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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 numberTitle of the applicationFiling DateStatus
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 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 181 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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
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