
Robert C. Watson
Examiner (ID: 18496)
| Most Active Art Unit | 3203 |
| Art Unit(s) | 3723, 3727, 3104, 2103, 3203, 2901, 2899 |
| Total Applications | 4229 |
| Issued Applications | 3664 |
| Pending Applications | 83 |
| Abandoned Applications | 482 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 12468690
[patent_doc_number] => 09988144
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2018-06-05
[patent_title] => Steering device for an aircraft
[patent_app_type] => utility
[patent_app_number] => 15/074810
[patent_app_country] => US
[patent_app_date] => 2016-03-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 15
[patent_no_of_words] => 5714
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 127
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15074810
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/074810 | Steering device for an aircraft | Mar 17, 2016 | Issued |
Array
(
[id] => 11075333
[patent_doc_number] => 20160272297
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-09-22
[patent_title] => 'LOAD TRANSFER APPARATUS FOR TRANSFERRING LOADS IN AN AIRCRAFT STRUCTURE'
[patent_app_type] => utility
[patent_app_number] => 15/072399
[patent_app_country] => US
[patent_app_date] => 2016-03-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 4282
[patent_no_of_claims] => 13
[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] => 15072399
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/072399 | Load transfer apparatus for transferring loads in an aircraft structure | Mar 16, 2016 | Issued |
Array
(
[id] => 12106013
[patent_doc_number] => 09862483
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2018-01-09
[patent_title] => 'Aircraft landing gear assembly'
[patent_app_type] => utility
[patent_app_number] => 15/072953
[patent_app_country] => US
[patent_app_date] => 2016-03-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 11
[patent_no_of_words] => 3920
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 234
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15072953
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/072953 | Aircraft landing gear assembly | Mar 16, 2016 | Issued |
Array
(
[id] => 11075339
[patent_doc_number] => 20160272303
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-09-22
[patent_title] => 'AIRCRAFT LANDING GEAR ASSEMBLY'
[patent_app_type] => utility
[patent_app_number] => 15/072974
[patent_app_country] => US
[patent_app_date] => 2016-03-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 3818
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 4
[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] => 15072974
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/072974 | Aircraft landing gear assembly | Mar 16, 2016 | Issued |
Array
(
[id] => 11075334
[patent_doc_number] => 20160272298
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-09-22
[patent_title] => 'CONNECTOR BETWEEN TWO AIRCRAFT COMPONENTS, SUCH AS A WING AND WING TIP DEVICE'
[patent_app_type] => utility
[patent_app_number] => 15/072401
[patent_app_country] => US
[patent_app_date] => 2016-03-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 4860
[patent_no_of_claims] => 23
[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] => 15072401
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/072401 | Connector between two aircraft components, such as a wing and wing tip device | Mar 16, 2016 | Issued |
Array
(
[id] => 11114581
[patent_doc_number] => 20160311553
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-10-27
[patent_title] => 'TAIL SITTER VEHICLE WITH AERIAL AND GROUND REFUELING SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 15/070599
[patent_app_country] => US
[patent_app_date] => 2016-03-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 3418
[patent_no_of_claims] => 15
[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] => 15070599
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/070599 | Tail sitter vehicle with aerial and ground refueling system | Mar 14, 2016 | Issued |
Array
(
[id] => 11955758
[patent_doc_number] => 20170259909
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-09-14
[patent_title] => 'AIRCRAFT WING STRUCTURE AND ASSOCIATED METHOD FOR ADDRESSING LIFT AND DRAG'
[patent_app_type] => utility
[patent_app_number] => 15/069117
[patent_app_country] => US
[patent_app_date] => 2016-03-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 26
[patent_figures_cnt] => 26
[patent_no_of_words] => 10882
[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] => 15069117
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/069117 | Aircraft wing structure and associated method for addressing lift and drag | Mar 13, 2016 | Issued |
Array
(
[id] => 12407658
[patent_doc_number] => 09969484
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2018-05-15
[patent_title] => Adjustable height cyclic control assembly and method
[patent_app_type] => utility
[patent_app_number] => 15/056337
[patent_app_country] => US
[patent_app_date] => 2016-02-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 3
[patent_no_of_words] => 2054
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 462
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15056337
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/056337 | Adjustable height cyclic control assembly and method | Feb 28, 2016 | Issued |
Array
(
[id] => 12386940
[patent_doc_number] => 09963216
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2018-05-08
[patent_title] => Filling apparatus for high-altitude balloons
[patent_app_type] => utility
[patent_app_number] => 15/054598
[patent_app_country] => US
[patent_app_date] => 2016-02-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 15
[patent_no_of_words] => 6051
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 1
[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] => 15054598
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/054598 | Filling apparatus for high-altitude balloons | Feb 25, 2016 | Issued |
Array
(
[id] => 12386970
[patent_doc_number] => 09963226
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2018-05-08
[patent_title] => Tail assembly for a rotorcraft, rotorcraft and method of manufacture of a strengthened tail assembly
[patent_app_type] => utility
[patent_app_number] => 15/054485
[patent_app_country] => US
[patent_app_date] => 2016-02-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 9
[patent_no_of_words] => 5437
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 286
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15054485
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/054485 | Tail assembly for a rotorcraft, rotorcraft and method of manufacture of a strengthened tail assembly | Feb 25, 2016 | Issued |
Array
(
[id] => 13036921
[patent_doc_number] => 10040578
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2018-08-07
[patent_title] => Battery arm sensor assembly
[patent_app_type] => utility
[patent_app_number] => 15/054368
[patent_app_country] => US
[patent_app_date] => 2016-02-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 15
[patent_figures_cnt] => 15
[patent_no_of_words] => 20472
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 154
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15054368
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/054368 | Battery arm sensor assembly | Feb 25, 2016 | Issued |
Array
(
[id] => 11054131
[patent_doc_number] => 20160251093
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-09-01
[patent_title] => 'TRUSS STRUCTURE'
[patent_app_type] => utility
[patent_app_number] => 15/053998
[patent_app_country] => US
[patent_app_date] => 2016-02-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 15
[patent_figures_cnt] => 15
[patent_no_of_words] => 8632
[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] => 15053998
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/053998 | Truss structure | Feb 24, 2016 | Issued |
Array
(
[id] => 14004999
[patent_doc_number] => 10220934
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2019-03-05
[patent_title] => Fire-resistant aviation laminate
[patent_app_type] => utility
[patent_app_number] => 15/052515
[patent_app_country] => US
[patent_app_date] => 2016-02-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 1422
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 31
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15052515
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/052515 | Fire-resistant aviation laminate | Feb 23, 2016 | Issued |
Array
(
[id] => 12325206
[patent_doc_number] => 09944383
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2018-04-17
[patent_title] => Pneumatic yaw control effector for aircraft
[patent_app_type] => utility
[patent_app_number] => 15/052558
[patent_app_country] => US
[patent_app_date] => 2016-02-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 14
[patent_figures_cnt] => 25
[patent_no_of_words] => 8858
[patent_no_of_claims] => 22
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 105
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15052558
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/052558 | Pneumatic yaw control effector for aircraft | Feb 23, 2016 | Issued |
Array
(
[id] => 11936123
[patent_doc_number] => 20170240273
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-08-24
[patent_title] => 'FIXED-WING VTOL AIRCRAFT WITH ROTORS ON OUTRIGGERS'
[patent_app_type] => utility
[patent_app_number] => 15/052773
[patent_app_country] => US
[patent_app_date] => 2016-02-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
[patent_figures_cnt] => 13
[patent_no_of_words] => 4779
[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] => 15052773
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/052773 | FIXED-WING VTOL AIRCRAFT WITH ROTORS ON OUTRIGGERS | Feb 23, 2016 | Abandoned |
Array
(
[id] => 11047204
[patent_doc_number] => 20160244162
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-08-25
[patent_title] => 'ENCLOSED UNMANNED AERIAL VEHICLE'
[patent_app_type] => utility
[patent_app_number] => 15/050619
[patent_app_country] => US
[patent_app_date] => 2016-02-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 4598
[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] => 15050619
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/050619 | Enclosed unmanned aerial vehicle | Feb 22, 2016 | Issued |
Array
(
[id] => 10821595
[patent_doc_number] => 20160167760
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-06-16
[patent_title] => 'ADDITIONAL SYSTEMS AND METHODS FOR LONG ENDURANCE AIRSHIP OPERATIONS USING A FREE-FLYING TETHERED AIRSHIP SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 15/050291
[patent_app_country] => US
[patent_app_date] => 2016-02-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 12
[patent_no_of_words] => 10013
[patent_no_of_claims] => 12
[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] => 15050291
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/050291 | Additional systems and methods for long endurance airship operations using a free-flying tethered airship system | Feb 21, 2016 | Issued |
Array
(
[id] => 11382569
[patent_doc_number] => 20170008626
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-01-12
[patent_title] => 'SPOOLER FOR UNMANNED AERIAL VEHICLE SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 15/041211
[patent_app_country] => US
[patent_app_date] => 2016-02-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 12
[patent_no_of_words] => 5642
[patent_no_of_claims] => 20
[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] => 15041211
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/041211 | Spooler for unmanned aerial vehicle system | Feb 10, 2016 | Issued |
Array
(
[id] => 11054125
[patent_doc_number] => 20160251087
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-09-01
[patent_title] => 'UAV PAYLOAD MODULE CAMERA ASSEMBLY AND RETRACTION MECHANISM'
[patent_app_type] => utility
[patent_app_number] => 15/007206
[patent_app_country] => US
[patent_app_date] => 2016-01-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 3967
[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] => 15007206
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/007206 | UAV payload module camera assembly and retraction mechanism | Jan 25, 2016 | Issued |
Array
(
[id] => 12489090
[patent_doc_number] => 09994306
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2018-06-12
[patent_title] => Aircraft landing gear assembly stop member
[patent_app_type] => utility
[patent_app_number] => 14/993437
[patent_app_country] => US
[patent_app_date] => 2016-01-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 12
[patent_no_of_words] => 2420
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 216
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14993437
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/993437 | Aircraft landing gear assembly stop member | Jan 11, 2016 | Issued |