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] => 11922380 [patent_doc_number] => 09789950 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2017-10-17 [patent_title] => 'Unmanned aerial vehicle (UAV) with multi-part foldable wings' [patent_app_type] => utility [patent_app_number] => 14/260889 [patent_app_country] => US [patent_app_date] => 2014-04-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 3039 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 94 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14260889 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/260889
Unmanned aerial vehicle (UAV) with multi-part foldable wings Apr 23, 2014 Issued
Array ( [id] => 10909158 [patent_doc_number] => 20140312173 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-10-23 [patent_title] => 'DOUBLE CABIN ATTENDANT SEAT' [patent_app_type] => utility [patent_app_number] => 14/258580 [patent_app_country] => US [patent_app_date] => 2014-04-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 3846 [patent_no_of_claims] => 11 [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] => 14258580 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/258580
Double cabin attendant seat Apr 21, 2014 Issued
Array ( [id] => 11357112 [patent_doc_number] => 09533754 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2017-01-03 [patent_title] => 'Wing aerial refueling system' [patent_app_type] => utility [patent_app_number] => 14/256935 [patent_app_country] => US [patent_app_date] => 2014-04-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 10 [patent_no_of_words] => 3002 [patent_no_of_claims] => 26 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 83 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14256935 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/256935
Wing aerial refueling system Apr 18, 2014 Issued
Array ( [id] => 10964478 [patent_doc_number] => 20140367509 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-12-18 [patent_title] => 'AIRCRAFT WITH FREEWHEELING ENGINE' [patent_app_type] => utility [patent_app_number] => 14/251850 [patent_app_country] => US [patent_app_date] => 2014-04-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 11372 [patent_no_of_claims] => 21 [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] => 14251850 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/251850
AIRCRAFT WITH FREEWHEELING ENGINE Apr 13, 2014 Abandoned
Array ( [id] => 11304465 [patent_doc_number] => 09511850 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2016-12-06 [patent_title] => 'Wing tip device for an aircraft wing' [patent_app_type] => utility [patent_app_number] => 14/251601 [patent_app_country] => US [patent_app_date] => 2014-04-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 15 [patent_no_of_words] => 8498 [patent_no_of_claims] => 24 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 83 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14251601 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/251601
Wing tip device for an aircraft wing Apr 11, 2014 Issued
Array ( [id] => 10964494 [patent_doc_number] => 20140367525 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-12-18 [patent_title] => 'AIRCRAFT USING TURBO-ELECTRIC HYBRID PROPULSION SYSTEM' [patent_app_type] => utility [patent_app_number] => 14/247608 [patent_app_country] => US [patent_app_date] => 2014-04-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 5325 [patent_no_of_claims] => 18 [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] => 14247608 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/247608
Aircraft using turbo-electric hybrid propulsion system Apr 7, 2014 Issued
Array ( [id] => 12106035 [patent_doc_number] => 09862505 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2018-01-09 [patent_title] => 'Techniques for emplacing an unmanned aerial vehicle launcher prior to launching an unmanned aerial vehicle' [patent_app_type] => utility [patent_app_number] => 14/225751 [patent_app_country] => US [patent_app_date] => 2014-03-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 5515 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 288 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14225751 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/225751
Techniques for emplacing an unmanned aerial vehicle launcher prior to launching an unmanned aerial vehicle Mar 25, 2014 Issued
Array ( [id] => 13153403 [patent_doc_number] => 10093411 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2018-10-09 [patent_title] => Apparatus and method for reducing a sonic boom signature [patent_app_type] => utility [patent_app_number] => 14/217547 [patent_app_country] => US [patent_app_date] => 2014-03-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 12 [patent_no_of_words] => 4529 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 100 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14217547 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/217547
Apparatus and method for reducing a sonic boom signature Mar 17, 2014 Issued
Array ( [id] => 11736826 [patent_doc_number] => 09701399 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2017-07-11 [patent_title] => 'Parasitic drag induced boundary layer reduction system and method' [patent_app_type] => utility [patent_app_number] => 14/218819 [patent_app_country] => US [patent_app_date] => 2014-03-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 13 [patent_no_of_words] => 8091 [patent_no_of_claims] => 22 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 141 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14218819 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/218819
Parasitic drag induced boundary layer reduction system and method Mar 17, 2014 Issued
Array ( [id] => 13647357 [patent_doc_number] => 09849980 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2017-12-26 [patent_title] => Personal propulsion devices with improved balance [patent_app_type] => utility [patent_app_number] => 14/210102 [patent_app_country] => US [patent_app_date] => 2014-03-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2775 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 1 [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] => 14210102 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/210102
Personal propulsion devices with improved balance Mar 12, 2014 Issued
Array ( [id] => 9728142 [patent_doc_number] => 20140263848 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-09-18 [patent_title] => 'REVERSIBLE FLIGHT CONTROL SYSTEMS' [patent_app_type] => utility [patent_app_number] => 14/195419 [patent_app_country] => US [patent_app_date] => 2014-03-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 6223 [patent_no_of_claims] => 38 [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] => 14195419 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/195419
Reversible flight control systems Mar 2, 2014 Issued
Array ( [id] => 9969627 [patent_doc_number] => 09016624 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2015-04-28 [patent_title] => 'Aircraft cabin bin retrofit' [patent_app_type] => utility [patent_app_number] => 14/189872 [patent_app_country] => US [patent_app_date] => 2014-02-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 7 [patent_no_of_words] => 3883 [patent_no_of_claims] => 5 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 111 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14189872 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/189872
Aircraft cabin bin retrofit Feb 24, 2014 Issued
Array ( [id] => 11763647 [patent_doc_number] => 09372055 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2016-06-21 [patent_title] => 'Passive control fin stops for air launched boosted (two stage) high speed vehicles' [patent_app_type] => utility [patent_app_number] => 14/170143 [patent_app_country] => US [patent_app_date] => 2014-01-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 16 [patent_no_of_words] => 2240 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 87 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14170143 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/170143
Passive control fin stops for air launched boosted (two stage) high speed vehicles Jan 30, 2014 Issued
Array ( [id] => 10541036 [patent_doc_number] => 09266143 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2016-02-23 [patent_title] => 'Fireproof bulkhead of a highly porous structure with intumescent coating and method for its production' [patent_app_type] => utility [patent_app_number] => 14/163673 [patent_app_country] => US [patent_app_date] => 2014-01-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 3 [patent_no_of_words] => 3208 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 73 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14163673 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/163673
Fireproof bulkhead of a highly porous structure with intumescent coating and method for its production Jan 23, 2014 Issued
Array ( [id] => 9634543 [patent_doc_number] => 20140212652 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-07-31 [patent_title] => 'FIREPROOF BULKHEAD OF A HIGHLY POROUS STRUCTURE WITH INTUMESCENT COATING AND METHOD FOR ITS PRODUCTION' [patent_app_type] => utility [patent_app_number] => 14/163664 [patent_app_country] => US [patent_app_date] => 2014-01-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 3208 [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] => 14163664 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/163664
Fireproof bulkhead of a highly porous structure with intumescent coating and method for its production Jan 23, 2014 Issued
Array ( [id] => 10929612 [patent_doc_number] => 20140332633 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-11-13 [patent_title] => 'EMERGENCY COLLECTIVE ACTUATOR AND METHOD FOR A HELICOPTER' [patent_app_type] => utility [patent_app_number] => 14/161877 [patent_app_country] => US [patent_app_date] => 2014-01-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 15 [patent_figures_cnt] => 15 [patent_no_of_words] => 10355 [patent_no_of_claims] => 20 [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] => 14161877 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/161877
Emergency collective actuator and method for a helicopter Jan 22, 2014 Issued
Array ( [id] => 10111029 [patent_doc_number] => 09146438 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2015-09-29 [patent_title] => 'Self-powered dimmable windows with integrated controls' [patent_app_type] => utility [patent_app_number] => 14/159267 [patent_app_country] => US [patent_app_date] => 2014-01-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 20 [patent_no_of_words] => 5247 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 2 [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] => 14159267 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/159267
Self-powered dimmable windows with integrated controls Jan 19, 2014 Issued
Array ( [id] => 10482929 [patent_doc_number] => 20150367947 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-12-24 [patent_title] => 'AIRCRAFT PROPULSION ASSEMBLY COMPRISING AT LEAST ONE BRUSH SEAL RESISTANT TO HIGH-TEMPERATURE' [patent_app_type] => utility [patent_app_number] => 14/762085 [patent_app_country] => US [patent_app_date] => 2014-01-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 4057 [patent_no_of_claims] => 16 [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] => 14762085 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/762085
AIRCRAFT PROPULSION ASSEMBLY COMPRISING AT LEAST ONE BRUSH SEAL RESISTANT TO HIGH-TEMPERATURE Jan 19, 2014 Abandoned
Array ( [id] => 9565587 [patent_doc_number] => 20140183301 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-07-03 [patent_title] => 'AIRCRAFT VENTRAL FAIRING WITH AN IMPROVED STORAGE CAPACITY' [patent_app_type] => utility [patent_app_number] => 14/140665 [patent_app_country] => US [patent_app_date] => 2013-12-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 2862 [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] => 14140665 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/140665
Aircraft ventral fairing with an improved storage capacity Dec 25, 2013 Issued
Array ( [id] => 10298511 [patent_doc_number] => 20150183511 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-07-02 [patent_title] => 'CONTROL PANEL INTEGRATION INTO AIRCRAFT THROTTLE CONTROL' [patent_app_type] => utility [patent_app_number] => 14/141150 [patent_app_country] => US [patent_app_date] => 2013-12-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 2658 [patent_no_of_claims] => 21 [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] => 14141150 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/141150
CONTROL PANEL INTEGRATION INTO AIRCRAFT THROTTLE CONTROL Dec 25, 2013 Abandoned
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