
Keith L. Dixon
Examiner (ID: 14316, Phone: (571)270-3319 , Office: P/3644 )
| Most Active Art Unit | 3644 |
| Art Unit(s) | 3644 |
| Total Applications | 522 |
| Issued Applications | 427 |
| Pending Applications | 1 |
| Abandoned Applications | 98 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 8356442
[patent_doc_number] => 20120211603
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-08-23
[patent_title] => 'WING PANEL AND AIRCRAFT MAIN WING'
[patent_app_type] => utility
[patent_app_number] => 13/399393
[patent_app_country] => US
[patent_app_date] => 2012-02-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 2269
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13399393
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/399393 | WING PANEL AND AIRCRAFT MAIN WING | Feb 16, 2012 | Abandoned |
Array
(
[id] => 8973484
[patent_doc_number] => 20130206914
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-08-15
[patent_title] => 'Sensor Pod Mount for an Aircraft'
[patent_app_type] => utility
[patent_app_number] => 13/372230
[patent_app_country] => US
[patent_app_date] => 2012-02-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/372230 | Sensor pod mount for an aircraft | Feb 12, 2012 | Issued |
Array
(
[id] => 8960613
[patent_doc_number] => 20130200215
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-08-08
[patent_title] => 'Structural Joint Having Continuous Skin With Inside And Outside Stringers'
[patent_app_type] => utility
[patent_app_number] => 13/367782
[patent_app_country] => US
[patent_app_date] => 2012-02-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13367782
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/367782 | Structural joint having continuous skin with inside and outside stringers | Feb 6, 2012 | Issued |
Array
(
[id] => 9237562
[patent_doc_number] => 08602347
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-12-10
[patent_title] => 'Tilt rotor aircraft with fixed engine arrangement'
[patent_app_type] => utility
[patent_app_number] => 13/357981
[patent_app_country] => US
[patent_app_date] => 2012-01-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
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[patent_no_of_words] => 2809
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/357981 | Tilt rotor aircraft with fixed engine arrangement | Jan 24, 2012 | Issued |
Array
(
[id] => 8937210
[patent_doc_number] => 20130187007
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-07-25
[patent_title] => 'BLEED AIR SYSTEMS FOR USE WITH AIRCRAFTS AND RELATED METHODS'
[patent_app_type] => utility
[patent_app_number] => 13/357293
[patent_app_country] => US
[patent_app_date] => 2012-01-24
[patent_effective_date] => 0000-00-00
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/357293 | Bleed air systems for use with aircrafts and related methods | Jan 23, 2012 | Issued |
Array
(
[id] => 8321064
[patent_doc_number] => 20120193475
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-08-02
[patent_title] => 'CONNECTOR FOR STIFFENING FRAMES BETWEEN AN AIRCRAFT FUSELAGE AND A WING BOX'
[patent_app_type] => utility
[patent_app_number] => 13/348110
[patent_app_country] => US
[patent_app_date] => 2012-01-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13348110
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/348110 | Connector for stiffening frames between an aircraft fuselage and a wing box | Jan 10, 2012 | Issued |
Array
(
[id] => 8913759
[patent_doc_number] => 20130175384
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-07-11
[patent_title] => 'Bearing Restraint for Rotor Systems'
[patent_app_type] => utility
[patent_app_number] => 13/346912
[patent_app_country] => US
[patent_app_date] => 2012-01-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_no_of_words] => 2804
[patent_no_of_claims] => 20
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13346912
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/346912 | Bearing restraint for rotor systems | Jan 9, 2012 | Issued |
Array
(
[id] => 8298810
[patent_doc_number] => 20120181377
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-07-19
[patent_title] => 'VIBRATION CONTROL SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 13/347249
[patent_app_country] => US
[patent_app_date] => 2012-01-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[patent_no_of_words] => 2461
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13347249
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/347249 | Vibration control system | Jan 9, 2012 | Issued |
Array
(
[id] => 13920137
[patent_doc_number] => 10204192
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2019-02-12
[patent_title] => System and method for drag reduction
[patent_app_type] => utility
[patent_app_number] => 13/344673
[patent_app_country] => US
[patent_app_date] => 2012-01-06
[patent_effective_date] => 0000-00-00
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/344673 | System and method for drag reduction | Jan 5, 2012 | Issued |
Array
(
[id] => 8274239
[patent_doc_number] => 20120168115
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-07-05
[patent_title] => 'INTEGRATION OF A SURFACE HEAT-EXCHANGER WITH REGULATED AIR FLOW IN AN AIRPLANE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 13/334422
[patent_app_country] => US
[patent_app_date] => 2011-12-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[patent_no_of_words] => 3737
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13334422
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/334422 | INTEGRATION OF A SURFACE HEAT-EXCHANGER WITH REGULATED AIR FLOW IN AN AIRPLANE ENGINE | Dec 21, 2011 | Abandoned |
Array
(
[id] => 9018874
[patent_doc_number] => 08528855
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-09-10
[patent_title] => 'Magnus and transverse flow hybrid rotor'
[patent_app_type] => utility
[patent_app_number] => 13/332460
[patent_app_country] => US
[patent_app_date] => 2011-12-21
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13332460
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/332460 | Magnus and transverse flow hybrid rotor | Dec 20, 2011 | Issued |
Array
(
[id] => 11778856
[patent_doc_number] => 09387940
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-07-12
[patent_title] => 'Intelligent self-leveling docking system'
[patent_app_type] => utility
[patent_app_number] => 13/991063
[patent_app_country] => US
[patent_app_date] => 2011-11-09
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/991063 | Intelligent self-leveling docking system | Nov 8, 2011 | Issued |
Array
(
[id] => 8165644
[patent_doc_number] => 20120104182
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-05-03
[patent_title] => 'PNEUMATIC CONTROL SYSTEM FOR AERODYNAMIC SURFACES'
[patent_app_type] => utility
[patent_app_number] => 13/267614
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[pdf_file] => publications/A1/0104/20120104182.pdf
[firstpage_image] =>[orig_patent_app_number] => 13267614
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/267614 | Pneumatic control system for aerodynamic surfaces | Oct 5, 2011 | Issued |
Array
(
[id] => 8089903
[patent_doc_number] => 20120080555
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-04-05
[patent_title] => 'TAKE-UP DEVICE FOR THRUST FORCES WITH CONNECTING RODS FOR AIRCRAFT ENGINE ATTACHMENT PYLON, INTEGRATING THREE ALIGNED BALL JOINTS'
[patent_app_type] => utility
[patent_app_number] => 13/239939
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[pdf_file] => publications/A1/0080/20120080555.pdf
[firstpage_image] =>[orig_patent_app_number] => 13239939
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/239939 | Take-up device for thrust forces with connecting rods for aircraft engine attachment pylon, integrating three aligned ball joints | Sep 21, 2011 | Issued |
Array
(
[id] => 8049055
[patent_doc_number] => 20120074258
[patent_country] => US
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[patent_title] => 'INTEGRATED AIRCRAFT INTERIOR'
[patent_app_type] => utility
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[firstpage_image] =>[orig_patent_app_number] => 13239294
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/239294 | INTEGRATED AIRCRAFT INTERIOR | Sep 20, 2011 | Abandoned |
Array
(
[id] => 8402919
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[patent_kind] => A1
[patent_issue_date] => 2012-09-20
[patent_title] => 'Decompression Device and Decompression System'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/230903 | Decompression device and decompression system | Sep 12, 2011 | Issued |
Array
(
[id] => 8036553
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[patent_issue_date] => 2012-03-22
[patent_title] => 'ROTARY WING AIRCRAFT PROVIDED WITH PROPULSION MEANS, AND A METHOD APPLIED BY SAID AIRCRAFT'
[patent_app_type] => utility
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/230965 | Rotary wing aircraft provided with propulsion means, and a method applied by said aircraft | Sep 12, 2011 | Issued |
Array
(
[id] => 7814898
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[patent_title] => 'APPARATUS AND METHOD FOR QUICKLY RELEASING A DOME IN A DOMED SATELLITE ANTENNA'
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Array
(
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Array
(
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[firstpage_image] =>[orig_patent_app_number] => 13223704
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/223704 | THERMOPLASTIC HOSES FOR AIRBORNE VEHICLES | Aug 31, 2011 | Abandoned |