
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] => 4941562
[patent_doc_number] => 20080078885
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-04-03
[patent_title] => 'Canted solar array and method for using same'
[patent_app_type] => utility
[patent_app_number] => 11/521672
[patent_app_country] => US
[patent_app_date] => 2006-09-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
[patent_figures_cnt] => 13
[patent_no_of_words] => 3498
[patent_no_of_claims] => 19
[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/A1/0078/20080078885.pdf
[firstpage_image] =>[orig_patent_app_number] => 11521672
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/521672 | Canted solar array and method for using same | Sep 14, 2006 | Issued |
Array
(
[id] => 5419543
[patent_doc_number] => 20090145997
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-06-11
[patent_title] => 'INTEGRAL POWERED WING AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 11/521597
[patent_app_country] => US
[patent_app_date] => 2006-09-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 12
[patent_no_of_words] => 4088
[patent_no_of_claims] => 12
[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/A1/0145/20090145997.pdf
[firstpage_image] =>[orig_patent_app_number] => 11521597
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/521597 | Integral powered wing aircraft | Sep 13, 2006 | Issued |
Array
(
[id] => 7701858
[patent_doc_number] => 08087608
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-01-03
[patent_title] => 'System for connecting a crossbar to an aircraft engine pylon'
[patent_app_type] => utility
[patent_app_number] => 12/064916
[patent_app_country] => US
[patent_app_date] => 2006-08-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 12
[patent_no_of_words] => 6594
[patent_no_of_claims] => 21
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 239
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/087/08087608.pdf
[firstpage_image] =>[orig_patent_app_number] => 12064916
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/064916 | System for connecting a crossbar to an aircraft engine pylon | Aug 30, 2006 | Issued |
Array
(
[id] => 5578492
[patent_doc_number] => 20090173838
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-07-09
[patent_title] => 'Narrow Wing System for Airplanes'
[patent_app_type] => utility
[patent_app_number] => 11/464679
[patent_app_country] => US
[patent_app_date] => 2006-08-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 472
[patent_no_of_claims] => 18
[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/A1/0173/20090173838.pdf
[firstpage_image] =>[orig_patent_app_number] => 11464679
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/464679 | Narrow Wing System for Airplanes | Aug 14, 2006 | Abandoned |
Array
(
[id] => 1981
[patent_doc_number] => 07815143
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-10-19
[patent_title] => 'Aircraft landing gear truck orientation for noise reduction'
[patent_app_type] => utility
[patent_app_number] => 11/464105
[patent_app_country] => US
[patent_app_date] => 2006-08-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 22
[patent_no_of_words] => 5197
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 168
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/815/07815143.pdf
[firstpage_image] =>[orig_patent_app_number] => 11464105
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/464105 | Aircraft landing gear truck orientation for noise reduction | Aug 10, 2006 | Issued |
Array
(
[id] => 4648532
[patent_doc_number] => 20080035787
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-02-14
[patent_title] => 'Lighter-than-air gas handling system and method'
[patent_app_type] => utility
[patent_app_number] => 11/501608
[patent_app_country] => US
[patent_app_date] => 2006-08-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 8138
[patent_no_of_claims] => 40
[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/A1/0035/20080035787.pdf
[firstpage_image] =>[orig_patent_app_number] => 11501608
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/501608 | Lighter-than-air gas handling system and method | Aug 7, 2006 | Abandoned |
Array
(
[id] => 7737223
[patent_doc_number] => 08104711
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-01-31
[patent_title] => 'Landing gear'
[patent_app_type] => utility
[patent_app_number] => 11/997720
[patent_app_country] => US
[patent_app_date] => 2006-08-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 21
[patent_figures_cnt] => 22
[patent_no_of_words] => 7672
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 417
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/104/08104711.pdf
[firstpage_image] =>[orig_patent_app_number] => 11997720
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/997720 | Landing gear | Aug 3, 2006 | Issued |
Array
(
[id] => 4695283
[patent_doc_number] => 20080217467
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-09-11
[patent_title] => 'Assembly For Aircraft Comprising a Wing System Element as Well as an Attachment Mast'
[patent_app_type] => utility
[patent_app_number] => 11/995110
[patent_app_country] => US
[patent_app_date] => 2006-07-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 4710
[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/A1/0217/20080217467.pdf
[firstpage_image] =>[orig_patent_app_number] => 11995110
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/995110 | Assembly for aircraft comprising a wing system element as well as an attachment mast | Jul 27, 2006 | Issued |
Array
(
[id] => 4906985
[patent_doc_number] => 20080017751
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-01-24
[patent_title] => 'Recipfan plane'
[patent_app_type] => utility
[patent_app_number] => 11/489205
[patent_app_country] => US
[patent_app_date] => 2006-07-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 1220
[patent_no_of_claims] => 9
[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/A1/0017/20080017751.pdf
[firstpage_image] =>[orig_patent_app_number] => 11489205
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/489205 | Recipfan plane | Jul 18, 2006 | Abandoned |
Array
(
[id] => 4802500
[patent_doc_number] => 20080014087
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-01-17
[patent_title] => 'Tail rotor for remotely controlled toy helicopter'
[patent_app_type] => utility
[patent_app_number] => 11/487493
[patent_app_country] => US
[patent_app_date] => 2006-07-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 1359
[patent_no_of_claims] => 1
[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/A1/0014/20080014087.pdf
[firstpage_image] =>[orig_patent_app_number] => 11487493
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/487493 | Tail rotor for remotely controlled toy helicopter | Jul 16, 2006 | Abandoned |
Array
(
[id] => 183681
[patent_doc_number] => 07644892
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2010-01-12
[patent_title] => 'Blended winglet'
[patent_app_type] => utility
[patent_app_number] => 11/481571
[patent_app_country] => US
[patent_app_date] => 2006-07-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 10
[patent_no_of_words] => 4019
[patent_no_of_claims] => 34
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 78
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/644/07644892.pdf
[firstpage_image] =>[orig_patent_app_number] => 11481571
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/481571 | Blended winglet | Jul 5, 2006 | Issued |
Array
(
[id] => 4457117
[patent_doc_number] => 07878457
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-02-01
[patent_title] => 'Retractable vortex generator'
[patent_app_type] => utility
[patent_app_number] => 11/477806
[patent_app_country] => US
[patent_app_date] => 2006-06-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 9
[patent_no_of_words] => 1995
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 178
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/878/07878457.pdf
[firstpage_image] =>[orig_patent_app_number] => 11477806
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/477806 | Retractable vortex generator | Jun 29, 2006 | Issued |
Array
(
[id] => 7974695
[patent_doc_number] => 08070093
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-12-06
[patent_title] => 'Turbojet engine mounting structure for aircraft'
[patent_app_type] => utility
[patent_app_number] => 12/089058
[patent_app_country] => US
[patent_app_date] => 2006-06-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 12
[patent_no_of_words] => 9156
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 127
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/070/08070093.pdf
[firstpage_image] =>[orig_patent_app_number] => 12089058
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/089058 | Turbojet engine mounting structure for aircraft | Jun 28, 2006 | Issued |
Array
(
[id] => 202729
[patent_doc_number] => 07628356
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2009-12-08
[patent_title] => 'Yaw control device for a nozzle having a rectangular outlet section'
[patent_app_type] => utility
[patent_app_number] => 11/476310
[patent_app_country] => US
[patent_app_date] => 2006-06-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 8
[patent_no_of_words] => 2644
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 146
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/628/07628356.pdf
[firstpage_image] =>[orig_patent_app_number] => 11476310
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/476310 | Yaw control device for a nozzle having a rectangular outlet section | Jun 27, 2006 | Issued |
Array
(
[id] => 4870499
[patent_doc_number] => 20080197233
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-08-21
[patent_title] => 'Engine Mounting Structure For an Aircraft'
[patent_app_type] => utility
[patent_app_number] => 11/914560
[patent_app_country] => US
[patent_app_date] => 2006-06-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 4954
[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/A1/0197/20080197233.pdf
[firstpage_image] =>[orig_patent_app_number] => 11914560
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/914560 | Engine mounting structure for an aircraft | Jun 26, 2006 | Issued |
Array
(
[id] => 5196546
[patent_doc_number] => 20070295864
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-12-27
[patent_title] => 'Heili-kite, having an cambered streamedline airfoil inflated keel, filled with air or lighter than air substance, with a streamlined airfoil inflated keel, wing, nose, and tail uni-body, pleated stealth like shaped wings, with a bats wing shaped trailing edge and a curved downward cambered airfoil tail design'
[patent_app_type] => utility
[patent_app_number] => 11/475408
[patent_app_country] => US
[patent_app_date] => 2006-06-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 4135
[patent_no_of_claims] => 32
[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/A1/0295/20070295864.pdf
[firstpage_image] =>[orig_patent_app_number] => 11475408
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/475408 | Heili-kite, having an cambered streamedline airfoil inflated keel, filled with air or lighter than air substance, with a streamlined airfoil inflated keel, wing, nose, and tail uni-body, pleated stealth like shaped wings, with a bats wing shaped trailing edge and a curved downward cambered airfoil tail design | Jun 26, 2006 | Abandoned |
Array
(
[id] => 4436085
[patent_doc_number] => 07926761
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-04-19
[patent_title] => 'Mechanical part and method of manufacturing such a part'
[patent_app_type] => utility
[patent_app_number] => 11/425082
[patent_app_country] => US
[patent_app_date] => 2006-06-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 20
[patent_no_of_words] => 3989
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 224
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/926/07926761.pdf
[firstpage_image] =>[orig_patent_app_number] => 11425082
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/425082 | Mechanical part and method of manufacturing such a part | Jun 18, 2006 | Issued |
Array
(
[id] => 183420
[patent_doc_number] => 07648104
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2010-01-19
[patent_title] => 'Store ejector rack'
[patent_app_type] => utility
[patent_app_number] => 11/453413
[patent_app_country] => US
[patent_app_date] => 2006-06-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
[patent_figures_cnt] => 13
[patent_no_of_words] => 3349
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/648/07648104.pdf
[firstpage_image] =>[orig_patent_app_number] => 11453413
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/453413 | Store ejector rack | Jun 14, 2006 | Issued |
Array
(
[id] => 5685689
[patent_doc_number] => 20060284004
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-12-21
[patent_title] => 'Method of scavenging atmospheric energy, causing rainfall, and for dissipating severe weather formations using an electrostatic dirigible'
[patent_app_type] => utility
[patent_app_number] => 11/453274
[patent_app_country] => US
[patent_app_date] => 2006-06-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 1809
[patent_no_of_claims] => 4
[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/A1/0284/20060284004.pdf
[firstpage_image] =>[orig_patent_app_number] => 11453274
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/453274 | Method of scavenging atmospheric energy, causing rainfall, and for dissipating severe weather formations using an electrostatic dirigible | Jun 13, 2006 | Abandoned |
Array
(
[id] => 5133009
[patent_doc_number] => 20070074636
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-04-05
[patent_title] => 'Jettisonable nosecone and missile with a jettisonable nosecone'
[patent_app_type] => utility
[patent_app_number] => 11/438825
[patent_app_country] => US
[patent_app_date] => 2006-05-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 4378
[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/A1/0074/20070074636.pdf
[firstpage_image] =>[orig_patent_app_number] => 11438825
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/438825 | Jettisonable nosecone and missile with a jettisonable nosecone | May 22, 2006 | Issued |