Search

Don M. Anderson

Examiner (ID: 18785, Phone: (571)272-4923 , Office: P/3781 )

Most Active Art Unit
3733
Art Unit(s)
3733, 3781
Total Applications
696
Issued Applications
390
Pending Applications
70
Abandoned Applications
254

Applications

Application numberTitle of the applicationFiling DateStatus
Array ( [id] => 17657810 [patent_doc_number] => 20220178275 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-06-09 [patent_title] => CONTROLLING LUBRICANT FLOW IN EPICYCLIC GEARBOX [patent_app_type] => utility [patent_app_number] => 17/676520 [patent_app_country] => US [patent_app_date] => 2022-02-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 4257 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -16 [patent_words_short_claim] => 102 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17676520 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/676520
Controlling lubricant flow in epicyclic gearbox Feb 20, 2022 Issued
Array ( [id] => 18583747 [patent_doc_number] => 20230266008 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2023-08-24 [patent_title] => FUEL INJECTOR WITH SPLASH PLATE FOR AN ENGINE [patent_app_type] => utility [patent_app_number] => 17/675584 [patent_app_country] => US [patent_app_date] => 2022-02-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 6685 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 65 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17675584 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/675584
Fuel injector with splash plate for an engine Feb 17, 2022 Issued
Array ( [id] => 19412544 [patent_doc_number] => 12078356 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2024-09-03 [patent_title] => Subassembly comprising means for compensating for a difference in expansion [patent_app_type] => utility [patent_app_number] => 18/546205 [patent_app_country] => US [patent_app_date] => 2022-02-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 4 [patent_no_of_words] => 2475 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 125 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18546205 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/546205
Subassembly comprising means for compensating for a difference in expansion Feb 13, 2022 Issued
Array ( [id] => 18567795 [patent_doc_number] => 20230258130 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2023-08-17 [patent_title] => TURBINE ENGINE WITH MASS REJECTION [patent_app_type] => utility [patent_app_number] => 17/669632 [patent_app_country] => US [patent_app_date] => 2022-02-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 9065 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -19 [patent_words_short_claim] => 108 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17669632 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/669632
Turbine engine with mass rejection Feb 10, 2022 Issued
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 Issued
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 Abandoned
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 Abandoned
Array ( [id] => 19433337 [patent_doc_number] => 20240301835 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2024-09-12 [patent_title] => METHOD OF CONTROLLING A COMBUSTOR [patent_app_type] => utility [patent_app_number] => 18/254865 [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] => 7010 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -15 [patent_words_short_claim] => 263 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18254865 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/254865
Method of controlling a combustor Nov 25, 2021 Issued
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
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