
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] => 7666546
[patent_doc_number] => 20110315815
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-12-29
[patent_title] => 'MULTI-SOURCE EMERGENCY POWER OPTIMIZATION'
[patent_app_type] => utility
[patent_app_number] => 12/821255
[patent_app_country] => US
[patent_app_date] => 2010-06-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 1920
[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] =>[firstpage_image] =>[orig_patent_app_number] => 12821255
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/821255 | Multi-source emergency power optimization | Jun 22, 2010 | Issued |
Array
(
[id] => 8641082
[patent_doc_number] => 08366055
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-02-05
[patent_title] => 'Controllable miniature mono-wing aircraft'
[patent_app_type] => utility
[patent_app_number] => 12/818826
[patent_app_country] => US
[patent_app_date] => 2010-06-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 33
[patent_figures_cnt] => 85
[patent_no_of_words] => 18663
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 81
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12818826
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/818826 | Controllable miniature mono-wing aircraft | Jun 17, 2010 | Issued |
Array
(
[id] => 10064483
[patent_doc_number] => 09103319
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-08-11
[patent_title] => 'Wind turbine generator service by airship'
[patent_app_type] => utility
[patent_app_number] => 13/377382
[patent_app_country] => US
[patent_app_date] => 2010-06-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 4838
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 2
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13377382
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/377382 | Wind turbine generator service by airship | Jun 14, 2010 | Issued |
Array
(
[id] => 8770867
[patent_doc_number] => 08424808
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-04-23
[patent_title] => 'Compensating for wind prior to engaging airborne propulsion devices'
[patent_app_type] => utility
[patent_app_number] => 12/816267
[patent_app_country] => US
[patent_app_date] => 2010-06-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 4108
[patent_no_of_claims] => 22
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 157
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12816267
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/816267 | Compensating for wind prior to engaging airborne propulsion devices | Jun 14, 2010 | Issued |
Array
(
[id] => 8133451
[patent_doc_number] => 20120091274
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-04-19
[patent_title] => 'WIND TURBINE GENERATOR INSTALLATION BY AIRSHIP'
[patent_app_type] => utility
[patent_app_number] => 13/377380
[patent_app_country] => US
[patent_app_date] => 2010-06-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 16
[patent_figures_cnt] => 16
[patent_no_of_words] => 7078
[patent_no_of_claims] => 17
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0091/20120091274.pdf
[firstpage_image] =>[orig_patent_app_number] => 13377380
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/377380 | Wind turbine generator installation by airship | Jun 14, 2010 | Issued |
Array
(
[id] => 8373931
[patent_doc_number] => 08256717
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-09-04
[patent_title] => 'Ground impact cargo parachute release mechanism'
[patent_app_type] => utility
[patent_app_number] => 12/794931
[patent_app_country] => US
[patent_app_date] => 2010-06-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 4
[patent_no_of_words] => 1589
[patent_no_of_claims] => 3
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12794931
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/794931 | Ground impact cargo parachute release mechanism | Jun 6, 2010 | Issued |
Array
(
[id] => 8628293
[patent_doc_number] => 08360357
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-01-29
[patent_title] => 'Aircraft with a wing movable along the longitudinal axis of the fuselage'
[patent_app_type] => utility
[patent_app_number] => 12/789845
[patent_app_country] => US
[patent_app_date] => 2010-05-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 16
[patent_no_of_words] => 6784
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 178
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12789845
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/789845 | Aircraft with a wing movable along the longitudinal axis of the fuselage | May 27, 2010 | Issued |
Array
(
[id] => 14293797
[patent_doc_number] => 10287011
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2019-05-14
[patent_title] => Air vehicle
[patent_app_type] => utility
[patent_app_number] => 13/322496
[patent_app_country] => US
[patent_app_date] => 2010-05-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 22
[patent_no_of_words] => 17787
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 641
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13322496
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/322496 | Air vehicle | May 25, 2010 | Issued |
Array
(
[id] => 10083225
[patent_doc_number] => 09120562
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-09-01
[patent_title] => 'Aircraft winglet design having a compound curve profile'
[patent_app_type] => utility
[patent_app_number] => 13/319220
[patent_app_country] => US
[patent_app_date] => 2010-05-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 28
[patent_figures_cnt] => 33
[patent_no_of_words] => 17645
[patent_no_of_claims] => 14
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13319220
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/319220 | Aircraft winglet design having a compound curve profile | May 4, 2010 | Issued |
Array
(
[id] => 6183749
[patent_doc_number] => 20110168840
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-07-14
[patent_title] => 'Aircraft frame and method for obtaining the same'
[patent_app_type] => utility
[patent_app_number] => 12/798502
[patent_app_country] => US
[patent_app_date] => 2010-04-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 3463
[patent_no_of_claims] => 8
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[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0168/20110168840.pdf
[firstpage_image] =>[orig_patent_app_number] => 12798502
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/798502 | Aircraft frame and method for obtaining the same | Apr 5, 2010 | Abandoned |
Array
(
[id] => 6319830
[patent_doc_number] => 20100243792
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-09-30
[patent_title] => 'METHOD AND A DEVICE FOR OPTIMIZING THE OPERATION OF PROPULSIVE PROPELLERS DISPOSED ON EITHER SIDE OF A ROTORCRAFT FUSELAGE'
[patent_app_type] => utility
[patent_app_number] => 12/724453
[patent_app_country] => US
[patent_app_date] => 2010-03-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_no_of_words] => 8679
[patent_no_of_claims] => 11
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0243/20100243792.pdf
[firstpage_image] =>[orig_patent_app_number] => 12724453
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/724453 | Method and a device for optimizing the operation of propulsive propellers disposed on either side of a rotorcraft fuselage | Mar 15, 2010 | Issued |
Array
(
[id] => 9400060
[patent_doc_number] => 08690106
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2014-04-08
[patent_title] => 'Ejector driven flow control for reducing velocity deficit profile downstream of an aerodynamic body'
[patent_app_type] => utility
[patent_app_number] => 12/723678
[patent_app_country] => US
[patent_app_date] => 2010-03-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12723678
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/723678 | Ejector driven flow control for reducing velocity deficit profile downstream of an aerodynamic body | Mar 13, 2010 | Issued |
Array
(
[id] => 8444870
[patent_doc_number] => 08286914
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-10-16
[patent_title] => 'Conveyor device for airplanes'
[patent_app_type] => utility
[patent_app_number] => 12/723386
[patent_app_country] => US
[patent_app_date] => 2010-03-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12723386
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/723386 | Conveyor device for airplanes | Mar 11, 2010 | Issued |
Array
(
[id] => 9272324
[patent_doc_number] => 08636250
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-01-28
[patent_title] => 'External cargo hook system for rotary-wing aircraft'
[patent_app_type] => utility
[patent_app_number] => 13/258545
[patent_app_country] => US
[patent_app_date] => 2010-03-08
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13258545
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/258545 | External cargo hook system for rotary-wing aircraft | Mar 7, 2010 | Issued |
Array
(
[id] => 10896491
[patent_doc_number] => 08919692
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-12-30
[patent_title] => 'Proximity sensor valve and lock system using same'
[patent_app_type] => utility
[patent_app_number] => 13/258506
[patent_app_country] => US
[patent_app_date] => 2010-03-04
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13258506
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/258506 | Proximity sensor valve and lock system using same | Mar 3, 2010 | Issued |
Array
(
[id] => 8736736
[patent_doc_number] => 08408495
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-04-02
[patent_title] => 'Fittings for attaching the vertical tail stabilizer of an aircraft'
[patent_app_type] => utility
[patent_app_number] => 12/714333
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[patent_app_date] => 2010-02-26
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12714333
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/714333 | Fittings for attaching the vertical tail stabilizer of an aircraft | Feb 25, 2010 | Issued |
Array
(
[id] => 6476494
[patent_doc_number] => 20100213319
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-08-26
[patent_title] => 'Craft and Method of Coupling a Propulsion System to a Regenerative Fuel Cell System'
[patent_app_type] => utility
[patent_app_number] => 12/711955
[patent_app_country] => US
[patent_app_date] => 2010-02-24
[patent_effective_date] => 0000-00-00
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[pdf_file] => publications/A1/0213/20100213319.pdf
[firstpage_image] =>[orig_patent_app_number] => 12711955
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/711955 | Craft and method of coupling a propulsion system to a regenerative fuel cell system | Feb 23, 2010 | Issued |
Array
(
[id] => 5962628
[patent_doc_number] => 20110147517
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-06-23
[patent_title] => 'PIVOTING STABILISING SURFACE FOR AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 12/710849
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[pdf_file] => publications/A1/0147/20110147517.pdf
[firstpage_image] =>[orig_patent_app_number] => 12710849
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/710849 | Pivoting stabilising surface for aircraft | Feb 22, 2010 | Issued |
Array
(
[id] => 7727872
[patent_doc_number] => 20120012709
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-01-19
[patent_title] => 'FIRING PREVENTION STRUCTURE OF FUEL TANK'
[patent_app_type] => utility
[patent_app_number] => 13/203323
[patent_app_country] => US
[patent_app_date] => 2010-02-17
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[pdf_file] => publications/A1/0012/20120012709.pdf
[firstpage_image] =>[orig_patent_app_number] => 13203323
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/203323 | Firing prevention structure of fuel tank | Feb 16, 2010 | Issued |
Array
(
[id] => 9873341
[patent_doc_number] => 08960600
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-02-24
[patent_title] => 'Variable surface landing platform (VARSLAP)'
[patent_app_type] => utility
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13576830
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/576830 | Variable surface landing platform (VARSLAP) | Feb 7, 2010 | Issued |