_of_claims] => 23 [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] => 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 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 4182 [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] => 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 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 6 [patent_no_of_words] => 2926 [patent_no_of_claims] => 23 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 134 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [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 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 3773 [patent_no_of_claims] => 14 [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] => 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 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 12 [patent_no_of_words] => 4193 [patent_no_of_claims] => 23 [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] => 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
Array ( [id] => 9513910 [patent_doc_number] => 20140150402 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-06-05 [patent_title] => 'SYSTEM AND METHOD FOR BURNING VANADIUM-CONTAINING FUELS' [patent_app_type] => utility [patent_app_number] => 13/690057 [patent_app_country] => US [patent_app_date] => 2012-11-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 7338 [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] => 13690057 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/690057
SYSTEM AND METHOD FOR BURNING VANADIUM-CONTAINING FUELS Nov 29, 2012 Abandoned
Array ( [id] => 9513960 [patent_doc_number] => 20140150452 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-06-05 [patent_title] => 'TRANSITION PIECE FOR A GAS TURBINE SYSTEM' [patent_app_type] => utility [patent_app_number] => 13/991419 [patent_app_country] => US [patent_app_date] => 2012-11-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 4321 [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] => 13991419 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/991419
TRANSITION PIECE FOR A GAS TURBINE SYSTEM Nov 29, 2012 Abandoned
Array ( [id] => 9507631 [patent_doc_number] => 20140144121 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-05-29 [patent_title] => 'GAS TURBINE ENGINE WITH BEARING OIL LEAK RECUPERATION SYSTEM' [patent_app_type] => utility [patent_app_number] => 13/687511 [patent_app_country] => US [patent_app_date] => 2012-11-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 4876 [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] => 13687511 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/687511
GAS TURBINE ENGINE WITH BEARING OIL LEAK RECUPERATION SYSTEM Nov 27, 2012 Abandoned
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