
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] => 8688391
[patent_doc_number] => 08387912
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-03-05
[patent_title] => 'Lifting foil'
[patent_app_type] => utility
[patent_app_number] => 12/508650
[patent_app_country] => US
[patent_app_date] => 2009-07-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 110
[patent_figures_cnt] => 196
[patent_no_of_words] => 30849
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 316
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12508650
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/508650 | Lifting foil | Jul 23, 2009 | Issued |
Array
(
[id] => 8270683
[patent_doc_number] => 08212194
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-07-03
[patent_title] => 'Aerospace articles made from quasi-isotropic chopped prepreg'
[patent_app_type] => utility
[patent_app_number] => 12/508777
[patent_app_country] => US
[patent_app_date] => 2009-07-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 3
[patent_no_of_words] => 3280
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 47
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12508777
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/508777 | Aerospace articles made from quasi-isotropic chopped prepreg | Jul 23, 2009 | Issued |
Array
(
[id] => 8590331
[patent_doc_number] => 08348201
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-01-08
[patent_title] => 'Actuator device based on a shape memory alloy, and a wing flap assembly fitted with such an actuator device'
[patent_app_type] => utility
[patent_app_number] => 12/507677
[patent_app_country] => US
[patent_app_date] => 2009-07-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 11
[patent_no_of_words] => 2677
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 2
[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] => 12507677
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/507677 | Actuator device based on a shape memory alloy, and a wing flap assembly fitted with such an actuator device | Jul 21, 2009 | Issued |
Array
(
[id] => 7985265
[patent_doc_number] => 08074925
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-12-13
[patent_title] => 'Aircraft attitude control configuration'
[patent_app_type] => utility
[patent_app_number] => 12/507573
[patent_app_country] => US
[patent_app_date] => 2009-07-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 34
[patent_no_of_words] => 12393
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 123
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/074/08074925.pdf
[firstpage_image] =>[orig_patent_app_number] => 12507573
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/507573 | Aircraft attitude control configuration | Jul 21, 2009 | Issued |
Array
(
[id] => 8673941
[patent_doc_number] => 08382045
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-02-26
[patent_title] => 'Shape-changing control surface'
[patent_app_type] => utility
[patent_app_number] => 12/506462
[patent_app_country] => US
[patent_app_date] => 2009-07-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
[patent_figures_cnt] => 14
[patent_no_of_words] => 6864
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 97
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12506462
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/506462 | Shape-changing control surface | Jul 20, 2009 | Issued |
Array
(
[id] => 8553663
[patent_doc_number] => 08328130
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-12-11
[patent_title] => 'Vertical take off and landing unmanned aerial vehicle airframe structure'
[patent_app_type] => utility
[patent_app_number] => 12/506052
[patent_app_country] => US
[patent_app_date] => 2009-07-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 16
[patent_no_of_words] => 5941
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[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] => 12506052
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/506052 | Vertical take off and landing unmanned aerial vehicle airframe structure | Jul 19, 2009 | Issued |
Array
(
[id] => 6573214
[patent_doc_number] => 20100096508
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-04-22
[patent_title] => 'Aircraft and method of retrieving a rescue cradle into the aircraft fuselage'
[patent_app_type] => utility
[patent_app_number] => 12/459877
[patent_app_country] => US
[patent_app_date] => 2009-07-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 2211
[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] => publications/A1/0096/20100096508.pdf
[firstpage_image] =>[orig_patent_app_number] => 12459877
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/459877 | Aircraft and method of retrieving a rescue cradle into the aircraft fuselage | Jul 8, 2009 | Issued |
Array
(
[id] => 8531958
[patent_doc_number] => 08308108
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-11-13
[patent_title] => 'Fuselage arrangement for airplane'
[patent_app_type] => utility
[patent_app_number] => 12/494919
[patent_app_country] => US
[patent_app_date] => 2009-06-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 7
[patent_no_of_words] => 4654
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 292
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12494919
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/494919 | Fuselage arrangement for airplane | Jun 29, 2009 | Issued |
Array
(
[id] => 8547783
[patent_doc_number] => 08322659
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-12-04
[patent_title] => 'Method for lightening the weight of fuel stowed onboard during an interplanetary mission'
[patent_app_type] => utility
[patent_app_number] => 12/494877
[patent_app_country] => US
[patent_app_date] => 2009-06-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 5
[patent_no_of_words] => 3787
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 160
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12494877
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/494877 | Method for lightening the weight of fuel stowed onboard during an interplanetary mission | Jun 29, 2009 | Issued |
Array
(
[id] => 8197723
[patent_doc_number] => 08186620
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-05-29
[patent_title] => 'Adjustable landing gear system'
[patent_app_type] => utility
[patent_app_number] => 12/491021
[patent_app_country] => US
[patent_app_date] => 2009-06-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 4420
[patent_no_of_claims] => 22
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 162
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/186/08186620.pdf
[firstpage_image] =>[orig_patent_app_number] => 12491021
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/491021 | Adjustable landing gear system | Jun 23, 2009 | Issued |
Array
(
[id] => 8434276
[patent_doc_number] => 08282042
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-10-09
[patent_title] => 'Skin panel joint for improved airflow'
[patent_app_type] => utility
[patent_app_number] => 12/489142
[patent_app_country] => US
[patent_app_date] => 2009-06-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 21
[patent_figures_cnt] => 28
[patent_no_of_words] => 10970
[patent_no_of_claims] => 24
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[patent_words_short_claim] => 184
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12489142
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/489142 | Skin panel joint for improved airflow | Jun 21, 2009 | Issued |
Array
(
[id] => 9284666
[patent_doc_number] => 08640985
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-02-04
[patent_title] => 'Co-rotating stacked rotor disks for improved hover performance'
[patent_app_type] => utility
[patent_app_number] => 13/321429
[patent_app_country] => US
[patent_app_date] => 2009-05-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_no_of_words] => 2555
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13321429
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/321429 | Co-rotating stacked rotor disks for improved hover performance | May 21, 2009 | Issued |
Array
(
[id] => 9284664
[patent_doc_number] => 08640983
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-02-04
[patent_title] => 'Rotor hub and controls for multi-bladed rotor system'
[patent_app_type] => utility
[patent_app_number] => 13/266729
[patent_app_country] => US
[patent_app_date] => 2009-05-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13266729
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/266729 | Rotor hub and controls for multi-bladed rotor system | May 20, 2009 | Issued |
Array
(
[id] => 7817277
[patent_doc_number] => 20120063897
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-03-15
[patent_title] => 'Differential Pitch-Control to Optimize Co-Rotating Stacked Rotor Performance'
[patent_app_type] => utility
[patent_app_number] => 13/321312
[patent_app_country] => US
[patent_app_date] => 2009-05-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0063/20120063897.pdf
[firstpage_image] =>[orig_patent_app_number] => 13321312
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/321312 | Differential pitch-control to optimize co-rotating stacked rotor performance | May 20, 2009 | Issued |
Array
(
[id] => 8758439
[patent_doc_number] => 08418955
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-04-16
[patent_title] => 'Control system for a hydraulically actuatable horizontal stabilizer and test method for testing the integrity of a control system'
[patent_app_type] => utility
[patent_app_number] => 12/992668
[patent_app_country] => US
[patent_app_date] => 2009-05-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
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[patent_no_of_words] => 6158
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12992668
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/992668 | Control system for a hydraulically actuatable horizontal stabilizer and test method for testing the integrity of a control system | May 14, 2009 | Issued |
Array
(
[id] => 8161100
[patent_doc_number] => 08172173
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-05-08
[patent_title] => 'Covert sensor emplacement using autorotational delivery mechanism'
[patent_app_type] => utility
[patent_app_number] => 12/436203
[patent_app_country] => US
[patent_app_date] => 2009-05-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
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[patent_no_of_words] => 4052
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/172/08172173.pdf
[firstpage_image] =>[orig_patent_app_number] => 12436203
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/436203 | Covert sensor emplacement using autorotational delivery mechanism | May 5, 2009 | Issued |
Array
(
[id] => 6326646
[patent_doc_number] => 20100327115
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-12-30
[patent_title] => 'AIRCRAFT POD STORE SEPARATION CHARACTERISTICS'
[patent_app_type] => utility
[patent_app_number] => 12/433142
[patent_app_country] => US
[patent_app_date] => 2009-04-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0327/20100327115.pdf
[firstpage_image] =>[orig_patent_app_number] => 12433142
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/433142 | AIRCRAFT POD STORE SEPARATION CHARACTERISTICS | Apr 29, 2009 | Abandoned |
Array
(
[id] => 5493179
[patent_doc_number] => 20090261207
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-10-22
[patent_title] => 'Stable aircraft'
[patent_app_type] => utility
[patent_app_number] => 12/386454
[patent_app_country] => US
[patent_app_date] => 2009-04-17
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[pdf_file] => publications/A1/0261/20090261207.pdf
[firstpage_image] =>[orig_patent_app_number] => 12386454
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/386454 | Stable aircraft | Apr 16, 2009 | Abandoned |
Array
(
[id] => 7554332
[patent_doc_number] => 08066229
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-11-29
[patent_title] => 'Attachable wing'
[patent_app_type] => utility
[patent_app_number] => 12/420038
[patent_app_country] => US
[patent_app_date] => 2009-04-07
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[pdf_file] => patents/08/066/08066229.pdf
[firstpage_image] =>[orig_patent_app_number] => 12420038
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/420038 | Attachable wing | Apr 6, 2009 | Issued |
Array
(
[id] => 8186229
[patent_doc_number] => 08181906
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-05-22
[patent_title] => 'Method and apparatus for ram deceleration in a launch system'
[patent_app_type] => utility
[patent_app_number] => 12/417418
[patent_app_country] => US
[patent_app_date] => 2009-04-02
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/181/08181906.pdf
[firstpage_image] =>[orig_patent_app_number] => 12417418
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/417418 | Method and apparatus for ram deceleration in a launch system | Apr 1, 2009 | Issued |