
Mesfin T. Asfaw
Examiner (ID: 7501, Phone: (571)270-5247 , Office: P/2882 )
| Most Active Art Unit | 2882 |
| Art Unit(s) | 2851, 2882 |
| Total Applications | 1100 |
| Issued Applications | 877 |
| Pending Applications | 71 |
| Abandoned Applications | 175 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 18128677
[patent_doc_number] => 11554875
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2023-01-17
[patent_title] => Method of electrically powering an electricity network, and an electrical architecture
[patent_app_type] => utility
[patent_app_number] => 16/903580
[patent_app_country] => US
[patent_app_date] => 2020-06-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 4
[patent_no_of_words] => 6973
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 189
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16903580
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/903580 | Method of electrically powering an electricity network, and an electrical architecture | Jun 16, 2020 | Issued |
Array
(
[id] => 17822366
[patent_doc_number] => 11427301
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2022-08-30
[patent_title] => Load relieving carrier beam
[patent_app_type] => utility
[patent_app_number] => 16/900630
[patent_app_country] => US
[patent_app_date] => 2020-06-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 13
[patent_no_of_words] => 2734
[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] => 16900630
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/900630 | Load relieving carrier beam | Jun 11, 2020 | Issued |
Array
(
[id] => 17696818
[patent_doc_number] => 11370527
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2022-06-28
[patent_title] => Variable camber trim units, aircraft comprising the same, and associated methods of operation
[patent_app_type] => utility
[patent_app_number] => 16/895235
[patent_app_country] => US
[patent_app_date] => 2020-06-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 12
[patent_no_of_words] => 12456
[patent_no_of_claims] => 23
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 363
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16895235
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/895235 | Variable camber trim units, aircraft comprising the same, and associated methods of operation | Jun 7, 2020 | Issued |
Array
(
[id] => 17696819
[patent_doc_number] => 11370528
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2022-06-28
[patent_title] => Variable camber trim units, aircraft comprising the same, and associated methods of operation
[patent_app_type] => utility
[patent_app_number] => 16/895260
[patent_app_country] => US
[patent_app_date] => 2020-06-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 12
[patent_no_of_words] => 11145
[patent_no_of_claims] => 21
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 129
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16895260
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/895260 | Variable camber trim units, aircraft comprising the same, and associated methods of operation | Jun 7, 2020 | Issued |
Array
(
[id] => 17784382
[patent_doc_number] => 11407491
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2022-08-09
[patent_title] => Lift-sharing wing with rotatable trailing edge
[patent_app_type] => utility
[patent_app_number] => 16/894224
[patent_app_country] => US
[patent_app_date] => 2020-06-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 12
[patent_no_of_words] => 5842
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 76
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16894224
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/894224 | Lift-sharing wing with rotatable trailing edge | Jun 4, 2020 | Issued |
Array
(
[id] => 18071232
[patent_doc_number] => 11530051
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2022-12-20
[patent_title] => Noise-reducing aircraft landing gear tow bar fitting
[patent_app_type] => utility
[patent_app_number] => 16/893028
[patent_app_country] => US
[patent_app_date] => 2020-06-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 16
[patent_no_of_words] => 9637
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 60
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16893028
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/893028 | Noise-reducing aircraft landing gear tow bar fitting | Jun 3, 2020 | Issued |
Array
(
[id] => 16312007
[patent_doc_number] => 20200290745
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2020-09-17
[patent_title] => PROPULSION SYSTEM FOR AN AIRCRAFT
[patent_app_type] => utility
[patent_app_number] => 16/891316
[patent_app_country] => US
[patent_app_date] => 2020-06-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 12002
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -17
[patent_words_short_claim] => 93
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16891316
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/891316 | Propulsion system for an aircraft | Jun 2, 2020 | Issued |
Array
(
[id] => 18963847
[patent_doc_number] => 11897593
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2024-02-13
[patent_title] => Telescoping support structure
[patent_app_type] => utility
[patent_app_number] => 16/888999
[patent_app_country] => US
[patent_app_date] => 2020-06-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 12
[patent_no_of_words] => 7188
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 117
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16888999
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/888999 | Telescoping support structure | May 31, 2020 | Issued |
Array
(
[id] => 17634750
[patent_doc_number] => 11345460
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2022-05-31
[patent_title] => Rotatable empennage for an aircraft
[patent_app_type] => utility
[patent_app_number] => 16/886932
[patent_app_country] => US
[patent_app_date] => 2020-05-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 5
[patent_no_of_words] => 2514
[patent_no_of_claims] => 21
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 60
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16886932
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/886932 | Rotatable empennage for an aircraft | May 28, 2020 | Issued |
Array
(
[id] => 17258101
[patent_doc_number] => 20210371086
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2021-12-02
[patent_title] => ACTUATION ASSEMBLIES FOR FLIGHT CONTROL SURFACES
[patent_app_type] => utility
[patent_app_number] => 16/887164
[patent_app_country] => US
[patent_app_date] => 2020-05-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 7405
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -18
[patent_words_short_claim] => 40
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16887164
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/887164 | Actuation assemblies for flight control surfaces | May 28, 2020 | Issued |
Array
(
[id] => 17481768
[patent_doc_number] => 20220089272
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2022-03-24
[patent_title] => ANTIVIBRATION KIT-OF-PARTS AND PARTS THEREFOR, AIRFOIL STRUCTURE AND AIRCRAFT PROVIDED THEREWITH
[patent_app_type] => utility
[patent_app_number] => 17/424808
[patent_app_country] => US
[patent_app_date] => 2020-05-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 5894
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -16
[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] => 17424808
[rel_patent_id] =>[rel_patent_doc_number] =>) 17/424808 | Antivibration kit-of-parts and parts therefor, airfoil structure and aircraft provided therewith | May 25, 2020 | Issued |
Array
(
[id] => 17369506
[patent_doc_number] => 20220024558
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2022-01-27
[patent_title] => ARRANGEMENT FOR AVOIDING CLASHING BETWEEN AN ACTUATION ASSEMBLY AND AN UPPER COVER OF A FOLDING WING TIP
[patent_app_type] => utility
[patent_app_number] => 17/296644
[patent_app_country] => US
[patent_app_date] => 2020-05-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 4592
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -8
[patent_words_short_claim] => 171
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17296644
[rel_patent_id] =>[rel_patent_doc_number] =>) 17/296644 | Arrangement for avoiding clashing between an actuation assembly and an upper cover of a folding wing tip | May 20, 2020 | Issued |
Array
(
[id] => 17749273
[patent_doc_number] => 20220227477
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2022-07-21
[patent_title] => Aircraft having a folding system
[patent_app_type] => utility
[patent_app_number] => 17/614065
[patent_app_country] => US
[patent_app_date] => 2020-05-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 8559
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -21
[patent_words_short_claim] => 362
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17614065
[rel_patent_id] =>[rel_patent_doc_number] =>) 17/614065 | Aircraft having a folding system | May 19, 2020 | Issued |
Array
(
[id] => 17727448
[patent_doc_number] => 11383822
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2022-07-12
[patent_title] => Distributed active brakes for aircraft high-lift devices
[patent_app_type] => utility
[patent_app_number] => 16/879502
[patent_app_country] => US
[patent_app_date] => 2020-05-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 6455
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 177
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16879502
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/879502 | Distributed active brakes for aircraft high-lift devices | May 19, 2020 | Issued |
Array
(
[id] => 17343289
[patent_doc_number] => 20220009620
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2022-01-13
[patent_title] => LANDING GEAR ASSEMBLY
[patent_app_type] => utility
[patent_app_number] => 17/296788
[patent_app_country] => US
[patent_app_date] => 2020-05-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 6513
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -11
[patent_words_short_claim] => 67
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17296788
[rel_patent_id] =>[rel_patent_doc_number] =>) 17/296788 | Landing gear assembly | May 18, 2020 | Issued |
Array
(
[id] => 19105542
[patent_doc_number] => 11958622
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2024-04-16
[patent_title] => Protection functions
[patent_app_type] => utility
[patent_app_number] => 16/875095
[patent_app_country] => US
[patent_app_date] => 2020-05-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 2396
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 61
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16875095
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/875095 | Protection functions | May 14, 2020 | Issued |
Array
(
[id] => 18665901
[patent_doc_number] => 11772776
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2023-10-03
[patent_title] => Arrangement for avoiding clashing on a folding wing tip
[patent_app_type] => utility
[patent_app_number] => 17/297827
[patent_app_country] => US
[patent_app_date] => 2020-05-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 10
[patent_no_of_words] => 5737
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 133
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17297827
[rel_patent_id] =>[rel_patent_doc_number] =>) 17/297827 | Arrangement for avoiding clashing on a folding wing tip | May 13, 2020 | Issued |
Array
(
[id] => 16556825
[patent_doc_number] => 20210001973
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2021-01-07
[patent_title] => Hinged wing ribs for fabric covered wings and method for folding wings
[patent_app_type] => utility
[patent_app_number] => 16/873572
[patent_app_country] => US
[patent_app_date] => 2020-05-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 5607
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -16
[patent_words_short_claim] => 166
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16873572
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/873572 | Hinged wing ribs for fabric covered wings and method for folding wings | May 6, 2020 | Issued |
Array
(
[id] => 17125758
[patent_doc_number] => 20210300526
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2021-09-30
[patent_title] => Feedback mechanism and circuit design for flight control boost actuators
[patent_app_type] => utility
[patent_app_number] => 16/873559
[patent_app_country] => US
[patent_app_date] => 2020-05-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 2916
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -6
[patent_words_short_claim] => 183
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16873559
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/873559 | Feedback mechanism and circuit design for flight control boost actuators | May 3, 2020 | Abandoned |
Array
(
[id] => 16421564
[patent_doc_number] => 20200346762
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2020-11-05
[patent_title] => SYSTEM FOR AN AIRCRAFT
[patent_app_type] => utility
[patent_app_number] => 16/856442
[patent_app_country] => US
[patent_app_date] => 2020-04-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 7289
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -14
[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] => 16856442
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/856442 | System for an aircraft | Apr 22, 2020 | Issued |