Search

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 numberTitle of the applicationFiling DateStatus
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 [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] => 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 [patent_no_of_claims] => 20 [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] => 14231610 [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 [patent_no_of_words] => 4619 [patent_no_of_claims] => 3 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 185 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14223882 [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 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 145 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_figures_cnt] => 7 [patent_no_of_words] => 5736 [patent_no_of_claims] => 15 [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] => 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 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 197 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [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] => 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 [patent_figures_cnt] => 10 [patent_no_of_words] => 6197 [patent_no_of_claims] => 25 [patent_no_of_ind_claims] => 4 [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] => 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 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 1822 [patent_no_of_claims] => 7 [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] => 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 [patent_figures_cnt] => 5 [patent_no_of_words] => 3578 [patent_no_of_claims] => 20 [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] => 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' [patent_app_type] => utility [patent_app_number] => 14/198418 [patent_app_country] => US [patent_app_date] => 2014-03-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 44 [patent_figures_cnt] => 44 [patent_no_of_words] => 11133 [patent_no_of_claims] => 21 [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] => 14198418 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/198418
Air vehicle flight mechanism and control method Mar 4, 2014 Issued
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' [patent_app_type] => utility [patent_app_number] => 14/198418 [patent_app_country] => US [patent_app_date] => 2014-03-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 44 [patent_figures_cnt] => 44 [patent_no_of_words] => 11133 [patent_no_of_claims] => 21 [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] => 14198418 [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 [patent_country] => US [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 [patent_app_country] => US [patent_app_date] => 2014-03-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 10412 [patent_no_of_claims] => 21 [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] => 14196102 [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' [patent_app_type] => utility [patent_app_number] => 14/185804 [patent_app_country] => US [patent_app_date] => 2014-02-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 3832 [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] => 14185804 [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 [patent_kind] => A1 [patent_issue_date] => 2014-10-23 [patent_title] => 'Aircraft System for Reduced Observer Visibility' [patent_app_type] => utility [patent_app_number] => 14/184542 [patent_app_country] => US [patent_app_date] => 2014-02-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 14 [patent_figures_cnt] => 14 [patent_no_of_words] => 5277 [patent_no_of_claims] => 32 [patent_no_of_ind_claims] => 4 [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] => 14184542 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/184542
Aircraft system for reduced observer visibility Feb 18, 2014 Issued
Array ( [id] => 10413787 [patent_doc_number] => 20150298797 [patent_country] => US [patent_kind] => A1 [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' [patent_app_type] => utility [patent_app_number] => 14/181797 [patent_app_country] => US [patent_app_date] => 2014-02-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 5581 [patent_no_of_claims] => 15 [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] => 14181797 [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' [patent_app_type] => utility [patent_app_number] => 14/178463 [patent_app_country] => US [patent_app_date] => 2014-02-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 2995 [patent_no_of_claims] => 15 [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] => 14178463 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/178463
Drain masts Feb 11, 2014 Issued
Array ( [id] => 9653921 [patent_doc_number] => 20140224926 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-08-14 [patent_title] => 'SYSTEMS AND METHODS FOR CONTROLLING A MAGNITUDE OF A SONIC BOOM' [patent_app_type] => utility [patent_app_number] => 14/176865 [patent_app_country] => US [patent_app_date] => 2014-02-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 12 [patent_no_of_words] => 9762 [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] => 14176865 [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 ( [id] => 11773167 [patent_doc_number] => 09381993 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2016-07-05 [patent_title] => 'Airframe panel for aircraft and aircraft wing' [patent_app_type] => utility [patent_app_number] => 14/161047 [patent_app_country] => US [patent_app_date] => 2014-01-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 13 [patent_no_of_words] => 3581 [patent_no_of_claims] => 5 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 229 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14161047 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/161047
Airframe panel for aircraft and aircraft wing Jan 21, 2014 Issued
Array ( [id] => 11568345 [patent_doc_number] => 20170106989 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2017-04-20 [patent_title] => 'LINK MEMBER FOR CONNECTING AIRCRAFT PYLON TO WING OF AIRCRAFT, AIRCRAFT PYLON, AND AIRCRAFT' [patent_app_type] => utility [patent_app_number] => 14/161113 [patent_app_country] => US [patent_app_date] => 2014-01-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 4296 [patent_no_of_claims] => 8 [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] => 14161113 [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
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