Search

Scott J. Walthour

Examiner (ID: 7255, Phone: (571)272-4999 , Office: P/3741 )

Most Active Art Unit
3741
Art Unit(s)
3741
Total Applications
786
Issued Applications
588
Pending Applications
68
Abandoned Applications
145

Applications

Application numberTitle of the applicationFiling DateStatus
Array ( [id] => 11402712 [patent_doc_number] => 20170023250 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2017-01-26 [patent_title] => 'COWLING PART AND COMBUSTOR ASSEMBLY FOR A GAS TURBINE' [patent_app_type] => utility [patent_app_number] => 15/208315 [patent_app_country] => US [patent_app_date] => 2016-07-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 5127 [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] => 15208315 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/208315
COWLING PART AND COMBUSTOR ASSEMBLY FOR A GAS TURBINE Jul 11, 2016 Abandoned
Array ( [id] => 12139174 [patent_doc_number] => 20180017257 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2018-01-18 [patent_title] => 'COMBUSTOR CASSETTE LINER MOUNTING ASSEMBLY' [patent_app_type] => utility [patent_app_number] => 15/208290 [patent_app_country] => US [patent_app_date] => 2016-07-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 6391 [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] => 15208290 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/208290
Combustor cassette liner mounting assembly Jul 11, 2016 Issued
Array ( [id] => 12126879 [patent_doc_number] => 20180010465 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2018-01-11 [patent_title] => 'COOLING HOLE WITH SHAPED METER' [patent_app_type] => utility [patent_app_number] => 15/207472 [patent_app_country] => US [patent_app_date] => 2016-07-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 7213 [patent_no_of_claims] => 21 [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] => 15207472 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/207472
Cooling hole with shaped meter Jul 10, 2016 Issued
Array ( [id] => 12911644 [patent_doc_number] => 20180195724 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2018-07-12 [patent_title] => BURNER FOR A GAS TURBINE [patent_app_type] => utility [patent_app_number] => 15/742162 [patent_app_country] => US [patent_app_date] => 2016-07-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 3680 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -14 [patent_words_short_claim] => 121 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15742162 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/742162
BURNER FOR A GAS TURBINE Jul 7, 2016 Abandoned
Array ( [id] => 17105230 [patent_doc_number] => 11125435 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2021-09-21 [patent_title] => Bent combustion chamber from a turbine engine [patent_app_type] => utility [patent_app_number] => 15/742447 [patent_app_country] => US [patent_app_date] => 2016-07-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 9 [patent_no_of_words] => 3173 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 501 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15742447 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/742447
Bent combustion chamber from a turbine engine Jul 6, 2016 Issued
Array ( [id] => 11108695 [patent_doc_number] => 20160305665 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2016-10-20 [patent_title] => 'AFTERBURNER AND AIRCRAFT ENGINE' [patent_app_type] => utility [patent_app_number] => 15/196271 [patent_app_country] => US [patent_app_date] => 2016-06-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 4213 [patent_no_of_claims] => 4 [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] => 15196271 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/196271
Afterburner and aircraft engine Jun 28, 2016 Issued
Array ( [id] => 13718673 [patent_doc_number] => 20170370291 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2017-12-28 [patent_title] => SYSTEM AND METHOD OF COOLING A TURBINE ENGINE [patent_app_type] => utility [patent_app_number] => 15/193981 [patent_app_country] => US [patent_app_date] => 2016-06-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 4486 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 43 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15193981 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/193981
System and method of cooling a turbine engine Jun 26, 2016 Issued
Array ( [id] => 13888929 [patent_doc_number] => 10197011 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2019-02-05 [patent_title] => Afterburner and aircraft engine [patent_app_type] => utility [patent_app_number] => 15/193286 [patent_app_country] => US [patent_app_date] => 2016-06-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 3760 [patent_no_of_claims] => 2 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 369 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15193286 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/193286
Afterburner and aircraft engine Jun 26, 2016 Issued
Array ( [id] => 16185211 [patent_doc_number] => 10718525 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2020-07-21 [patent_title] => Fuel injection locations based on combustor flow path [patent_app_type] => utility [patent_app_number] => 15/194203 [patent_app_country] => US [patent_app_date] => 2016-06-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 24 [patent_figures_cnt] => 42 [patent_no_of_words] => 10163 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 293 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15194203 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/194203
Fuel injection locations based on combustor flow path Jun 26, 2016 Issued
Array ( [id] => 13704681 [patent_doc_number] => 20170363295 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2017-12-21 [patent_title] => SMALL EXIT DUCT FOR A REVERSE FLOW COMBUSTOR WITH INTEGRATED COOLING ELEMENTS [patent_app_type] => utility [patent_app_number] => 15/185317 [patent_app_country] => US [patent_app_date] => 2016-06-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 3401 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 116 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15185317 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/185317
Small exit duct for a reverse flow combustor with integrated cooling elements Jun 16, 2016 Issued
Array ( [id] => 12911641 [patent_doc_number] => 20180195723 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2018-07-12 [patent_title] => BURNER FOR A GAS TURBINE [patent_app_type] => utility [patent_app_number] => 15/742151 [patent_app_country] => US [patent_app_date] => 2016-06-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 3745 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -13 [patent_words_short_claim] => 136 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15742151 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/742151
Burner for a gas turbine Jun 9, 2016 Issued
Array ( [id] => 11743629 [patent_doc_number] => 20170197701 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2017-07-13 [patent_title] => 'COOLING OF AEROSPACE FLIGHT SYSTEMS' [patent_app_type] => utility [patent_app_number] => 15/168812 [patent_app_country] => US [patent_app_date] => 2016-05-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 11 [patent_no_of_words] => 4508 [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] => 15168812 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/168812
COOLING OF AEROSPACE FLIGHT SYSTEMS May 30, 2016 Abandoned
Array ( [id] => 12981952 [patent_doc_number] => 20170342903 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2017-11-30 [patent_title] => SYSTEM AND METHOD OF COMPRESSOR INLET TEMPERATURE CONTROL WITH MIXING CHAMBER [patent_app_type] => utility [patent_app_number] => 15/167328 [patent_app_country] => US [patent_app_date] => 2016-05-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 10174 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -18 [patent_words_short_claim] => 88 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15167328 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/167328
System and method of compressor inlet temperature control with mixing chamber May 26, 2016 Issued
Array ( [id] => 14007241 [patent_doc_number] => 10222066 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2019-03-05 [patent_title] => Ducting arrangement with injector assemblies arranged in an expanding cross-sectional area of a downstream combustion stage in a gas turbine engine [patent_app_type] => utility [patent_app_number] => 15/165195 [patent_app_country] => US [patent_app_date] => 2016-05-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 19 [patent_no_of_words] => 4081 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 360 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15165195 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/165195
Ducting arrangement with injector assemblies arranged in an expanding cross-sectional area of a downstream combustion stage in a gas turbine engine May 25, 2016 Issued
Array ( [id] => 12981784 [patent_doc_number] => 20170342839 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2017-11-30 [patent_title] => SYSTEM FOR A LOW SWIRL LOW PRESSURE TURBINE [patent_app_type] => utility [patent_app_number] => 15/164648 [patent_app_country] => US [patent_app_date] => 2016-05-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 3849 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 109 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15164648 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/164648
SYSTEM FOR A LOW SWIRL LOW PRESSURE TURBINE May 24, 2016 Abandoned
Array ( [id] => 14666219 [patent_doc_number] => 10371003 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2019-08-06 [patent_title] => Aircraft vapour trail control system [patent_app_type] => utility [patent_app_number] => 15/163318 [patent_app_country] => US [patent_app_date] => 2016-05-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 13 [patent_no_of_words] => 8157 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 213 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15163318 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/163318
Aircraft vapour trail control system May 23, 2016 Issued
Array ( [id] => 16941906 [patent_doc_number] => 11054135 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2021-07-06 [patent_title] => Gas turbine fuel nozzle with integrated flame ionization sensor and gas turbine engine [patent_app_type] => utility [patent_app_number] => 15/576036 [patent_app_country] => US [patent_app_date] => 2016-05-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 9 [patent_no_of_words] => 1905 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 204 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15576036 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/576036
Gas turbine fuel nozzle with integrated flame ionization sensor and gas turbine engine May 22, 2016 Issued
Array ( [id] => 17267969 [patent_doc_number] => 11193386 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2021-12-07 [patent_title] => Shaped cooling passages for turbine blade outer air seal [patent_app_type] => utility [patent_app_number] => 15/157857 [patent_app_country] => US [patent_app_date] => 2016-05-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 10 [patent_no_of_words] => 4567 [patent_no_of_claims] => 2 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 154 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15157857 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/157857
Shaped cooling passages for turbine blade outer air seal May 17, 2016 Issued
Array ( [id] => 14640035 [patent_doc_number] => 10364752 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2019-07-30 [patent_title] => System and method for an integral drive engine with a forward main gearbox [patent_app_type] => utility [patent_app_number] => 15/156476 [patent_app_country] => US [patent_app_date] => 2016-05-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 4413 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 124 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15156476 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/156476
System and method for an integral drive engine with a forward main gearbox May 16, 2016 Issued
Array ( [id] => 11271154 [patent_doc_number] => 20160333700 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2016-11-17 [patent_title] => 'METHOD FOR COOLING A GAS TURBINE AND GAS TURBINE FOR CONDUCTING SAID METHOD' [patent_app_type] => utility [patent_app_number] => 15/154322 [patent_app_country] => US [patent_app_date] => 2016-05-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 3050 [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] => 15154322 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/154322
Method for cooling a gas turbine and gas turbine for conducting said method May 12, 2016 Issued
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