
Assres H. Woldemaryam
Examiner (ID: 10832, Phone: (571)272-6607 , Office: P/3647 )
| Most Active Art Unit | 3642 |
| Art Unit(s) | 3647, 3642, 3645, RD00 |
| Total Applications | 894 |
| Issued Applications | 700 |
| Pending Applications | 89 |
| Abandoned Applications | 126 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 13443313
[patent_doc_number] => 20180273199
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2018-09-27
[patent_title] => AERODYNAMIC CONTROL SURFACE MOVEMENT MONITORING SYSTEM FOR AIRCRAFT
[patent_app_type] => utility
[patent_app_number] => 15/469740
[patent_app_country] => US
[patent_app_date] => 2017-03-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 5053
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -18
[patent_words_short_claim] => 184
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15469740
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/469740 | Aerodynamic control surface movement monitoring system for aircraft | Mar 26, 2017 | Issued |
Array
(
[id] => 14947777
[patent_doc_number] => 10435145
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2019-10-08
[patent_title] => Vehicle with tension wing assembly
[patent_app_type] => utility
[patent_app_number] => 15/469542
[patent_app_country] => US
[patent_app_date] => 2017-03-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 28
[patent_figures_cnt] => 35
[patent_no_of_words] => 18122
[patent_no_of_claims] => 22
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 225
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15469542
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/469542 | Vehicle with tension wing assembly | Mar 25, 2017 | Issued |
Array
(
[id] => 16140869
[patent_doc_number] => 10703493
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2020-07-07
[patent_title] => Danger avoidance apparatus and method of use
[patent_app_type] => utility
[patent_app_number] => 15/468539
[patent_app_country] => US
[patent_app_date] => 2017-03-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 14
[patent_figures_cnt] => 14
[patent_no_of_words] => 13150
[patent_no_of_claims] => 28
[patent_no_of_ind_claims] => 1
[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] => 15468539
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/468539 | Danger avoidance apparatus and method of use | Mar 23, 2017 | Issued |
Array
(
[id] => 16060319
[patent_doc_number] => 10689089
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2020-06-23
[patent_title] => Entry handle for an aircraft doorway
[patent_app_type] => utility
[patent_app_number] => 15/468650
[patent_app_country] => US
[patent_app_date] => 2017-03-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 18
[patent_figures_cnt] => 22
[patent_no_of_words] => 4579
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 115
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15468650
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/468650 | Entry handle for an aircraft doorway | Mar 23, 2017 | Issued |
Array
(
[id] => 13443301
[patent_doc_number] => 20180273193
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2018-09-27
[patent_title] => ELECTRICALLY OPERATED PROPELLANT THRUST ASSIST FOR SUPPLEMENTING AIRPLANE TAKEOFF, LANDING OR IN-FLIGHT MANEUVERABILITY
[patent_app_type] => utility
[patent_app_number] => 15/469026
[patent_app_country] => US
[patent_app_date] => 2017-03-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 6111
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -18
[patent_words_short_claim] => 280
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15469026
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/469026 | ELECTRICALLY OPERATED PROPELLANT THRUST ASSIST FOR SUPPLEMENTING AIRPLANE TAKEOFF, LANDING OR IN-FLIGHT MANEUVERABILITY | Mar 23, 2017 | Abandoned |
Array
(
[id] => 13443271
[patent_doc_number] => 20180273178
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2018-09-27
[patent_title] => CARPET DISPLAY SYSTEMS AND METHODS
[patent_app_type] => utility
[patent_app_number] => 15/468166
[patent_app_country] => US
[patent_app_date] => 2017-03-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 7852
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -17
[patent_words_short_claim] => 55
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15468166
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/468166 | Carpet display systems and methods | Mar 23, 2017 | Issued |
Array
(
[id] => 13443249
[patent_doc_number] => 20180273167
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2018-09-27
[patent_title] => ROTORCRAFT ANTI-TORQUE AND DIRECTIONAL CONTROL USING A CENTRIFUGAL BLOWER
[patent_app_type] => utility
[patent_app_number] => 15/468069
[patent_app_country] => US
[patent_app_date] => 2017-03-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 5153
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -22
[patent_words_short_claim] => 48
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15468069
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/468069 | Rotorcraft anti-torque and directional control using a centrifugal blower | Mar 22, 2017 | Issued |
Array
(
[id] => 13777075
[patent_doc_number] => 20190002076
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2019-01-03
[patent_title] => LOW STALL OR MINIMUM CONTROL SPEED AIRCRAFT
[patent_app_type] => utility
[patent_app_number] => 16/062973
[patent_app_country] => US
[patent_app_date] => 2017-03-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 5678
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -30
[patent_words_short_claim] => 683
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16062973
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/062973 | Low stall or minimum control speed aircraft | Mar 22, 2017 | Issued |
Array
(
[id] => 15542321
[patent_doc_number] => 10570931
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2020-02-25
[patent_title] => Aircraft hydraulic systems having shared components
[patent_app_type] => utility
[patent_app_number] => 15/466655
[patent_app_country] => US
[patent_app_date] => 2017-03-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 6
[patent_no_of_words] => 4875
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 196
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15466655
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/466655 | Aircraft hydraulic systems having shared components | Mar 21, 2017 | Issued |
Array
(
[id] => 15784351
[patent_doc_number] => 10625882
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2020-04-21
[patent_title] => Service satellite for providing in-orbit services using variable thruster control
[patent_app_type] => utility
[patent_app_number] => 15/450601
[patent_app_country] => US
[patent_app_date] => 2017-03-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
[patent_figures_cnt] => 16
[patent_no_of_words] => 18544
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 160
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15450601
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/450601 | Service satellite for providing in-orbit services using variable thruster control | Mar 5, 2017 | Issued |
Array
(
[id] => 14229787
[patent_doc_number] => 20190127066
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2019-05-02
[patent_title] => REMOTE-CONTROLLED UNMANNED FOLDABLE AIRCRAFT
[patent_app_type] => utility
[patent_app_number] => 16/080237
[patent_app_country] => US
[patent_app_date] => 2017-02-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 3762
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -9
[patent_words_short_claim] => 64
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16080237
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/080237 | REMOTE-CONTROLLED UNMANNED FOLDABLE AIRCRAFT | Feb 27, 2017 | Abandoned |
Array
(
[id] => 12211835
[patent_doc_number] => 09908629
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2018-03-06
[patent_title] => 'Inflatable parachute airbag system'
[patent_app_type] => utility
[patent_app_number] => 15/436604
[patent_app_country] => US
[patent_app_date] => 2017-02-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 28
[patent_figures_cnt] => 43
[patent_no_of_words] => 12531
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 147
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15436604
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/436604 | Inflatable parachute airbag system | Feb 16, 2017 | Issued |
Array
(
[id] => 16321021
[patent_doc_number] => 10780977
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2020-09-22
[patent_title] => Aerodynamic control surface movement monitoring system
[patent_app_type] => utility
[patent_app_number] => 15/433021
[patent_app_country] => US
[patent_app_date] => 2017-02-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2444
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 183
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15433021
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/433021 | Aerodynamic control surface movement monitoring system | Feb 14, 2017 | Issued |
Array
(
[id] => 11865822
[patent_doc_number] => 20170233107
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-08-17
[patent_title] => 'AIRCRAFT HIGH-LIFT DEVICE EQUIPPED WITH AT LEAST ONE DIFFERENTIATED COUPLING SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 15/429809
[patent_app_country] => US
[patent_app_date] => 2017-02-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2682
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15429809
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/429809 | Aircraft high-lift device equipped with at least one differentiated coupling system | Feb 9, 2017 | Issued |
Array
(
[id] => 11978886
[patent_doc_number] => 20170283040
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-10-05
[patent_title] => 'FORCE FIGHT MITIGATION'
[patent_app_type] => utility
[patent_app_number] => 15/409808
[patent_app_country] => US
[patent_app_date] => 2017-01-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 3136
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15409808
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/409808 | FORCE FIGHT MITIGATION | Jan 18, 2017 | Abandoned |
Array
(
[id] => 13299637
[patent_doc_number] => 20180201355
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2018-07-19
[patent_title] => Hot Air Balloon Steering System
[patent_app_type] => utility
[patent_app_number] => 15/407861
[patent_app_country] => US
[patent_app_date] => 2017-01-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 2114
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -13
[patent_words_short_claim] => 98
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15407861
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/407861 | Hot air balloon steering system | Jan 16, 2017 | Issued |
Array
(
[id] => 13303867
[patent_doc_number] => 20180203470
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2018-07-19
[patent_title] => AUTONOMOUS SECURITY DRONE SYSTEM AND METHOD
[patent_app_type] => utility
[patent_app_number] => 15/407650
[patent_app_country] => US
[patent_app_date] => 2017-01-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 8692
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -17
[patent_words_short_claim] => 57
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15407650
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/407650 | Autonomous security drone system and method | Jan 16, 2017 | Issued |
Array
(
[id] => 12192476
[patent_doc_number] => 09896195
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2018-02-20
[patent_title] => 'Aerial vehicle and a signal line protection assembly thereof'
[patent_app_type] => utility
[patent_app_number] => 15/388439
[patent_app_country] => US
[patent_app_date] => 2016-12-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 4
[patent_no_of_words] => 2903
[patent_no_of_claims] => 27
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 85
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15388439
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/388439 | Aerial vehicle and a signal line protection assembly thereof | Dec 21, 2016 | Issued |
Array
(
[id] => 16352776
[patent_doc_number] => 10793274
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2020-10-06
[patent_title] => Payload coupling apparatus for UAV and method of delivering a payload
[patent_app_type] => utility
[patent_app_number] => 15/389074
[patent_app_country] => US
[patent_app_date] => 2016-12-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 55
[patent_figures_cnt] => 77
[patent_no_of_words] => 45626
[patent_no_of_claims] => 21
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 74
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15389074
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/389074 | Payload coupling apparatus for UAV and method of delivering a payload | Dec 21, 2016 | Issued |
Array
(
[id] => 15101495
[patent_doc_number] => 10472046
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2019-11-12
[patent_title] => Internal wing control surface linkage system
[patent_app_type] => utility
[patent_app_number] => 15/389048
[patent_app_country] => US
[patent_app_date] => 2016-12-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 18
[patent_figures_cnt] => 23
[patent_no_of_words] => 8650
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 206
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15389048
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/389048 | Internal wing control surface linkage system | Dec 21, 2016 | Issued |