
Nusrat Quddus
Examiner (ID: 15150, Phone: (571)270-7921 , Office: P/2838 )
| Most Active Art Unit | 2838 |
| Art Unit(s) | 2839, 2838 |
| Total Applications | 943 |
| Issued Applications | 815 |
| Pending Applications | 68 |
| Abandoned Applications | 87 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 15196591
[patent_doc_number] => 10495784
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2019-12-03
[patent_title] => Balloon-launching apparatus
[patent_app_type] => utility
[patent_app_number] => 15/507594
[patent_app_country] => US
[patent_app_date] => 2016-01-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 9
[patent_no_of_words] => 3826
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 132
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15507594
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/507594 | Balloon-launching apparatus | Jan 18, 2016 | Issued |
Array
(
[id] => 15573539
[patent_doc_number] => 10577134
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2020-03-03
[patent_title] => Separation device
[patent_app_type] => utility
[patent_app_number] => 15/539802
[patent_app_country] => US
[patent_app_date] => 2015-12-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 12
[patent_no_of_words] => 7223
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 1
[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] => 15539802
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/539802 | Separation device | Dec 23, 2015 | Issued |
Array
(
[id] => 12199439
[patent_doc_number] => 09902492
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2018-02-27
[patent_title] => 'Apparatus and method for roll moment equalization at high advance ratios for rotary wing aircraft'
[patent_app_type] => utility
[patent_app_number] => 14/756420
[patent_app_country] => US
[patent_app_date] => 2015-12-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 14
[patent_no_of_words] => 7772
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 281
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14756420
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/756420 | Apparatus and method for roll moment equalization at high advance ratios for rotary wing aircraft | Dec 3, 2015 | Issued |
Array
(
[id] => 12325236
[patent_doc_number] => 09944393
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2018-04-17
[patent_title] => Narrow-outlet splitter for a personal propulsion system
[patent_app_type] => utility
[patent_app_number] => 14/941660
[patent_app_country] => US
[patent_app_date] => 2015-11-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 10
[patent_no_of_words] => 5273
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 134
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14941660
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/941660 | Narrow-outlet splitter for a personal propulsion system | Nov 15, 2015 | Issued |
Array
(
[id] => 10768731
[patent_doc_number] => 20160114887
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-04-28
[patent_title] => 'AMPHIBIOUS VERTICAL TAKEOFF AND LANDING UNMANNED SYSTEM AND FLYING CAR WITH MULTIPLE AERIAL AND AQUATIC FLIGHT MODES FOR CAPTURING PANORAMIC VIRTUAL REALITY VIEWS, INTERACTIVE VIDEO AND TRANSPORTATION WITH MOBILE AND WEARABLE APPLICATION'
[patent_app_type] => utility
[patent_app_number] => 14/940379
[patent_app_country] => US
[patent_app_date] => 2015-11-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 23
[patent_figures_cnt] => 23
[patent_no_of_words] => 9718
[patent_no_of_claims] => 30
[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] => 14940379
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/940379 | Amphibious vertical takeoff and landing unmanned device | Nov 12, 2015 | Issued |
Array
(
[id] => 10821614
[patent_doc_number] => 20160167778
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-06-16
[patent_title] => 'Unmanned Flying Device'
[patent_app_type] => utility
[patent_app_number] => 14/936822
[patent_app_country] => US
[patent_app_date] => 2015-11-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 7274
[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] => 14936822
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/936822 | Unmanned flying device | Nov 9, 2015 | Issued |
Array
(
[id] => 12044314
[patent_doc_number] => 09821904
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2017-11-21
[patent_title] => 'Landing gear with structural load path diverter bracket'
[patent_app_type] => utility
[patent_app_number] => 14/936875
[patent_app_country] => US
[patent_app_date] => 2015-11-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2842
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 85
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14936875
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/936875 | Landing gear with structural load path diverter bracket | Nov 9, 2015 | Issued |
Array
(
[id] => 11641864
[patent_doc_number] => 09663217
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2017-05-30
[patent_title] => 'Assemblies and methods for reconfiguring aircraft fuselage doors'
[patent_app_type] => utility
[patent_app_number] => 14/937011
[patent_app_country] => US
[patent_app_date] => 2015-11-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 3842
[patent_no_of_claims] => 29
[patent_no_of_ind_claims] => 6
[patent_words_short_claim] => 158
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14937011
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/937011 | Assemblies and methods for reconfiguring aircraft fuselage doors | Nov 9, 2015 | Issued |
Array
(
[id] => 10713810
[patent_doc_number] => 20160059957
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-03-03
[patent_title] => 'AUTOROTATIVE ENHANCEMENT SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 14/934477
[patent_app_country] => US
[patent_app_date] => 2015-11-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 4278
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 4
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14934477
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/934477 | Autorotative enhancement system | Nov 5, 2015 | Issued |
Array
(
[id] => 10783837
[patent_doc_number] => 20160129993
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-05-12
[patent_title] => 'AIRCRAFT WING FOR RECEIVING A PLURALITY OF DIFFERENT WING TIP DEVICES'
[patent_app_type] => utility
[patent_app_number] => 14/933126
[patent_app_country] => US
[patent_app_date] => 2015-11-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 3258
[patent_no_of_claims] => 13
[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] => 14933126
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/933126 | AIRCRAFT WING FOR RECEIVING A PLURALITY OF DIFFERENT WING TIP DEVICES | Nov 4, 2015 | Abandoned |
Array
(
[id] => 10783834
[patent_doc_number] => 20160129990
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-05-12
[patent_title] => 'ROTARY ACTUATOR FOR CONTROLLING A FLIGHT CONTROL SURFACE'
[patent_app_type] => utility
[patent_app_number] => 14/933016
[patent_app_country] => US
[patent_app_date] => 2015-11-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2691
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 4
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14933016
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/933016 | Rotary actuator for controlling a flight control surface | Nov 4, 2015 | Issued |
Array
(
[id] => 11536637
[patent_doc_number] => 09611034
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2017-04-04
[patent_title] => 'Wide fuselage aircraft with increased boundary layer ingestion'
[patent_app_type] => utility
[patent_app_number] => 14/930712
[patent_app_country] => US
[patent_app_date] => 2015-11-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[patent_no_of_words] => 1649
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14930712
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/930712 | Wide fuselage aircraft with increased boundary layer ingestion | Nov 2, 2015 | Issued |
Array
(
[id] => 12386979
[patent_doc_number] => 09963229
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2018-05-08
[patent_title] => Structure and manufacturing process for unmanned aerial vehicle
[patent_app_type] => utility
[patent_app_number] => 14/924866
[patent_app_country] => US
[patent_app_date] => 2015-10-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 15
[patent_figures_cnt] => 15
[patent_no_of_words] => 3627
[patent_no_of_claims] => 5
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14924866
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/924866 | Structure and manufacturing process for unmanned aerial vehicle | Oct 27, 2015 | Issued |
Array
(
[id] => 12407667
[patent_doc_number] => 09969487
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2018-05-15
[patent_title] => Multiple controllable airflow modification devices
[patent_app_type] => utility
[patent_app_number] => 14/887139
[patent_app_country] => US
[patent_app_date] => 2015-10-19
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14887139
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/887139 | Multiple controllable airflow modification devices | Oct 18, 2015 | Issued |
Array
(
[id] => 12092182
[patent_doc_number] => 20170349275
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-12-07
[patent_title] => 'ELEVATOR AND RUDDER CONTROL OF A ROTORCRAFT'
[patent_app_type] => utility
[patent_app_number] => 15/510131
[patent_app_country] => US
[patent_app_date] => 2015-09-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 17
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15510131
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/510131 | ELEVATOR AND RUDDER CONTROL OF A ROTORCRAFT | Sep 29, 2015 | Abandoned |
Array
(
[id] => 11978891
[patent_doc_number] => 20170283045
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-10-05
[patent_title] => 'TRANSLATION THRUST SYSTEM ENGAGEMENT AND DISENGAGMENT FOR ROTARY WING AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 15/508991
[patent_app_country] => US
[patent_app_date] => 2015-09-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 19
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15508991
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/508991 | TRANSLATION THRUST SYSTEM ENGAGEMENT AND DISENGAGMENT FOR ROTARY WING AIRCRAFT | Sep 27, 2015 | Abandoned |
Array
(
[id] => 11838328
[patent_doc_number] => 20170220048
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-08-03
[patent_title] => 'ROTARY WING AIRCRAFT AND METHOD OF CONTROLLING A ROTARY WING AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 15/500388
[patent_app_country] => US
[patent_app_date] => 2015-09-25
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15500388
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/500388 | ROTARY WING AIRCRAFT AND METHOD OF CONTROLLING A ROTARY WING AIRCRAFT | Sep 24, 2015 | Abandoned |
Array
(
[id] => 16027553
[patent_doc_number] => 10676181
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2020-06-09
[patent_title] => Gearbox for a dual rotor, rotary wing aircraft
[patent_app_type] => utility
[patent_app_number] => 15/507178
[patent_app_country] => US
[patent_app_date] => 2015-09-25
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/507178 | Gearbox for a dual rotor, rotary wing aircraft | Sep 24, 2015 | Issued |
Array
(
[id] => 11973047
[patent_doc_number] => 20170277201
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-09-28
[patent_title] => 'NOSE ATTITUDE CONTROL OF A ROTARY WING AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 15/509446
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15509446
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/509446 | NOSE ATTITUDE CONTROL OF A ROTARY WING AIRCRAFT | Sep 23, 2015 | Abandoned |
Array
(
[id] => 11837267
[patent_doc_number] => 20170218986
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-08-03
[patent_title] => 'Profiled Element for Generating a Force'
[patent_app_type] => utility
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15500662
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/500662 | Profiled Element for Generating a Force | Sep 23, 2015 | Abandoned |