
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] => 6335042
[patent_doc_number] => 20100019079
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-01-28
[patent_title] => 'THRUST GENERATOR FOR A ROTARY WING AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 11/765695
[patent_app_country] => US
[patent_app_date] => 2007-06-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 3903
[patent_no_of_claims] => 24
[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/A1/0019/20100019079.pdf
[firstpage_image] =>[orig_patent_app_number] => 11765695
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/765695 | THRUST GENERATOR FOR A ROTARY WING AIRCRAFT | Jun 19, 2007 | Abandoned |
Array
(
[id] => 4849300
[patent_doc_number] => 20080315042
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-12-25
[patent_title] => 'THRUST GENERATOR FOR A PROPULSION SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 11/765666
[patent_app_country] => US
[patent_app_date] => 2007-06-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 5172
[patent_no_of_claims] => 25
[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/A1/0315/20080315042.pdf
[firstpage_image] =>[orig_patent_app_number] => 11765666
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/765666 | THRUST GENERATOR FOR A PROPULSION SYSTEM | Jun 19, 2007 | Abandoned |
Array
(
[id] => 4756459
[patent_doc_number] => 20080308684
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-12-18
[patent_title] => 'NACELLE WITH ARTICULATING LEADING EDGE SLATES'
[patent_app_type] => utility
[patent_app_number] => 11/763673
[patent_app_country] => US
[patent_app_date] => 2007-06-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 1741
[patent_no_of_claims] => 16
[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/A1/0308/20080308684.pdf
[firstpage_image] =>[orig_patent_app_number] => 11763673
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/763673 | NACELLE WITH ARTICULATING LEADING EDGE SLATES | Jun 14, 2007 | Abandoned |
Array
(
[id] => 4930250
[patent_doc_number] => 20080001025
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-01-03
[patent_title] => 'Amphibious Aircraft'
[patent_app_type] => utility
[patent_app_number] => 11/758404
[patent_app_country] => US
[patent_app_date] => 2007-06-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 11
[patent_no_of_words] => 3025
[patent_no_of_claims] => 17
[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/A1/0001/20080001025.pdf
[firstpage_image] =>[orig_patent_app_number] => 11758404
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/758404 | Amphibious aircraft | Jun 4, 2007 | Issued |
Array
(
[id] => 30060
[patent_doc_number] => 07789347
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-09-07
[patent_title] => 'Device for articulating a door of a nacelle of an aircraft and nacelle provided with said articulation device'
[patent_app_type] => utility
[patent_app_number] => 11/802132
[patent_app_country] => US
[patent_app_date] => 2007-05-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 18
[patent_no_of_words] => 3171
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 414
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/789/07789347.pdf
[firstpage_image] =>[orig_patent_app_number] => 11802132
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/802132 | Device for articulating a door of a nacelle of an aircraft and nacelle provided with said articulation device | May 20, 2007 | Issued |
Array
(
[id] => 4481310
[patent_doc_number] => 07883060
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-02-08
[patent_title] => 'Apparatus and method for twisting a wing to increase lift on aircraft and other vehicles'
[patent_app_type] => utility
[patent_app_number] => 11/805226
[patent_app_country] => US
[patent_app_date] => 2007-05-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 14
[patent_figures_cnt] => 34
[patent_no_of_words] => 13576
[patent_no_of_claims] => 76
[patent_no_of_ind_claims] => 6
[patent_words_short_claim] => 59
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/883/07883060.pdf
[firstpage_image] =>[orig_patent_app_number] => 11805226
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/805226 | Apparatus and method for twisting a wing to increase lift on aircraft and other vehicles | May 20, 2007 | Issued |
Array
(
[id] => 120696
[patent_doc_number] => 07703716
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-04-27
[patent_title] => 'Hinged device for doors of an aircraft nacelle and nacelle equipped with said hinged device'
[patent_app_type] => utility
[patent_app_number] => 11/798375
[patent_app_country] => US
[patent_app_date] => 2007-05-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 30
[patent_no_of_words] => 3705
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 175
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/703/07703716.pdf
[firstpage_image] =>[orig_patent_app_number] => 11798375
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/798375 | Hinged device for doors of an aircraft nacelle and nacelle equipped with said hinged device | May 13, 2007 | Issued |
Array
(
[id] => 4890519
[patent_doc_number] => 20080099615
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-05-01
[patent_title] => 'Modular aircraft window'
[patent_app_type] => utility
[patent_app_number] => 11/801960
[patent_app_country] => US
[patent_app_date] => 2007-05-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 15
[patent_figures_cnt] => 15
[patent_no_of_words] => 2959
[patent_no_of_claims] => 14
[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/A1/0099/20080099615.pdf
[firstpage_image] =>[orig_patent_app_number] => 11801960
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/801960 | Modular aircraft window | May 10, 2007 | Issued |
Array
(
[id] => 251850
[patent_doc_number] => 07578480
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2009-08-25
[patent_title] => 'Reefing apparatus for controlling the inflation of a gliding wing parachute'
[patent_app_type] => utility
[patent_app_number] => 11/788431
[patent_app_country] => US
[patent_app_date] => 2007-04-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 5130
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 695
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/578/07578480.pdf
[firstpage_image] =>[orig_patent_app_number] => 11788431
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/788431 | Reefing apparatus for controlling the inflation of a gliding wing parachute | Apr 19, 2007 | Issued |
Array
(
[id] => 5208019
[patent_doc_number] => 20070246603
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-10-25
[patent_title] => 'Aeroengine mounting'
[patent_app_type] => utility
[patent_app_number] => 11/785826
[patent_app_country] => US
[patent_app_date] => 2007-04-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 3557
[patent_no_of_claims] => 21
[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/A1/0246/20070246603.pdf
[firstpage_image] =>[orig_patent_app_number] => 11785826
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/785826 | Aeroengine mounting | Apr 19, 2007 | Issued |
Array
(
[id] => 4638211
[patent_doc_number] => 08016236
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-09-13
[patent_title] => 'Method and apparatus for attaching a wing to a body'
[patent_app_type] => utility
[patent_app_number] => 11/696482
[patent_app_country] => US
[patent_app_date] => 2007-04-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 22
[patent_figures_cnt] => 28
[patent_no_of_words] => 6525
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 99
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/016/08016236.pdf
[firstpage_image] =>[orig_patent_app_number] => 11696482
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/696482 | Method and apparatus for attaching a wing to a body | Apr 3, 2007 | Issued |
Array
(
[id] => 9226371
[patent_doc_number] => 08632034
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-01-21
[patent_title] => 'Self-powered dimmable windows with integrated controls'
[patent_app_type] => utility
[patent_app_number] => 11/690316
[patent_app_country] => US
[patent_app_date] => 2007-03-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 20
[patent_no_of_words] => 5141
[patent_no_of_claims] => 24
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 125
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 11690316
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/690316 | Self-powered dimmable windows with integrated controls | Mar 22, 2007 | Issued |
Array
(
[id] => 5287913
[patent_doc_number] => 20090020643
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-01-22
[patent_title] => 'AIRCRAFT HAVING REDUCED ENVIRONMENTAL IMPACT'
[patent_app_type] => utility
[patent_app_number] => 12/162756
[patent_app_country] => US
[patent_app_date] => 2007-03-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2930
[patent_no_of_claims] => 11
[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/A1/0020/20090020643.pdf
[firstpage_image] =>[orig_patent_app_number] => 12162756
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/162756 | Aircraft having reduced environmental impact | Mar 14, 2007 | Issued |
Array
(
[id] => 4547914
[patent_doc_number] => 07841563
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-11-30
[patent_title] => 'Ducted fan air data system'
[patent_app_type] => utility
[patent_app_number] => 11/685532
[patent_app_country] => US
[patent_app_date] => 2007-03-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 5268
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 99
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/841/07841563.pdf
[firstpage_image] =>[orig_patent_app_number] => 11685532
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/685532 | Ducted fan air data system | Mar 12, 2007 | Issued |
Array
(
[id] => 4695282
[patent_doc_number] => 20080217466
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-09-11
[patent_title] => 'AUXILIARY ON BOARD POWER SYSTEM FOR AN AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 11/683711
[patent_app_country] => US
[patent_app_date] => 2007-03-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 3481
[patent_no_of_claims] => 15
[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/A1/0217/20080217466.pdf
[firstpage_image] =>[orig_patent_app_number] => 11683711
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/683711 | AUXILIARY ON BOARD POWER SYSTEM FOR AN AIRCRAFT | Mar 7, 2007 | Abandoned |
Array
(
[id] => 4723683
[patent_doc_number] => 20080203224
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-08-28
[patent_title] => 'Load optimized redundant flight control surface actuation system and method'
[patent_app_type] => utility
[patent_app_number] => 11/711295
[patent_app_country] => US
[patent_app_date] => 2007-02-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 5578
[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/A1/0203/20080203224.pdf
[firstpage_image] =>[orig_patent_app_number] => 11711295
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/711295 | Load optimized redundant flight control surface actuation system and method | Feb 26, 2007 | Issued |
Array
(
[id] => 4723692
[patent_doc_number] => 20080203233
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-08-28
[patent_title] => 'Flueted aircraft wing'
[patent_app_type] => utility
[patent_app_number] => 11/709674
[patent_app_country] => US
[patent_app_date] => 2007-02-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 770
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 1
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0203/20080203233.pdf
[firstpage_image] =>[orig_patent_app_number] => 11709674
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/709674 | Flueted aircraft wing | Feb 22, 2007 | Abandoned |
Array
(
[id] => 5001624
[patent_doc_number] => 20070199188
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-08-30
[patent_title] => 'Door pod assembly'
[patent_app_type] => utility
[patent_app_number] => 11/710037
[patent_app_country] => US
[patent_app_date] => 2007-02-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
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[patent_no_of_words] => 3507
[patent_no_of_claims] => 19
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0199/20070199188.pdf
[firstpage_image] =>[orig_patent_app_number] => 11710037
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/710037 | Door pod assembly | Feb 21, 2007 | Issued |
Array
(
[id] => 4870501
[patent_doc_number] => 20080197235
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-08-21
[patent_title] => 'Technique for preventing the thermal insulating foam falling off the space shuttle and its external tank (ET)'
[patent_app_type] => utility
[patent_app_number] => 11/706162
[patent_app_country] => US
[patent_app_date] => 2007-02-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[patent_no_of_words] => 2236
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0197/20080197235.pdf
[firstpage_image] =>[orig_patent_app_number] => 11706162
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/706162 | Technique for preventing the thermal insulating foam falling off the space shuttle and its external tank (ET) | Feb 14, 2007 | Abandoned |
Array
(
[id] => 4951882
[patent_doc_number] => 20080184906
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-08-07
[patent_title] => 'Long range hybrid electric airplane'
[patent_app_type] => utility
[patent_app_number] => 11/703362
[patent_app_country] => US
[patent_app_date] => 2007-02-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
[patent_figures_cnt] => 13
[patent_no_of_words] => 4281
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 6
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0184/20080184906.pdf
[firstpage_image] =>[orig_patent_app_number] => 11703362
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/703362 | Long range hybrid electric airplane | Feb 6, 2007 | Abandoned |