Search

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 numberTitle of the applicationFiling DateStatus
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 [patent_no_of_claims] => 7 [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] => 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 [patent_figures_cnt] => 5 [patent_no_of_words] => 6236 [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] => 13372230 [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 [patent_figures_cnt] => 6 [patent_no_of_words] => 4874 [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] => 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 [patent_figures_cnt] => 10 [patent_no_of_words] => 2809 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 118 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13357981 [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 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 11 [patent_no_of_words] => 10183 [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] => 13357293 [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 [patent_figures_cnt] => 5 [patent_no_of_words] => 1969 [patent_no_of_claims] => 10 [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] => 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 [patent_figures_cnt] => 5 [patent_no_of_words] => 2804 [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] => 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 [patent_figures_cnt] => 7 [patent_no_of_words] => 2461 [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] => 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 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 17 [patent_no_of_words] => 4867 [patent_no_of_claims] => 7 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 119 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13344673 [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 [patent_figures_cnt] => 3 [patent_no_of_words] => 3737 [patent_no_of_claims] => 15 [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] => 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 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 11 [patent_no_of_words] => 6917 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 176 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 5640 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 3 [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] => 13991063 [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 [patent_app_country] => US [patent_app_date] => 2011-10-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 6266 [patent_no_of_claims] => 21 [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] => 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 [patent_app_country] => US [patent_app_date] => 2011-09-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 7737 [patent_no_of_claims] => 7 [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] => 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 [patent_kind] => A1 [patent_issue_date] => 2012-03-29 [patent_title] => 'INTEGRATED AIRCRAFT INTERIOR' [patent_app_type] => utility [patent_app_number] => 13/239294 [patent_app_country] => US [patent_app_date] => 2011-09-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 14 [patent_figures_cnt] => 14 [patent_no_of_words] => 2354 [patent_no_of_claims] => 19 [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] => publications/A1/0074/20120074258.pdf [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 [patent_doc_number] => 20120234973 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-09-20 [patent_title] => 'Decompression Device and Decompression System' [patent_app_type] => utility [patent_app_number] => 13/230903 [patent_app_country] => US [patent_app_date] => 2011-09-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 6127 [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] => 13230903 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/230903
Decompression device and decompression system Sep 12, 2011 Issued
Array ( [id] => 8036553 [patent_doc_number] => 20120068007 [patent_country] => US [patent_kind] => A1 [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 [patent_app_number] => 13/230965 [patent_app_country] => US [patent_app_date] => 2011-09-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 6114 [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] => publications/A1/0068/20120068007.pdf [firstpage_image] =>[orig_patent_app_number] => 13230965 [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 [patent_doc_number] => 20120061518 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-03-15 [patent_title] => 'APPARATUS AND METHOD FOR QUICKLY RELEASING A DOME IN A DOMED SATELLITE ANTENNA' [patent_app_type] => utility [patent_app_number] => 13/227876 [patent_app_country] => US [patent_app_date] => 2011-09-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 3338 [patent_no_of_claims] => 13 [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] => publications/A1/0061/20120061518.pdf [firstpage_image] =>[orig_patent_app_number] => 13227876 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/227876
APPARATUS AND METHOD FOR QUICKLY RELEASING A DOME IN A DOMED SATELLITE ANTENNA Sep 7, 2011 Abandoned
Array ( [id] => 8192401 [patent_doc_number] => 20120119032 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-05-17 [patent_title] => 'SECOND HOSE WALL' [patent_app_type] => utility [patent_app_number] => 13/226670 [patent_app_country] => US [patent_app_date] => 2011-09-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 3117 [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] => publications/A1/0119/20120119032.pdf [firstpage_image] =>[orig_patent_app_number] => 13226670 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/226670
SECOND HOSE WALL Sep 6, 2011 Abandoned
Array ( [id] => 8035431 [patent_doc_number] => 20120067452 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-03-22 [patent_title] => 'THERMOPLASTIC HOSES FOR AIRBORNE VEHICLES' [patent_app_type] => utility [patent_app_number] => 13/223704 [patent_app_country] => US [patent_app_date] => 2011-09-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 3100 [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] => publications/A1/0067/20120067452.pdf [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
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