Search

Thomas P. Burke

Examiner (ID: 9758, Phone: (571)270-5407 , Office: P/3741 )

Most Active Art Unit
3741
Art Unit(s)
3741
Total Applications
418
Issued Applications
146
Pending Applications
82
Abandoned Applications
215

Applications

Application numberTitle of the applicationFiling DateStatus
15/285701 THERMAL MANAGEMENT SYSTEM AND METHOD OF USING SAME Oct 4, 2016 Abandoned
Array ( [id] => 17713235 [patent_doc_number] => 11377216 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2022-07-05 [patent_title] => Advanced method and aircraft for pre-cooling an environmental control system using a dual compressor four wheel turbo-machine [patent_app_type] => utility [patent_app_number] => 15/244497 [patent_app_country] => US [patent_app_date] => 2016-08-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 11714 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 252 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15244497 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/244497
Advanced method and aircraft for pre-cooling an environmental control system using a dual compressor four wheel turbo-machine Aug 22, 2016 Issued
Array ( [id] => 12218811 [patent_doc_number] => 20180057170 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2018-03-01 [patent_title] => 'ENHANCED METHOD AND AIRCRAFT FOR PRE-COOLING AN ENVIRONMENTAL CONTROL SYSTEM USING A TWO WHEEL TURBO-MACHINE WITH SUPPLEMENTAL HEAT EXCHANGER' [patent_app_type] => utility [patent_app_number] => 15/244086 [patent_app_country] => US [patent_app_date] => 2016-08-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 9805 [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] => 15244086 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/244086
ENHANCED METHOD AND AIRCRAFT FOR PRE-COOLING AN ENVIRONMENTAL CONTROL SYSTEM USING A TWO WHEEL TURBO-MACHINE WITH SUPPLEMENTAL HEAT EXCHANGER Aug 22, 2016 Abandoned
Array ( [id] => 12205586 [patent_doc_number] => 20180050812 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2018-02-22 [patent_title] => 'AIRCRAFT FUEL PUMP SYSTEMS' [patent_app_type] => utility [patent_app_number] => 15/237905 [patent_app_country] => US [patent_app_date] => 2016-08-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 3183 [patent_no_of_claims] => 18 [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] => 15237905 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/237905
AIRCRAFT FUEL PUMP SYSTEMS Aug 15, 2016 Abandoned
Array ( [id] => 13358811 [patent_doc_number] => 20180230945 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2018-08-16 [patent_title] => AIRCRAFT COMPRISING A REAR FAIRING PROPULSION SYSTEM WITH INLET STATOR COMPRISING A BLOWING FUNCTION [patent_app_type] => utility [patent_app_number] => 15/745932 [patent_app_country] => US [patent_app_date] => 2016-07-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 7136 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -9 [patent_words_short_claim] => 163 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15745932 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/745932
Aircraft comprising a rear fairing propulsion system with inlet stator comprising a blowing function Jul 20, 2016 Issued
Array ( [id] => 16665700 [patent_doc_number] => 10934937 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2021-03-02 [patent_title] => Method and apparatus for variable supplemental airflow to cool aircraft components [patent_app_type] => utility [patent_app_number] => 15/213491 [patent_app_country] => US [patent_app_date] => 2016-07-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 5 [patent_no_of_words] => 3918 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 6 [patent_words_short_claim] => 160 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15213491 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/213491
Method and apparatus for variable supplemental airflow to cool aircraft components Jul 18, 2016 Issued
Array ( [id] => 12138937 [patent_doc_number] => 20180017019 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2018-01-18 [patent_title] => 'TURBOFAN ENGINE WTH A SPLITTERED ROTOR FAN' [patent_app_type] => utility [patent_app_number] => 15/211787 [patent_app_country] => US [patent_app_date] => 2016-07-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 4897 [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] => 15211787 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/211787
TURBOFAN ENGINE WTH A SPLITTERED ROTOR FAN Jul 14, 2016 Abandoned
Array ( [id] => 13704103 [patent_doc_number] => 20170363006 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2017-12-21 [patent_title] => SYSTEM TO ENABLE SPRAY INTERCOOLING IN ISOCHRONOUS OPERATION FOR POWER AUGMENTATION FOR SPRAY INTERCOOLING ENGINES [patent_app_type] => utility [patent_app_number] => 15/187338 [patent_app_country] => US [patent_app_date] => 2016-06-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 5105 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 86 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15187338 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/187338
SYSTEM TO ENABLE SPRAY INTERCOOLING IN ISOCHRONOUS OPERATION FOR POWER AUGMENTATION FOR SPRAY INTERCOOLING ENGINES Jun 19, 2016 Abandoned
Array ( [id] => 13690775 [patent_doc_number] => 20170356342 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2017-12-14 [patent_title] => CIRCUIT-LEVEL HEATING FOR WIDE WOBBE FUELS IN DLN GAS TURBINE COMBUSTION [patent_app_type] => utility [patent_app_number] => 15/182003 [patent_app_country] => US [patent_app_date] => 2016-06-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 4509 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 127 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15182003 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/182003
CIRCUIT-LEVEL HEATING FOR WIDE WOBBE FUELS IN DLN GAS TURBINE COMBUSTION Jun 13, 2016 Abandoned
Array ( [id] => 12981979 [patent_doc_number] => 20170342913 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2017-11-30 [patent_title] => GAS TURBINE ENGINE INLET TEMPERATURE SENSOR CONFIGURATION [patent_app_type] => utility [patent_app_number] => 15/162727 [patent_app_country] => US [patent_app_date] => 2016-05-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 3469 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 51 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15162727 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/162727
GAS TURBINE ENGINE INLET TEMPERATURE SENSOR CONFIGURATION May 23, 2016 Abandoned
Array ( [id] => 14215521 [patent_doc_number] => 20190120145 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2019-04-25 [patent_title] => GAS TURBINE HAVING FUEL GAS MONITORING SYSTEM [patent_app_type] => utility [patent_app_number] => 16/094484 [patent_app_country] => US [patent_app_date] => 2016-05-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 3855 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -18 [patent_words_short_claim] => 159 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16094484 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/094484
GAS TURBINE HAVING FUEL GAS MONITORING SYSTEM May 22, 2016 Abandoned
Array ( [id] => 12752185 [patent_doc_number] => 20180142562 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2018-05-24 [patent_title] => Turbine Engine Comprising a Lobed Mixer Having Scoops [patent_app_type] => utility [patent_app_number] => 15/572430 [patent_app_country] => US [patent_app_date] => 2016-05-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 3351 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -7 [patent_words_short_claim] => 211 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15572430 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/572430
Turbine Engine Comprising a Lobed Mixer Having Scoops May 10, 2016 Abandoned
Array ( [id] => 12031501 [patent_doc_number] => 20170321600 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2017-11-09 [patent_title] => 'SYSTEM AND METHOD FOR A GAS TURBINE POWER GENERATION SYSTEM WITH A HIGH PRESSURE COMPRESSOR WITH AN ADDED FORWARD STAGE' [patent_app_type] => utility [patent_app_number] => 15/148801 [patent_app_country] => US [patent_app_date] => 2016-05-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 3086 [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] => 15148801 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/148801
SYSTEM AND METHOD FOR A GAS TURBINE POWER GENERATION SYSTEM WITH A HIGH PRESSURE COMPRESSOR WITH AN ADDED FORWARD STAGE May 5, 2016 Abandoned
Array ( [id] => 11130008 [patent_doc_number] => 20160326983 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2016-11-10 [patent_title] => 'INTEGRATED TEC/MIXER STRUT AXIAL POSITION' [patent_app_type] => utility [patent_app_number] => 15/137257 [patent_app_country] => US [patent_app_date] => 2016-04-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 3751 [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] => 15137257 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/137257
Integrated TEC/mixer strut axial position Apr 24, 2016 Issued
Array ( [id] => 11978919 [patent_doc_number] => 20170283073 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2017-10-05 [patent_title] => 'INTEGRATED AIRCRAFT ENVIRONMENTAL CONTROL AND BUFFER SYSTEM' [patent_app_type] => utility [patent_app_number] => 15/089713 [patent_app_country] => US [patent_app_date] => 2016-04-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 4196 [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] => 15089713 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/089713
INTEGRATED AIRCRAFT ENVIRONMENTAL CONTROL AND BUFFER SYSTEM Apr 3, 2016 Abandoned
Array ( [id] => 16277466 [patent_doc_number] => 10760486 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2020-09-01 [patent_title] => Turbine engine fan module including a turbine engine inlet cone de-icing system, and a de-icing method [patent_app_type] => utility [patent_app_number] => 15/561116 [patent_app_country] => US [patent_app_date] => 2016-03-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 4 [patent_no_of_words] => 3551 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 227 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15561116 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/561116
Turbine engine fan module including a turbine engine inlet cone de-icing system, and a de-icing method Mar 30, 2016 Issued
Array ( [id] => 11980520 [patent_doc_number] => 20170284674 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2017-10-05 [patent_title] => 'CLOSED TRAPPED VORTEX CAVITY PILOT FOR A GAS TURBINE ENGINE AUGMENTOR' [patent_app_type] => utility [patent_app_number] => 15/085165 [patent_app_country] => US [patent_app_date] => 2016-03-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 5375 [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] => 15085165 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/085165
Closed trapped vortex cavity pilot for a gas turbine engine augmentor Mar 29, 2016 Issued
Array ( [id] => 10799897 [patent_doc_number] => 20160146055 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2016-05-26 [patent_title] => 'LINER HANGER WITH SPHERICAL WASHERS' [patent_app_type] => utility [patent_app_number] => 15/014131 [patent_app_country] => US [patent_app_date] => 2016-02-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 3071 [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] => 15014131 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/014131
LINER HANGER WITH SPHERICAL WASHERS Feb 2, 2016 Abandoned
Array ( [id] => 14666979 [patent_doc_number] => 10371384 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2019-08-06 [patent_title] => Fuel injection system for aircraft turbomachine, comprising a variable section air through duct [patent_app_type] => utility [patent_app_number] => 15/542860 [patent_app_country] => US [patent_app_date] => 2016-01-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 7 [patent_no_of_words] => 2798 [patent_no_of_claims] => 7 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 202 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15542860 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/542860
Fuel injection system for aircraft turbomachine, comprising a variable section air through duct Jan 19, 2016 Issued
Array ( [id] => 10737949 [patent_doc_number] => 20160084100 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2016-03-24 [patent_title] => 'SYSTEM AND APPARATUS FOR SEAL RETENTION AND PROTECTION' [patent_app_type] => utility [patent_app_number] => 14/951665 [patent_app_country] => US [patent_app_date] => 2015-11-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 3733 [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] => 14951665 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/951665
SYSTEM AND APPARATUS FOR SEAL RETENTION AND PROTECTION Nov 24, 2015 Abandoned
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