Search

William H. Rodriguez

Examiner (ID: 10133, Phone: (571)272-4831 , Office: P/3741 )

Most Active Art Unit
3741
Art Unit(s)
3746, 3741
Total Applications
1830
Issued Applications
1603
Pending Applications
89
Abandoned Applications
161

Applications

Application numberTitle of the applicationFiling DateStatus
Array ( [id] => 18718543 [patent_doc_number] => 11795879 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2023-10-24 [patent_title] => Combustor with an igniter provided within at least one of a fuel injector or a compressed air passage [patent_app_type] => utility [patent_app_number] => 17/589145 [patent_app_country] => US [patent_app_date] => 2022-01-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 6981 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 158 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17589145 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/589145
Combustor with an igniter provided within at least one of a fuel injector or a compressed air passage Jan 30, 2022 Issued
Array ( [id] => 18538402 [patent_doc_number] => 20230243505 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2023-08-03 [patent_title] => TURBINE ENGINE WITH FUEL SYSTEM INCLUDING A CATALYTIC REFORMER [patent_app_type] => utility [patent_app_number] => 17/588876 [patent_app_country] => US [patent_app_date] => 2022-01-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 6204 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 2 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17588876 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/588876
Turbine engine with fuel system including a catalytic reformer Jan 30, 2022 Issued
Array ( [id] => 18964763 [patent_doc_number] => 11898519 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2024-02-13 [patent_title] => Heating system for a spacecraft [patent_app_type] => utility [patent_app_number] => 17/588088 [patent_app_country] => US [patent_app_date] => 2022-01-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 1 [patent_no_of_words] => 4578 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 127 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17588088 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/588088
Heating system for a spacecraft Jan 27, 2022 Issued
Array ( [id] => 18188299 [patent_doc_number] => 11578871 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2023-02-14 [patent_title] => Gas turbine engine combustor with primary and secondary fuel injectors [patent_app_type] => utility [patent_app_number] => 17/587634 [patent_app_country] => US [patent_app_date] => 2022-01-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 5994 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 148 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17587634 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/587634
Gas turbine engine combustor with primary and secondary fuel injectors Jan 27, 2022 Issued
Array ( [id] => 18329978 [patent_doc_number] => 11635209 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2023-04-25 [patent_title] => Gas turbine combustor dome with integrated flare swirler [patent_app_type] => utility [patent_app_number] => 17/649128 [patent_app_country] => US [patent_app_date] => 2022-01-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 15 [patent_no_of_words] => 8956 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 288 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17649128 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/649128
Gas turbine combustor dome with integrated flare swirler Jan 26, 2022 Issued
Array ( [id] => 18469929 [patent_doc_number] => 20230204214 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2023-06-29 [patent_title] => FUEL-AIR MIXING ASSEMBLY IN A TURBINE ENGINE [patent_app_type] => utility [patent_app_number] => 17/586082 [patent_app_country] => US [patent_app_date] => 2022-01-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 11927 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -14 [patent_words_short_claim] => 2 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17586082 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/586082
Fuel-air mixing assembly in a turbine engine Jan 26, 2022 Issued
Array ( [id] => 18233738 [patent_doc_number] => 11598289 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2023-03-07 [patent_title] => Propellant volume and mixture ratio control [patent_app_type] => utility [patent_app_number] => 17/647498 [patent_app_country] => US [patent_app_date] => 2022-01-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 7 [patent_no_of_words] => 5630 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 173 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17647498 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/647498
Propellant volume and mixture ratio control Jan 9, 2022 Issued
Array ( [id] => 19624659 [patent_doc_number] => 12163471 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2024-12-10 [patent_title] => Fuel system and method for supplying a combustion chamber in an aircraft turboshaft engine with fuel [patent_app_type] => utility [patent_app_number] => 18/261185 [patent_app_country] => US [patent_app_date] => 2022-01-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 10 [patent_no_of_words] => 6327 [patent_no_of_claims] => 20 [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] => 18261185 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/261185
Fuel system and method for supplying a combustion chamber in an aircraft turboshaft engine with fuel Jan 6, 2022 Issued
Array ( [id] => 17548874 [patent_doc_number] => 20220120215 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-04-21 [patent_title] => GAS TURBINE ENGINE AND METHOD FOR OPERATING SAME [patent_app_type] => utility [patent_app_number] => 17/567592 [patent_app_country] => US [patent_app_date] => 2022-01-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 4732 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -18 [patent_words_short_claim] => 80 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17567592 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/567592
Gas turbine engine having electric motor for applying power to a spool shaft and method for operating same Jan 2, 2022 Issued
Array ( [id] => 17688671 [patent_doc_number] => 20220195963 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-06-23 [patent_title] => INJECTION MANIFOLD WITH TESLA VALVES FOR ROTATING DETONATION ENGINES [patent_app_type] => utility [patent_app_number] => 17/553550 [patent_app_country] => US [patent_app_date] => 2021-12-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 5851 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -16 [patent_words_short_claim] => 71 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17553550 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/553550
Injection manifold with tesla valves for rotating detonation engines Dec 15, 2021 Issued
Array ( [id] => 18445149 [patent_doc_number] => 11680710 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2023-06-20 [patent_title] => Fuel nozzle, fuel nozzle module having the same, and combustor [patent_app_type] => utility [patent_app_number] => 17/550099 [patent_app_country] => US [patent_app_date] => 2021-12-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 13 [patent_no_of_words] => 5095 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 188 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17550099 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/550099
Fuel nozzle, fuel nozzle module having the same, and combustor Dec 13, 2021 Issued
Array ( [id] => 17750536 [patent_doc_number] => 20220228741 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-07-21 [patent_title] => NOZZLE ASSEMBLY, COMBUSTOR, AND GAS TURBINE HAVING SAME [patent_app_type] => utility [patent_app_number] => 17/548498 [patent_app_country] => US [patent_app_date] => 2021-12-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 5048 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 186 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17548498 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/548498
Nozzle assembly, combustor, and gas turbine having same Dec 10, 2021 Issued
Array ( [id] => 17688673 [patent_doc_number] => 20220195965 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-06-23 [patent_title] => COMBUSTION CHAMBER, METHOD OF MANUFACTURING A COMBUSTION CHAMBER AND ENGINE [patent_app_type] => utility [patent_app_number] => 17/544032 [patent_app_country] => US [patent_app_date] => 2021-12-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 5042 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -14 [patent_words_short_claim] => 142 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17544032 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/544032
Rocket combustion chamber wall having cooling channels and method for making thereof Dec 6, 2021 Issued
Array ( [id] => 18749151 [patent_doc_number] => 11808455 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2023-11-07 [patent_title] => Gas turbine engine combustor with integral fuel conduit(s) [patent_app_type] => utility [patent_app_number] => 17/535133 [patent_app_country] => US [patent_app_date] => 2021-11-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 8 [patent_no_of_words] => 4441 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 77 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17535133 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/535133
Gas turbine engine combustor with integral fuel conduit(s) Nov 23, 2021 Issued
Array ( [id] => 19068228 [patent_doc_number] => 20240102654 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2024-03-28 [patent_title] => BURNER WITH A BILAMINAR COUNTERDIRECTIONAL VORTEX FLOW [patent_app_type] => utility [patent_app_number] => 18/272178 [patent_app_country] => US [patent_app_date] => 2021-11-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 1322 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => 0 [patent_words_short_claim] => 118 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18272178 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/272178
Burner with two-layer vortex countercurrent flow Nov 16, 2021 Issued
Array ( [id] => 18917115 [patent_doc_number] => 11879388 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2024-01-23 [patent_title] => System and method for monitoring fuel additives [patent_app_type] => utility [patent_app_number] => 17/521024 [patent_app_country] => US [patent_app_date] => 2021-11-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 8 [patent_no_of_words] => 4422 [patent_no_of_claims] => 7 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 214 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17521024 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/521024
System and method for monitoring fuel additives Nov 7, 2021 Issued
Array ( [id] => 18879947 [patent_doc_number] => 20240003316 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2024-01-04 [patent_title] => TURBOJET ENGINE REAR PART COMPRISING A NOZZLE HAVING FLAPS COMPRISING LEVERS THAT ARE MOVABLE BY MEANS OF UPSTREAM AND DOWNSTREAM BEARING WALLS [patent_app_type] => utility [patent_app_number] => 18/252079 [patent_app_country] => US [patent_app_date] => 2021-11-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 4571 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -7 [patent_words_short_claim] => 317 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18252079 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/252079
Turbojet engine rear part comprising a nozzle having flaps comprising levers that are movable by means of upstream and downstream bearing walls Nov 4, 2021 Issued
Array ( [id] => 18355601 [patent_doc_number] => 11643995 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2023-05-09 [patent_title] => Liquid rocket engine injector with variable flow area [patent_app_type] => utility [patent_app_number] => 17/453580 [patent_app_country] => US [patent_app_date] => 2021-11-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 8 [patent_no_of_words] => 7931 [patent_no_of_claims] => 22 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 163 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17453580 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/453580
Liquid rocket engine injector with variable flow area Nov 3, 2021 Issued
Array ( [id] => 18845416 [patent_doc_number] => 20230407820 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2023-12-21 [patent_title] => COMBUSTOR INCLUDING HEAT EXCHANGE STRUCTURE AND ROCKET COMPRISING SAME [patent_app_type] => utility [patent_app_number] => 18/251617 [patent_app_country] => US [patent_app_date] => 2021-11-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 9257 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -20 [patent_words_short_claim] => 75 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18251617 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/251617
Combustor including heat exchange structure and rocket comprising same Nov 3, 2021 Issued
Array ( [id] => 18879946 [patent_doc_number] => 20240003315 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2024-01-04 [patent_title] => FASTENING OF AN EXHAUST CONE IN A TURBOMACHINE NOZZLE [patent_app_type] => utility [patent_app_number] => 18/251798 [patent_app_country] => US [patent_app_date] => 2021-11-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 4117 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -15 [patent_words_short_claim] => 155 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18251798 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/251798
Fastening of an exhaust cone in a turbomachine nozzle Nov 2, 2021 Issued
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