
Terri L. Filosi
Examiner (ID: 15877, Phone: (571)270-1988 , Office: P/2143 )
| Most Active Art Unit | 3644 |
| Art Unit(s) | 3644, 2178, 3762, 2143 |
| Total Applications | 473 |
| Issued Applications | 280 |
| Pending Applications | 38 |
| Abandoned Applications | 165 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 15434555
[patent_doc_number] => 20200031460
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2020-01-30
[patent_title] => UNMANNED AERIAL VEHICLE FOR DELIVERING CARGO
[patent_app_type] => utility
[patent_app_number] => 16/516529
[patent_app_country] => US
[patent_app_date] => 2019-07-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 8835
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -17
[patent_words_short_claim] => 87
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16516529
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/516529 | UNMANNED AERIAL VEHICLE FOR DELIVERING CARGO | Jul 18, 2019 | Abandoned |
Array
(
[id] => 16869668
[patent_doc_number] => 20210163135
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2021-06-03
[patent_title] => DRONE STATION
[patent_app_type] => utility
[patent_app_number] => 17/261452
[patent_app_country] => US
[patent_app_date] => 2019-07-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 8440
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -19
[patent_words_short_claim] => 56
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17261452
[rel_patent_id] =>[rel_patent_doc_number] =>) 17/261452 | Drone station | Jul 18, 2019 | Issued |
Array
(
[id] => 17267218
[patent_doc_number] => 11192628
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2021-12-07
[patent_title] => Articulated flap support forward fairing
[patent_app_type] => utility
[patent_app_number] => 16/458100
[patent_app_country] => US
[patent_app_date] => 2019-06-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 12
[patent_no_of_words] => 2330
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 156
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16458100
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/458100 | Articulated flap support forward fairing | Jun 29, 2019 | Issued |
Array
(
[id] => 18526137
[patent_doc_number] => 11713119
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2023-08-01
[patent_title] => Rotorcraft
[patent_app_type] => utility
[patent_app_number] => 16/396795
[patent_app_country] => US
[patent_app_date] => 2019-04-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 6
[patent_no_of_words] => 3594
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 170
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16396795
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/396795 | Rotorcraft | Apr 28, 2019 | Issued |
Array
(
[id] => 16436723
[patent_doc_number] => 20200354049
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2020-11-12
[patent_title] => VERTICAL TAKE-OFF AND LANDING VEHICLE
[patent_app_type] => utility
[patent_app_number] => 16/640347
[patent_app_country] => US
[patent_app_date] => 2019-04-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 45509
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -33
[patent_words_short_claim] => 25
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16640347
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/640347 | Vertical take-off and landing vehicle | Apr 16, 2019 | Issued |
Array
(
[id] => 18589977
[patent_doc_number] => 11738855
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2023-08-29
[patent_title] => System and method for propeller response enhancement during transition from ground to flight configuration for a turbopropeller engine
[patent_app_type] => utility
[patent_app_number] => 16/982312
[patent_app_country] => US
[patent_app_date] => 2019-03-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 12
[patent_no_of_words] => 5111
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 3
[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] => 16982312
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/982312 | System and method for propeller response enhancement during transition from ground to flight configuration for a turbopropeller engine | Mar 21, 2019 | Issued |
Array
(
[id] => 14896167
[patent_doc_number] => 20190291849
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2019-09-26
[patent_title] => AIRCRAFT HAVING ARTICULATED HORIZONTAL TAIL UNITS
[patent_app_type] => utility
[patent_app_number] => 16/297841
[patent_app_country] => US
[patent_app_date] => 2019-03-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 2045
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -7
[patent_words_short_claim] => 154
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16297841
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/297841 | Aircraft having articulated horizontal tail units | Mar 10, 2019 | Issued |
Array
(
[id] => 16436728
[patent_doc_number] => 20200354054
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2020-11-12
[patent_title] => A VERTICAL TAKE OFF AND LANDING FLYING MACHINE
[patent_app_type] => utility
[patent_app_number] => 16/964754
[patent_app_country] => US
[patent_app_date] => 2019-01-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 7419
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -19
[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] => 16964754
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/964754 | Vertical take off and landing flying machine | Jan 21, 2019 | Issued |
Array
(
[id] => 16360581
[patent_doc_number] => 20200317332
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2020-10-08
[patent_title] => TANDEM WING TAIL-SITTING AIRCRAFT WITH TILTING BODY
[patent_app_type] => utility
[patent_app_number] => 16/956658
[patent_app_country] => US
[patent_app_date] => 2018-12-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 13776
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -12
[patent_words_short_claim] => 43
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16956658
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/956658 | TANDEM WING TAIL-SITTING AIRCRAFT WITH TILTING BODY | Dec 20, 2018 | Abandoned |
Array
(
[id] => 14835483
[patent_doc_number] => 20190276142
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2019-09-12
[patent_title] => Torque Path Coupling Assemblies for Tiltrotor Aircraft
[patent_app_type] => utility
[patent_app_number] => 16/212045
[patent_app_country] => US
[patent_app_date] => 2018-12-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 6516
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -17
[patent_words_short_claim] => 258
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16212045
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/212045 | Torque path coupling assemblies for tiltrotor aircraft | Dec 5, 2018 | Issued |
Array
(
[id] => 16343125
[patent_doc_number] => 20200307775
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2020-10-01
[patent_title] => SYSTEM AND METHOD FOR ACTUATING HIGH-LIFT FLIGHT CONTROL SURFACES
[patent_app_type] => utility
[patent_app_number] => 16/765591
[patent_app_country] => US
[patent_app_date] => 2018-11-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 5101
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -22
[patent_words_short_claim] => 96
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16765591
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/765591 | System and method for actuating high-lift flight control surfaces | Nov 18, 2018 | Issued |
Array
(
[id] => 15849899
[patent_doc_number] => 10640212
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2020-05-05
[patent_title] => Double wing aircraft
[patent_app_type] => utility
[patent_app_number] => 16/194366
[patent_app_country] => US
[patent_app_date] => 2018-11-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 17
[patent_no_of_words] => 6863
[patent_no_of_claims] => 3
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 211
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16194366
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/194366 | Double wing aircraft | Nov 17, 2018 | Issued |
Array
(
[id] => 15588873
[patent_doc_number] => 20200070971
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2020-03-05
[patent_title] => RING-SHAPED AIRFOIL AIRCRAFT CAPABLE OF TAKING OFF AND LANDING VERTICALLY, AND HOVERING
[patent_app_type] => utility
[patent_app_number] => 16/191448
[patent_app_country] => US
[patent_app_date] => 2018-11-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 3928
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -6
[patent_words_short_claim] => 262
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16191448
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/191448 | Ring-shaped airfoil aircraft capable of taking off and landing vertically, and hovering | Nov 14, 2018 | Issued |
Array
(
[id] => 17192863
[patent_doc_number] => 11161600
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2021-11-02
[patent_title] => Methods of moving an aircraft undercarriage between a retracted position and a deployed position
[patent_app_type] => utility
[patent_app_number] => 16/191313
[patent_app_country] => US
[patent_app_date] => 2018-11-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 5
[patent_no_of_words] => 2898
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 111
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16191313
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/191313 | Methods of moving an aircraft undercarriage between a retracted position and a deployed position | Nov 13, 2018 | Issued |
Array
(
[id] => 15897673
[patent_doc_number] => 20200148355
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2020-05-14
[patent_title] => Modular Weapon Carriage and Deployment (MWCD) System
[patent_app_type] => utility
[patent_app_number] => 16/190711
[patent_app_country] => US
[patent_app_date] => 2018-11-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 5125
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -15
[patent_words_short_claim] => 115
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16190711
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/190711 | Modular weapon carriage and deployment (MWCD) system | Nov 13, 2018 | Issued |
Array
(
[id] => 16222409
[patent_doc_number] => 20200247525
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2020-08-06
[patent_title] => ASSEMBLY OF THREE COMPOSITE WINGS FOR AERIAL, WATER, LAND OR SPACE VEHICLES
[patent_app_type] => utility
[patent_app_number] => 16/758442
[patent_app_country] => US
[patent_app_date] => 2018-10-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 3873
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -9
[patent_words_short_claim] => 374
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16758442
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/758442 | ASSEMBLY OF THREE COMPOSITE WINGS FOR AERIAL, WATER, LAND OR SPACE VEHICLES | Oct 29, 2018 | Abandoned |
Array
(
[id] => 17267222
[patent_doc_number] => 11192632
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2021-12-07
[patent_title] => Slat end seal and method for manufacturing the same
[patent_app_type] => utility
[patent_app_number] => 16/160002
[patent_app_country] => US
[patent_app_date] => 2018-10-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 14
[patent_no_of_words] => 6240
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 141
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16160002
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/160002 | Slat end seal and method for manufacturing the same | Oct 14, 2018 | Issued |
Array
(
[id] => 14229741
[patent_doc_number] => 20190127043
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2019-05-02
[patent_title] => WING SEGMENT AND AIRCRAFT HAVING A WING SEGMENT
[patent_app_type] => utility
[patent_app_number] => 16/160171
[patent_app_country] => US
[patent_app_date] => 2018-10-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 12033
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -9
[patent_words_short_claim] => 106
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16160171
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/160171 | WING SEGMENT AND AIRCRAFT HAVING A WING SEGMENT | Oct 14, 2018 | Abandoned |
Array
(
[id] => 17207488
[patent_doc_number] => 11167845
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2021-11-09
[patent_title] => High speed rotorcraft propulsion configuration
[patent_app_type] => utility
[patent_app_number] => 16/143240
[patent_app_country] => US
[patent_app_date] => 2018-09-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 12
[patent_no_of_words] => 6086
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 144
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16143240
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/143240 | High speed rotorcraft propulsion configuration | Sep 25, 2018 | Issued |
Array
(
[id] => 14101561
[patent_doc_number] => 20190092456
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2019-03-28
[patent_title] => DUCTS FOR LAMINAR FLOW CONTROL SYSTEMS
[patent_app_type] => utility
[patent_app_number] => 16/142716
[patent_app_country] => US
[patent_app_date] => 2018-09-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 3930
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -17
[patent_words_short_claim] => 86
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16142716
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/142716 | DUCTS FOR LAMINAR FLOW CONTROL SYSTEMS | Sep 25, 2018 | Abandoned |