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] => 11218507 [patent_doc_number] => 09446834 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2016-09-20 [patent_title] => 'Self-stiffened skin for aircraft fuselage including stringers with a closed section and associated manufacturing method' [patent_app_type] => utility [patent_app_number] => 14/140513 [patent_app_country] => US [patent_app_date] => 2013-12-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 13 [patent_no_of_words] => 5280 [patent_no_of_claims] => 4 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 251 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14140513 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/140513
Self-stiffened skin for aircraft fuselage including stringers with a closed section and associated manufacturing method Dec 24, 2013 Issued
Array ( [id] => 9565586 [patent_doc_number] => 20140183299 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-07-03 [patent_title] => 'AN AIRCRAFT COMPRISING A COCKPIT DELOCALIZED OUTSIDED THE NOSE' [patent_app_type] => utility [patent_app_number] => 14/138417 [patent_app_country] => US [patent_app_date] => 2013-12-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 3294 [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] =>[firstpage_image] =>[orig_patent_app_number] => 14138417 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/138417
AN AIRCRAFT COMPRISING A COCKPIT DELOCALIZED OUTSIDED THE NOSE Dec 22, 2013 Abandoned
Array ( [id] => 10628390 [patent_doc_number] => 09346534 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2016-05-24 [patent_title] => 'Support assembly' [patent_app_type] => utility [patent_app_number] => 14/101791 [patent_app_country] => US [patent_app_date] => 2013-12-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 3194 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 199 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14101791 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/101791
Support assembly Dec 9, 2013 Issued
Array ( [id] => 10274590 [patent_doc_number] => 20150159587 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-06-11 [patent_title] => 'CLUSTER ROCKET MOTOR BOOSTERS' [patent_app_type] => utility [patent_app_number] => 14/100362 [patent_app_country] => US [patent_app_date] => 2013-12-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 11 [patent_no_of_words] => 5355 [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] => 14100362 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/100362
Cluster rocket motor boosters Dec 8, 2013 Issued
Array ( [id] => 10594180 [patent_doc_number] => 09315254 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2016-04-19 [patent_title] => 'Joint assembly and method of assembling same' [patent_app_type] => utility [patent_app_number] => 14/051926 [patent_app_country] => US [patent_app_date] => 2013-10-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 9 [patent_no_of_words] => 2831 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 109 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14051926 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/051926
Joint assembly and method of assembling same Oct 10, 2013 Issued
Array ( [id] => 10198879 [patent_doc_number] => 20150083865 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-03-26 [patent_title] => 'MULTIPLE SPACECRAFT LAUNCH SYSTEM' [patent_app_type] => utility [patent_app_number] => 14/034328 [patent_app_country] => US [patent_app_date] => 2013-09-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 2441 [patent_no_of_claims] => 20 [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] => 14034328 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/034328
MULTIPLE SPACECRAFT LAUNCH SYSTEM Sep 22, 2013 Abandoned
Array ( [id] => 10044974 [patent_doc_number] => 09085361 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2015-07-21 [patent_title] => 'Landing gear provided with a stiffener for increasing its stiffness in roll, and an aircraft' [patent_app_type] => utility [patent_app_number] => 14/033630 [patent_app_country] => US [patent_app_date] => 2013-09-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 12 [patent_no_of_words] => 4971 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 115 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14033630 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/033630
Landing gear provided with a stiffener for increasing its stiffness in roll, and an aircraft Sep 22, 2013 Issued
Array ( [id] => 9220004 [patent_doc_number] => 20140014779 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-01-16 [patent_title] => 'Direct Flight Far Space Shuttle' [patent_app_type] => utility [patent_app_number] => 14/026791 [patent_app_country] => US [patent_app_date] => 2013-09-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 18 [patent_figures_cnt] => 18 [patent_no_of_words] => 6432 [patent_no_of_claims] => 24 [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] => 14026791 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/026791
Direct Flight Far Space Shuttle Sep 12, 2013 Abandoned
Array ( [id] => 10361728 [patent_doc_number] => 20150246733 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-09-03 [patent_title] => 'DEVICE AND METHOD FOR SUPPLYING NON-PROPULSIVE POWER FOR AN AIRCRAFT' [patent_app_type] => utility [patent_app_number] => 14/427625 [patent_app_country] => US [patent_app_date] => 2013-09-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 4484 [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] =>[firstpage_image] =>[orig_patent_app_number] => 14427625 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/427625
DEVICE AND METHOD FOR SUPPLYING NON-PROPULSIVE POWER FOR AN AIRCRAFT Sep 9, 2013 Abandoned
Array ( [id] => 10340078 [patent_doc_number] => 20150225082 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-08-13 [patent_title] => 'CARGO HANDLING SYSTEM, METHOD AND APPARATUS' [patent_app_type] => utility [patent_app_number] => 14/430505 [patent_app_country] => US [patent_app_date] => 2013-09-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 21 [patent_figures_cnt] => 21 [patent_no_of_words] => 20447 [patent_no_of_claims] => 29 [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] => 14430505 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/430505
Cargo handling system, method and apparatus Sep 8, 2013 Issued
Array ( [id] => 9861574 [patent_doc_number] => 20150041591 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-02-12 [patent_title] => 'MULTIPURPOSE FLYING BOOM' [patent_app_type] => utility [patent_app_number] => 13/960614 [patent_app_country] => US [patent_app_date] => 2013-08-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 3504 [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] => 13960614 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/960614
Multipurpose flying boom Aug 5, 2013 Issued
Array ( [id] => 9343307 [patent_doc_number] => 08662445 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-03-04 [patent_title] => 'Hybrid power system architecture for an aircraft' [patent_app_type] => utility [patent_app_number] => 13/953164 [patent_app_country] => US [patent_app_date] => 2013-07-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 1 [patent_no_of_words] => 2609 [patent_no_of_claims] => 5 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13953164 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/953164
Hybrid power system architecture for an aircraft Jul 28, 2013 Issued
Array ( [id] => 9343301 [patent_doc_number] => 08662439 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-03-04 [patent_title] => 'System and method for limiting cyclic control inputs' [patent_app_type] => utility [patent_app_number] => 13/949814 [patent_app_country] => US [patent_app_date] => 2013-07-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 12 [patent_no_of_words] => 5051 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 121 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13949814 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/949814
System and method for limiting cyclic control inputs Jul 23, 2013 Issued
Array ( [id] => 9277600 [patent_doc_number] => 20140027568 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-01-30 [patent_title] => 'METHOD FOR GENERATING HYDRAULIC POWER IN AN AIRCRAFT, USE OF A HYBRID POWER CONTROL UNIT AND DRIVE SYSTEM' [patent_app_type] => utility [patent_app_number] => 13/946422 [patent_app_country] => US [patent_app_date] => 2013-07-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 3660 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13946422 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/946422
Method for generating hydraulic power in an aircraft, use of a hybrid power control unit and drive system Jul 18, 2013 Issued
Array ( [id] => 9474054 [patent_doc_number] => 20140131517 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-05-15 [patent_title] => 'AERODYNAMIC, BLUNT AFT BODY' [patent_app_type] => utility [patent_app_number] => 13/944144 [patent_app_country] => US [patent_app_date] => 2013-07-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 3068 [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] => 13944144 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/944144
Aerodynamic, blunt aft body Jul 16, 2013 Issued
Array ( [id] => 10175733 [patent_doc_number] => 09205922 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2015-12-08 [patent_title] => 'Systems and methods for implementing a payload distribution system' [patent_app_type] => utility [patent_app_number] => 13/943965 [patent_app_country] => US [patent_app_date] => 2013-07-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 8 [patent_no_of_words] => 5783 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 91 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13943965 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/943965
Systems and methods for implementing a payload distribution system Jul 16, 2013 Issued
Array ( [id] => 10169012 [patent_doc_number] => 09199713 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2015-12-01 [patent_title] => 'Pressure panels' [patent_app_type] => utility [patent_app_number] => 13/936468 [patent_app_country] => US [patent_app_date] => 2013-07-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 10 [patent_no_of_words] => 7479 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 198 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13936468 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/936468
Pressure panels Jul 7, 2013 Issued
Array ( [id] => 10514516 [patent_doc_number] => 09241545 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2016-01-26 [patent_title] => 'Buckle assembly' [patent_app_type] => utility [patent_app_number] => 13/932416 [patent_app_country] => US [patent_app_date] => 2013-07-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 11 [patent_no_of_words] => 3859 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 197 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13932416 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/932416
Buckle assembly Jun 30, 2013 Issued
Array ( [id] => 9272320 [patent_doc_number] => 08636246 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-01-28 [patent_title] => 'Aircraft wing extension and nozzle system' [patent_app_type] => utility [patent_app_number] => 13/921736 [patent_app_country] => US [patent_app_date] => 2013-06-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 16 [patent_no_of_words] => 4404 [patent_no_of_claims] => 4 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 67 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13921736 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/921736
Aircraft wing extension and nozzle system Jun 18, 2013 Issued
Array ( [id] => 13078807 [patent_doc_number] => 10059460 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2018-08-28 [patent_title] => Method and architecture for the optimized transfer of power between an auxiliary power motor and the main engines of a helicopter [patent_app_type] => utility [patent_app_number] => 14/406054 [patent_app_country] => US [patent_app_date] => 2013-06-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 5 [patent_no_of_words] => 3051 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 171 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14406054 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/406054
Method and architecture for the optimized transfer of power between an auxiliary power motor and the main engines of a helicopter Jun 11, 2013 Issued
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