
William H. Rodriguez
Examiner (ID: 13536)
| Most Active Art Unit | 3741 |
| Art Unit(s) | 3746, 3741 |
| Total Applications | 1829 |
| Issued Applications | 1600 |
| Pending Applications | 88 |
| Abandoned Applications | 161 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 19904797
[patent_doc_number] => 12281795
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2025-04-22
[patent_title] => Cluster of swirled mini-mixers for fuel-staged, axially staged combustion
[patent_app_type] => utility
[patent_app_number] => 18/601912
[patent_app_country] => US
[patent_app_date] => 2024-03-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 1082
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 179
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18601912
[rel_patent_id] =>[rel_patent_doc_number] =>) 18/601912 | Cluster of swirled mini-mixers for fuel-staged, axially staged combustion | Mar 10, 2024 | Issued |
Array
(
[id] => 19301141
[patent_doc_number] => 20240229710
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2024-07-11
[patent_title] => SYSTEM AND METHOD HAVING MULTI-FLUID INJECTORS FOR ISOTHERMAL EXPANSION IN TURBINE STAGE OF GAS TURBINE ENGINE
[patent_app_type] => utility
[patent_app_number] => 18/433223
[patent_app_country] => US
[patent_app_date] => 2024-02-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 28939
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -17
[patent_words_short_claim] => 85
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18433223
[rel_patent_id] =>[rel_patent_doc_number] =>) 18/433223 | System and method having multi-fluid injectors for isothermal expansion in turbine stage of gas turbine engine | Feb 4, 2024 | Issued |
Array
(
[id] => 19709948
[patent_doc_number] => 20250020090
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2025-01-16
[patent_title] => REUSABLE UPPER STAGE ROCKET WITH AEROSPIKE ENGINE
[patent_app_type] => utility
[patent_app_number] => 18/433160
[patent_app_country] => US
[patent_app_date] => 2024-02-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 9188
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -21
[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] => 18433160
[rel_patent_id] =>[rel_patent_doc_number] =>) 18/433160 | Reusable upper stage rocket with aerospike engine | Feb 4, 2024 | Issued |
Array
(
[id] => 19739043
[patent_doc_number] => 12215868
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2025-02-04
[patent_title] => Injector with disc for hydrogen-driven gas turbine engine
[patent_app_type] => utility
[patent_app_number] => 18/423649
[patent_app_country] => US
[patent_app_date] => 2024-01-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 7
[patent_no_of_words] => 2888
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 121
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18423649
[rel_patent_id] =>[rel_patent_doc_number] =>) 18/423649 | Injector with disc for hydrogen-driven gas turbine engine | Jan 25, 2024 | Issued |
Array
(
[id] => 20144587
[patent_doc_number] => 12378920
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2025-08-05
[patent_title] => Gas turbine engine comprising fuel-oil heat exchangers fluidly connected to fuel spray nozzles
[patent_app_type] => utility
[patent_app_number] => 18/421471
[patent_app_country] => US
[patent_app_date] => 2024-01-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 9
[patent_no_of_words] => 18664
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 192
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18421471
[rel_patent_id] =>[rel_patent_doc_number] =>) 18/421471 | Gas turbine engine comprising fuel-oil heat exchangers fluidly connected to fuel spray nozzles | Jan 23, 2024 | Issued |
Array
(
[id] => 19218832
[patent_doc_number] => 20240183536
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2024-06-06
[patent_title] => TURBINE ENGINE WITH FUEL NOZZLE ASSEMBLY
[patent_app_type] => utility
[patent_app_number] => 18/409690
[patent_app_country] => US
[patent_app_date] => 2024-01-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 8710
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -18
[patent_words_short_claim] => 79
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18409690
[rel_patent_id] =>[rel_patent_doc_number] =>) 18/409690 | Gas turbine fuel nozzle having an inner air passage and plural outer fuel passages | Jan 9, 2024 | Issued |
Array
(
[id] => 19301525
[patent_doc_number] => 20240230096
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2024-07-11
[patent_title] => METHOD OF OPERATING GAS TURBINE COMBUSTOR WITH MULTIPLE FUEL STAGES
[patent_app_type] => utility
[patent_app_number] => 18/401572
[patent_app_country] => US
[patent_app_date] => 2023-12-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 15835
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -18
[patent_words_short_claim] => 238
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18401572
[rel_patent_id] =>[rel_patent_doc_number] =>) 18/401572 | Method of operating gas turbine combustor with multiple fuel stages | Dec 30, 2023 | Issued |
Array
(
[id] => 19970406
[patent_doc_number] => 12339006
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2025-06-24
[patent_title] => Turbine engine having a combustion section with a fuel nozzle assembly
[patent_app_type] => utility
[patent_app_number] => 18/394407
[patent_app_country] => US
[patent_app_date] => 2023-12-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 16
[patent_figures_cnt] => 16
[patent_no_of_words] => 10868
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 208
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18394407
[rel_patent_id] =>[rel_patent_doc_number] =>) 18/394407 | Turbine engine having a combustion section with a fuel nozzle assembly | Dec 21, 2023 | Issued |
Array
(
[id] => 19480584
[patent_doc_number] => 20240328626
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2024-10-03
[patent_title] => CENTRAL STAGED COMBUSTION CHAMBER WITH SELF-EXCITED SWEEPING OSCILLATING FUEL INJECTION NOZZLES
[patent_app_type] => utility
[patent_app_number] => 18/541041
[patent_app_country] => US
[patent_app_date] => 2023-12-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 5116
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -9
[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] => 18541041
[rel_patent_id] =>[rel_patent_doc_number] =>) 18/541041 | Central staged combustion chamber with self-excited sweeping oscillating fuel injection nozzles | Dec 14, 2023 | Issued |
Array
(
[id] => 19068230
[patent_doc_number] => 20240102656
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2024-03-28
[patent_title] => COMBUSTOR FOR A GAS TURBINE ENGINE
[patent_app_type] => utility
[patent_app_number] => 18/529360
[patent_app_country] => US
[patent_app_date] => 2023-12-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 12087
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -19
[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] => 18529360
[rel_patent_id] =>[rel_patent_doc_number] =>) 18/529360 | Method of operating a gas turbine combustor comprising injecting a diluent into the primary and secondary combustion zones | Dec 4, 2023 | Issued |
Array
(
[id] => 20159022
[patent_doc_number] => 12385642
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2025-08-12
[patent_title] => Sequential combustion gas turbine engine including a steam system for injecting steam to each combustor
[patent_app_type] => utility
[patent_app_number] => 18/507877
[patent_app_country] => US
[patent_app_date] => 2023-11-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 9081
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 199
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18507877
[rel_patent_id] =>[rel_patent_doc_number] =>) 18/507877 | Sequential combustion gas turbine engine including a steam system for injecting steam to each combustor | Nov 12, 2023 | Issued |
Array
(
[id] => 19301105
[patent_doc_number] => 20240229674
[patent_country] => US
[patent_kind] => A9
[patent_issue_date] => 2024-07-11
[patent_title] => METHOD OF STARTING A GAS TURBINE ENGINE
[patent_app_type] => utility
[patent_app_number] => 18/488217
[patent_app_country] => US
[patent_app_date] => 2023-10-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 9416
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -13
[patent_words_short_claim] => 117
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18488217
[rel_patent_id] =>[rel_patent_doc_number] =>) 18/488217 | Method of starting a gas turbine engine | Oct 16, 2023 | Issued |
Array
(
[id] => 19301105
[patent_doc_number] => 20240229674
[patent_country] => US
[patent_kind] => A9
[patent_issue_date] => 2024-07-11
[patent_title] => METHOD OF STARTING A GAS TURBINE ENGINE
[patent_app_type] => utility
[patent_app_number] => 18/488217
[patent_app_country] => US
[patent_app_date] => 2023-10-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 9416
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -13
[patent_words_short_claim] => 117
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18488217
[rel_patent_id] =>[rel_patent_doc_number] =>) 18/488217 | Method of starting a gas turbine engine | Oct 16, 2023 | Issued |
Array
(
[id] => 19113539
[patent_doc_number] => 20240125289
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2024-04-18
[patent_title] => DRIVE SYSTEM FOR AN AIRCRAFT, AIRCRAFT HAVING A DRIVE SYSTEM AND METHOD FOR OPERATING AN AIRCRAFT
[patent_app_type] => utility
[patent_app_number] => 18/484827
[patent_app_country] => US
[patent_app_date] => 2023-10-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 3934
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -13
[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] => 18484827
[rel_patent_id] =>[rel_patent_doc_number] =>) 18/484827 | Drive system for an aircraft, aircraft having a drive system and method for operating an aircraft | Oct 10, 2023 | Issued |
Array
(
[id] => 19580557
[patent_doc_number] => 12146662
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2024-11-19
[patent_title] => Fuel-air mixing assembly in a turbine engine
[patent_app_type] => utility
[patent_app_number] => 18/482949
[patent_app_country] => US
[patent_app_date] => 2023-10-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 18
[patent_no_of_words] => 11941
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 113
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18482949
[rel_patent_id] =>[rel_patent_doc_number] =>) 18/482949 | Fuel-air mixing assembly in a turbine engine | Oct 8, 2023 | Issued |
Array
(
[id] => 19898510
[patent_doc_number] => 12276424
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2025-04-15
[patent_title] => Fuel nozzle having inner and outer mixing chambers fed with fuel via first and second hole patterns
[patent_app_type] => utility
[patent_app_number] => 18/377776
[patent_app_country] => US
[patent_app_date] => 2023-10-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 5
[patent_no_of_words] => 0
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 3
[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] => 18377776
[rel_patent_id] =>[rel_patent_doc_number] =>) 18/377776 | Fuel nozzle having inner and outer mixing chambers fed with fuel via first and second hole patterns | Oct 6, 2023 | Issued |
Array
(
[id] => 19890933
[patent_doc_number] => 20250116245
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2025-04-10
[patent_title] => DEAERATOR IMPELLER ROTOR WITH GEAR ROTOR
[patent_app_type] => utility
[patent_app_number] => 18/377469
[patent_app_country] => US
[patent_app_date] => 2023-10-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 5577
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -17
[patent_words_short_claim] => 110
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18377469
[rel_patent_id] =>[rel_patent_doc_number] =>) 18/377469 | DEAERATOR IMPELLER ROTOR WITH GEAR ROTOR | Oct 5, 2023 | Pending |
Array
(
[id] => 18923810
[patent_doc_number] => 20240026814
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2024-01-25
[patent_title] => COMBUSTION DEVICE AND GAS TURBINE SYSTEM
[patent_app_type] => utility
[patent_app_number] => 18/479992
[patent_app_country] => US
[patent_app_date] => 2023-10-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 12138
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -17
[patent_words_short_claim] => 44
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18479992
[rel_patent_id] =>[rel_patent_doc_number] =>) 18/479992 | Gas turbine combustion system having an ammonia autothermal cracking device | Oct 2, 2023 | Issued |
Array
(
[id] => 18903641
[patent_doc_number] => 20240019126
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2024-01-18
[patent_title] => INJECTION MANIFOLD WITH TESLA VALVES FOR ROTATING DETONATION ENGINES
[patent_app_type] => utility
[patent_app_number] => 18/372796
[patent_app_country] => US
[patent_app_date] => 2023-09-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 5969
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -16
[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] => 18372796
[rel_patent_id] =>[rel_patent_doc_number] =>) 18/372796 | Injection manifold with Tesla valves for rotating detonation engines | Sep 25, 2023 | Issued |
Array
(
[id] => 19218834
[patent_doc_number] => 20240183538
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2024-06-06
[patent_title] => COMBUSTOR AND GAS TURBINE INCLUDING SAME
[patent_app_type] => utility
[patent_app_number] => 18/473246
[patent_app_country] => US
[patent_app_date] => 2023-09-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 5773
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -16
[patent_words_short_claim] => 168
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18473246
[rel_patent_id] =>[rel_patent_doc_number] =>) 18/473246 | Gas turbine combustor injector assembly comprising an air supply unit having an inclined surface relative to an inclined injection pipe | Sep 23, 2023 | Issued |