
Keith L. Dixon
Examiner (ID: 15768, 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] => 6442104
[patent_doc_number] => 20100282901
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-11-11
[patent_title] => 'Pneumatic Blow-Down Actuator'
[patent_app_type] => utility
[patent_app_number] => 12/463207
[patent_app_country] => US
[patent_app_date] => 2009-05-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2011
[patent_no_of_claims] => 20
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0282/20100282901.pdf
[firstpage_image] =>[orig_patent_app_number] => 12463207
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/463207 | Pneumatic blow-down actuator | May 7, 2009 | Issued |
Array
(
[id] => 5299926
[patent_doc_number] => 20090294578
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-12-03
[patent_title] => 'AIRCRAFT LANDING GEAR STEERING SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 12/431811
[patent_app_country] => US
[patent_app_date] => 2009-04-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_no_of_words] => 3411
[patent_no_of_claims] => 15
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0294/20090294578.pdf
[firstpage_image] =>[orig_patent_app_number] => 12431811
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/431811 | Aircraft landing gear steering system | Apr 28, 2009 | Issued |
Array
(
[id] => 8316310
[patent_doc_number] => 08231082
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-07-31
[patent_title] => 'Method and device for correcting the lateral dissymmetry of an aircraft'
[patent_app_type] => utility
[patent_app_number] => 12/431662
[patent_app_country] => US
[patent_app_date] => 2009-04-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
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[patent_no_of_words] => 1934
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12431662
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/431662 | Method and device for correcting the lateral dissymmetry of an aircraft | Apr 27, 2009 | Issued |
Array
(
[id] => 6492620
[patent_doc_number] => 20100200705
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-08-12
[patent_title] => 'CONTROL AND COMMAND ASSEMBLY FOR AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 12/422386
[patent_app_country] => US
[patent_app_date] => 2009-04-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 3548
[patent_no_of_claims] => 8
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[pdf_file] => publications/A1/0200/20100200705.pdf
[firstpage_image] =>[orig_patent_app_number] => 12422386
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/422386 | CONTROL AND COMMAND ASSEMBLY FOR AIRCRAFT | Apr 12, 2009 | Abandoned |
Array
(
[id] => 5455125
[patent_doc_number] => 20090255277
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-10-15
[patent_title] => 'OPTIMIZED DEFROSTING REGULATION OF PARALLEL ARRANGED FRESH AIR OUTLETS OF AIR CONDITIONERS'
[patent_app_type] => utility
[patent_app_number] => 12/421086
[patent_app_country] => US
[patent_app_date] => 2009-04-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_no_of_words] => 5958
[patent_no_of_claims] => 22
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[pdf_file] => publications/A1/0255/20090255277.pdf
[firstpage_image] =>[orig_patent_app_number] => 12421086
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/421086 | OPTIMIZED DEFROSTING REGULATION OF PARALLEL ARRANGED FRESH AIR OUTLETS OF AIR CONDITIONERS | Apr 8, 2009 | Abandoned |
Array
(
[id] => 8327235
[patent_doc_number] => 08235327
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-08-07
[patent_title] => 'Adjustable servomechanism assemblies and associated systems and methods'
[patent_app_type] => utility
[patent_app_number] => 12/406908
[patent_app_country] => US
[patent_app_date] => 2009-03-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12406908
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/406908 | Adjustable servomechanism assemblies and associated systems and methods | Mar 17, 2009 | Issued |
Array
(
[id] => 6536290
[patent_doc_number] => 20100218225
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-08-26
[patent_title] => 'AIRCRAFT VIDEO CONTROL STATION WITH STOWABLE SEAT'
[patent_app_type] => utility
[patent_app_number] => 12/391880
[patent_app_country] => US
[patent_app_date] => 2009-02-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
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[patent_no_of_words] => 6067
[patent_no_of_claims] => 26
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[pdf_file] => publications/A1/0218/20100218225.pdf
[firstpage_image] =>[orig_patent_app_number] => 12391880
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/391880 | Aircraft video control station with stowable seat | Feb 23, 2009 | Issued |
Array
(
[id] => 6568173
[patent_doc_number] => 20100320321
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-12-23
[patent_title] => 'METHOD FOR JOINING TWO FUSELAGE SECTIONS BY CREATING A TRANSVERSE BUTT JOINT AS WELL AS TRANSVERSE BUTT JOINT CONNECTION'
[patent_app_type] => utility
[patent_app_number] => 12/735776
[patent_app_country] => US
[patent_app_date] => 2009-02-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 4475
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 1
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0320/20100320321.pdf
[firstpage_image] =>[orig_patent_app_number] => 12735776
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/735776 | Method for joining two fuselage sections by creating a transverse butt joint as well as transverse butt joint connection | Feb 10, 2009 | Issued |
Array
(
[id] => 6430671
[patent_doc_number] => 20100187369
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-07-29
[patent_title] => 'DUCTED FAN UAV CONTROL ALTERNATIVES'
[patent_app_type] => utility
[patent_app_number] => 12/359407
[patent_app_country] => US
[patent_app_date] => 2009-01-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_no_of_words] => 3056
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[pdf_file] => publications/A1/0187/20100187369.pdf
[firstpage_image] =>[orig_patent_app_number] => 12359407
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/359407 | Ducted fan UAV control alternatives | Jan 25, 2009 | Issued |
Array
(
[id] => 6224253
[patent_doc_number] => 20100181414
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-07-22
[patent_title] => 'Personal transportation vehicle'
[patent_app_type] => utility
[patent_app_number] => 12/320136
[patent_app_country] => US
[patent_app_date] => 2009-01-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_no_of_words] => 1340
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[pdf_file] => publications/A1/0181/20100181414.pdf
[firstpage_image] =>[orig_patent_app_number] => 12320136
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/320136 | Personal transportation vehicle | Jan 20, 2009 | Abandoned |
Array
(
[id] => 5340459
[patent_doc_number] => 20090179109
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-07-16
[patent_title] => 'System and method for adjusting control surfaces for wind tunnel models'
[patent_app_type] => utility
[patent_app_number] => 12/319470
[patent_app_country] => US
[patent_app_date] => 2009-01-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_no_of_words] => 2766
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[pdf_file] => publications/A1/0179/20090179109.pdf
[firstpage_image] =>[orig_patent_app_number] => 12319470
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/319470 | System and method for adjusting control surfaces for wind tunnel models | Jan 6, 2009 | Issued |
Array
(
[id] => 6602663
[patent_doc_number] => 20100170993
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-07-08
[patent_title] => 'Aerodynamic Fairing for aircraft lift strut'
[patent_app_type] => utility
[patent_app_number] => 12/319207
[patent_app_country] => US
[patent_app_date] => 2009-01-05
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[firstpage_image] =>[orig_patent_app_number] => 12319207
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/319207 | Aerodynamic Fairing for aircraft lift strut | Jan 4, 2009 | Abandoned |
Array
(
[id] => 6517068
[patent_doc_number] => 20100123039
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-05-20
[patent_title] => 'Tail rotor system and method for controlling a tail rotor system'
[patent_app_type] => utility
[patent_app_number] => 12/317313
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[firstpage_image] =>[orig_patent_app_number] => 12317313
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/317313 | Tail rotor system and method for controlling a tail rotor system | Dec 21, 2008 | Abandoned |
Array
(
[id] => 6531047
[patent_doc_number] => 20100270419
[patent_country] => US
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[patent_issue_date] => 2010-10-28
[patent_title] => 'REDUNDANCIES AND FLOWS IN VEHICLES'
[patent_app_type] => utility
[patent_app_number] => 12/747830
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[patent_app_date] => 2008-12-15
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/747830 | REDUNDANCIES AND FLOWS IN VEHICLES | Dec 14, 2008 | Abandoned |
Array
(
[id] => 7799753
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[patent_kind] => B2
[patent_issue_date] => 2012-03-06
[patent_title] => 'Hybrid power for ducted fan unmanned aerial systems'
[patent_app_type] => utility
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[pdf_file] => patents/08/128/08128019.pdf
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/334098 | Hybrid power for ducted fan unmanned aerial systems | Dec 11, 2008 | Issued |
Array
(
[id] => 6090493
[patent_doc_number] => 20110001016
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[patent_issue_date] => 2011-01-06
[patent_title] => 'Telescoping and sweeping wing that is reconfigurable during flight'
[patent_app_type] => utility
[patent_app_number] => 12/314534
[patent_app_country] => US
[patent_app_date] => 2008-12-12
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/314534 | Telescoping and sweeping wing that is reconfigurable during flight | Dec 11, 2008 | Abandoned |
Array
(
[id] => 10896494
[patent_doc_number] => 08919695
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-12-30
[patent_title] => 'Storage compartment configuration'
[patent_app_type] => utility
[patent_app_number] => 12/747237
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/747237 | Storage compartment configuration | Dec 10, 2008 | Issued |
Array
(
[id] => 6263548
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[patent_title] => 'AIRCRAFT NACELLE INCLUDING AN OPTIMISED ICE TREATMENT SYSTEM'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/745957 | Aircraft nacelle including an optimised ice treatment system | Nov 30, 2008 | Issued |
Array
(
[id] => 6364491
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[patent_title] => 'AIRCRAFT NACELLE INCLUDING HOT AIR DISCHARGE MEANS'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/745953 | Aircraft nacelle including hot air discharge means | Nov 30, 2008 | Issued |
Array
(
[id] => 6341528
[patent_doc_number] => 20100084512
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[patent_title] => 'Luno Geo Wind Mill'
[patent_app_type] => utility
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[pdf_file] => publications/A1/0084/20100084512.pdf
[firstpage_image] =>[orig_patent_app_number] => 12315067
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/315067 | Luno Geo Wind Mill | Nov 27, 2008 | Abandoned |