Search

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 numberTitle of the applicationFiling DateStatus
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 [patent_figures_cnt] => 3 [patent_no_of_words] => 3711 [patent_no_of_claims] => 7 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 146 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_figures_cnt] => 6 [patent_no_of_words] => 5995 [patent_no_of_claims] => 15 [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/A1/0001/20080001028.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 [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] => 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 [patent_figures_cnt] => 11 [patent_no_of_words] => 11972 [patent_no_of_claims] => 42 [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] => 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 [patent_no_of_ind_claims] => 1 [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 [patent_figures_cnt] => 0 [patent_no_of_words] => 271 [patent_no_of_claims] => 5 [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/A1/0267/20070267542.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 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 3054 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 121 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_app_date] => 2007-03-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 6482 [patent_no_of_claims] => 19 [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] => 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 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 11 [patent_no_of_words] => 7414 [patent_no_of_claims] => 19 [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/A1/0235/20070235583.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
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