Search

Diana C. Vieira

Examiner (ID: 10543, Phone: (571)270-5026 , Office: P/2817 )

Most Active Art Unit
2814
Art Unit(s)
2814, 2817
Total Applications
286
Issued Applications
187
Pending Applications
0
Abandoned Applications
99

Applications

Application numberTitle of the applicationFiling DateStatus
Array ( [id] => 14699461 [patent_doc_number] => 10377461 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2019-08-13 [patent_title] => Aircraft structural component [patent_app_type] => utility [patent_app_number] => 14/747707 [patent_app_country] => US [patent_app_date] => 2015-06-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 7 [patent_no_of_words] => 4952 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 290 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14747707 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/747707
Aircraft structural component Jun 22, 2015 Issued
Array ( [id] => 11416146 [patent_doc_number] => 09562966 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2017-02-07 [patent_title] => 'Surface distance determination using reflected light' [patent_app_type] => utility [patent_app_number] => 14/742218 [patent_app_country] => US [patent_app_date] => 2015-06-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 14 [patent_no_of_words] => 9342 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 192 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14742218 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/742218
Surface distance determination using reflected light Jun 16, 2015 Issued
Array ( [id] => 12253933 [patent_doc_number] => 09926069 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2018-03-27 [patent_title] => 'Load-bearing fairing element for a flap adjustment mechanism and aircraft having such a fairing element' [patent_app_type] => utility [patent_app_number] => 14/713089 [patent_app_country] => US [patent_app_date] => 2015-05-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 4 [patent_no_of_words] => 5237 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 283 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14713089 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/713089
Load-bearing fairing element for a flap adjustment mechanism and aircraft having such a fairing element May 14, 2015 Issued
Array ( [id] => 12253933 [patent_doc_number] => 09926069 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2018-03-27 [patent_title] => 'Load-bearing fairing element for a flap adjustment mechanism and aircraft having such a fairing element' [patent_app_type] => utility [patent_app_number] => 14/713089 [patent_app_country] => US [patent_app_date] => 2015-05-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 4 [patent_no_of_words] => 5237 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 283 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14713089 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/713089
Load-bearing fairing element for a flap adjustment mechanism and aircraft having such a fairing element May 14, 2015 Issued
Array ( [id] => 13078737 [patent_doc_number] => 10059425 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2018-08-28 [patent_title] => Aircraft having a self-erecting partition element in a compartment inside the fuselage [patent_app_type] => utility [patent_app_number] => 14/706476 [patent_app_country] => US [patent_app_date] => 2015-05-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 4 [patent_no_of_words] => 4368 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 357 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14706476 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/706476
Aircraft having a self-erecting partition element in a compartment inside the fuselage May 6, 2015 Issued
Array ( [id] => 13250613 [patent_doc_number] => 10137982 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2018-11-27 [patent_title] => Propeller units [patent_app_type] => utility [patent_app_number] => 14/706162 [patent_app_country] => US [patent_app_date] => 2015-05-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 18 [patent_figures_cnt] => 21 [patent_no_of_words] => 31256 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 328 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14706162 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/706162
Propeller units May 6, 2015 Issued
Array ( [id] => 12944812 [patent_doc_number] => 09834296 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2017-12-05 [patent_title] => Ballonet deployment control paneling system [patent_app_type] => utility [patent_app_number] => 14/704625 [patent_app_country] => US [patent_app_date] => 2015-05-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 12 [patent_no_of_words] => 11370 [patent_no_of_claims] => 22 [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] =>[firstpage_image] =>[orig_patent_app_number] => 14704625 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/704625
Ballonet deployment control paneling system May 4, 2015 Issued
Array ( [id] => 11442834 [patent_doc_number] => 20170043855 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2017-02-16 [patent_title] => 'BUFFER ZONE FOR INTERIOR AIRCRAFT FEATURES' [patent_app_type] => utility [patent_app_number] => 15/306241 [patent_app_country] => US [patent_app_date] => 2015-04-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 4543 [patent_no_of_claims] => 23 [patent_no_of_ind_claims] => 6 [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] => 15306241 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/306241
Buffer zone for interior aircraft features Apr 19, 2015 Issued
Array ( [id] => 11568309 [patent_doc_number] => 20170106953 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2017-04-20 [patent_title] => 'AERIAL DEPLOYABLE RESCUE PACKAGE' [patent_app_type] => utility [patent_app_number] => 15/128790 [patent_app_country] => US [patent_app_date] => 2015-03-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 21 [patent_figures_cnt] => 21 [patent_no_of_words] => 10874 [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] => 15128790 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/128790
AERIAL DEPLOYABLE RESCUE PACKAGE Mar 30, 2015 Abandoned
Array ( [id] => 11821531 [patent_doc_number] => 20170210468 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2017-07-27 [patent_title] => 'SPHERICAL VTOL AERIAL VEHICLE' [patent_app_type] => utility [patent_app_number] => 15/129555 [patent_app_country] => US [patent_app_date] => 2015-03-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 16 [patent_figures_cnt] => 16 [patent_no_of_words] => 6496 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 5 [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] => 15129555 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/129555
Spherical VTOL aerial vehicle Mar 26, 2015 Issued
Array ( [id] => 16940795 [patent_doc_number] => 11053015 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2021-07-06 [patent_title] => Engine pylon having a drain [patent_app_type] => utility [patent_app_number] => 14/629736 [patent_app_country] => US [patent_app_date] => 2015-02-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 11 [patent_no_of_words] => 5628 [patent_no_of_claims] => 23 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 154 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14629736 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/629736
Engine pylon having a drain Feb 23, 2015 Issued
Array ( [id] => 16940795 [patent_doc_number] => 11053015 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2021-07-06 [patent_title] => Engine pylon having a drain [patent_app_type] => utility [patent_app_number] => 14/629736 [patent_app_country] => US [patent_app_date] => 2015-02-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 11 [patent_no_of_words] => 5628 [patent_no_of_claims] => 23 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 154 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14629736 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/629736
Engine pylon having a drain Feb 23, 2015 Issued
Array ( [id] => 10273598 [patent_doc_number] => 20150158595 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-06-11 [patent_title] => 'AIRCRAFT THROTTLE CONTROL SYSTEM WITH AN EMITTER UNIT AND A RECEIVER UNIT' [patent_app_type] => utility [patent_app_number] => 14/559187 [patent_app_country] => US [patent_app_date] => 2014-12-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 3172 [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] => 14559187 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/559187
AIRCRAFT THROTTLE CONTROL SYSTEM WITH AN EMITTER UNIT AND A RECEIVER UNIT Dec 2, 2014 Abandoned
Array ( [id] => 11698502 [patent_doc_number] => 09688404 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2017-06-27 [patent_title] => 'Stabilized airborne drop delivery' [patent_app_type] => utility [patent_app_number] => 14/558046 [patent_app_country] => US [patent_app_date] => 2014-12-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 13 [patent_no_of_words] => 8863 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 124 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14558046 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/558046
Stabilized airborne drop delivery Dec 1, 2014 Issued
Array ( [id] => 11100559 [patent_doc_number] => 20160297529 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2016-10-13 [patent_title] => 'HIGH END BUSINESS CLASS SEATING ARRANGEMENT' [patent_app_type] => utility [patent_app_number] => 15/101000 [patent_app_country] => US [patent_app_date] => 2014-12-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 3770 [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] => 15101000 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/101000
High end business class seating arrangement Dec 1, 2014 Issued
Array ( [id] => 12105817 [patent_doc_number] => 09862285 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2018-01-09 [patent_title] => 'Post-type apparatus for containing and charging unmanned vertical take-off and landing aircraft and method of containing and charging unmanned vertical take-off and landing aircraft using the same' [patent_app_type] => utility [patent_app_number] => 14/556296 [patent_app_country] => US [patent_app_date] => 2014-12-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 13 [patent_figures_cnt] => 13 [patent_no_of_words] => 6231 [patent_no_of_claims] => 28 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 167 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14556296 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/556296
Post-type apparatus for containing and charging unmanned vertical take-off and landing aircraft and method of containing and charging unmanned vertical take-off and landing aircraft using the same Nov 30, 2014 Issued
Array ( [id] => 14793403 [patent_doc_number] => 10399692 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2019-09-03 [patent_title] => Aircraft fuel system with heating of stored fuel [patent_app_type] => utility [patent_app_number] => 15/101786 [patent_app_country] => US [patent_app_date] => 2014-11-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 1736 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 177 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15101786 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/101786
Aircraft fuel system with heating of stored fuel Nov 26, 2014 Issued
Array ( [id] => 10266849 [patent_doc_number] => 20150151846 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-06-04 [patent_title] => 'AIRCRAFT FUEL TANK INERTING ARRANGEMENT' [patent_app_type] => utility [patent_app_number] => 14/554862 [patent_app_country] => US [patent_app_date] => 2014-11-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 3534 [patent_no_of_claims] => 31 [patent_no_of_ind_claims] => 14 [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] => 14554862 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/554862
AIRCRAFT FUEL TANK INERTING ARRANGEMENT Nov 25, 2014 Abandoned
Array ( [id] => 11114546 [patent_doc_number] => 20160311518 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2016-10-27 [patent_title] => 'WING STRUCTURE UTILIZING CARBON FIBER SPAR AND SHAPED FOAM' [patent_app_type] => utility [patent_app_number] => 14/555471 [patent_app_country] => US [patent_app_date] => 2014-11-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 2051 [patent_no_of_claims] => 1 [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] => 14555471 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/555471
WING STRUCTURE UTILIZING CARBON FIBER SPAR AND SHAPED FOAM Nov 25, 2014 Abandoned
Array ( [id] => 10399099 [patent_doc_number] => 20150284107 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-10-08 [patent_title] => 'HOSE&DROGUE IN-FLIGHT REFUELING SYSTEM WITH AN ACTIVE FUEL PRESSURE CONTROL' [patent_app_type] => utility [patent_app_number] => 14/553314 [patent_app_country] => US [patent_app_date] => 2014-11-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2387 [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] => 14553314 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/553314
HOSE&DROGUE IN-FLIGHT REFUELING SYSTEM WITH AN ACTIVE FUEL PRESSURE CONTROL Nov 24, 2014 Abandoned
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