
Tho Dac Ta
Examiner (ID: 4422, Phone: (571)272-2014 , Office: P/2831 )
| Most Active Art Unit | 2833 |
| Art Unit(s) | 3202, 2831, 2839, 2833, 2834, 2832, 2899 |
| Total Applications | 4120 |
| Issued Applications | 3646 |
| Pending Applications | 156 |
| Abandoned Applications | 358 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 9550500
[patent_doc_number] => 08757539
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-06-24
[patent_title] => 'System for transporting an airplane from a parking location to a takeoff location and from a landing location to a parking location'
[patent_app_type] => utility
[patent_app_number] => 13/575322
[patent_app_country] => US
[patent_app_date] => 2011-01-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 4
[patent_no_of_words] => 953
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 116
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13575322
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/575322 | System for transporting an airplane from a parking location to a takeoff location and from a landing location to a parking location | Jan 25, 2011 | Issued |
Array
(
[id] => 7701866
[patent_doc_number] => 08087616
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-01-03
[patent_title] => 'Method and system for aviation navigation'
[patent_app_type] => utility
[patent_app_number] => 13/013653
[patent_app_country] => US
[patent_app_date] => 2011-01-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 5
[patent_no_of_words] => 4895
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 118
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/087/08087616.pdf
[firstpage_image] =>[orig_patent_app_number] => 13013653
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/013653 | Method and system for aviation navigation | Jan 24, 2011 | Issued |
Array
(
[id] => 8100901
[patent_doc_number] => 08152096
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-04-10
[patent_title] => 'Apparatus and method for vertical take-off and landing aircraft'
[patent_app_type] => utility
[patent_app_number] => 13/012763
[patent_app_country] => US
[patent_app_date] => 2011-01-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 11
[patent_no_of_words] => 10160
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 153
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/152/08152096.pdf
[firstpage_image] =>[orig_patent_app_number] => 13012763
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/012763 | Apparatus and method for vertical take-off and landing aircraft | Jan 23, 2011 | Issued |
Array
(
[id] => 5955396
[patent_doc_number] => 20110180672
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-07-28
[patent_title] => 'Airplane with aerodynamic stall-prevention layout and pertinent longitudinal stability arrangement'
[patent_app_type] => utility
[patent_app_number] => 13/011680
[patent_app_country] => US
[patent_app_date] => 2011-01-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2763
[patent_no_of_claims] => 2
[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/A1/0180/20110180672.pdf
[firstpage_image] =>[orig_patent_app_number] => 13011680
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/011680 | Airplane with aerodynamic stall-prevention layout and pertinent longitudinal stability arrangement | Jan 20, 2011 | Abandoned |
Array
(
[id] => 8310215
[patent_doc_number] => 20120187238
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-07-26
[patent_title] => 'HELICOPTER WITH REMOTE CONTROL'
[patent_app_type] => utility
[patent_app_number] => 13/009983
[patent_app_country] => US
[patent_app_date] => 2011-01-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 2744
[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] => 13009983
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/009983 | HELICOPTER WITH REMOTE CONTROL | Jan 19, 2011 | Abandoned |
Array
(
[id] => 9098066
[patent_doc_number] => 08561936
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-10-22
[patent_title] => 'Hang glider electric propulsion system and method'
[patent_app_type] => utility
[patent_app_number] => 13/010275
[patent_app_country] => US
[patent_app_date] => 2011-01-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 9
[patent_no_of_words] => 3550
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 151
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13010275
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/010275 | Hang glider electric propulsion system and method | Jan 19, 2011 | Issued |
Array
(
[id] => 6169277
[patent_doc_number] => 20110174930
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-07-21
[patent_title] => 'FUSE LINK DEVICE BETWEEN A MOBILE PART AND A FIXED PART OF AN AIRCRAFT NACELLE'
[patent_app_type] => utility
[patent_app_number] => 13/008592
[patent_app_country] => US
[patent_app_date] => 2011-01-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2795
[patent_no_of_claims] => 11
[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/A1/0174/20110174930.pdf
[firstpage_image] =>[orig_patent_app_number] => 13008592
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/008592 | Fuse link device between a mobile part and a fixed part of an aircraft nacelle | Jan 17, 2011 | Issued |
Array
(
[id] => 9646932
[patent_doc_number] => 08800936
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-08-12
[patent_title] => 'Unmanned aerial vehicle drag augmentation by reverse propeller rotation'
[patent_app_type] => utility
[patent_app_number] => 13/007515
[patent_app_country] => US
[patent_app_date] => 2011-01-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 10
[patent_no_of_words] => 2900
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 69
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13007515
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/007515 | Unmanned aerial vehicle drag augmentation by reverse propeller rotation | Jan 13, 2011 | Issued |
Array
(
[id] => 8772830
[patent_doc_number] => 08426788
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-04-23
[patent_title] => 'Guidance control for spinning or rolling projectile'
[patent_app_type] => utility
[patent_app_number] => 13/005175
[patent_app_country] => US
[patent_app_date] => 2011-01-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 17
[patent_no_of_words] => 4860
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 51
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13005175
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/005175 | Guidance control for spinning or rolling projectile | Jan 11, 2011 | Issued |
Array
(
[id] => 8384639
[patent_doc_number] => 08262030
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-09-11
[patent_title] => 'Apparatus for twisting a wing to increase lift on aircraft and other vehicles'
[patent_app_type] => utility
[patent_app_number] => 12/987231
[patent_app_country] => US
[patent_app_date] => 2011-01-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 14
[patent_figures_cnt] => 34
[patent_no_of_words] => 13524
[patent_no_of_claims] => 42
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 66
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12987231
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/987231 | Apparatus for twisting a wing to increase lift on aircraft and other vehicles | Jan 9, 2011 | Issued |
Array
(
[id] => 8519514
[patent_doc_number] => 20120318922
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-12-20
[patent_title] => 'DEICING DEVICE FOR WING LEADING EDGE OF AIRCRAFT AND AIRCRAFT MAIN WING'
[patent_app_type] => utility
[patent_app_number] => 13/579128
[patent_app_country] => US
[patent_app_date] => 2011-01-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 7133
[patent_no_of_claims] => 9
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13579128
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/579128 | DEICING DEVICE FOR WING LEADING EDGE OF AIRCRAFT AND AIRCRAFT MAIN WING | Jan 5, 2011 | Abandoned |
Array
(
[id] => 8227500
[patent_doc_number] => 20120141703
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-06-07
[patent_title] => 'AIRCRAFT OR SPACECRAFT CASING'
[patent_app_type] => utility
[patent_app_number] => 13/380066
[patent_app_country] => US
[patent_app_date] => 2010-12-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_no_of_words] => 3494
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13380066
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/380066 | AIRCRAFT OR SPACECRAFT CASING | Dec 29, 2010 | Abandoned |
Array
(
[id] => 8261533
[patent_doc_number] => 20120160965
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-06-28
[patent_title] => 'METHOD TO ACHIEVE A RAPID AND LOW POWER SLEW OF A SATELLITE'
[patent_app_type] => utility
[patent_app_number] => 12/977397
[patent_app_country] => US
[patent_app_date] => 2010-12-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_no_of_words] => 3062
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12977397
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/977397 | METHOD TO ACHIEVE A RAPID AND LOW POWER SLEW OF A SATELLITE | Dec 22, 2010 | Abandoned |
Array
(
[id] => 7480064
[patent_doc_number] => 20110233333
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-09-29
[patent_title] => 'SMALL DIAMETER PRESSURE STRUCTURE COMMERCIAL AIRCRAFT CREW REST'
[patent_app_type] => utility
[patent_app_number] => 12/964059
[patent_app_country] => US
[patent_app_date] => 2010-12-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 12
[patent_no_of_words] => 2954
[patent_no_of_claims] => 18
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0233/20110233333.pdf
[firstpage_image] =>[orig_patent_app_number] => 12964059
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/964059 | Small diameter pressure structure commercial aircraft crew rest | Dec 8, 2010 | Issued |
Array
(
[id] => 6177043
[patent_doc_number] => 20110121137
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-05-26
[patent_title] => 'METHOD AND APPARATUS FOR DIRECTING WASTE AWAY FROM AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 12/952650
[patent_app_country] => US
[patent_app_date] => 2010-11-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_no_of_words] => 1527
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0121/20110121137.pdf
[firstpage_image] =>[orig_patent_app_number] => 12952650
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/952650 | METHOD AND APPARATUS FOR DIRECTING WASTE AWAY FROM AIRCRAFT | Nov 22, 2010 | Abandoned |
Array
(
[id] => 6177022
[patent_doc_number] => 20110121126
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-05-26
[patent_title] => 'EMERGENCY COLLECTIVE ACTUATOR AND METHOD FOR A HELICOPTER'
[patent_app_type] => utility
[patent_app_number] => 12/953294
[patent_app_country] => US
[patent_app_date] => 2010-11-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
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[patent_no_of_words] => 7450
[patent_no_of_claims] => 26
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0121/20110121126.pdf
[firstpage_image] =>[orig_patent_app_number] => 12953294
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/953294 | Emergency collective actuator and method for a helicopter | Nov 22, 2010 | Issued |
Array
(
[id] => 6177027
[patent_doc_number] => 20110121127
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-05-26
[patent_title] => 'POWER PLANT, A HELICOPTER INCLUDING SUCH A POWER PLANT, AND A METHOD IMPLEMENTED BY SAID POWER PLANT'
[patent_app_type] => utility
[patent_app_number] => 12/951206
[patent_app_country] => US
[patent_app_date] => 2010-11-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0121/20110121127.pdf
[firstpage_image] =>[orig_patent_app_number] => 12951206
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/951206 | Power plant, a helicopter including such a power plant, and a method implemented by said power plant | Nov 21, 2010 | Issued |
Array
(
[id] => 9045633
[patent_doc_number] => 08540184
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-09-24
[patent_title] => 'Long-range aircraft with high forward speed in cruising flight'
[patent_app_type] => utility
[patent_app_number] => 12/946932
[patent_app_country] => US
[patent_app_date] => 2010-11-16
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12946932
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/946932 | Long-range aircraft with high forward speed in cruising flight | Nov 15, 2010 | Issued |
Array
(
[id] => 5996161
[patent_doc_number] => 20110114784
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-05-19
[patent_title] => 'HUMAN-POWERED, BIRD-LIKE WINGS FLYING DEVICE'
[patent_app_type] => utility
[patent_app_number] => 12/947060
[patent_app_country] => US
[patent_app_date] => 2010-11-16
[patent_effective_date] => 0000-00-00
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[pdf_file] => publications/A1/0114/20110114784.pdf
[firstpage_image] =>[orig_patent_app_number] => 12947060
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/947060 | HUMAN-POWERED, BIRD-LIKE WINGS FLYING DEVICE | Nov 15, 2010 | Abandoned |
Array
(
[id] => 8513508
[patent_doc_number] => 20120312916
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-12-13
[patent_title] => 'Propulsive Anti-Torque Nozzle System with Rotating Thrust Director for a Rotorcraft'
[patent_app_type] => utility
[patent_app_number] => 13/580577
[patent_app_country] => US
[patent_app_date] => 2010-11-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 3100
[patent_no_of_claims] => 17
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13580577
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/580577 | Propulsive anti-torque nozzle system with rotating thrust director for a rotorcraft | Nov 11, 2010 | Issued |