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] => 5098484
[patent_doc_number] => 20070181744
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-08-09
[patent_title] => 'Rotorcraft skid undercarriage and a rotorcraft including such an undercarriage'
[patent_app_type] => utility
[patent_app_number] => 11/644844
[patent_app_country] => US
[patent_app_date] => 2006-12-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 3770
[patent_no_of_claims] => 17
[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/A1/0181/20070181744.pdf
[firstpage_image] =>[orig_patent_app_number] => 11644844
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/644844 | Rotorcraft skid undercarriage and a rotorcraft including such an undercarriage | Dec 25, 2006 | Issued |
Array
(
[id] => 139591
[patent_doc_number] => 07686247
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2010-03-30
[patent_title] => 'Vehicle recovery'
[patent_app_type] => utility
[patent_app_number] => 11/644141
[patent_app_country] => US
[patent_app_date] => 2006-12-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 12
[patent_no_of_words] => 7601
[patent_no_of_claims] => 21
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 145
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/686/07686247.pdf
[firstpage_image] =>[orig_patent_app_number] => 11644141
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/644141 | Vehicle recovery | Dec 21, 2006 | Issued |
Array
(
[id] => 8256361
[patent_doc_number] => 08205833
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-06-26
[patent_title] => 'Composite leg structure for a lightweight aircraft seat assembly'
[patent_app_type] => utility
[patent_app_number] => 11/614978
[patent_app_country] => US
[patent_app_date] => 2006-12-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 24
[patent_figures_cnt] => 31
[patent_no_of_words] => 13474
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 215
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 11614978
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/614978 | Composite leg structure for a lightweight aircraft seat assembly | Dec 21, 2006 | Issued |
Array
(
[id] => 8338694
[patent_doc_number] => 08240614
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-08-14
[patent_title] => 'Elastomer-based modular multi-axis vibration/shock isolation device'
[patent_app_type] => utility
[patent_app_number] => 12/158083
[patent_app_country] => US
[patent_app_date] => 2006-12-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 17
[patent_no_of_words] => 11028
[patent_no_of_claims] => 36
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 213
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12158083
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/158083 | Elastomer-based modular multi-axis vibration/shock isolation device | Dec 20, 2006 | Issued |
Array
(
[id] => 7709193
[patent_doc_number] => 08091828
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-01-10
[patent_title] => 'Structural element and method of manufacture'
[patent_app_type] => utility
[patent_app_number] => 12/093151
[patent_app_country] => US
[patent_app_date] => 2006-12-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 13
[patent_no_of_words] => 5955
[patent_no_of_claims] => 30
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 284
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/091/08091828.pdf
[firstpage_image] =>[orig_patent_app_number] => 12093151
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/093151 | Structural element and method of manufacture | Dec 14, 2006 | Issued |
Array
(
[id] => 4544901
[patent_doc_number] => 07837153
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-11-23
[patent_title] => 'Local observable area and self inspection system'
[patent_app_type] => utility
[patent_app_number] => 11/638021
[patent_app_country] => US
[patent_app_date] => 2006-12-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 10
[patent_no_of_words] => 3707
[patent_no_of_claims] => 21
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 92
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/837/07837153.pdf
[firstpage_image] =>[orig_patent_app_number] => 11638021
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/638021 | Local observable area and self inspection system | Dec 12, 2006 | Issued |
Array
(
[id] => 183419
[patent_doc_number] => 07648103
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-01-19
[patent_title] => 'Aircraft fuel tanks, systems and methods for increasing an aircraft\'s on-board fuel capacity'
[patent_app_type] => utility
[patent_app_number] => 11/637922
[patent_app_country] => US
[patent_app_date] => 2006-12-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 11
[patent_no_of_words] => 7701
[patent_no_of_claims] => 32
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 362
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/648/07648103.pdf
[firstpage_image] =>[orig_patent_app_number] => 11637922
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/637922 | Aircraft fuel tanks, systems and methods for increasing an aircraft's on-board fuel capacity | Dec 12, 2006 | Issued |
Array
(
[id] => 100140
[patent_doc_number] => 07721995
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-05-25
[patent_title] => 'Rib support for wing panels'
[patent_app_type] => utility
[patent_app_number] => 11/610444
[patent_app_country] => US
[patent_app_date] => 2006-12-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 1148
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 131
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/721/07721995.pdf
[firstpage_image] =>[orig_patent_app_number] => 11610444
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/610444 | Rib support for wing panels | Dec 12, 2006 | Issued |
Array
(
[id] => 6541718
[patent_doc_number] => 20100044518
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-02-25
[patent_title] => 'METHOD AND DEVICE FOR PROVIDING AUTOMATIC LOAD ALLEVIATION TO A HIGH LIFT SURFACE SYSTEM, IN PARTICULAR TO A LANDING FLAP SYSTEM, OF AN AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 12/086467
[patent_app_country] => US
[patent_app_date] => 2006-12-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 4505
[patent_no_of_claims] => 22
[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/A1/0044/20100044518.pdf
[firstpage_image] =>[orig_patent_app_number] => 12086467
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/086467 | Method and device for providing automatic load alleviation to a high lift surface system, in particular to a landing flap system, of an aircraft | Dec 7, 2006 | Issued |
Array
(
[id] => 6541718
[patent_doc_number] => 20100044518
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-02-25
[patent_title] => 'METHOD AND DEVICE FOR PROVIDING AUTOMATIC LOAD ALLEVIATION TO A HIGH LIFT SURFACE SYSTEM, IN PARTICULAR TO A LANDING FLAP SYSTEM, OF AN AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 12/086467
[patent_app_country] => US
[patent_app_date] => 2006-12-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 4505
[patent_no_of_claims] => 22
[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/A1/0044/20100044518.pdf
[firstpage_image] =>[orig_patent_app_number] => 12086467
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/086467 | Method and device for providing automatic load alleviation to a high lift surface system, in particular to a landing flap system, of an aircraft | Dec 7, 2006 | Issued |
Array
(
[id] => 4782357
[patent_doc_number] => 20080135686
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-06-12
[patent_title] => 'METHOD AND SYSTEM FOR SPACECRAFT POWER ACQUISITION USING SINGLE-AXIS SLIT SUN SENSOR'
[patent_app_type] => utility
[patent_app_number] => 11/608140
[patent_app_country] => US
[patent_app_date] => 2006-12-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 4102
[patent_no_of_claims] => 21
[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/A1/0135/20080135686.pdf
[firstpage_image] =>[orig_patent_app_number] => 11608140
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/608140 | Method and system for spacecraft power acquisition using single-axis slit sun sensor | Dec 6, 2006 | Issued |
Array
(
[id] => 4782356
[patent_doc_number] => 20080135685
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-06-12
[patent_title] => 'POWER OPTIMIZED SYSTEM FOR ELECTRIC PROPULSION STATIONKEEPING GEOSYNCHRONOUS SPACECRAFT'
[patent_app_type] => utility
[patent_app_number] => 11/608229
[patent_app_country] => US
[patent_app_date] => 2006-12-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 3867
[patent_no_of_claims] => 21
[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/A1/0135/20080135685.pdf
[firstpage_image] =>[orig_patent_app_number] => 11608229
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/608229 | Power optimized system for electric propulsion stationkeeping geosynchronous spacecraft | Dec 6, 2006 | Issued |
Array
(
[id] => 4782358
[patent_doc_number] => 20080135687
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-06-12
[patent_title] => 'UNIVERSAL LAUNCH VEHICLE PAYLOAD ADAPTER'
[patent_app_type] => utility
[patent_app_number] => 11/608231
[patent_app_country] => US
[patent_app_date] => 2006-12-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 11
[patent_no_of_words] => 3174
[patent_no_of_claims] => 21
[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/A1/0135/20080135687.pdf
[firstpage_image] =>[orig_patent_app_number] => 11608231
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/608231 | Universal launch vehicle payload adapter | Dec 6, 2006 | Issued |
Array
(
[id] => 5123322
[patent_doc_number] => 20070235592
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-10-11
[patent_title] => 'Minimum time or thrust separation trajectory for spacecraft emergency separation'
[patent_app_type] => utility
[patent_app_number] => 11/633910
[patent_app_country] => US
[patent_app_date] => 2006-12-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 4582
[patent_no_of_claims] => 25
[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/A1/0235/20070235592.pdf
[firstpage_image] =>[orig_patent_app_number] => 11633910
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/633910 | Minimum time or thrust separation trajectory for spacecraft emergency separation | Dec 4, 2006 | Abandoned |
Array
(
[id] => 5268314
[patent_doc_number] => 20090072089
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-03-19
[patent_title] => 'AIRCRAFT DOOR ASSEMBLY, AND AIRCRAFT FUSELAGE COMPRISING SUCH AN AIRCRAFT DOOR ASSEMBLY'
[patent_app_type] => utility
[patent_app_number] => 12/158317
[patent_app_country] => US
[patent_app_date] => 2006-12-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 6109
[patent_no_of_claims] => 25
[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/A1/0072/20090072089.pdf
[firstpage_image] =>[orig_patent_app_number] => 12158317
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/158317 | Aircraft door assembly, and aircraft fuselage comprising such an aircraft door assembly | Dec 1, 2006 | Issued |
Array
(
[id] => 8651791
[patent_doc_number] => 08371533
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-02-12
[patent_title] => 'Aircraft auxiliary fuel tank system and method'
[patent_app_type] => utility
[patent_app_number] => 12/158061
[patent_app_country] => US
[patent_app_date] => 2006-12-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 5097
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 5
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12158061
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/158061 | Aircraft auxiliary fuel tank system and method | Nov 30, 2006 | Issued |
Array
(
[id] => 5002467
[patent_doc_number] => 20070200032
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-08-30
[patent_title] => 'RADIO FREQUENCY EMITTING HOOK SYSTEM FOR A ROTARY-WING AIRCRAFT EXTERNAL LOAD HANDLING'
[patent_app_type] => utility
[patent_app_number] => 11/565697
[patent_app_country] => US
[patent_app_date] => 2006-12-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 2964
[patent_no_of_claims] => 24
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0200/20070200032.pdf
[firstpage_image] =>[orig_patent_app_number] => 11565697
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/565697 | RADIO FREQUENCY EMITTING HOOK SYSTEM FOR A ROTARY-WING AIRCRAFT EXTERNAL LOAD HANDLING | Nov 30, 2006 | Abandoned |
Array
(
[id] => 4828839
[patent_doc_number] => 20080128554
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-06-05
[patent_title] => 'COMPOSITE SHEAR TIE'
[patent_app_type] => utility
[patent_app_number] => 11/564964
[patent_app_country] => US
[patent_app_date] => 2006-11-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 12
[patent_no_of_words] => 4933
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0128/20080128554.pdf
[firstpage_image] =>[orig_patent_app_number] => 11564964
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/564964 | Composite shear tie | Nov 29, 2006 | Issued |
Array
(
[id] => 4775667
[patent_doc_number] => 20080283665
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-11-20
[patent_title] => 'Aircraft Ventral Fairing Partition Wall and Aircraft Equipped with a Ventral Fairing'
[patent_app_type] => utility
[patent_app_number] => 12/096459
[patent_app_country] => US
[patent_app_date] => 2006-11-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 4955
[patent_no_of_claims] => 10
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0283/20080283665.pdf
[firstpage_image] =>[orig_patent_app_number] => 12096459
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/096459 | Aircraft ventral fairing partition wall and aircraft equipped with a ventral fairing | Nov 22, 2006 | Issued |
Array
(
[id] => 4896708
[patent_doc_number] => 20080116321
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-05-22
[patent_title] => 'Lift spoiler for parked aircraft'
[patent_app_type] => utility
[patent_app_number] => 11/602592
[patent_app_country] => US
[patent_app_date] => 2006-11-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2580
[patent_no_of_claims] => 8
[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/A1/0116/20080116321.pdf
[firstpage_image] =>[orig_patent_app_number] => 11602592
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/602592 | Lift spoiler for parked aircraft | Nov 21, 2006 | Abandoned |