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] => 8036567 [patent_doc_number] => 20120068021 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-03-22 [patent_title] => 'CRAFT AND METHOD FOR ASSEMBLING CRAFT WITH CONTROLLED SPIN' [patent_app_type] => utility [patent_app_number] => 12/792494 [patent_app_country] => US [patent_app_date] => 2010-06-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 2920 [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/A1/0068/20120068021.pdf [firstpage_image] =>[orig_patent_app_number] => 12792494 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/792494
Craft and method for assembling craft with controlled spin Jun 1, 2010 Issued
Array ( [id] => 10614632 [patent_doc_number] => 09334062 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2016-05-10 [patent_title] => 'Assisted in-flight refuelling system' [patent_app_type] => utility [patent_app_number] => 12/792440 [patent_app_country] => US [patent_app_date] => 2010-06-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 10 [patent_no_of_words] => 6408 [patent_no_of_claims] => 21 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 398 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12792440 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/792440
Assisted in-flight refuelling system Jun 1, 2010 Issued
Array ( [id] => 8248745 [patent_doc_number] => 20120153077 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-06-21 [patent_title] => 'LANDING SYSTEM FOR A BODY AND SPACE PROBE PROVIDED WITH SUCH A SYSTEM' [patent_app_type] => utility [patent_app_number] => 13/376231 [patent_app_country] => US [patent_app_date] => 2010-05-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 2530 [patent_no_of_claims] => 16 [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/A1/0153/20120153077.pdf [firstpage_image] =>[orig_patent_app_number] => 13376231 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/376231
Landing system for a body and space probe provided with such a system May 27, 2010 Issued
Array ( [id] => 8224549 [patent_doc_number] => 20120138751 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-06-07 [patent_title] => 'AIRCRAFT HAVING A VERTICAL LIFT SYSTEM' [patent_app_type] => utility [patent_app_number] => 13/322486 [patent_app_country] => US [patent_app_date] => 2010-05-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 9231 [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] => 13322486 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/322486
Aircraft having a vertical lift system May 25, 2010 Issued
Array ( [id] => 6374336 [patent_doc_number] => 20100301174 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-12-02 [patent_title] => 'SYSTEM FOR CONTROLLING AT LEAST ONE AIRCRAFT ENGINE AND AN AIRCRAFT COMPRISING SUCH A CONTROL SYSTEM' [patent_app_type] => utility [patent_app_number] => 12/787272 [patent_app_country] => US [patent_app_date] => 2010-05-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 3051 [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/A1/0301/20100301174.pdf [firstpage_image] =>[orig_patent_app_number] => 12787272 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/787272
SYSTEM FOR CONTROLLING AT LEAST ONE AIRCRAFT ENGINE AND AN AIRCRAFT COMPRISING SUCH A CONTROL SYSTEM May 24, 2010 Abandoned
Array ( [id] => 10594199 [patent_doc_number] => 09315273 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2016-04-19 [patent_title] => 'Apparatus for supporting a parachute flight controller and flight controller for a parachute' [patent_app_type] => utility [patent_app_number] => 13/320672 [patent_app_country] => US [patent_app_date] => 2010-05-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 41 [patent_figures_cnt] => 64 [patent_no_of_words] => 16626 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 149 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13320672 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/320672
Apparatus for supporting a parachute flight controller and flight controller for a parachute May 16, 2010 Issued
Array ( [id] => 6183747 [patent_doc_number] => 20110168838 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-07-14 [patent_title] => 'Launch tube deployable surveillance and reconnaissance system' [patent_app_type] => utility [patent_app_number] => 12/799297 [patent_app_country] => US [patent_app_date] => 2010-04-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 2318 [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/A1/0168/20110168838.pdf [firstpage_image] =>[orig_patent_app_number] => 12799297 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/799297
Launch tube deployable surveillance and reconnaissance system Apr 20, 2010 Abandoned
Array ( [id] => 6136797 [patent_doc_number] => 20110127374 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-06-02 [patent_title] => 'METHODS AND SYSTEMS FOR MINIMIZING FLOW DISTURBANCES IN AIRCRAFT PROPELLER BLADES CAUSED BY UPSTREAM PYLONS' [patent_app_type] => utility [patent_app_number] => 12/755711 [patent_app_country] => US [patent_app_date] => 2010-04-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2670 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 7 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0127/20110127374.pdf [firstpage_image] =>[orig_patent_app_number] => 12755711 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/755711
METHODS AND SYSTEMS FOR MINIMIZING FLOW DISTURBANCES IN AIRCRAFT PROPELLER BLADES CAUSED BY UPSTREAM PYLONS Apr 6, 2010 Abandoned
Array ( [id] => 8531954 [patent_doc_number] => 08308104 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-11-13 [patent_title] => 'Aircraft having a rotating turbine engine' [patent_app_type] => utility [patent_app_number] => 12/755365 [patent_app_country] => US [patent_app_date] => 2010-04-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 14 [patent_no_of_words] => 5368 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 140 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12755365 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/755365
Aircraft having a rotating turbine engine Apr 5, 2010 Issued
Array ( [id] => 10836417 [patent_doc_number] => 08864083 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2014-10-21 [patent_title] => 'Low noise wing slat system with a fixed wing leading edge and deployable bridging panels' [patent_app_type] => utility [patent_app_number] => 12/751514 [patent_app_country] => US [patent_app_date] => 2010-03-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 18 [patent_no_of_words] => 4828 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 3 [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] => 12751514 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/751514
Low noise wing slat system with a fixed wing leading edge and deployable bridging panels Mar 30, 2010 Issued
Array ( [id] => 8770870 [patent_doc_number] => 08424810 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2013-04-23 [patent_title] => 'Low noise wing slat system with rigid cove-filled slat' [patent_app_type] => utility [patent_app_number] => 12/751468 [patent_app_country] => US [patent_app_date] => 2010-03-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 10 [patent_no_of_words] => 5271 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 139 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12751468 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/751468
Low noise wing slat system with rigid cove-filled slat Mar 30, 2010 Issued
Array ( [id] => 7727873 [patent_doc_number] => 20120012710 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-01-19 [patent_title] => 'COMPOSITE TANK, WING, AND METHOD FOR MANUFACTURING COMPOSITE TANK' [patent_app_type] => utility [patent_app_number] => 13/258179 [patent_app_country] => US [patent_app_date] => 2010-03-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 6956 [patent_no_of_claims] => 7 [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] => publications/A1/0012/20120012710.pdf [firstpage_image] =>[orig_patent_app_number] => 13258179 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/258179
Composite tank, wing, and method for manufacturing composite tank Mar 16, 2010 Issued
Array ( [id] => 6405941 [patent_doc_number] => 20100179711 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-07-15 [patent_title] => 'SPACECRAFT PAYLOAD ORIENTATION STEERING' [patent_app_type] => utility [patent_app_number] => 12/629707 [patent_app_country] => US [patent_app_date] => 2009-12-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 4582 [patent_no_of_claims] => 28 [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/A1/0179/20100179711.pdf [firstpage_image] =>[orig_patent_app_number] => 12629707 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/629707
Spacecraft payload orientation steering Dec 1, 2009 Issued
Array ( [id] => 6517100 [patent_doc_number] => 20100123042 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-05-20 [patent_title] => 'Devices, Systems and Methods for Modular Payload Integration for Unmanned Aerial Vehicles' [patent_app_type] => utility [patent_app_number] => 12/621257 [patent_app_country] => US [patent_app_date] => 2009-11-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 19 [patent_figures_cnt] => 19 [patent_no_of_words] => 7803 [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] => publications/A1/0123/20100123042.pdf [firstpage_image] =>[orig_patent_app_number] => 12621257 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/621257
Devices, systems and methods for modular payload integration for unmanned aerial vehicles Nov 17, 2009 Issued
Array ( [id] => 6398688 [patent_doc_number] => 20100148011 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-06-17 [patent_title] => 'TELESCOPING STRUCTURE AND METHOD' [patent_app_type] => utility [patent_app_number] => 12/616806 [patent_app_country] => US [patent_app_date] => 2009-11-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 3185 [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] => publications/A1/0148/20100148011.pdf [firstpage_image] =>[orig_patent_app_number] => 12616806 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/616806
TELESCOPING STRUCTURE AND METHOD Nov 11, 2009 Abandoned
Array ( [id] => 6407570 [patent_doc_number] => 20100140416 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-06-10 [patent_title] => 'Ducted Fans with Flow Control Synthetic Jet Actuators and Methods for Ducted Fan Force and Moment Control' [patent_app_type] => utility [patent_app_number] => 12/611463 [patent_app_country] => US [patent_app_date] => 2009-11-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 34 [patent_figures_cnt] => 34 [patent_no_of_words] => 10925 [patent_no_of_claims] => 20 [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] => publications/A1/0140/20100140416.pdf [firstpage_image] =>[orig_patent_app_number] => 12611463 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/611463
Ducted Fans with Flow Control Synthetic Jet Actuators and Methods for Ducted Fan Force and Moment Control Nov 2, 2009 Abandoned
Array ( [id] => 6391017 [patent_doc_number] => 20100163668 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-07-01 [patent_title] => 'Helicopter Rotor' [patent_app_type] => utility [patent_app_number] => 12/610930 [patent_app_country] => US [patent_app_date] => 2009-11-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 2396 [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] => publications/A1/0163/20100163668.pdf [firstpage_image] =>[orig_patent_app_number] => 12610930 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/610930
Helicopter rotor Nov 1, 2009 Issued
Array ( [id] => 8547778 [patent_doc_number] => 08322654 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-12-04 [patent_title] => 'Aircraft galley units' [patent_app_type] => utility [patent_app_number] => 12/611086 [patent_app_country] => US [patent_app_date] => 2009-11-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 2589 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 180 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12611086 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/611086
Aircraft galley units Nov 1, 2009 Issued
Array ( [id] => 9587625 [patent_doc_number] => 08777157 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-07-15 [patent_title] => 'Tethered hovering platform' [patent_app_type] => utility [patent_app_number] => 12/610055 [patent_app_country] => US [patent_app_date] => 2009-10-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 21 [patent_figures_cnt] => 31 [patent_no_of_words] => 15395 [patent_no_of_claims] => 30 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 128 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12610055 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/610055
Tethered hovering platform Oct 29, 2009 Issued
Array ( [id] => 6310330 [patent_doc_number] => 20100193638 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-08-05 [patent_title] => 'ANGULAR PROFILE FOR SKIN SECURING OF A BODY' [patent_app_type] => utility [patent_app_number] => 12/607527 [patent_app_country] => US [patent_app_date] => 2009-10-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 1301 [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/A1/0193/20100193638.pdf [firstpage_image] =>[orig_patent_app_number] => 12607527 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/607527
ANGULAR PROFILE FOR SKIN SECURING OF A BODY Oct 27, 2009 Abandoned
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