Search

Nicholas R. Pasko

Examiner (ID: 17269, Phone: (571)270-1876 , Office: P/2872 )

Most Active Art Unit
2896
Art Unit(s)
2872, 2896
Total Applications
625
Issued Applications
363
Pending Applications
83
Abandoned Applications
201

Applications

Application numberTitle of the applicationFiling DateStatus
Array ( [id] => 16628378 [patent_doc_number] => 20210047031 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2021-02-18 [patent_title] => ROTORCRAFT INCLUDING VARIABLE BLADE TORSIONAL ANGLE MECHANISM [patent_app_type] => utility [patent_app_number] => 16/898458 [patent_app_country] => US [patent_app_date] => 2020-06-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 7136 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 181 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16898458 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/898458
Rotorcraft including variable blade torsional angle mechanism Jun 10, 2020 Issued
Array ( [id] => 17815164 [patent_doc_number] => 11420761 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2022-08-23 [patent_title] => Autonomous propeller propulsion system for an aircraft, said autonomous propeller propulsion system comprising a fuel cell [patent_app_type] => utility [patent_app_number] => 16/898960 [patent_app_country] => US [patent_app_date] => 2020-06-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 5 [patent_no_of_words] => 4373 [patent_no_of_claims] => 7 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 256 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16898960 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/898960
Autonomous propeller propulsion system for an aircraft, said autonomous propeller propulsion system comprising a fuel cell Jun 10, 2020 Issued
Array ( [id] => 16505869 [patent_doc_number] => 20200385125 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2020-12-10 [patent_title] => Consolidated Electronics Packages for Staggered Aircraft Seats [patent_app_type] => utility [patent_app_number] => 16/891919 [patent_app_country] => US [patent_app_date] => 2020-06-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 7829 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -13 [patent_words_short_claim] => 132 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16891919 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/891919
Consolidated electronics packages for staggered aircraft seats Jun 2, 2020 Issued
Array ( [id] => 17258094 [patent_doc_number] => 20210371079 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2021-12-02 [patent_title] => AIRCRAFT WITH MULTI SPAR BOX CONNECTION TO FUSELAGE [patent_app_type] => utility [patent_app_number] => 16/884911 [patent_app_country] => US [patent_app_date] => 2020-05-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 11293 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -18 [patent_words_short_claim] => 344 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16884911 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/884911
Aircraft with multi spar box connection to fuselage May 26, 2020 Issued
Array ( [id] => 17258095 [patent_doc_number] => 20210371080 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2021-12-02 [patent_title] => AIRCRAFT WITH MULTI SPAR BOX CONNECTION TO FUSELAGE [patent_app_type] => utility [patent_app_number] => 16/885022 [patent_app_country] => US [patent_app_date] => 2020-05-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 11916 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -18 [patent_words_short_claim] => 261 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16885022 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/885022
Aircraft with multi spar box connection to fuselage May 26, 2020 Issued
Array ( [id] => 17245306 [patent_doc_number] => 20210365049 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2021-11-25 [patent_title] => Yaw Control Systems for Tailsitting Biplane Aircraft [patent_app_type] => utility [patent_app_number] => 16/879081 [patent_app_country] => US [patent_app_date] => 2020-05-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 13804 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -18 [patent_words_short_claim] => 139 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16879081 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/879081
Yaw control systems for tailsitting biplane aircraft May 19, 2020 Issued
Array ( [id] => 18793622 [patent_doc_number] => 11827372 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2023-11-28 [patent_title] => Engine characteristics matching [patent_app_type] => utility [patent_app_number] => 16/875196 [patent_app_country] => US [patent_app_date] => 2020-05-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 5 [patent_no_of_words] => 1996 [patent_no_of_claims] => 5 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 201 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16875196 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/875196
Engine characteristics matching May 14, 2020 Issued
Array ( [id] => 18717587 [patent_doc_number] => 11794916 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2023-10-24 [patent_title] => Control systems for hybrid electric power plants [patent_app_type] => utility [patent_app_number] => 16/875941 [patent_app_country] => US [patent_app_date] => 2020-05-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 6861 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 231 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16875941 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/875941
Control systems for hybrid electric power plants May 14, 2020 Issued
Array ( [id] => 16991405 [patent_doc_number] => 20210229825 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2021-07-29 [patent_title] => PROVIDING A LOAD FROM A MOTOR TO INHIBIT FURTHER ROTATION OF A PROPELLER OF AN AERIAL VEHICLE WHILE IN FLIGHT [patent_app_type] => utility [patent_app_number] => 16/874038 [patent_app_country] => US [patent_app_date] => 2020-05-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 6454 [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] => 16874038 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/874038
Providing a load from a motor to inhibit further rotation of a propeller of an aerial vehicle while in flight May 13, 2020 Issued
Array ( [id] => 17687287 [patent_doc_number] => 20220194579 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-06-23 [patent_title] => UAV HAVING CONFIGURABLE FUEL CELL POWER SYSTEM [patent_app_type] => utility [patent_app_number] => 17/603890 [patent_app_country] => US [patent_app_date] => 2020-04-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 5811 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -18 [patent_words_short_claim] => 82 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17603890 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/603890
UAV HAVING CONFIGURABLE FUEL CELL POWER SYSTEM Apr 22, 2020 Abandoned
Array ( [id] => 17594862 [patent_doc_number] => 20220144435 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-05-12 [patent_title] => SYSTEMS AND METHODS FOR LIFTING AN OBJECT [patent_app_type] => utility [patent_app_number] => 17/440857 [patent_app_country] => US [patent_app_date] => 2020-04-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 9378 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -11 [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] => 17440857 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/440857
SYSTEMS AND METHODS FOR LIFTING AN OBJECT Apr 1, 2020 Abandoned
Array ( [id] => 17111367 [patent_doc_number] => 20210291964 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2021-09-23 [patent_title] => OPEN ROTOR BOUNDARY LAYER INGESTION BOOSTER [patent_app_type] => utility [patent_app_number] => 16/826727 [patent_app_country] => US [patent_app_date] => 2020-03-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 6492 [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] => 16826727 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/826727
Open rotor boundary layer ingestion booster Mar 22, 2020 Issued
Array ( [id] => 17578044 [patent_doc_number] => 20220134899 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-05-05 [patent_title] => DOCKING PORT AND BATTERY CHARGING DEPOT FOR AN UNMANNED AERIAL VEHICLE AND A METHOD FOR DOCKING AND CHARGING THE VEHICLE [patent_app_type] => utility [patent_app_number] => 17/430032 [patent_app_country] => US [patent_app_date] => 2020-02-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 5708 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -14 [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] => 17430032 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/430032
DOCKING PORT AND BATTERY CHARGING DEPOT FOR AN UNMANNED AERIAL VEHICLE AND A METHOD FOR DOCKING AND CHARGING THE VEHICLE Feb 10, 2020 Abandoned
Array ( [id] => 16991401 [patent_doc_number] => 20210229821 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2021-07-29 [patent_title] => AIRCRAFT WITH ELECTRICAL ENERGY STORAGE IN NACELLES [patent_app_type] => utility [patent_app_number] => 16/774606 [patent_app_country] => US [patent_app_date] => 2020-01-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 4175 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -18 [patent_words_short_claim] => 188 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16774606 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/774606
Aircraft with electrical energy storage in nacelles Jan 27, 2020 Issued
Array ( [id] => 17526602 [patent_doc_number] => 11299273 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2022-04-12 [patent_title] => Contoured passenger seat privacy shell shape of aircraft passenger compartment suites [patent_app_type] => utility [patent_app_number] => 16/744653 [patent_app_country] => US [patent_app_date] => 2020-01-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 8 [patent_no_of_words] => 7769 [patent_no_of_claims] => 15 [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] => 16744653 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/744653
Contoured passenger seat privacy shell shape of aircraft passenger compartment suites Jan 15, 2020 Issued
Array ( [id] => 17603779 [patent_doc_number] => 11332249 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2022-05-17 [patent_title] => Actuatable display devices for aircraft passenger compartment suites [patent_app_type] => utility [patent_app_number] => 16/742720 [patent_app_country] => US [patent_app_date] => 2020-01-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 14 [patent_figures_cnt] => 14 [patent_no_of_words] => 10415 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 267 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16742720 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/742720
Actuatable display devices for aircraft passenger compartment suites Jan 13, 2020 Issued
Array ( [id] => 17443333 [patent_doc_number] => 20220063838 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-03-03 [patent_title] => SYSTEM AND METHOD FOR IMPROVED SECURING OF AN AEROSTAT TO A RECEIVING STRUCTURE [patent_app_type] => utility [patent_app_number] => 17/416970 [patent_app_country] => US [patent_app_date] => 2019-12-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 2921 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -16 [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] => 17416970 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/416970
System and method for improved securing of an aerostat to a receiving structure Dec 17, 2019 Issued
Array ( [id] => 16900333 [patent_doc_number] => 20210179249 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2021-06-17 [patent_title] => LONGITUDINAL BEAM JOINT FOR A PRESSURE DECK ASSEMBLY [patent_app_type] => utility [patent_app_number] => 16/716379 [patent_app_country] => US [patent_app_date] => 2019-12-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 10128 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 80 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16716379 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/716379
Longitudinal beam joint for a pressure deck assembly Dec 15, 2019 Issued
Array ( [id] => 16283476 [patent_doc_number] => 20200277078 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2020-09-03 [patent_title] => ELECTRICAL POWER SYSTEM FOR AIRCRAFT HAVING HYBRID-ELECTRIC PROPULSION SYSTEM [patent_app_type] => utility [patent_app_number] => 16/707669 [patent_app_country] => US [patent_app_date] => 2019-12-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 2556 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -22 [patent_words_short_claim] => 63 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16707669 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/707669
ELECTRICAL POWER SYSTEM FOR AIRCRAFT HAVING HYBRID-ELECTRIC PROPULSION SYSTEM Dec 8, 2019 Abandoned
Array ( [id] => 19754011 [patent_doc_number] => 20250042576 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2025-02-06 [patent_title] => SKYPORT FOR ESTOL [patent_app_type] => utility [patent_app_number] => 17/309525 [patent_app_country] => US [patent_app_date] => 2019-12-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 4195 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -13 [patent_words_short_claim] => 87 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17309525 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/309525
Skyport for eSTOL Dec 1, 2019 Issued
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