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 number | Title of the application | Filing Date | Status |
---|---|---|---|
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
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[patent_no_of_words] => 7672
[patent_no_of_claims] => 18
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[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
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[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
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[patent_no_of_claims] => 9
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[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
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[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 |