Search

Dixomara Vargas

Examiner (ID: 15547, Phone: (571)272-2252 , Office: P/2866 )

Most Active Art Unit
2866
Art Unit(s)
2831, 2866, 2862, 3793, 2858, 3798, 2859
Total Applications
1885
Issued Applications
1670
Pending Applications
114
Abandoned Applications
121

Applications

Application numberTitle of the applicationFiling DateStatus
Array ( [id] => 18733214 [patent_doc_number] => 11801937 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2023-10-31 [patent_title] => Systems and methods for avian flock flight path modification using UAVs [patent_app_type] => utility [patent_app_number] => 16/523889 [patent_app_country] => US [patent_app_date] => 2019-07-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 14 [patent_figures_cnt] => 14 [patent_no_of_words] => 8366 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 242 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16523889 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/523889
Systems and methods for avian flock flight path modification using UAVs Jul 25, 2019 Issued
Array ( [id] => 17051818 [patent_doc_number] => 20210261252 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2021-08-26 [patent_title] => A FLIGHT SYSTEM WITH A PAYLOAD LAUNCHER [patent_app_type] => utility [patent_app_number] => 17/261020 [patent_app_country] => US [patent_app_date] => 2019-07-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 7061 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 2 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17261020 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/261020
A FLIGHT SYSTEM WITH A PAYLOAD LAUNCHER Jul 15, 2019 Abandoned
Array ( [id] => 19012708 [patent_doc_number] => 11919619 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2024-03-05 [patent_title] => Aircraft-floor element, aircraft zone and aircraft having an aircraft-floor element [patent_app_type] => utility [patent_app_number] => 16/509748 [patent_app_country] => US [patent_app_date] => 2019-07-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 16 [patent_no_of_words] => 7609 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 217 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16509748 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/509748
Aircraft-floor element, aircraft zone and aircraft having an aircraft-floor element Jul 11, 2019 Issued
Array ( [id] => 17704183 [patent_doc_number] => 20220204189 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-06-30 [patent_title] => SPACECRAFT RADIATION SHIELD SYSTEM [patent_app_type] => utility [patent_app_number] => 17/263512 [patent_app_country] => US [patent_app_date] => 2019-07-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 6303 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -8 [patent_words_short_claim] => 23 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17263512 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/263512
SPACECRAFT RADIATION SHIELD SYSTEM Jul 4, 2019 Abandoned
Array ( [id] => 16556832 [patent_doc_number] => 20210001980 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2021-01-07 [patent_title] => SYSTEM AND METHOD FOR VIBRATORY MOTION REDUCTION FOR A PYLON ASSEMBLY [patent_app_type] => utility [patent_app_number] => 16/504057 [patent_app_country] => US [patent_app_date] => 2019-07-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 7502 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -25 [patent_words_short_claim] => 91 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16504057 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/504057
System and method for vibratory motion reduction for a pylon assembly Jul 4, 2019 Issued
Array ( [id] => 19730901 [patent_doc_number] => 12208890 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2025-01-28 [patent_title] => Connector [patent_app_type] => utility [patent_app_number] => 16/460104 [patent_app_country] => US [patent_app_date] => 2019-07-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 19 [patent_no_of_words] => 4735 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 155 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16460104 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/460104
Connector Jul 1, 2019 Issued
Array ( [id] => 18518291 [patent_doc_number] => 11708168 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2023-07-25 [patent_title] => Aircraft propulsion unit comprising an assembly of at least two coaxial shafts, one being connected to the fan and the other to the assembly of fixed blades [patent_app_type] => utility [patent_app_number] => 16/452634 [patent_app_country] => US [patent_app_date] => 2019-06-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 5594 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 195 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16452634 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/452634
Aircraft propulsion unit comprising an assembly of at least two coaxial shafts, one being connected to the fan and the other to the assembly of fixed blades Jun 25, 2019 Issued
Array ( [id] => 16522888 [patent_doc_number] => 20200396968 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2020-12-24 [patent_title] => OYSTER AQUACULTURE METHOD AND APPARATUS [patent_app_type] => utility [patent_app_number] => 16/450019 [patent_app_country] => US [patent_app_date] => 2019-06-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 4942 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 92 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16450019 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/450019
Oyster aquaculture method and apparatus Jun 23, 2019 Issued
Array ( [id] => 16524906 [patent_doc_number] => 20200398986 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2020-12-24 [patent_title] => SYSTEMS FOR STORAGE AND DEPLOYMENT OF AN AERIAL DRONE [patent_app_type] => utility [patent_app_number] => 16/450222 [patent_app_country] => US [patent_app_date] => 2019-06-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 4938 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 145 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16450222 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/450222
SYSTEMS FOR STORAGE AND DEPLOYMENT OF AN AERIAL DRONE Jun 23, 2019 Abandoned
Array ( [id] => 16507049 [patent_doc_number] => 20200386305 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2020-12-10 [patent_title] => Bondable Cooling Fin Arrays for Use on Aircraft Gearboxes [patent_app_type] => utility [patent_app_number] => 16/434142 [patent_app_country] => US [patent_app_date] => 2019-06-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 5739 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -18 [patent_words_short_claim] => 54 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16434142 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/434142
Bondable Cooling Fin Arrays for Use on Aircraft Gearboxes Jun 5, 2019 Abandoned
Array ( [id] => 18260500 [patent_doc_number] => 11608192 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2023-03-21 [patent_title] => Drone elevator systems and methods [patent_app_type] => utility [patent_app_number] => 16/406841 [patent_app_country] => US [patent_app_date] => 2019-05-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 7346 [patent_no_of_claims] => 20 [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] => 16406841 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/406841
Drone elevator systems and methods May 7, 2019 Issued
Array ( [id] => 19667208 [patent_doc_number] => 12179934 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2024-12-31 [patent_title] => Method and apparatus for auxiliary power unit installation [patent_app_type] => utility [patent_app_number] => 16/404559 [patent_app_country] => US [patent_app_date] => 2019-05-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 8 [patent_no_of_words] => 6618 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [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] => 16404559 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/404559
Method and apparatus for auxiliary power unit installation May 5, 2019 Issued
Array ( [id] => 16421231 [patent_doc_number] => 20200346429 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2020-11-05 [patent_title] => Aircraft Monument Composite Construction Using Carbon Uni-Directional Spread Flat Tow Woven Fabric [patent_app_type] => utility [patent_app_number] => 16/401440 [patent_app_country] => US [patent_app_date] => 2019-05-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 6542 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 126 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16401440 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/401440
Aircraft monument composite construction using carbon uni-directional spread flat tow woven fabric May 1, 2019 Issued
Array ( [id] => 18621350 [patent_doc_number] => 11754378 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2023-09-12 [patent_title] => Deployable flap for high-G maneuvers [patent_app_type] => utility [patent_app_number] => 16/399453 [patent_app_country] => US [patent_app_date] => 2019-04-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 13 [patent_figures_cnt] => 18 [patent_no_of_words] => 14548 [patent_no_of_claims] => 25 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 191 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16399453 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/399453
Deployable flap for high-G maneuvers Apr 29, 2019 Issued
Array ( [id] => 15118633 [patent_doc_number] => 20190345949 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2019-11-14 [patent_title] => AIRCRAFT PROPULSION SYSTEM [patent_app_type] => utility [patent_app_number] => 16/395996 [patent_app_country] => US [patent_app_date] => 2019-04-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 2626 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -18 [patent_words_short_claim] => 86 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16395996 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/395996
Aircraft propulsion system Apr 25, 2019 Issued
Array ( [id] => 16376042 [patent_doc_number] => 20200324884 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2020-10-15 [patent_title] => ENGAGEMENT AND DISENGAGEMENT OF TAIL ROTOR [patent_app_type] => utility [patent_app_number] => 16/382052 [patent_app_country] => US [patent_app_date] => 2019-04-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 3180 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -18 [patent_words_short_claim] => 91 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16382052 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/382052
ENGAGEMENT AND DISENGAGEMENT OF TAIL ROTOR Apr 10, 2019 Abandoned
Array ( [id] => 16343140 [patent_doc_number] => 20200307790 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2020-10-01 [patent_title] => LIGHT TWIN ENGINE AIRCRAFT [patent_app_type] => utility [patent_app_number] => 16/369311 [patent_app_country] => US [patent_app_date] => 2019-03-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 6779 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -13 [patent_words_short_claim] => 91 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16369311 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/369311
LIGHT TWIN ENGINE AIRCRAFT Mar 28, 2019 Abandoned
Array ( [id] => 18963874 [patent_doc_number] => 11897622 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2024-02-13 [patent_title] => Propeller propulsion unit comprising a heat engine and an electric motor and aircraft comprising such a propeller propulsion unit [patent_app_type] => utility [patent_app_number] => 16/368305 [patent_app_country] => US [patent_app_date] => 2019-03-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 12 [patent_no_of_words] => 5577 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 204 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16368305 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/368305
Propeller propulsion unit comprising a heat engine and an electric motor and aircraft comprising such a propeller propulsion unit Mar 27, 2019 Issued
Array ( [id] => 16343156 [patent_doc_number] => 20200307806 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2020-10-01 [patent_title] => SEAT ADJUSTMENT SYSTEM AND METHOD [patent_app_type] => utility [patent_app_number] => 16/365788 [patent_app_country] => US [patent_app_date] => 2019-03-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 5234 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 83 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16365788 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/365788
SEAT ADJUSTMENT SYSTEM AND METHOD Mar 26, 2019 Abandoned
Array ( [id] => 15085607 [patent_doc_number] => 20190337614 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2019-11-07 [patent_title] => VERTICAL TAKEOFF AND LANDING AIRCRAFT [patent_app_type] => utility [patent_app_number] => 16/356359 [patent_app_country] => US [patent_app_date] => 2019-03-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 9046 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -19 [patent_words_short_claim] => 124 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16356359 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/356359
VERTICAL TAKEOFF AND LANDING AIRCRAFT Mar 17, 2019 Abandoned
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