
Ingrid D. Wright
Examiner (ID: 10815, Phone: (571)272-8392 , Office: P/2835 )
| Most Active Art Unit | 2835 |
| Art Unit(s) | 2846, 2835 |
| Total Applications | 928 |
| Issued Applications | 636 |
| Pending Applications | 2 |
| Abandoned Applications | 290 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 17490174
[patent_doc_number] => 11279461
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2022-03-22
[patent_title] => Flight deck barrier door, aircraft comprising flight deck barrier door, and method of using flight deck barrier door
[patent_app_type] => utility
[patent_app_number] => 15/611155
[patent_app_country] => US
[patent_app_date] => 2017-06-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
[patent_figures_cnt] => 16
[patent_no_of_words] => 5576
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 104
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15611155
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/611155 | Flight deck barrier door, aircraft comprising flight deck barrier door, and method of using flight deck barrier door | May 31, 2017 | Issued |
Array
(
[id] => 13078783
[patent_doc_number] => 10059448
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2018-08-28
[patent_title] => Rescue device for distressed swimmer
[patent_app_type] => utility
[patent_app_number] => 15/603853
[patent_app_country] => US
[patent_app_date] => 2017-05-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 1477
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 75
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15603853
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/603853 | Rescue device for distressed swimmer | May 23, 2017 | Issued |
Array
(
[id] => 15085671
[patent_doc_number] => 20190337646
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2019-11-07
[patent_title] => SPACECRAFT
[patent_app_type] => utility
[patent_app_number] => 16/303376
[patent_app_country] => US
[patent_app_date] => 2017-05-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 6524
[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] => 16303376
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/303376 | SPACECRAFT | May 22, 2017 | Abandoned |
Array
(
[id] => 16230250
[patent_doc_number] => 10737786
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2020-08-11
[patent_title] => Distributed propulsion system for vertical take off and landing closed wing aircraft
[patent_app_type] => utility
[patent_app_number] => 15/593575
[patent_app_country] => US
[patent_app_date] => 2017-05-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 29
[patent_figures_cnt] => 32
[patent_no_of_words] => 7787
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 246
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15593575
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/593575 | Distributed propulsion system for vertical take off and landing closed wing aircraft | May 11, 2017 | Issued |
Array
(
[id] => 16027557
[patent_doc_number] => 10676183
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2020-06-09
[patent_title] => Forward folding rotor blades
[patent_app_type] => utility
[patent_app_number] => 15/593521
[patent_app_country] => US
[patent_app_date] => 2017-05-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 17
[patent_figures_cnt] => 18
[patent_no_of_words] => 4387
[patent_no_of_claims] => 24
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 135
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15593521
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/593521 | Forward folding rotor blades | May 11, 2017 | Issued |
Array
(
[id] => 16214826
[patent_doc_number] => 10730624
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2020-08-04
[patent_title] => Modular fuselage sections for vertical take off and landing distributed airframe aircraft
[patent_app_type] => utility
[patent_app_number] => 15/593607
[patent_app_country] => US
[patent_app_date] => 2017-05-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 14
[patent_figures_cnt] => 17
[patent_no_of_words] => 4376
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 229
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15593607
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/593607 | Modular fuselage sections for vertical take off and landing distributed airframe aircraft | May 11, 2017 | Issued |
Array
(
[id] => 15482695
[patent_doc_number] => 10556680
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2020-02-11
[patent_title] => Distributed propulsion system
[patent_app_type] => utility
[patent_app_number] => 15/593458
[patent_app_country] => US
[patent_app_date] => 2017-05-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 29
[patent_figures_cnt] => 29
[patent_no_of_words] => 6794
[patent_no_of_claims] => 28
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 197
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15593458
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/593458 | Distributed propulsion system | May 11, 2017 | Issued |
Array
(
[id] => 16735345
[patent_doc_number] => 10960978
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2021-03-30
[patent_title] => Vertical take off and landing closed wing aircraft
[patent_app_type] => utility
[patent_app_number] => 15/593554
[patent_app_country] => US
[patent_app_date] => 2017-05-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 36
[patent_figures_cnt] => 40
[patent_no_of_words] => 6696
[patent_no_of_claims] => 37
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 164
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15593554
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/593554 | Vertical take off and landing closed wing aircraft | May 11, 2017 | Issued |
Array
(
[id] => 16071451
[patent_doc_number] => 20200189712
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2020-06-18
[patent_title] => UNMANNED AERIAL VEHICLE AND PROTECTIVE OUTER CAGE THEREFOR
[patent_app_type] => utility
[patent_app_number] => 16/097745
[patent_app_country] => US
[patent_app_date] => 2017-05-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 10491
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -35
[patent_words_short_claim] => 104
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16097745
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/097745 | Unmanned aerial vehicle and protective outer cage therefor | Apr 30, 2017 | Issued |
Array
(
[id] => 15882241
[patent_doc_number] => 10647451
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2020-05-12
[patent_title] => Vented launch vehicle adaptor for a manned spacecraft with pusher launch abort system
[patent_app_type] => utility
[patent_app_number] => 15/581979
[patent_app_country] => US
[patent_app_date] => 2017-04-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 3116
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 112
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15581979
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/581979 | Vented launch vehicle adaptor for a manned spacecraft with pusher launch abort system | Apr 27, 2017 | Issued |
Array
(
[id] => 13506421
[patent_doc_number] => 20180304753
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2018-10-25
[patent_title] => Propulsion System for an Aircraft
[patent_app_type] => utility
[patent_app_number] => 15/493544
[patent_app_country] => US
[patent_app_date] => 2017-04-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 9137
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -18
[patent_words_short_claim] => 73
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15493544
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/493544 | Propulsion system for an aircraft | Apr 20, 2017 | Issued |
Array
(
[id] => 14184687
[patent_doc_number] => 20190112048
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2019-04-18
[patent_title] => SYSTEMS AND METHODS FOR UNMANNED AERIAL VEHICLES
[patent_app_type] => utility
[patent_app_number] => 16/090176
[patent_app_country] => US
[patent_app_date] => 2017-03-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 11383
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -17
[patent_words_short_claim] => 16
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16090176
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/090176 | SYSTEMS AND METHODS FOR UNMANNED AERIAL VEHICLES | Mar 28, 2017 | Abandoned |
Array
(
[id] => 11936121
[patent_doc_number] => 20170240270
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-08-24
[patent_title] => 'AERODYNAMIC LIFT ENHANCING SYSTEM FOR A FLYING AUTOMOTIVE VEHICLE'
[patent_app_type] => utility
[patent_app_number] => 15/449951
[patent_app_country] => US
[patent_app_date] => 2017-03-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 3761
[patent_no_of_claims] => 21
[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] => 15449951
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/449951 | Aerodynamic lift enhancing system for a flying automotive vehicle | Mar 3, 2017 | Issued |
Array
(
[id] => 15665871
[patent_doc_number] => 10597151
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2020-03-24
[patent_title] => Failure tolerant rotor blade pitch angle controlling device
[patent_app_type] => utility
[patent_app_number] => 15/445939
[patent_app_country] => US
[patent_app_date] => 2017-02-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2035
[patent_no_of_claims] => 1
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 383
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15445939
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/445939 | Failure tolerant rotor blade pitch angle controlling device | Feb 27, 2017 | Issued |
Array
(
[id] => 11963214
[patent_doc_number] => 20170267368
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-09-21
[patent_title] => 'FUEL PIPE OF AIRCRAFT AND AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 15/438928
[patent_app_country] => US
[patent_app_date] => 2017-02-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 5389
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 3
[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] => 15438928
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/438928 | Fuel pipe of aircraft and aircraft | Feb 21, 2017 | Issued |
Array
(
[id] => 11835852
[patent_doc_number] => 20170217571
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-08-03
[patent_title] => 'UAV WITH TRANSFORMABLE ARMS'
[patent_app_type] => utility
[patent_app_number] => 15/439854
[patent_app_country] => US
[patent_app_date] => 2017-02-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
[patent_figures_cnt] => 13
[patent_no_of_words] => 28398
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[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] => 15439854
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/439854 | UAV with transformable arms | Feb 21, 2017 | Issued |
Array
(
[id] => 16352783
[patent_doc_number] => 10793281
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2020-10-06
[patent_title] => Propulsion system for an aircraft
[patent_app_type] => utility
[patent_app_number] => 15/429979
[patent_app_country] => US
[patent_app_date] => 2017-02-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 7286
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 128
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15429979
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/429979 | Propulsion system for an aircraft | Feb 9, 2017 | Issued |
Array
(
[id] => 12044315
[patent_doc_number] => 09821906
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2017-11-21
[patent_title] => 'Elongated nose structure to provide stability during boarding'
[patent_app_type] => utility
[patent_app_number] => 15/428038
[patent_app_country] => US
[patent_app_date] => 2017-02-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2293
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 2
[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] => 15428038
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/428038 | Elongated nose structure to provide stability during boarding | Feb 7, 2017 | Issued |
Array
(
[id] => 13342063
[patent_doc_number] => 20180222571
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2018-08-09
[patent_title] => Aerodynamic Control Surface and Associated Trailing Edge Close-out Method
[patent_app_type] => utility
[patent_app_number] => 15/427817
[patent_app_country] => US
[patent_app_date] => 2017-02-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 3495
[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] => 15427817
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/427817 | Aerodynamic control surface and associated trailing edge close-out method | Feb 7, 2017 | Issued |
Array
(
[id] => 17938096
[patent_doc_number] => 11472536
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2022-10-18
[patent_title] => System to control flow separation over an airfoil
[patent_app_type] => utility
[patent_app_number] => 15/425943
[patent_app_country] => US
[patent_app_date] => 2017-02-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 12
[patent_no_of_words] => 2053
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 295
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15425943
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/425943 | System to control flow separation over an airfoil | Feb 5, 2017 | Issued |