
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] => 8122627
[patent_doc_number] => 20120085861
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-04-12
[patent_title] => 'DEVICE FOR ACOUSTIC TREATMENT OF THE NOISE EMITTED BY A TURBOJET'
[patent_app_type] => utility
[patent_app_number] => 13/267327
[patent_app_country] => US
[patent_app_date] => 2011-10-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 4322
[patent_no_of_claims] => 13
[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] => publications/A1/0085/20120085861.pdf
[firstpage_image] =>[orig_patent_app_number] => 13267327
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/267327 | Device for acoustic treatment of the noise emitted by a turbojet | Oct 5, 2011 | Issued |
Array
(
[id] => 9045637
[patent_doc_number] => 08540188
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-09-24
[patent_title] => 'Aircraft actuator hydraulic apparatus'
[patent_app_type] => utility
[patent_app_number] => 13/250540
[patent_app_country] => US
[patent_app_date] => 2011-09-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 9328
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 189
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13250540
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/250540 | Aircraft actuator hydraulic apparatus | Sep 29, 2011 | Issued |
Array
(
[id] => 9880790
[patent_doc_number] => 08967543
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-03-03
[patent_title] => 'Aircraft ice protection system and aircraft provided with the same'
[patent_app_type] => utility
[patent_app_number] => 13/816562
[patent_app_country] => US
[patent_app_date] => 2011-08-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 9710
[patent_no_of_claims] => 11
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[patent_words_short_claim] => 133
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13816562
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/816562 | Aircraft ice protection system and aircraft provided with the same | Aug 29, 2011 | Issued |
Array
(
[id] => 8186245
[patent_doc_number] => 08181914
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-05-22
[patent_title] => 'Control stick adapted for use in a fly-by-wire flight control system, and linkage for use therein'
[patent_app_type] => utility
[patent_app_number] => 13/199008
[patent_app_country] => US
[patent_app_date] => 2011-08-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 10
[patent_no_of_words] => 6891
[patent_no_of_claims] => 32
[patent_no_of_ind_claims] => 1
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/181/08181914.pdf
[firstpage_image] =>[orig_patent_app_number] => 13199008
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/199008 | Control stick adapted for use in a fly-by-wire flight control system, and linkage for use therein | Aug 16, 2011 | Issued |
Array
(
[id] => 8186250
[patent_doc_number] => 08181915
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-05-22
[patent_title] => 'Control stick adapted for use in a fly-by-wire flight control system, and linkage for use therein'
[patent_app_type] => utility
[patent_app_number] => 13/199027
[patent_app_country] => US
[patent_app_date] => 2011-08-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 10
[patent_no_of_words] => 6891
[patent_no_of_claims] => 5
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[patent_words_short_claim] => 309
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/181/08181915.pdf
[firstpage_image] =>[orig_patent_app_number] => 13199027
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/199027 | Control stick adapted for use in a fly-by-wire flight control system, and linkage for use therein | Aug 16, 2011 | Issued |
Array
(
[id] => 8688390
[patent_doc_number] => 08387913
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-03-05
[patent_title] => 'Compact aircraft wing folding systems and methods'
[patent_app_type] => utility
[patent_app_number] => 13/206001
[patent_app_country] => US
[patent_app_date] => 2011-08-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 23
[patent_no_of_words] => 8172
[patent_no_of_claims] => 11
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13206001
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/206001 | Compact aircraft wing folding systems and methods | Aug 8, 2011 | Issued |
Array
(
[id] => 8705167
[patent_doc_number] => 20130062456
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-03-14
[patent_title] => 'Reconfigurable Rotor Blade'
[patent_app_type] => utility
[patent_app_number] => 13/698702
[patent_app_country] => US
[patent_app_date] => 2011-07-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 4202
[patent_no_of_claims] => 23
[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] => 13698702
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/698702 | Reconfigurable rotor blade | Jul 27, 2011 | Issued |
Array
(
[id] => 10868812
[patent_doc_number] => 08894002
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-11-25
[patent_title] => 'System and method for solar-powered airship'
[patent_app_type] => utility
[patent_app_number] => 13/182864
[patent_app_country] => US
[patent_app_date] => 2011-07-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 35
[patent_figures_cnt] => 38
[patent_no_of_words] => 12864
[patent_no_of_claims] => 39
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 220
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13182864
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/182864 | System and method for solar-powered airship | Jul 13, 2011 | Issued |
Array
(
[id] => 10862355
[patent_doc_number] => 08888039
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-11-18
[patent_title] => 'Method and device for the lateral stabilization of an aircraft'
[patent_app_type] => utility
[patent_app_number] => 13/810630
[patent_app_country] => US
[patent_app_date] => 2011-07-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_no_of_words] => 4323
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13810630
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/810630 | Method and device for the lateral stabilization of an aircraft | Jul 12, 2011 | Issued |
Array
(
[id] => 8954298
[patent_doc_number] => 08500065
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-08-06
[patent_title] => 'Device for supplying loads in the overhead area of a passenger cabin, in particular in commercial aircraft'
[patent_app_type] => utility
[patent_app_number] => 13/179794
[patent_app_country] => US
[patent_app_date] => 2011-07-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 1
[patent_no_of_words] => 944
[patent_no_of_claims] => 4
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 58
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13179794
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/179794 | Device for supplying loads in the overhead area of a passenger cabin, in particular in commercial aircraft | Jul 10, 2011 | Issued |
Array
(
[id] => 7814903
[patent_doc_number] => 20120061523
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-03-15
[patent_title] => 'SLATS WITH A FLEXIBLE TRAILING EDGE'
[patent_app_type] => utility
[patent_app_number] => 13/178533
[patent_app_country] => US
[patent_app_date] => 2011-07-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0061/20120061523.pdf
[firstpage_image] =>[orig_patent_app_number] => 13178533
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/178533 | Slats with a flexible trailing edge | Jul 7, 2011 | Issued |
Array
(
[id] => 7716731
[patent_doc_number] => 20120006945
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-01-12
[patent_title] => 'TRACTION KITE WITH HIGH PROJECTED LEADING EDGE'
[patent_app_type] => utility
[patent_app_number] => 13/178942
[patent_app_country] => US
[patent_app_date] => 2011-07-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[pdf_file] => publications/A1/0006/20120006945.pdf
[firstpage_image] =>[orig_patent_app_number] => 13178942
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/178942 | Traction kite with high projected leading edge | Jul 7, 2011 | Issued |
Array
(
[id] => 8764760
[patent_doc_number] => 20130092797
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-04-18
[patent_title] => 'WING TIP DEVICE'
[patent_app_type] => utility
[patent_app_number] => 13/805406
[patent_app_country] => US
[patent_app_date] => 2011-07-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
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[patent_no_of_words] => 5918
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13805406
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/805406 | Wing tip device | Jul 6, 2011 | Issued |
Array
(
[id] => 7750017
[patent_doc_number] => 20120025027
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-02-02
[patent_title] => 'System for Air Borne Deployment of Palletized Cargo'
[patent_app_type] => utility
[patent_app_number] => 13/173157
[patent_app_country] => US
[patent_app_date] => 2011-06-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0025/20120025027.pdf
[firstpage_image] =>[orig_patent_app_number] => 13173157
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/173157 | System for Air Borne Deployment of Palletized Cargo | Jun 29, 2011 | Abandoned |
Array
(
[id] => 8758441
[patent_doc_number] => 08418956
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-04-16
[patent_title] => 'Aircraft actuator hydraulic system'
[patent_app_type] => utility
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[patent_app_date] => 2011-06-27
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/169644 | Aircraft actuator hydraulic system | Jun 26, 2011 | Issued |
Array
(
[id] => 9748604
[patent_doc_number] => 08840070
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-09-23
[patent_title] => 'Power supply and control device for actuators, corresponding acutation assembly, and aircraft comprising such a device'
[patent_app_type] => utility
[patent_app_number] => 13/703341
[patent_app_country] => US
[patent_app_date] => 2011-06-17
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13703341
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/703341 | Power supply and control device for actuators, corresponding acutation assembly, and aircraft comprising such a device | Jun 16, 2011 | Issued |
Array
(
[id] => 8993428
[patent_doc_number] => 08517301
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2013-08-27
[patent_title] => 'Aircraft ground maintenance tether assembly'
[patent_app_type] => utility
[patent_app_number] => 13/153553
[patent_app_country] => US
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13153553
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/153553 | Aircraft ground maintenance tether assembly | Jun 5, 2011 | Issued |
Array
(
[id] => 7654514
[patent_doc_number] => 20110303783
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-12-15
[patent_title] => 'Stabilizer'
[patent_app_type] => utility
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[firstpage_image] =>[orig_patent_app_number] => 13150790
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/150790 | Stabilizer | May 31, 2011 | Issued |
Array
(
[id] => 8895250
[patent_doc_number] => 08474762
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[patent_kind] => B2
[patent_issue_date] => 2013-07-02
[patent_title] => 'Aircraft slat assembly'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/115864 | Aircraft slat assembly | May 24, 2011 | Issued |
Array
(
[id] => 7577051
[patent_doc_number] => 20110290933
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-12-01
[patent_title] => 'AIRCRAFT INCLUDING AN UNDERCARRIAGE MOTOR'
[patent_app_type] => utility
[patent_app_number] => 13/113627
[patent_app_country] => US
[patent_app_date] => 2011-05-23
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[pdf_file] => publications/A1/0290/20110290933.pdf
[firstpage_image] =>[orig_patent_app_number] => 13113627
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/113627 | Aircraft including an undercarriage motor | May 22, 2011 | Issued |