
Amanda Lee Bailey
Examiner (ID: 4785)
| Most Active Art Unit | 3673 |
| Art Unit(s) | 3673 |
| Total Applications | 468 |
| Issued Applications | 245 |
| Pending Applications | 48 |
| Abandoned Applications | 191 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 4856252
[patent_doc_number] => 20080265102
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-10-30
[patent_title] => 'DEPLOYABLE FLAP EDGE FENCE'
[patent_app_type] => utility
[patent_app_number] => 11/741713
[patent_app_country] => US
[patent_app_date] => 2007-04-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 5976
[patent_no_of_claims] => 30
[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] => publications/A1/0265/20080265102.pdf
[firstpage_image] =>[orig_patent_app_number] => 11741713
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/741713 | Deployable flap edge fence | Apr 26, 2007 | Issued |
Array
(
[id] => 78877
[patent_doc_number] => 07744032
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-06-29
[patent_title] => 'Power and imaging system for an airship'
[patent_app_type] => utility
[patent_app_number] => 11/796493
[patent_app_country] => US
[patent_app_date] => 2007-04-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 5
[patent_no_of_words] => 6031
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 151
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/744/07744032.pdf
[firstpage_image] =>[orig_patent_app_number] => 11796493
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/796493 | Power and imaging system for an airship | Apr 26, 2007 | Issued |
Array
(
[id] => 214488
[patent_doc_number] => 07618005
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2009-11-17
[patent_title] => 'Stealth bomber, transporter, air-to-air fueling tanker, and space plane'
[patent_app_type] => utility
[patent_app_number] => 11/789718
[patent_app_country] => US
[patent_app_date] => 2007-04-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 15
[patent_no_of_words] => 7682
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 181
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/618/07618005.pdf
[firstpage_image] =>[orig_patent_app_number] => 11789718
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/789718 | Stealth bomber, transporter, air-to-air fueling tanker, and space plane | Apr 24, 2007 | Issued |
Array
(
[id] => 4805804
[patent_doc_number] => 20080169382
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-07-17
[patent_title] => 'Sealing system for the gap existing between the fuselage and the elevator of an aircraft with orientable horizontal stabiliser'
[patent_app_type] => utility
[patent_app_number] => 11/790453
[patent_app_country] => US
[patent_app_date] => 2007-04-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 3651
[patent_no_of_claims] => 18
[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/A1/0169/20080169382.pdf
[firstpage_image] =>[orig_patent_app_number] => 11790453
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/790453 | Sealing system for the gap existing between the fuselage and the elevator of an aircraft with orientable horizontal stabilizer | Apr 24, 2007 | Issued |
Array
(
[id] => 172970
[patent_doc_number] => 07658349
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-02-09
[patent_title] => 'Pilot flight control stick haptic feedback system and method'
[patent_app_type] => utility
[patent_app_number] => 11/739479
[patent_app_country] => US
[patent_app_date] => 2007-04-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 6
[patent_no_of_words] => 4921
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 193
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/658/07658349.pdf
[firstpage_image] =>[orig_patent_app_number] => 11739479
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/739479 | Pilot flight control stick haptic feedback system and method | Apr 23, 2007 | Issued |
Array
(
[id] => 4843864
[patent_doc_number] => 20080180272
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-07-31
[patent_title] => 'Control System for an Aircraft'
[patent_app_type] => utility
[patent_app_number] => 11/739403
[patent_app_country] => US
[patent_app_date] => 2007-04-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 4186
[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] => publications/A1/0180/20080180272.pdf
[firstpage_image] =>[orig_patent_app_number] => 11739403
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/739403 | Control system for an aircraft | Apr 23, 2007 | Issued |
Array
(
[id] => 6491463
[patent_doc_number] => 20100209242
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-08-19
[patent_title] => 'Rotor Hub Vibration Attenuator'
[patent_app_type] => utility
[patent_app_number] => 12/595577
[patent_app_country] => US
[patent_app_date] => 2007-04-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 3997
[patent_no_of_claims] => 27
[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/A1/0209/20100209242.pdf
[firstpage_image] =>[orig_patent_app_number] => 12595577
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/595577 | Rotor hub vibration attenuator | Apr 23, 2007 | Issued |
Array
(
[id] => 4768471
[patent_doc_number] => 20080054125
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-03-06
[patent_title] => 'PARACHUTE RELEASE DEVICE'
[patent_app_type] => utility
[patent_app_number] => 11/739411
[patent_app_country] => US
[patent_app_date] => 2007-04-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 2108
[patent_no_of_claims] => 20
[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/A1/0054/20080054125.pdf
[firstpage_image] =>[orig_patent_app_number] => 11739411
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/739411 | PARACHUTE RELEASE DEVICE | Apr 23, 2007 | Abandoned |
Array
(
[id] => 99478
[patent_doc_number] => 07726601
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-06-01
[patent_title] => 'Device and method for affecting local climatic parameters'
[patent_app_type] => utility
[patent_app_number] => 11/785810
[patent_app_country] => US
[patent_app_date] => 2007-04-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 4
[patent_no_of_words] => 2456
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 91
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/726/07726601.pdf
[firstpage_image] =>[orig_patent_app_number] => 11785810
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/785810 | Device and method for affecting local climatic parameters | Apr 19, 2007 | Issued |
Array
(
[id] => 4925012
[patent_doc_number] => 20080164375
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-07-10
[patent_title] => 'Arrangement for coupling a coupling pivot for a trimmable horizontal stabiliser to the tail fuselage of an aircraft'
[patent_app_type] => utility
[patent_app_number] => 11/785729
[patent_app_country] => US
[patent_app_date] => 2007-04-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 3138
[patent_no_of_claims] => 19
[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/A1/0164/20080164375.pdf
[firstpage_image] =>[orig_patent_app_number] => 11785729
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/785729 | Arrangement for coupling a coupling pivot for a trimmable horizontal stabiliser to the tail fuselage of an aircraft | Apr 18, 2007 | Issued |
Array
(
[id] => 8531953
[patent_doc_number] => 08308103
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-11-13
[patent_title] => 'Insulation of an aircraft fuselage structure'
[patent_app_type] => utility
[patent_app_number] => 12/227499
[patent_app_country] => US
[patent_app_date] => 2007-04-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 7
[patent_no_of_words] => 4788
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 195
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12227499
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/227499 | Insulation of an aircraft fuselage structure | Apr 15, 2007 | Issued |
Array
(
[id] => 7594062
[patent_doc_number] => 07627404
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2009-12-01
[patent_title] => 'Singularity escape and avoidance using a virtual array rotation'
[patent_app_type] => utility
[patent_app_number] => 11/735145
[patent_app_country] => US
[patent_app_date] => 2007-04-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[patent_no_of_words] => 3711
[patent_no_of_claims] => 7
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/627/07627404.pdf
[firstpage_image] =>[orig_patent_app_number] => 11735145
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/735145 | Singularity escape and avoidance using a virtual array rotation | Apr 12, 2007 | Issued |
Array
(
[id] => 4930253
[patent_doc_number] => 20080001028
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-01-03
[patent_title] => 'Aircraft control system'
[patent_app_type] => utility
[patent_app_number] => 11/732109
[patent_app_country] => US
[patent_app_date] => 2007-04-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_no_of_words] => 5995
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0001/20080001028.pdf
[firstpage_image] =>[orig_patent_app_number] => 11732109
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/732109 | Aircraft control system | Apr 1, 2007 | Issued |
Array
(
[id] => 5123958
[patent_doc_number] => 20070236228
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-10-11
[patent_title] => 'BAGGAGE COMPARTMENT, IN PARTICULAR AN ENCLOSED COMPARTMENT FOR AN AIRCRAFT CABIN'
[patent_app_type] => utility
[patent_app_number] => 11/694278
[patent_app_country] => US
[patent_app_date] => 2007-03-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 2353
[patent_no_of_claims] => 8
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0236/20070236228.pdf
[firstpage_image] =>[orig_patent_app_number] => 11694278
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/694278 | Baggage compartment, in particular an enclosed compartment for an aircraft cabin | Mar 29, 2007 | Issued |
Array
(
[id] => 4820364
[patent_doc_number] => 20080121755
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-05-29
[patent_title] => 'Rankine-Brayton engine powered solar thermal aircraft'
[patent_app_type] => utility
[patent_app_number] => 11/731253
[patent_app_country] => US
[patent_app_date] => 2007-03-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0121/20080121755.pdf
[firstpage_image] =>[orig_patent_app_number] => 11731253
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/731253 | Rankine-Brayton engine powered solar thermal aircraft | Mar 28, 2007 | Issued |
Array
(
[id] => 165771
[patent_doc_number] => 07665694
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-02-23
[patent_title] => 'Dual action inlet door and method for use thereof'
[patent_app_type] => utility
[patent_app_number] => 11/691679
[patent_app_country] => US
[patent_app_date] => 2007-03-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 25
[patent_no_of_words] => 6906
[patent_no_of_claims] => 7
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[patent_words_short_claim] => 148
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/665/07665694.pdf
[firstpage_image] =>[orig_patent_app_number] => 11691679
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/691679 | Dual action inlet door and method for use thereof | Mar 26, 2007 | Issued |
Array
(
[id] => 5026096
[patent_doc_number] => 20070267542
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-11-22
[patent_title] => 'System and method for converting a passenger aircraft to a cargo aircraft'
[patent_app_type] => utility
[patent_app_number] => 11/728682
[patent_app_country] => US
[patent_app_date] => 2007-03-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0267/20070267542.pdf
[firstpage_image] =>[orig_patent_app_number] => 11728682
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/728682 | System and method for converting a passenger aircraft to a cargo aircraft | Mar 25, 2007 | Abandoned |
Array
(
[id] => 68871
[patent_doc_number] => 07753309
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-07-13
[patent_title] => 'VTOL/STOL tilt-prop flying wing'
[patent_app_type] => utility
[patent_app_number] => 11/689519
[patent_app_country] => US
[patent_app_date] => 2007-03-22
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/753/07753309.pdf
[firstpage_image] =>[orig_patent_app_number] => 11689519
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/689519 | VTOL/STOL tilt-prop flying wing | Mar 21, 2007 | Issued |
Array
(
[id] => 4836450
[patent_doc_number] => 20080277525
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-11-13
[patent_title] => 'HYDRAULIC DISTRIBUTOR FOR AIRPLANE LANDING GEAR'
[patent_app_type] => utility
[patent_app_number] => 11/689715
[patent_app_country] => US
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[pdf_file] => publications/A1/0277/20080277525.pdf
[firstpage_image] =>[orig_patent_app_number] => 11689715
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/689715 | Hydraulic distributor for airplane landing gear | Mar 21, 2007 | Issued |
Array
(
[id] => 5123313
[patent_doc_number] => 20070235583
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-10-11
[patent_title] => 'LIGHTER-THAN-AIR AIRCRAFT INCLUDING A CLOSED LOOP COMBUSTION GENERATING SYSTEM AND RELATED METHODS FOR POWERING THE SAME'
[patent_app_type] => utility
[patent_app_number] => 11/687970
[patent_app_country] => US
[patent_app_date] => 2007-03-19
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0235/20070235583.pdf
[firstpage_image] =>[orig_patent_app_number] => 11687970
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/687970 | LIGHTER-THAN-AIR AIRCRAFT INCLUDING A CLOSED LOOP COMBUSTION GENERATING SYSTEM AND RELATED METHODS FOR POWERING THE SAME | Mar 18, 2007 | Abandoned |