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] => 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 [patent_words_short_claim] => 36 [patent_maintenance] => 1 [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 [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/A1/0200/20070200032.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 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_no_of_ind_claims] => 7 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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
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