
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] => 6003690
[patent_doc_number] => 20110057073
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-03-10
[patent_title] => 'REST MODULE WITH A FIRST PARTIAL MODULE WITH DIRECT ACCESS TO A POSSIBLE SECOND PARTIAL MODULE'
[patent_app_type] => utility
[patent_app_number] => 12/743645
[patent_app_country] => US
[patent_app_date] => 2008-11-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 8059
[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/A1/0057/20110057073.pdf
[firstpage_image] =>[orig_patent_app_number] => 12743645
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/743645 | Rest module with a first partial module with direct access to a possible second partial module | Nov 13, 2008 | Issued |
Array
(
[id] => 6255482
[patent_doc_number] => 20100294890
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-11-25
[patent_title] => 'METHOD AND DEVICE FOR REDUCING THE INDUCED SPEEDS IN VORTICES IN THE WAKE OF AN AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 12/738214
[patent_app_country] => US
[patent_app_date] => 2008-10-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 6739
[patent_no_of_claims] => 10
[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/A1/0294/20100294890.pdf
[firstpage_image] =>[orig_patent_app_number] => 12738214
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/738214 | Method and device for reducing the induced speeds in vortices in the wake of an aircraft | Oct 15, 2008 | Issued |
Array
(
[id] => 5357848
[patent_doc_number] => 20090032642
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-02-05
[patent_title] => 'MODULE FOR PLACEMENT IN A PASSENGER CABIN OF A MEANS OF TRANSPORT, MORE PARTICULARLY AN AIRPLANE'
[patent_app_type] => utility
[patent_app_number] => 12/252865
[patent_app_country] => US
[patent_app_date] => 2008-10-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2890
[patent_no_of_claims] => 14
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0032/20090032642.pdf
[firstpage_image] =>[orig_patent_app_number] => 12252865
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/252865 | MODULE FOR PLACEMENT IN A PASSENGER CABIN OF A MEANS OF TRANSPORT, MORE PARTICULARLY AN AIRPLANE | Oct 15, 2008 | Abandoned |
Array
(
[id] => 5530449
[patent_doc_number] => 20090230237
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-09-17
[patent_title] => 'APPARATUS AND METHOD FOR MAKING OPTIMAL USE OF A PHOTOVOLTAIC ARRAY ON AN AIRBORNE POWER SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 12/251331
[patent_app_country] => US
[patent_app_date] => 2008-10-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 18
[patent_figures_cnt] => 18
[patent_no_of_words] => 5813
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0230/20090230237.pdf
[firstpage_image] =>[orig_patent_app_number] => 12251331
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/251331 | Apparatus and method for making optimal use of a photovoltaic array on an airborne power system | Oct 13, 2008 | Issued |
Array
(
[id] => 5425615
[patent_doc_number] => 20090084925
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-04-02
[patent_title] => 'COMPOSITE LEG STRUCTURE FOR A LIGHTWEIGHT AIRCRAFT SEAT ASSEMBLY'
[patent_app_type] => utility
[patent_app_number] => 12/200790
[patent_app_country] => US
[patent_app_date] => 2008-08-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 30
[patent_figures_cnt] => 30
[patent_no_of_words] => 15969
[patent_no_of_claims] => 22
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0084/20090084925.pdf
[firstpage_image] =>[orig_patent_app_number] => 12200790
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/200790 | Composite leg structure for a lightweight aircraft seat assembly | Aug 27, 2008 | Issued |
Array
(
[id] => 7748975
[patent_doc_number] => 08109465
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2012-02-07
[patent_title] => 'Electro-magnetic up-lock for retractable landing gear'
[patent_app_type] => utility
[patent_app_number] => 12/220401
[patent_app_country] => US
[patent_app_date] => 2008-07-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 2493
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 111
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/109/08109465.pdf
[firstpage_image] =>[orig_patent_app_number] => 12220401
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/220401 | Electro-magnetic up-lock for retractable landing gear | Jul 23, 2008 | Issued |
Array
(
[id] => 5275260
[patent_doc_number] => 20090127392
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-05-21
[patent_title] => 'PROTECTION DEVICE'
[patent_app_type] => utility
[patent_app_number] => 12/142475
[patent_app_country] => US
[patent_app_date] => 2008-06-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 1414
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 1
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0127/20090127392.pdf
[firstpage_image] =>[orig_patent_app_number] => 12142475
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/142475 | PROTECTION DEVICE | Jun 18, 2008 | Abandoned |
Array
(
[id] => 5371411
[patent_doc_number] => 20090308971
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-12-17
[patent_title] => 'Airfoil System for Cruising Flight'
[patent_app_type] => utility
[patent_app_number] => 12/138709
[patent_app_country] => US
[patent_app_date] => 2008-06-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 1966
[patent_no_of_claims] => 26
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0308/20090308971.pdf
[firstpage_image] =>[orig_patent_app_number] => 12138709
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/138709 | Airfoil system for cruising flight | Jun 12, 2008 | Issued |
Array
(
[id] => 5268305
[patent_doc_number] => 20090072080
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-03-19
[patent_title] => 'ON BOARD SECONDARY PROPULSION SYSTEM FOR AN AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 12/137789
[patent_app_country] => US
[patent_app_date] => 2008-06-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_no_of_words] => 4388
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0072/20090072080.pdf
[firstpage_image] =>[orig_patent_app_number] => 12137789
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/137789 | ON BOARD SECONDARY PROPULSION SYSTEM FOR AN AIRCRAFT | Jun 11, 2008 | Abandoned |
Array
(
[id] => 5364607
[patent_doc_number] => 20090302166
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-12-10
[patent_title] => 'Space station, launch vehicle, and method of assembly'
[patent_app_type] => utility
[patent_app_number] => 12/155605
[patent_app_country] => US
[patent_app_date] => 2008-06-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
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[patent_no_of_words] => 4489
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0302/20090302166.pdf
[firstpage_image] =>[orig_patent_app_number] => 12155605
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/155605 | Space station, launch vehicle, and method of assembly | Jun 5, 2008 | Abandoned |
Array
(
[id] => 5287924
[patent_doc_number] => 20090020654
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-01-22
[patent_title] => 'Harness with mounted engine frame'
[patent_app_type] => utility
[patent_app_number] => 12/157024
[patent_app_country] => US
[patent_app_date] => 2008-06-06
[patent_effective_date] => 0000-00-00
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[pdf_file] => publications/A1/0020/20090020654.pdf
[firstpage_image] =>[orig_patent_app_number] => 12157024
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/157024 | Harness with mounted engine frame | Jun 5, 2008 | Abandoned |
Array
(
[id] => 5364591
[patent_doc_number] => 20090302150
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-12-10
[patent_title] => 'TUBULAR AIR TRANSPORT VEHICLE'
[patent_app_type] => utility
[patent_app_number] => 12/134004
[patent_app_country] => US
[patent_app_date] => 2008-06-05
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[pdf_file] => publications/A1/0302/20090302150.pdf
[firstpage_image] =>[orig_patent_app_number] => 12134004
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/134004 | Tubular air transport vehicle | Jun 4, 2008 | Issued |
Array
(
[id] => 5364957
[patent_doc_number] => 20090302516
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-12-10
[patent_title] => 'SYSTEM, METHOD AND APPARATUS FOR CONTROL SURFACE WITH DYNAMIC COMPENSATION'
[patent_app_type] => utility
[patent_app_number] => 12/133822
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[patent_app_date] => 2008-06-05
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[pdf_file] => publications/A1/0302/20090302516.pdf
[firstpage_image] =>[orig_patent_app_number] => 12133822
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/133822 | SYSTEM, METHOD AND APPARATUS FOR CONTROL SURFACE WITH DYNAMIC COMPENSATION | Jun 4, 2008 | Abandoned |
| 12/157180 | Aircraft having VTOL, translational and traverse flight | Jun 4, 2008 | Abandoned |
Array
(
[id] => 10880980
[patent_doc_number] => 08905353
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-12-09
[patent_title] => 'Bi-convex airship'
[patent_app_type] => utility
[patent_app_number] => 12/131671
[patent_app_country] => US
[patent_app_date] => 2008-06-02
[patent_effective_date] => 0000-00-00
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/131671 | Bi-convex airship | Jun 1, 2008 | Issued |
Array
(
[id] => 5529868
[patent_doc_number] => 20090229656
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-09-17
[patent_title] => 'AIRBORNE POWER STATION'
[patent_app_type] => utility
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[patent_app_country] => US
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[pdf_file] => publications/A1/0229/20090229656.pdf
[firstpage_image] =>[orig_patent_app_number] => 12128561
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/128561 | Airborne power station | May 27, 2008 | Issued |
Array
(
[id] => 6285465
[patent_doc_number] => 20100237189
[patent_country] => US
[patent_kind] => A9
[patent_issue_date] => 2010-09-23
[patent_title] => 'LANDING GEAR CASING PROVIDED WITH A BOX STRUCTURE'
[patent_app_type] => utility
[patent_app_number] => 12/123958
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[patent_app_date] => 2008-05-20
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[firstpage_image] =>[orig_patent_app_number] => 12123958
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/123958 | Landing gear casing provided with a box structure | May 19, 2008 | Issued |
Array
(
[id] => 6285465
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Array
(
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[patent_title] => 'THRUST VECTORING SHROUD FOR FLUID DYNAMIC DEVICE'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/121362 | THRUST VECTORING SHROUD FOR FLUID DYNAMIC DEVICE | May 14, 2008 | Abandoned |
Array
(
[id] => 7549329
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[patent_country] => US
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[patent_issue_date] => 2011-11-22
[patent_title] => 'Latching device for an escape chute in an aircraft'
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[pdf_file] => patents/08/061/08061658.pdf
[firstpage_image] =>[orig_patent_app_number] => 12153021
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/153021 | Latching device for an escape chute in an aircraft | May 12, 2008 | Issued |