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] => 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 |
Array
(
[id] => 4501911
[patent_doc_number] => 07971825
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-07-05
[patent_title] => 'Aircraft jet engine pylon suspension attachment'
[patent_app_type] => utility
[patent_app_number] => 11/915223
[patent_app_country] => US
[patent_app_date] => 2006-05-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 8
[patent_no_of_words] => 5483
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 153
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/971/07971825.pdf
[firstpage_image] =>[orig_patent_app_number] => 11915223
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/915223 | Aircraft jet engine pylon suspension attachment | May 21, 2006 | Issued |
Array
(
[id] => 4547901
[patent_doc_number] => 07841561
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-11-30
[patent_title] => 'Internal support structure for an airship'
[patent_app_type] => utility
[patent_app_number] => 11/383996
[patent_app_country] => US
[patent_app_date] => 2006-05-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 1
[patent_no_of_words] => 2673
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 343
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/841/07841561.pdf
[firstpage_image] =>[orig_patent_app_number] => 11383996
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/383996 | Internal support structure for an airship | May 17, 2006 | Issued |
Array
(
[id] => 5133554
[patent_doc_number] => 20070075183
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-04-05
[patent_title] => 'Wing arrangement as well as a missile'
[patent_app_type] => utility
[patent_app_number] => 11/434712
[patent_app_country] => US
[patent_app_date] => 2006-05-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2685
[patent_no_of_claims] => 10
[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/A1/0075/20070075183.pdf
[firstpage_image] =>[orig_patent_app_number] => 11434712
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/434712 | Wing arrangement as well as a missile | May 15, 2006 | Abandoned |
Array
(
[id] => 6602784
[patent_doc_number] => 20100171002
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-07-08
[patent_title] => 'METHOD FOR REDUCING THE TURBULENCE AND GUST INFLUENCES ON THE FLYING CHARACTERISTICS OF AIRCRAFT, AND A CONTROL DEVICE FOR THIS PURPOSE'
[patent_app_type] => utility
[patent_app_number] => 11/381192
[patent_app_country] => US
[patent_app_date] => 2006-05-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2756
[patent_no_of_claims] => 9
[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/A1/0171/20100171002.pdf
[firstpage_image] =>[orig_patent_app_number] => 11381192
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/381192 | Method for reducing the turbulence and gust influences on the flying characteristics of aircraft, and a control device for this purpose | May 1, 2006 | Issued |
Array
(
[id] => 8111989
[patent_doc_number] => 08157208
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-04-17
[patent_title] => 'Landing flap drive system'
[patent_app_type] => utility
[patent_app_number] => 11/911231
[patent_app_country] => US
[patent_app_date] => 2006-04-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 9
[patent_no_of_words] => 3126
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 277
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/157/08157208.pdf
[firstpage_image] =>[orig_patent_app_number] => 11911231
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/911231 | Landing flap drive system | Apr 11, 2006 | Issued |
Array
(
[id] => 355158
[patent_doc_number] => 07487937
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2009-02-10
[patent_title] => 'Airfoil for micro air vehicle'
[patent_app_type] => utility
[patent_app_number] => 11/394018
[patent_app_country] => US
[patent_app_date] => 2006-03-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 8
[patent_no_of_words] => 5301
[patent_no_of_claims] => 37
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 249
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/487/07487937.pdf
[firstpage_image] =>[orig_patent_app_number] => 11394018
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/394018 | Airfoil for micro air vehicle | Mar 29, 2006 | Issued |
Array
(
[id] => 5631235
[patent_doc_number] => 20060147704
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-07-06
[patent_title] => 'Method to eliminate undulations in a composite panel'
[patent_app_type] => utility
[patent_app_number] => 11/378791
[patent_app_country] => US
[patent_app_date] => 2006-03-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2530
[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/A1/0147/20060147704.pdf
[firstpage_image] =>[orig_patent_app_number] => 11378791
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/378791 | Aircraft structure including composite beam and composite panel with metal foil therebetween | Mar 15, 2006 | Issued |
Array
(
[id] => 4691077
[patent_doc_number] => 20080083847
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-04-10
[patent_title] => 'Air Locomotion Method and Multi-Purpose Aircraft Having Inflatable Wings(S) Using Two Different Inflating Systems'
[patent_app_type] => utility
[patent_app_number] => 11/813584
[patent_app_country] => US
[patent_app_date] => 2006-01-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
[patent_figures_cnt] => 13
[patent_no_of_words] => 9324
[patent_no_of_claims] => 15
[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/A1/0083/20080083847.pdf
[firstpage_image] =>[orig_patent_app_number] => 11813584
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/813584 | Air Locomotion Method and Multi-Purpose Aircraft Having Inflatable Wings(S) Using Two Different Inflating Systems | Jan 17, 2006 | Abandoned |
Array
(
[id] => 4506110
[patent_doc_number] => 07909287
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-03-22
[patent_title] => 'Super-transporter aircraft'
[patent_app_type] => utility
[patent_app_number] => 11/792759
[patent_app_country] => US
[patent_app_date] => 2005-11-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 10
[patent_no_of_words] => 4203
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 278
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/909/07909287.pdf
[firstpage_image] =>[orig_patent_app_number] => 11792759
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/792759 | Super-transporter aircraft | Nov 23, 2005 | Issued |
Array
(
[id] => 4843042
[patent_doc_number] => 20080179450
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-07-31
[patent_title] => 'Lifting-Type Aeroplane Fuselage'
[patent_app_type] => utility
[patent_app_number] => 11/791082
[patent_app_country] => US
[patent_app_date] => 2005-11-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2200
[patent_no_of_claims] => 4
[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/A1/0179/20080179450.pdf
[firstpage_image] =>[orig_patent_app_number] => 11791082
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/791082 | Lifting-Type Aeroplane Fuselage | Nov 17, 2005 | Abandoned |