
Medhat Badawi
Examiner (ID: 9809, Phone: (571)270-5983 , Office: P/3644 )
| Most Active Art Unit | 3642 |
| Art Unit(s) | 3642, 3647, 3644 |
| Total Applications | 1174 |
| Issued Applications | 964 |
| Pending Applications | 72 |
| Abandoned Applications | 176 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 10399104
[patent_doc_number] => 20150284112
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-10-08
[patent_title] => 'UNIFIED ORBIT AND ATTITUDE CONTROL FOR NANOSATELLITES USING PULSED ABLATIVE THRUSTERS'
[patent_app_type] => utility
[patent_app_number] => 14/245695
[patent_app_country] => US
[patent_app_date] => 2014-04-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 3026
[patent_no_of_claims] => 21
[patent_no_of_ind_claims] => 3
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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] => 14245695
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/245695 | Unified orbit and attitude control for nanosatellites using pulsed ablative thrusters | Apr 3, 2014 | Issued |
Array
(
[id] => 10389282
[patent_doc_number] => 20150274289
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-10-01
[patent_title] => 'VERTICALLY LANDING AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 14/231610
[patent_app_country] => US
[patent_app_date] => 2014-03-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2059
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/231610 | VERTICALLY LANDING AIRCRAFT | Mar 30, 2014 | Abandoned |
Array
(
[id] => 10185093
[patent_doc_number] => 09214777
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-12-15
[patent_title] => 'Landing gear electrical swivel'
[patent_app_type] => utility
[patent_app_number] => 14/223882
[patent_app_country] => US
[patent_app_date] => 2014-03-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 11
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/223882 | Landing gear electrical swivel | Mar 23, 2014 | Issued |
Array
(
[id] => 11225105
[patent_doc_number] => 09452819
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-09-27
[patent_title] => 'Flight control surface seal'
[patent_app_type] => utility
[patent_app_number] => 14/223062
[patent_app_country] => US
[patent_app_date] => 2014-03-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 6
[patent_no_of_words] => 2616
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14223062
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/223062 | Flight control surface seal | Mar 23, 2014 | Issued |
Array
(
[id] => 9755989
[patent_doc_number] => 20140286691
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-09-25
[patent_title] => 'Fuselage Structure For A Means Of Transport, Means Of Transport And Method For Producing A Fuselage Structure For A Means Of Transport'
[patent_app_type] => utility
[patent_app_number] => 14/218006
[patent_app_country] => US
[patent_app_date] => 2014-03-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14218006
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/218006 | Fuselage Structure For A Means Of Transport, Means Of Transport And Method For Producing A Fuselage Structure For A Means Of Transport | Mar 17, 2014 | Abandoned |
Array
(
[id] => 11153918
[patent_doc_number] => 09387921
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2016-07-12
[patent_title] => 'Self closing net door for aircraft'
[patent_app_type] => utility
[patent_app_number] => 14/206647
[patent_app_country] => US
[patent_app_date] => 2014-03-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 2170
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14206647
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/206647 | Self closing net door for aircraft | Mar 11, 2014 | Issued |
Array
(
[id] => 10775850
[patent_doc_number] => 20160122006
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-05-05
[patent_title] => 'LOW DRAG TURBULENCE GENERATORS FOR AIRCRAFT WINGS'
[patent_app_type] => utility
[patent_app_number] => 14/206015
[patent_app_country] => US
[patent_app_date] => 2014-03-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 1402
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14206015
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/206015 | LOW DRAG TURBULENCE GENERATORS FOR AIRCRAFT WINGS | Mar 11, 2014 | Abandoned |
Array
(
[id] => 12092209
[patent_doc_number] => 20170349302
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-12-07
[patent_title] => 'THRUSTER ARRANGEMENT FOR GEOSYNCHRONOUS ORBIT SPACECRAFT'
[patent_app_type] => utility
[patent_app_number] => 14/207389
[patent_app_country] => US
[patent_app_date] => 2014-03-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
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[patent_no_of_words] => 6197
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14207389
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/207389 | Thruster arrangement for geosynchronous orbit spacecraft | Mar 11, 2014 | Issued |
Array
(
[id] => 9728129
[patent_doc_number] => 20140263835
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-09-18
[patent_title] => 'INTEGRATED AIRCRAFT GALLEY SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 14/207106
[patent_app_country] => US
[patent_app_date] => 2014-03-12
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14207106
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/207106 | Integrated aircraft galley system | Mar 11, 2014 | Issued |
Array
(
[id] => 9716474
[patent_doc_number] => 20140252172
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-09-11
[patent_title] => 'SINGLE SURFACE ELECTRO-MECHANICAL ACTUATOR ASSEMBLY'
[patent_app_type] => utility
[patent_app_number] => 14/198090
[patent_app_country] => US
[patent_app_date] => 2014-03-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_no_of_words] => 3578
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14198090
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/198090 | SINGLE SURFACE ELECTRO-MECHANICAL ACTUATOR ASSEMBLY | Mar 4, 2014 | Abandoned |
Array
(
[id] => 12260309
[patent_doc_number] => 20180079504
[patent_country] => US
[patent_kind] => A9
[patent_issue_date] => 2018-03-22
[patent_title] => 'AIR VEHICLE FLIGHT MECHANISM AND CONTROL METHOD'
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[patent_app_number] => 14/198418
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14198418
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/198418 | Air vehicle flight mechanism and control method | Mar 4, 2014 | Issued |
Array
(
[id] => 12260309
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/198418 | Air vehicle flight mechanism and control method | Mar 4, 2014 | Issued |
Array
(
[id] => 9696855
[patent_doc_number] => 20140246541
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[patent_kind] => A1
[patent_issue_date] => 2014-09-04
[patent_title] => 'METHOD FOR THE GUIDANCE OF A ROTORCRAFT, WHICH METHOD LIMITS NOISE DISCOMFORT IN A PROCEDURE FOR THE APPROACH TO A LANDING POINT'
[patent_app_type] => utility
[patent_app_number] => 14/196102
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/196102 | Method for the guidance of a rotorcraft, which method limits noise discomfort in a procedure for the approach to a landing point | Mar 3, 2014 | Issued |
Array
(
[id] => 10347167
[patent_doc_number] => 20150232172
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-08-20
[patent_title] => 'AIRFOIL ASSEMBLY AND METHOD'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/185804 | AIRFOIL ASSEMBLY AND METHOD | Feb 19, 2014 | Abandoned |
Array
(
[id] => 10909154
[patent_doc_number] => 20140312169
[patent_country] => US
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[patent_issue_date] => 2014-10-23
[patent_title] => 'Aircraft System for Reduced Observer Visibility'
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Array
(
[id] => 10413787
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[patent_issue_date] => 2015-10-22
[patent_title] => 'Aircraft Having A System For Influencing The Yaw Moment And A Method For Influencing The Yaw Moment Of An Aircraft'
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[patent_app_number] => 14/181797
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/181797 | Aircraft Having A System For Influencing The Yaw Moment And A Method For Influencing The Yaw Moment Of An Aircraft | Feb 16, 2014 | Abandoned |
Array
(
[id] => 9927470
[patent_doc_number] => 20150075662
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-03-19
[patent_title] => 'DRAIN MASTS'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/178463 | Drain masts | Feb 11, 2014 | Issued |
Array
(
[id] => 9653921
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[patent_title] => 'SYSTEMS AND METHODS FOR CONTROLLING A MAGNITUDE OF A SONIC BOOM'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/176865 | Systems and methods for controlling a magnitude of a sonic boom | Feb 9, 2014 | Issued |
Array
(
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Array
(
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/161113 | Link member for connecting aircraft pylon to wing of aircraft, aircraft pylon, and aircraft | Jan 21, 2014 | Issued |