Search

Minh Chau Thi Pham

Examiner (ID: 10502, Phone: (571)272-1163 , Office: P/1776 )

Most Active Art Unit
1776
Art Unit(s)
1773, 1724, 3621, 1776, 1305, 1797
Total Applications
2849
Issued Applications
2227
Pending Applications
153
Abandoned Applications
469

Applications

Application numberTitle of the applicationFiling DateStatus
Array ( [id] => 4707911 [patent_doc_number] => 20080296437 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-12-04 [patent_title] => 'Method and Device to Generate a Transverse Casimir Force for Propulsion, Guidance and Maneuvering of a Space Vehicle' [patent_app_type] => utility [patent_app_number] => 11/561839 [patent_app_country] => US [patent_app_date] => 2006-11-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 3868 [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/A1/0296/20080296437.pdf [firstpage_image] =>[orig_patent_app_number] => 11561839 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/561839
Method and Device to Generate a Transverse Casimir Force for Propulsion, Guidance and Maneuvering of a Space Vehicle Nov 19, 2006 Abandoned
Array ( [id] => 4962963 [patent_doc_number] => 20080105783 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-05-08 [patent_title] => 'Fuselage design for sonic boom suppression of supersonic aircraft' [patent_app_type] => utility [patent_app_number] => 11/592546 [patent_app_country] => US [patent_app_date] => 2006-11-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 11 [patent_no_of_words] => 3055 [patent_no_of_claims] => 10 [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/A1/0105/20080105783.pdf [firstpage_image] =>[orig_patent_app_number] => 11592546 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/592546
Fuselage design for sonic boom suppression of supersonic aircraft Nov 2, 2006 Abandoned
Array ( [id] => 4673189 [patent_doc_number] => 20080210817 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-09-04 [patent_title] => 'Energy-absorbing Square Tube Composite Stanchion' [patent_app_type] => utility [patent_app_number] => 11/553391 [patent_app_country] => US [patent_app_date] => 2006-10-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 1380 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 5 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0210/20080210817.pdf [firstpage_image] =>[orig_patent_app_number] => 11553391 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/553391
Energy-absorbing Square Tube Composite Stanchion Oct 25, 2006 Abandoned
Array ( [id] => 4890536 [patent_doc_number] => 20080099632 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-05-01 [patent_title] => 'Aircraft airframe architectures' [patent_app_type] => utility [patent_app_number] => 11/586175 [patent_app_country] => US [patent_app_date] => 2006-10-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 1957 [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/A1/0099/20080099632.pdf [firstpage_image] =>[orig_patent_app_number] => 11586175 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/586175
Aircraft airframe architectures Oct 24, 2006 Abandoned
Array ( [id] => 5092722 [patent_doc_number] => 20070114331 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-05-24 [patent_title] => 'Helicopter collapsible deck' [patent_app_type] => utility [patent_app_number] => 11/584463 [patent_app_country] => US [patent_app_date] => 2006-10-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 2935 [patent_no_of_claims] => 9 [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/A1/0114/20070114331.pdf [firstpage_image] =>[orig_patent_app_number] => 11584463 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/584463
Helicopter collapsible deck Oct 19, 2006 Issued
Array ( [id] => 4638220 [patent_doc_number] => 08016245 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2011-09-13 [patent_title] => 'Dynamic bumps for drag reduction at transonic-supersonic speeds' [patent_app_type] => utility [patent_app_number] => 11/583140 [patent_app_country] => US [patent_app_date] => 2006-10-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 15 [patent_no_of_words] => 5114 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 323 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/08/016/08016245.pdf [firstpage_image] =>[orig_patent_app_number] => 11583140 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/583140
Dynamic bumps for drag reduction at transonic-supersonic speeds Oct 17, 2006 Issued
Array ( [id] => 5116632 [patent_doc_number] => 20070138345 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-06-21 [patent_title] => 'Method and System For Aviation Navigation' [patent_app_type] => utility [patent_app_number] => 11/550391 [patent_app_country] => US [patent_app_date] => 2006-10-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 4824 [patent_no_of_claims] => 34 [patent_no_of_ind_claims] => 5 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0138/20070138345.pdf [firstpage_image] =>[orig_patent_app_number] => 11550391 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/550391
Method and system for aviation navigation Oct 16, 2006 Issued
Array ( [id] => 4531813 [patent_doc_number] => 07874513 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2011-01-25 [patent_title] => 'Apparatus and method for vertical take-off and landing aircraft' [patent_app_type] => utility [patent_app_number] => 11/581321 [patent_app_country] => US [patent_app_date] => 2006-10-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 11 [patent_no_of_words] => 8604 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 188 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/874/07874513.pdf [firstpage_image] =>[orig_patent_app_number] => 11581321 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/581321
Apparatus and method for vertical take-off and landing aircraft Oct 15, 2006 Issued
Array ( [id] => 4954761 [patent_doc_number] => 20080187785 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-08-07 [patent_title] => 'Fuel system for an aircraft including a fuel tank inerting system' [patent_app_type] => utility [patent_app_number] => 11/527009 [patent_app_country] => US [patent_app_date] => 2006-09-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 3006 [patent_no_of_claims] => 22 [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/A1/0187/20080187785.pdf [firstpage_image] =>[orig_patent_app_number] => 11527009 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/527009
Fuel system for an aircraft including a fuel tank inerting system Sep 25, 2006 Issued
Array ( [id] => 6310304 [patent_doc_number] => 20100193627 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-08-05 [patent_title] => 'ASSEMBLY FOR AN AIRCRAFT INCLUDING A WING ELEMENT AND A SUSPENSION PYLON' [patent_app_type] => utility [patent_app_number] => 11/525018 [patent_app_country] => US [patent_app_date] => 2006-09-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 2987 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 5 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0193/20100193627.pdf [firstpage_image] =>[orig_patent_app_number] => 11525018 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/525018
Assembly for an aircraft including a wing element and a suspension pylon Sep 21, 2006 Issued
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
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