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] => 9445989 [patent_doc_number] => 20140117157 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-05-01 [patent_title] => 'Circumference Splice for Joining Shell Structures' [patent_app_type] => utility [patent_app_number] => 13/665664 [patent_app_country] => US [patent_app_date] => 2012-10-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 11 [patent_no_of_words] => 5339 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13665664 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/665664
Circumference splice for joining shell structures Oct 30, 2012 Issued
Array ( [id] => 9445985 [patent_doc_number] => 20140117153 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-05-01 [patent_title] => 'SYSTEMS AND METHODS TO LAUNCH AIRCRAFT' [patent_app_type] => utility [patent_app_number] => 13/662269 [patent_app_country] => US [patent_app_date] => 2012-10-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 1668 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13662269 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/662269
Systems and methods to launch aircraft Oct 25, 2012 Issued
Array ( [id] => 10607805 [patent_doc_number] => 09327826 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2016-05-03 [patent_title] => 'Self-centering aircraft flap position command apparatus' [patent_app_type] => utility [patent_app_number] => 13/660729 [patent_app_country] => US [patent_app_date] => 2012-10-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 3056 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 183 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13660729 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/660729
Self-centering aircraft flap position command apparatus Oct 24, 2012 Issued
Array ( [id] => 9334592 [patent_doc_number] => 20140061374 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-03-06 [patent_title] => 'METHOD FOR INCREASING LANDING GEAR EFFECTIVE LIFE AND AIRCRAFT LANDING CYCLES' [patent_app_type] => utility [patent_app_number] => 13/659893 [patent_app_country] => US [patent_app_date] => 2012-10-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 5341 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 8 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13659893 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/659893
METHOD FOR INCREASING LANDING GEAR EFFECTIVE LIFE AND AIRCRAFT LANDING CYCLES Oct 23, 2012 Abandoned
Array ( [id] => 8788665 [patent_doc_number] => 20130105634 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-05-02 [patent_title] => 'COMPACT TWO AXIS GIMBAL FOR CONTROL STICK' [patent_app_type] => utility [patent_app_number] => 13/657294 [patent_app_country] => US [patent_app_date] => 2012-10-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 5300 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13657294 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/657294
Compact two axis gimbal for control stick Oct 21, 2012 Issued
Array ( [id] => 8788656 [patent_doc_number] => 20130105625 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-05-02 [patent_title] => 'AIRCRAFT PROVIDED WITH A BUOYANCY SYSTEM FOR A ROTARY ELEMENT' [patent_app_type] => utility [patent_app_number] => 13/654576 [patent_app_country] => US [patent_app_date] => 2012-10-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 2785 [patent_no_of_claims] => 6 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13654576 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/654576
Aircraft provided with a buoyancy system for a rotary element Oct 17, 2012 Issued
Array ( [id] => 9418509 [patent_doc_number] => 20140103159 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-04-17 [patent_title] => 'Tunnel wing system for lift, altitude flight, and ground effect flight' [patent_app_type] => utility [patent_app_number] => 13/654371 [patent_app_country] => US [patent_app_date] => 2012-10-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 443 [patent_no_of_claims] => 11 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13654371 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/654371
Tunnel wing system for lift, altitude flight, and ground effect flight Oct 16, 2012 Abandoned
Array ( [id] => 8850730 [patent_doc_number] => 20130140405 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-06-06 [patent_title] => 'Integral Powered Wing Aircraft Utilizing Full Rotary Disc Stacking With Aeronautical Enhancements' [patent_app_type] => utility [patent_app_number] => 13/650576 [patent_app_country] => US [patent_app_date] => 2012-10-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 11 [patent_no_of_words] => 4665 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13650576 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/650576
Integral Powered Wing Aircraft Utilizing Full Rotary Disc Stacking With Aeronautical Enhancements Oct 11, 2012 Abandoned
Array ( [id] => 9406041 [patent_doc_number] => 20140097293 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-04-10 [patent_title] => 'Airplane Shock Absorbing Suspension' [patent_app_type] => utility [patent_app_number] => 13/649086 [patent_app_country] => US [patent_app_date] => 2012-10-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 16 [patent_figures_cnt] => 16 [patent_no_of_words] => 1390 [patent_no_of_claims] => 7 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13649086 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/649086
Airplane Shock Absorbing Suspension Oct 9, 2012 Abandoned
Array ( [id] => 9188581 [patent_doc_number] => 20130327896 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-12-12 [patent_title] => 'ROTORCRAFT YAW PILOTING SYSTEM MAKING USE OF A MEMBER OF THE HUMAN-OPERATED TYPE AND OF A FLIGHT CONTROL GENERATOR FO THE OBJECTIVE TYPE' [patent_app_type] => utility [patent_app_number] => 13/647508 [patent_app_country] => US [patent_app_date] => 2012-10-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 6580 [patent_no_of_claims] => 12 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13647508 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/647508
Rotorcraft yaw piloting system making use of a member of the human-operated type and of a flight control generator of the objective type Oct 8, 2012 Issued
Array ( [id] => 10499331 [patent_doc_number] => 09227721 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2016-01-05 [patent_title] => 'Variable camber continuous aerodynamic control surfaces and methods for active wing shaping control' [patent_app_type] => utility [patent_app_number] => 13/648197 [patent_app_country] => US [patent_app_date] => 2012-10-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 39 [patent_figures_cnt] => 40 [patent_no_of_words] => 21908 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 179 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13648197 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/648197
Variable camber continuous aerodynamic control surfaces and methods for active wing shaping control Oct 8, 2012 Issued
Array ( [id] => 9709139 [patent_doc_number] => 08833696 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2014-09-16 [patent_title] => 'Balloon envelope adapted to direct sunlight towards payload' [patent_app_type] => utility [patent_app_number] => 13/631057 [patent_app_country] => US [patent_app_date] => 2012-09-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 10 [patent_no_of_words] => 11967 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 47 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13631057 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/631057
Balloon envelope adapted to direct sunlight towards payload Sep 27, 2012 Issued
Array ( [id] => 10083235 [patent_doc_number] => 09120573 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2015-09-01 [patent_title] => 'Sanitary module arrangement for installation in an aircraft cabin' [patent_app_type] => utility [patent_app_number] => 13/627759 [patent_app_country] => US [patent_app_date] => 2012-09-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 16 [patent_no_of_words] => 8224 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 257 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13627759 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/627759
Sanitary module arrangement for installation in an aircraft cabin Sep 25, 2012 Issued
Array ( [id] => 10614616 [patent_doc_number] => 09334046 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2016-05-10 [patent_title] => 'Device for maneuvering, on the ground, a door of an aircraft landing gear' [patent_app_type] => utility [patent_app_number] => 13/624181 [patent_app_country] => US [patent_app_date] => 2012-09-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 4 [patent_no_of_words] => 2208 [patent_no_of_claims] => 7 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 178 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13624181 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/624181
Device for maneuvering, on the ground, a door of an aircraft landing gear Sep 20, 2012 Issued
Array ( [id] => 9025034 [patent_doc_number] => 08534608 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2013-09-17 [patent_title] => 'Aerial emergency load release mechanism' [patent_app_type] => utility [patent_app_number] => 13/602748 [patent_app_country] => US [patent_app_date] => 2012-09-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 3 [patent_no_of_words] => 1733 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 97 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13602748 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/602748
Aerial emergency load release mechanism Sep 3, 2012 Issued
Array ( [id] => 9982189 [patent_doc_number] => 09027886 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2015-05-12 [patent_title] => 'High altitude escape pod' [patent_app_type] => utility [patent_app_number] => 13/595373 [patent_app_country] => US [patent_app_date] => 2012-08-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 7 [patent_no_of_words] => 4404 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 159 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13595373 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/595373
High altitude escape pod Aug 26, 2012 Issued
Array ( [id] => 10573867 [patent_doc_number] => 09296494 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2016-03-29 [patent_title] => 'Thruster orbit control method and configuration' [patent_app_type] => utility [patent_app_number] => 13/572586 [patent_app_country] => US [patent_app_date] => 2012-08-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 10 [patent_no_of_words] => 4264 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 152 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13572586 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/572586
Thruster orbit control method and configuration Aug 9, 2012 Issued
Array ( [id] => 10115435 [patent_doc_number] => 09150303 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2015-10-06 [patent_title] => 'Control quadrant' [patent_app_type] => utility [patent_app_number] => 13/571573 [patent_app_country] => US [patent_app_date] => 2012-08-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 14 [patent_figures_cnt] => 15 [patent_no_of_words] => 4278 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 97 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13571573 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/571573
Control quadrant Aug 9, 2012 Issued
Array ( [id] => 8680505 [patent_doc_number] => 20130048789 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-02-28 [patent_title] => 'AIRCRAFT STORE EJECTOR SYSTEM' [patent_app_type] => utility [patent_app_number] => 13/572504 [patent_app_country] => US [patent_app_date] => 2012-08-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 20 [patent_figures_cnt] => 20 [patent_no_of_words] => 15880 [patent_no_of_claims] => 42 [patent_no_of_ind_claims] => 34 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13572504 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/572504
Pitch control valve in an aircraft store ejector system Aug 9, 2012 Issued
Array ( [id] => 9303596 [patent_doc_number] => 20140042270 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-02-13 [patent_title] => 'STORAGE SYSTEM FOR STORING STATIC ELECTRICAL ENERGY IN ATMOSPHERE' [patent_app_type] => utility [patent_app_number] => 13/571105 [patent_app_country] => US [patent_app_date] => 2012-08-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 2224 [patent_no_of_claims] => 15 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13571105 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/571105
STORAGE SYSTEM FOR STORING STATIC ELECTRICAL ENERGY IN ATMOSPHERE Aug 8, 2012 Abandoned
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