Search

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 numberTitle of the applicationFiling DateStatus
Array ( [id] => 10768755 [patent_doc_number] => 20160114911 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2016-04-28 [patent_title] => 'Multi-Dimensional Damage Detection' [patent_app_type] => utility [patent_app_number] => 14/982369 [patent_app_country] => US [patent_app_date] => 2015-12-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 6767 [patent_no_of_claims] => 9 [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] => 14982369 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/982369
Multi-dimensional damage detection Dec 28, 2015 Issued
Array ( [id] => 11705857 [patent_doc_number] => 20170174356 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2017-06-22 [patent_title] => 'AUXILIARY POWER UNIT INLET DUCT ASSEMBLY FOR MITIGATING NOISE' [patent_app_type] => utility [patent_app_number] => 14/977106 [patent_app_country] => US [patent_app_date] => 2015-12-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 4114 [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] => 14977106 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/977106
Auxiliary power unit inlet duct assembly for mitigating noise Dec 20, 2015 Issued
Array ( [id] => 10979592 [patent_doc_number] => 20160176536 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2016-06-23 [patent_title] => 'FOOLPROOFING SYSTEM FOR PIPES BY MEANS OF AN OBSTACLE INSIDE A CONNECTOR IN AN AIRCRAFT DUCT' [patent_app_type] => utility [patent_app_number] => 14/976407 [patent_app_country] => US [patent_app_date] => 2015-12-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 5324 [patent_no_of_claims] => 10 [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] => 14976407 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/976407
Foolproofing system for pipes by means of an obstacle inside a connector in an aircraft duct Dec 20, 2015 Issued
Array ( [id] => 12037341 [patent_doc_number] => 09815559 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2017-11-14 [patent_title] => 'Aircraft' [patent_app_type] => utility [patent_app_number] => 14/976414 [patent_app_country] => US [patent_app_date] => 2015-12-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 2 [patent_no_of_words] => 3524 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 222 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14976414 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/976414
Aircraft Dec 20, 2015 Issued
Array ( [id] => 12545427 [patent_doc_number] => 10011346 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2018-07-03 [patent_title] => Propeller blade indentations for improved aerodynamic performance and sound control [patent_app_type] => utility [patent_app_number] => 14/975249 [patent_app_country] => US [patent_app_date] => 2015-12-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 29 [patent_figures_cnt] => 40 [patent_no_of_words] => 24590 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 96 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14975249 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/975249
Propeller blade indentations for improved aerodynamic performance and sound control Dec 17, 2015 Issued
Array ( [id] => 13647331 [patent_doc_number] => 09849966 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2017-12-26 [patent_title] => Fuselage structure for accommodating tails and canards of different sizes and shapes [patent_app_type] => utility [patent_app_number] => 14/975115 [patent_app_country] => US [patent_app_date] => 2015-12-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 7024 [patent_no_of_claims] => 23 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 89 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14975115 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/975115
Fuselage structure for accommodating tails and canards of different sizes and shapes Dec 17, 2015 Issued
Array ( [id] => 12112554 [patent_doc_number] => 09868534 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2018-01-16 [patent_title] => 'Heat removal structure of aircraft main landing gear bay' [patent_app_type] => utility [patent_app_number] => 14/973098 [patent_app_country] => US [patent_app_date] => 2015-12-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 9 [patent_no_of_words] => 6762 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 205 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14973098 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/973098
Heat removal structure of aircraft main landing gear bay Dec 16, 2015 Issued
Array ( [id] => 10979576 [patent_doc_number] => 20160176520 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2016-06-23 [patent_title] => 'SELF-ENCLOSED AIR VEHICLE' [patent_app_type] => utility [patent_app_number] => 14/973466 [patent_app_country] => US [patent_app_date] => 2015-12-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 11 [patent_no_of_words] => 3909 [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] => 14973466 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/973466
Self-enclosed air vehicle Dec 16, 2015 Issued
Array ( [id] => 11010683 [patent_doc_number] => 20160207636 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2016-07-21 [patent_title] => 'TRANSPORT MACHINE' [patent_app_type] => utility [patent_app_number] => 14/967829 [patent_app_country] => US [patent_app_date] => 2015-12-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 8414 [patent_no_of_claims] => 14 [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] => 14967829 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/967829
TRANSPORT MACHINE Dec 13, 2015 Abandoned
Array ( [id] => 12086602 [patent_doc_number] => 09840321 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2017-12-12 [patent_title] => 'Aircraft nose provided with a connecting frame between the landing gear housing and the outer skin of the fuselage' [patent_app_type] => utility [patent_app_number] => 14/966478 [patent_app_country] => US [patent_app_date] => 2015-12-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 11 [patent_no_of_words] => 3045 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 3 [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] => 14966478 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/966478
Aircraft nose provided with a connecting frame between the landing gear housing and the outer skin of the fuselage Dec 10, 2015 Issued
Array ( [id] => 11690579 [patent_doc_number] => 20170166294 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2017-06-15 [patent_title] => 'INCOMBUSTIBLE, NON-TELEGRAPHING SUBSTRATES FOR AVIATION PANEL ASSEMBLIES AND METHODS FOR INSTALLING THE INCOMBUSTIBLE, NON-TELEGRAPHING SUBSTRATE INTO AN AVIATION PANEL ASSEMBLY' [patent_app_type] => utility [patent_app_number] => 14/964173 [patent_app_country] => US [patent_app_date] => 2015-12-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 3867 [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] => 14964173 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/964173
Incombustible, non-telegraphing substrates for aviation panel assemblies and methods for installing the incombustible, non-telegraphing substrate into an aviation panel assembly Dec 8, 2015 Issued
Array ( [id] => 11024721 [patent_doc_number] => 20160221676 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2016-08-04 [patent_title] => 'RECONFIGURABLE BATTERY-OPERATED VEHICLE SYSTEM' [patent_app_type] => utility [patent_app_number] => 14/949805 [patent_app_country] => US [patent_app_date] => 2015-11-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 18 [patent_figures_cnt] => 18 [patent_no_of_words] => 7468 [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] => 14949805 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/949805
RECONFIGURABLE BATTERY-OPERATED VEHICLE SYSTEM Nov 22, 2015 Abandoned
Array ( [id] => 11756989 [patent_doc_number] => 20170203857 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2017-07-20 [patent_title] => 'Drone Docking Station and Delivery System' [patent_app_type] => utility [patent_app_number] => 15/328027 [patent_app_country] => US [patent_app_date] => 2015-11-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 7147 [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] => 15328027 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/328027
Drone docking station and delivery system Nov 20, 2015 Issued
Array ( [id] => 11767638 [patent_doc_number] => 09376201 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2016-06-28 [patent_title] => 'Dual boarding system for aircraft' [patent_app_type] => utility [patent_app_number] => 14/943019 [patent_app_country] => US [patent_app_date] => 2015-11-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 15 [patent_no_of_words] => 11071 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 124 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14943019 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/943019
Dual boarding system for aircraft Nov 15, 2015 Issued
Array ( [id] => 10783856 [patent_doc_number] => 20160130012 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2016-05-12 [patent_title] => 'AIRCRAFT WITH A WING TIP COMPRISING A FUEL POD' [patent_app_type] => utility [patent_app_number] => 14/933321 [patent_app_country] => US [patent_app_date] => 2015-11-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 4598 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 6 [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] => 14933321 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/933321
Aircraft with a wing tip comprising a fuel pod Nov 4, 2015 Issued
Array ( [id] => 10693390 [patent_doc_number] => 20160039536 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2016-02-11 [patent_title] => 'SYSTEMS AND DEVICES FOR REMOTELY OPERATED UNMANNED AERIAL VEHICLE REPORT-SUPPRESSING LAUNCHER WITH PORTABLE RF TRANSPARENT LAUNCH TUBE' [patent_app_type] => utility [patent_app_number] => 14/887675 [patent_app_country] => US [patent_app_date] => 2015-10-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 12 [patent_no_of_words] => 4234 [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] => 14887675 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/887675
Systems and devices for remotely operated unmanned aerial vehicle report-suppressing launcher with portable RF transparent launch tube Oct 19, 2015 Issued
Array ( [id] => 15407369 [patent_doc_number] => 20200024006 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2020-01-23 [patent_title] => SYSTEM FOR SPACE PROPULSION AND SPACE LOITERING (ABOVE-STRATOSPHERE AIR LOITERING) [patent_app_type] => utility [patent_app_number] => 15/519448 [patent_app_country] => US [patent_app_date] => 2015-10-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 1150 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -2 [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] => 15519448 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/519448
SYSTEM FOR SPACE PROPULSION AND SPACE LOITERING (ABOVE-STRATOSPHERE AIR LOITERING) Oct 16, 2015 Abandoned
Array ( [id] => 11554433 [patent_doc_number] => 20170100679 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2017-04-13 [patent_title] => 'Radially Extended Spindle Kite' [patent_app_type] => utility [patent_app_number] => 14/881214 [patent_app_country] => US [patent_app_date] => 2015-10-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 3092 [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] => 14881214 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/881214
Radially Extended Spindle Kite Oct 12, 2015 Abandoned
Array ( [id] => 11554922 [patent_doc_number] => 20170101168 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2017-04-13 [patent_title] => 'COMPOSITE STIFFENER WITH INTEGRAL CONDUCTIVE ELEMENT' [patent_app_type] => utility [patent_app_number] => 14/881530 [patent_app_country] => US [patent_app_date] => 2015-10-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 3604 [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] => 14881530 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/881530
Composite stiffener with integral conductive element Oct 12, 2015 Issued
Array ( [id] => 11915129 [patent_doc_number] => 09783306 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2017-10-10 [patent_title] => 'Bi-fold thrust recovery outflow valve with a ram air flap' [patent_app_type] => utility [patent_app_number] => 14/881788 [patent_app_country] => US [patent_app_date] => 2015-10-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 11 [patent_no_of_words] => 4985 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 222 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14881788 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/881788
Bi-fold thrust recovery outflow valve with a ram air flap Oct 12, 2015 Issued
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