Willis Little
Examiner (ID: 16938)
Most Active Art Unit | 3203 |
Art Unit(s) | 3203, 3643, 2107, 2103, 2406, 3616, 2401, 2899, 2403 |
Total Applications | 2327 |
Issued Applications | 2182 |
Pending Applications | 48 |
Abandoned Applications | 97 |
Applications
Application number | Title of the application | Filing Date | Status |
---|---|---|---|
Array
(
[id] => 18964711
[patent_doc_number] => 11898467
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2024-02-13
[patent_title] => Aircraft engine struts with stiffening protrusions
[patent_app_type] => utility
[patent_app_number] => 17/650756
[patent_app_country] => US
[patent_app_date] => 2022-02-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 7
[patent_no_of_words] => 3451
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 304
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17650756
[rel_patent_id] =>[rel_patent_doc_number] =>) 17/650756 | Aircraft engine struts with stiffening protrusions | Feb 10, 2022 | Issued |
Array
(
[id] => 19044139
[patent_doc_number] => 11933231
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2024-03-19
[patent_title] => Methods and systems for tuning a gas turbine engine
[patent_app_type] => utility
[patent_app_number] => 17/665935
[patent_app_country] => US
[patent_app_date] => 2022-02-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 9087
[patent_no_of_claims] => 30
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 191
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17665935
[rel_patent_id] =>[rel_patent_doc_number] =>) 17/665935 | Methods and systems for tuning a gas turbine engine | Feb 6, 2022 | Issued |
Array
(
[id] => 18315784
[patent_doc_number] => 11629858
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2023-04-18
[patent_title] => Turboexpander inter-stage heating and NH3 cracking
[patent_app_type] => utility
[patent_app_number] => 17/665063
[patent_app_country] => US
[patent_app_date] => 2022-02-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 10
[patent_no_of_words] => 4480
[patent_no_of_claims] => 29
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 184
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17665063
[rel_patent_id] =>[rel_patent_doc_number] =>) 17/665063 | Turboexpander inter-stage heating and NH3 cracking | Feb 3, 2022 | Issued |
Array
(
[id] => 18538208
[patent_doc_number] => 20230243311
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2023-08-03
[patent_title] => FUEL SUPPLY SYSTEM FOR A COMBUSTOR
[patent_app_type] => utility
[patent_app_number] => 17/590472
[patent_app_country] => US
[patent_app_date] => 2022-02-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 10312
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -19
[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] => 17590472
[rel_patent_id] =>[rel_patent_doc_number] =>) 17/590472 | FUEL SUPPLY SYSTEM FOR A COMBUSTOR | Jan 31, 2022 | Pending |
Array
(
[id] => 18948667
[patent_doc_number] => 11891953
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2024-02-06
[patent_title] => Aircraft skin heat exchanger
[patent_app_type] => utility
[patent_app_number] => 17/584909
[patent_app_country] => US
[patent_app_date] => 2022-01-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 5
[patent_no_of_words] => 2563
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 109
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17584909
[rel_patent_id] =>[rel_patent_doc_number] =>) 17/584909 | Aircraft skin heat exchanger | Jan 25, 2022 | Issued |
Array
(
[id] => 18478756
[patent_doc_number] => 11692489
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2023-07-04
[patent_title] => Igniter for gas turbine engine
[patent_app_type] => utility
[patent_app_number] => 17/584483
[patent_app_country] => US
[patent_app_date] => 2022-01-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 16
[patent_figures_cnt] => 28
[patent_no_of_words] => 14417
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 186
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17584483
[rel_patent_id] =>[rel_patent_doc_number] =>) 17/584483 | Igniter for gas turbine engine | Jan 25, 2022 | Issued |
Array
(
[id] => 18560587
[patent_doc_number] => 11725823
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2023-08-15
[patent_title] => Mounting a ceramic component to a non-ceramic component in a gas turbine engine
[patent_app_type] => utility
[patent_app_number] => 17/567533
[patent_app_country] => US
[patent_app_date] => 2022-01-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 21
[patent_figures_cnt] => 26
[patent_no_of_words] => 6811
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 142
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17567533
[rel_patent_id] =>[rel_patent_doc_number] =>) 17/567533 | Mounting a ceramic component to a non-ceramic component in a gas turbine engine | Jan 2, 2022 | Issued |
Array
(
[id] => 18948881
[patent_doc_number] => 11892169
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2024-02-06
[patent_title] => Gas turbine combustor structure
[patent_app_type] => utility
[patent_app_number] => 17/562395
[patent_app_country] => US
[patent_app_date] => 2021-12-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 7892
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 236
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17562395
[rel_patent_id] =>[rel_patent_doc_number] =>) 17/562395 | Gas turbine combustor structure | Dec 26, 2021 | Issued |
Array
(
[id] => 18102990
[patent_doc_number] => 11542871
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2023-01-03
[patent_title] => Injection nozzle, combustor including same, and gas turbine including same
[patent_app_type] => utility
[patent_app_number] => 17/561963
[patent_app_country] => US
[patent_app_date] => 2021-12-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 8
[patent_no_of_words] => 6336
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 265
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17561963
[rel_patent_id] =>[rel_patent_doc_number] =>) 17/561963 | Injection nozzle, combustor including same, and gas turbine including same | Dec 25, 2021 | Issued |
Array
(
[id] => 19397561
[patent_doc_number] => 12071914
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2024-08-27
[patent_title] => Rocket engine systems with a supercritical coolant
[patent_app_type] => utility
[patent_app_number] => 17/561621
[patent_app_country] => US
[patent_app_date] => 2021-12-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 1661
[patent_no_of_claims] => 3
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 302
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17561621
[rel_patent_id] =>[rel_patent_doc_number] =>) 17/561621 | Rocket engine systems with a supercritical coolant | Dec 22, 2021 | Issued |
Array
(
[id] => 18505186
[patent_doc_number] => 11702992
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2023-07-18
[patent_title] => Combustor wall core with resonator and/or damper elements
[patent_app_type] => utility
[patent_app_number] => 17/541758
[patent_app_country] => US
[patent_app_date] => 2021-12-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 18
[patent_figures_cnt] => 27
[patent_no_of_words] => 6274
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 195
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17541758
[rel_patent_id] =>[rel_patent_doc_number] =>) 17/541758 | Combustor wall core with resonator and/or damper elements | Dec 2, 2021 | Issued |
Array
(
[id] => 18972707
[patent_doc_number] => 20240052799
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2024-02-15
[patent_title] => JET VECTORING APPARATUS
[patent_app_type] => utility
[patent_app_number] => 18/260396
[patent_app_country] => US
[patent_app_date] => 2021-12-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 10342
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -17
[patent_words_short_claim] => 241
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18260396
[rel_patent_id] =>[rel_patent_doc_number] =>) 18/260396 | JET VECTORING APPARATUS | Nov 30, 2021 | Pending |
Array
(
[id] => 19035208
[patent_doc_number] => 20240085023
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2024-03-14
[patent_title] => PREMIXED COMBUSTION BURNER, FUEL INJECTOR, AND GAS TURBINE
[patent_app_type] => utility
[patent_app_number] => 18/270305
[patent_app_country] => US
[patent_app_date] => 2021-11-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 10268
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -10
[patent_words_short_claim] => 207
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18270305
[rel_patent_id] =>[rel_patent_doc_number] =>) 18/270305 | PREMIXED COMBUSTION BURNER, FUEL INJECTOR, AND GAS TURBINE | Nov 25, 2021 | Pending |
Array
(
[id] => 19121487
[patent_doc_number] => 11965458
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2024-04-23
[patent_title] => Multi-mode engine system with gas turbine engine and turbo-compressor
[patent_app_type] => utility
[patent_app_number] => 17/535128
[patent_app_country] => US
[patent_app_date] => 2021-11-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 14
[patent_no_of_words] => 4225
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 167
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17535128
[rel_patent_id] =>[rel_patent_doc_number] =>) 17/535128 | Multi-mode engine system with gas turbine engine and turbo-compressor | Nov 23, 2021 | Issued |
Array
(
[id] => 18685760
[patent_doc_number] => 11781485
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2023-10-10
[patent_title] => Unit cell resonator networks for gas turbine combustor tone damping
[patent_app_type] => utility
[patent_app_number] => 17/535270
[patent_app_country] => US
[patent_app_date] => 2021-11-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 22
[patent_figures_cnt] => 58
[patent_no_of_words] => 13686
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 174
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17535270
[rel_patent_id] =>[rel_patent_doc_number] =>) 17/535270 | Unit cell resonator networks for gas turbine combustor tone damping | Nov 23, 2021 | Issued |
Array
(
[id] => 18779671
[patent_doc_number] => 11821370
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2023-11-21
[patent_title] => Cooling system for tail cone mounted generator
[patent_app_type] => utility
[patent_app_number] => 17/529625
[patent_app_country] => US
[patent_app_date] => 2021-11-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 2286
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 243
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17529625
[rel_patent_id] =>[rel_patent_doc_number] =>) 17/529625 | Cooling system for tail cone mounted generator | Nov 17, 2021 | Issued |
Array
(
[id] => 17688650
[patent_doc_number] => 20220195942
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2022-06-23
[patent_title] => AIR TURBINE STARTER TORQUE CONTROL SYSTEM
[patent_app_type] => utility
[patent_app_number] => 17/523470
[patent_app_country] => US
[patent_app_date] => 2021-11-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 4965
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -17
[patent_words_short_claim] => 188
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17523470
[rel_patent_id] =>[rel_patent_doc_number] =>) 17/523470 | Air turbine starter torque control system | Nov 9, 2021 | Issued |
Array
(
[id] => 17721077
[patent_doc_number] => 20220213797
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2022-07-07
[patent_title] => TURBOMACHINE WITH LOW LEAKAGE SEAL ASSEMBLY FOR COMBUSTOR-TURBINE INTERFACE
[patent_app_type] => utility
[patent_app_number] => 17/453525
[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] => 4566
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -17
[patent_words_short_claim] => 150
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17453525
[rel_patent_id] =>[rel_patent_doc_number] =>) 17/453525 | TURBOMACHINE WITH LOW LEAKAGE SEAL ASSEMBLY FOR COMBUSTOR-TURBINE INTERFACE | Nov 3, 2021 | Abandoned |
Array
(
[id] => 17596258
[patent_doc_number] => 20220145832
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2022-05-12
[patent_title] => INJECTION DEVICE FOR LIQUID ROCKET
[patent_app_type] => utility
[patent_app_number] => 17/516465
[patent_app_country] => US
[patent_app_date] => 2021-11-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 3585
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -7
[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] => 17516465
[rel_patent_id] =>[rel_patent_doc_number] =>) 17/516465 | Injection device for liquid rocket | Oct 31, 2021 | Issued |
Array
(
[id] => 18872027
[patent_doc_number] => 11859819
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2024-01-02
[patent_title] => Ceramic composite combustor dome and liners
[patent_app_type] => utility
[patent_app_number] => 17/451102
[patent_app_country] => US
[patent_app_date] => 2021-10-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 12
[patent_no_of_words] => 5992
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 182
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17451102
[rel_patent_id] =>[rel_patent_doc_number] =>) 17/451102 | Ceramic composite combustor dome and liners | Oct 14, 2021 | Issued |