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] => 6819932 [patent_doc_number] => 20030218093 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2003-11-27 [patent_title] => 'TRANSMISSION FOR A COAXIAL COUNTER ROTATING ROTOR SYSTEM' [patent_app_type] => new [patent_app_number] => 10/153970 [patent_app_country] => US [patent_app_date] => 2002-05-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 2791 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 47 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0218/20030218093.pdf [firstpage_image] =>[orig_patent_app_number] => 10153970 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/153970
Transmission for a coaxial counter rotating rotor system May 22, 2002 Issued
Array ( [id] => 799848 [patent_doc_number] => 07424988 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2008-09-16 [patent_title] => 'Use of aerodynamic forces to assist in the control and positioning of aircraft control surfaces and variable geometry systems' [patent_app_type] => utility [patent_app_number] => 10/482314 [patent_app_country] => US [patent_app_date] => 2002-05-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 7052 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 191 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/424/07424988.pdf [firstpage_image] =>[orig_patent_app_number] => 10482314 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/482314
Use of aerodynamic forces to assist in the control and positioning of aircraft control surfaces and variable geometry systems May 22, 2002 Issued
Array ( [id] => 1051849 [patent_doc_number] => 06857602 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2005-02-22 [patent_title] => 'Environmental control system and method of using the same' [patent_app_type] => utility [patent_app_number] => 10/152907 [patent_app_country] => US [patent_app_date] => 2002-05-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 17 [patent_no_of_words] => 12151 [patent_no_of_claims] => 49 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 101 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/857/06857602.pdf [firstpage_image] =>[orig_patent_app_number] => 10152907 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/152907
Environmental control system and method of using the same May 21, 2002 Issued
Array ( [id] => 6723328 [patent_doc_number] => 20030205640 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2003-11-06 [patent_title] => 'HYPERSONIC WAVERIDER VARIABLE LEADING EDGE FLAPS' [patent_app_type] => new [patent_app_number] => 10/138610 [patent_app_country] => US [patent_app_date] => 2002-05-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 2120 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 120 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0205/20030205640.pdf [firstpage_image] =>[orig_patent_app_number] => 10138610 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/138610
Hypersonic waverider variable leading edge flaps May 2, 2002 Issued
Array ( [id] => 1316107 [patent_doc_number] => 06601801 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2003-08-05 [patent_title] => 'Gapped trailing-edge control surface for an airfoil' [patent_app_type] => B1 [patent_app_number] => 10/131109 [patent_app_country] => US [patent_app_date] => 2002-04-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 13 [patent_no_of_words] => 4001 [patent_no_of_claims] => 25 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 247 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/601/06601801.pdf [firstpage_image] =>[orig_patent_app_number] => 10131109 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/131109
Gapped trailing-edge control surface for an airfoil Apr 23, 2002 Issued
Array ( [id] => 1277849 [patent_doc_number] => 06637702 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2003-10-28 [patent_title] => 'Nested beam deployable solar array' [patent_app_type] => B1 [patent_app_number] => 10/128421 [patent_app_country] => US [patent_app_date] => 2002-04-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 4705 [patent_no_of_claims] => 22 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 60 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/637/06637702.pdf [firstpage_image] =>[orig_patent_app_number] => 10128421 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/128421
Nested beam deployable solar array Apr 23, 2002 Issued
Array ( [id] => 636233 [patent_doc_number] => 07124982 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2006-10-24 [patent_title] => 'Device for bracing a shell in an aircraft fuselage' [patent_app_type] => utility [patent_app_number] => 10/479663 [patent_app_country] => US [patent_app_date] => 2002-04-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 8 [patent_no_of_words] => 977 [patent_no_of_claims] => 2 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 168 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/124/07124982.pdf [firstpage_image] =>[orig_patent_app_number] => 10479663 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/479663
Device for bracing a shell in an aircraft fuselage Apr 22, 2002 Issued
Array ( [id] => 1145791 [patent_doc_number] => 06766979 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2004-07-27 [patent_title] => 'Guidance seeker system with optically triggered diverter elements' [patent_app_type] => B2 [patent_app_number] => 10/123459 [patent_app_country] => US [patent_app_date] => 2002-04-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 9 [patent_no_of_words] => 3212 [patent_no_of_claims] => 8 [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] => patents/06/766/06766979.pdf [firstpage_image] =>[orig_patent_app_number] => 10123459 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/123459
Guidance seeker system with optically triggered diverter elements Apr 15, 2002 Issued
Array ( [id] => 1013649 [patent_doc_number] => 06892988 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2005-05-17 [patent_title] => 'Cylindrical wing tip with helical slot' [patent_app_type] => utility [patent_app_number] => 10/474879 [patent_app_country] => US [patent_app_date] => 2002-04-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 4521 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 69 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/892/06892988.pdf [firstpage_image] =>[orig_patent_app_number] => 10474879 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/474879
Cylindrical wing tip with helical slot Apr 8, 2002 Issued
Array ( [id] => 1019520 [patent_doc_number] => 06886782 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2005-05-03 [patent_title] => 'System for supplying an aircraft with cool air' [patent_app_type] => utility [patent_app_number] => 10/121475 [patent_app_country] => US [patent_app_date] => 2002-04-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 2 [patent_no_of_words] => 1992 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 74 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/886/06886782.pdf [firstpage_image] =>[orig_patent_app_number] => 10121475 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/121475
System for supplying an aircraft with cool air Apr 7, 2002 Issued
Array ( [id] => 1277841 [patent_doc_number] => 06637701 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2003-10-28 [patent_title] => 'Gimbaled ion thruster arrangement for high efficiency stationkeeping' [patent_app_type] => B1 [patent_app_number] => 10/114472 [patent_app_country] => US [patent_app_date] => 2002-04-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 7 [patent_no_of_words] => 4503 [patent_no_of_claims] => 30 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 117 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/637/06637701.pdf [firstpage_image] =>[orig_patent_app_number] => 10114472 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/114472
Gimbaled ion thruster arrangement for high efficiency stationkeeping Apr 2, 2002 Issued
Array ( [id] => 6533941 [patent_doc_number] => 20020162916 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2002-11-07 [patent_title] => 'Fast evacuation device for aircraft' [patent_app_type] => new [patent_app_number] => 10/112727 [patent_app_country] => US [patent_app_date] => 2002-04-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 4856 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 118 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0162/20020162916.pdf [firstpage_image] =>[orig_patent_app_number] => 10112727 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/112727
Fast evacuation device for aircraft Apr 1, 2002 Issued
Array ( [id] => 6727529 [patent_doc_number] => 20030183719 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2003-10-02 [patent_title] => 'AIRCRAFT FERRYING SYSTEM AND METHOD THEREOF' [patent_app_type] => new [patent_app_number] => 10/112144 [patent_app_country] => US [patent_app_date] => 2002-04-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 3060 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 70 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0183/20030183719.pdf [firstpage_image] =>[orig_patent_app_number] => 10112144 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/112144
Aircraft ferrying system and method thereof Mar 31, 2002 Issued
Array ( [id] => 6727538 [patent_doc_number] => 20030183728 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2003-10-02 [patent_title] => 'Aircraft control surface controller and associated method' [patent_app_type] => new [patent_app_number] => 10/112815 [patent_app_country] => US [patent_app_date] => 2002-03-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 6117 [patent_no_of_claims] => 43 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 44 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0183/20030183728.pdf [firstpage_image] =>[orig_patent_app_number] => 10112815 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/112815
Aircraft control surface controller and associated method Mar 28, 2002 Abandoned
Array ( [id] => 792368 [patent_doc_number] => 06981671 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2006-01-03 [patent_title] => 'Airframe structure-integrated capacitor' [patent_app_type] => utility [patent_app_number] => 10/109396 [patent_app_country] => US [patent_app_date] => 2002-03-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 13 [patent_figures_cnt] => 18 [patent_no_of_words] => 19412 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 102 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/981/06981671.pdf [firstpage_image] =>[orig_patent_app_number] => 10109396 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/109396
Airframe structure-integrated capacitor Mar 27, 2002 Issued
Array ( [id] => 1341453 [patent_doc_number] => 06575404 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2003-06-10 [patent_title] => 'Air intake and flying device, particularly a missile, equipped with such an air intake' [patent_app_type] => B2 [patent_app_number] => 10/106209 [patent_app_country] => US [patent_app_date] => 2002-03-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 5 [patent_no_of_words] => 3463 [patent_no_of_claims] => 5 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 233 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/575/06575404.pdf [firstpage_image] =>[orig_patent_app_number] => 10106209 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/106209
Air intake and flying device, particularly a missile, equipped with such an air intake Mar 26, 2002 Issued
Array ( [id] => 7030601 [patent_doc_number] => 20050029402 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-02-10 [patent_title] => 'Aircraft configuration with improved aerodynamic performance' [patent_app_type] => utility [patent_app_number] => 10/491327 [patent_app_country] => US [patent_app_date] => 2002-03-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 3003 [patent_no_of_claims] => 11 [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/A1/0029/20050029402.pdf [firstpage_image] =>[orig_patent_app_number] => 10491327 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/491327
Aircraft configuration with improved aerodynamic performance Mar 26, 2002 Issued
Array ( [id] => 696520 [patent_doc_number] => 07066431 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2006-06-27 [patent_title] => 'Turbulent flow drag reduction' [patent_app_type] => utility [patent_app_number] => 10/474006 [patent_app_country] => US [patent_app_date] => 2002-03-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 6 [patent_no_of_words] => 3876 [patent_no_of_claims] => 29 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 106 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/066/07066431.pdf [firstpage_image] =>[orig_patent_app_number] => 10474006 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/474006
Turbulent flow drag reduction Mar 25, 2002 Issued
Array ( [id] => 750174 [patent_doc_number] => 07017863 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2006-03-28 [patent_title] => 'Turbulent flow drag reduction' [patent_app_type] => utility [patent_app_number] => 10/474008 [patent_app_country] => US [patent_app_date] => 2002-03-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 6 [patent_no_of_words] => 3277 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 113 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/017/07017863.pdf [firstpage_image] =>[orig_patent_app_number] => 10474008 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/474008
Turbulent flow drag reduction Mar 25, 2002 Issued
Array ( [id] => 6153596 [patent_doc_number] => 20020145076 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2002-10-10 [patent_title] => 'AIRCRAFT' [patent_app_type] => new [patent_app_number] => 10/105334 [patent_app_country] => US [patent_app_date] => 2002-03-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2849 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 55 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0145/20020145076.pdf [firstpage_image] =>[orig_patent_app_number] => 10105334 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/105334
AIRCRAFT Mar 25, 2002 Abandoned
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