
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] => 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
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[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
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[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
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[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
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[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
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[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
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[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
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[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
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[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
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[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
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[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
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[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
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[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'
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[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'
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[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
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[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
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[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
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[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
(
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[patent_title] => 'Radially Extended Spindle Kite'
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Array
(
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/881530 | Composite stiffener with integral conductive element | Oct 12, 2015 | Issued |
Array
(
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[patent_title] => 'Bi-fold thrust recovery outflow valve with a ram air flap'
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[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 |