Search

Thomas P. Burke

Examiner (ID: 15516, Phone: (571)270-5407 , Office: P/3741 )

Most Active Art Unit
3741
Art Unit(s)
3741
Total Applications
437
Issued Applications
152
Pending Applications
83
Abandoned Applications
217

Applications

Application numberTitle of the applicationFiling DateStatus
Array ( [id] => 9302718 [patent_doc_number] => 20140041392 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-02-13 [patent_title] => 'Regenerative Gas Generator' [patent_app_type] => utility [patent_app_number] => 13/913963 [patent_app_country] => US [patent_app_date] => 2013-06-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 11682 [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] => 13913963 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/913963
Regenerative Gas Generator Jun 9, 2013 Abandoned
Array ( [id] => 10935322 [patent_doc_number] => 20140338343 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-11-20 [patent_title] => 'SYSTEM FOR VIBRATION DAMPING OF A FUEL NOZZLE WITHIN A COMBUSTOR' [patent_app_type] => utility [patent_app_number] => 13/893721 [patent_app_country] => US [patent_app_date] => 2013-05-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 3444 [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] => 13893721 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/893721
SYSTEM FOR VIBRATION DAMPING OF A FUEL NOZZLE WITHIN A COMBUSTOR May 13, 2013 Abandoned
Array ( [id] => 14795427 [patent_doc_number] => 10400710 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2019-09-03 [patent_title] => Secondary nozzle for jet engine [patent_app_type] => utility [patent_app_number] => 13/889003 [patent_app_country] => US [patent_app_date] => 2013-05-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 8 [patent_no_of_words] => 5028 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 224 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13889003 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/889003
Secondary nozzle for jet engine May 6, 2013 Issued
Array ( [id] => 9935100 [patent_doc_number] => 08984893 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2015-03-24 [patent_title] => 'System and method for augmenting gas turbine power output' [patent_app_type] => utility [patent_app_number] => 13/859819 [patent_app_country] => US [patent_app_date] => 2013-04-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 5253 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 156 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13859819 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/859819
System and method for augmenting gas turbine power output Apr 9, 2013 Issued
Array ( [id] => 11894923 [patent_doc_number] => 09764846 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2017-09-19 [patent_title] => 'Contamination free reverse flow fitting' [patent_app_type] => utility [patent_app_number] => 13/856162 [patent_app_country] => US [patent_app_date] => 2013-04-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 1576 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 171 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13856162 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/856162
Contamination free reverse flow fitting Apr 2, 2013 Issued
Array ( [id] => 9752823 [patent_doc_number] => 20140283523 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-09-25 [patent_title] => 'SYSTEM AND METHOD FOR CONTROLLED FUEL BLENDING IN GAS TURBINES' [patent_app_type] => utility [patent_app_number] => 13/848500 [patent_app_country] => US [patent_app_date] => 2013-03-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 7266 [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] => 13848500 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/848500
System and method for controlled fuel blending in gas turbines Mar 20, 2013 Issued
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] => 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] => 9724562 [patent_doc_number] => 20140260263 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-09-18 [patent_title] => 'FUEL INJECTION INSERT FOR A TURBINE NOZZLE SEGMENT' [patent_app_type] => utility [patent_app_number] => 13/845334 [patent_app_country] => US [patent_app_date] => 2013-03-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 3744 [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] => 13845334 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/845334
Fuel injection insert for a turbine nozzle segment Mar 17, 2013 Issued
Array ( [id] => 11790521 [patent_doc_number] => 09400114 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2016-07-26 [patent_title] => 'Combustor support assembly for mounting a combustion module of a gas turbine' [patent_app_type] => utility [patent_app_number] => 13/845699 [patent_app_country] => US [patent_app_date] => 2013-03-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 8 [patent_no_of_words] => 4511 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 1 [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] => 13845699 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/845699
Combustor support assembly for mounting a combustion module of a gas turbine Mar 17, 2013 Issued
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] => 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 [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] => 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] => 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] => 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
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