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] => 7338004 [patent_doc_number] => 20040245390 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-12-09 [patent_title] => 'Emergency oxygen supply system for an aircraft' [patent_app_type] => new [patent_app_number] => 10/850655 [patent_app_country] => US [patent_app_date] => 2004-05-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2325 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 110 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0245/20040245390.pdf [firstpage_image] =>[orig_patent_app_number] => 10850655 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/850655
Emergency oxygen supply system for an aircraft May 20, 2004 Abandoned
Array ( [id] => 7337964 [patent_doc_number] => 20040245377 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-12-09 [patent_title] => 'Helicopter' [patent_app_type] => new [patent_app_number] => 10/849132 [patent_app_country] => US [patent_app_date] => 2004-05-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 4057 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 38 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0245/20040245377.pdf [firstpage_image] =>[orig_patent_app_number] => 10849132 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/849132
Helicopter having a fusilage section and a tail section coupled thereto May 19, 2004 Issued
Array ( [id] => 4737000 [patent_doc_number] => 20080230652 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-09-25 [patent_title] => 'COMPOSITE BARREL SECTIONS FOR AIRCRAFT FUSELAGES AND OTHER STRUCTURES, AND METHODS AND SYSTEMS FOR MANUFACTURING SUCH BARREL SECTIONS' [patent_app_type] => utility [patent_app_number] => 10/851381 [patent_app_country] => US [patent_app_date] => 2004-05-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 12 [patent_no_of_words] => 7642 [patent_no_of_claims] => 50 [patent_no_of_ind_claims] => 13 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0230/20080230652.pdf [firstpage_image] =>[orig_patent_app_number] => 10851381 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/851381
Composite barrel sections for aircraft fuselages and other structures, and methods and systems for manufacturing such barrel sections May 19, 2004 Issued
Array ( [id] => 436138 [patent_doc_number] => 07262395 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2007-08-28 [patent_title] => 'Expendable sonobuoy flight kit with aerodynamically assisted sonobuoy separation' [patent_app_type] => utility [patent_app_number] => 10/848131 [patent_app_country] => US [patent_app_date] => 2004-05-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 3935 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 173 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/262/07262395.pdf [firstpage_image] =>[orig_patent_app_number] => 10848131 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/848131
Expendable sonobuoy flight kit with aerodynamically assisted sonobuoy separation May 18, 2004 Issued
Array ( [id] => 7212863 [patent_doc_number] => 20050253021 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-11-17 [patent_title] => 'Operational ground support system' [patent_app_type] => utility [patent_app_number] => 10/847739 [patent_app_country] => US [patent_app_date] => 2004-05-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 22 [patent_figures_cnt] => 22 [patent_no_of_words] => 10329 [patent_no_of_claims] => 40 [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/A1/0253/20050253021.pdf [firstpage_image] =>[orig_patent_app_number] => 10847739 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/847739
Operational ground support system May 16, 2004 Abandoned
Array ( [id] => 7212827 [patent_doc_number] => 20050253016 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-11-17 [patent_title] => 'Structural mode shape alignment' [patent_app_type] => utility [patent_app_number] => 10/846861 [patent_app_country] => US [patent_app_date] => 2004-05-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 3967 [patent_no_of_claims] => 21 [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/A1/0253/20050253016.pdf [firstpage_image] =>[orig_patent_app_number] => 10846861 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/846861
Structural mode shape alignment May 13, 2004 Issued
Array ( [id] => 5087820 [patent_doc_number] => 20070227459 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-10-04 [patent_title] => 'Fish acclimation transfer line' [patent_app_type] => utility [patent_app_number] => 10/845428 [patent_app_country] => US [patent_app_date] => 2004-05-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 3054 [patent_no_of_claims] => 5 [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/A1/0227/20070227459.pdf [firstpage_image] =>[orig_patent_app_number] => 10845428 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/845428
Fish acclimation transfer line May 11, 2004 Abandoned
Array ( [id] => 716880 [patent_doc_number] => 07048230 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2006-05-23 [patent_title] => 'Laminar flow nacelle for an aircraft engine' [patent_app_type] => utility [patent_app_number] => 10/842446 [patent_app_country] => US [patent_app_date] => 2004-05-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 6 [patent_no_of_words] => 2732 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 169 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/048/07048230.pdf [firstpage_image] =>[orig_patent_app_number] => 10842446 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/842446
Laminar flow nacelle for an aircraft engine May 10, 2004 Issued
Array ( [id] => 450470 [patent_doc_number] => 07246773 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2007-07-24 [patent_title] => 'Low power, pulsed, electro-thermal ice protection system' [patent_app_type] => utility [patent_app_number] => 10/840736 [patent_app_country] => US [patent_app_date] => 2004-05-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 15 [patent_no_of_words] => 10535 [patent_no_of_claims] => 23 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 161 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/246/07246773.pdf [firstpage_image] =>[orig_patent_app_number] => 10840736 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/840736
Low power, pulsed, electro-thermal ice protection system May 5, 2004 Issued
Array ( [id] => 5832034 [patent_doc_number] => 20060243864 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-11-02 [patent_title] => 'UNITIZED ROTARY ACTUATOR HINGE FITTING' [patent_app_type] => utility [patent_app_number] => 10/838959 [patent_app_country] => US [patent_app_date] => 2004-05-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 2838 [patent_no_of_claims] => 20 [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/A1/0243/20060243864.pdf [firstpage_image] =>[orig_patent_app_number] => 10838959 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/838959
Unitized rotary actuator hinge fitting May 3, 2004 Issued
Array ( [id] => 424314 [patent_doc_number] => 07270295 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2007-09-18 [patent_title] => 'Solar thermal aircraft' [patent_app_type] => utility [patent_app_number] => 10/835665 [patent_app_country] => US [patent_app_date] => 2004-04-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 21 [patent_no_of_words] => 8592 [patent_no_of_claims] => 96 [patent_no_of_ind_claims] => 6 [patent_words_short_claim] => 30 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/270/07270295.pdf [firstpage_image] =>[orig_patent_app_number] => 10835665 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/835665
Solar thermal aircraft Apr 29, 2004 Issued
Array ( [id] => 7066852 [patent_doc_number] => 20050242234 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-11-03 [patent_title] => 'Lifters, methods of flight control and maneuver load alleviation' [patent_app_type] => utility [patent_app_number] => 10/837464 [patent_app_country] => US [patent_app_date] => 2004-04-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 6230 [patent_no_of_claims] => 43 [patent_no_of_ind_claims] => 9 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0242/20050242234.pdf [firstpage_image] =>[orig_patent_app_number] => 10837464 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/837464
Lifters, methods of flight control and maneuver load alleviation Apr 28, 2004 Abandoned
Array ( [id] => 424321 [patent_doc_number] => 07270302 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2007-09-18 [patent_title] => 'Scalable thermal control system for spacecraft mounted instrumentation' [patent_app_type] => utility [patent_app_number] => 10/829358 [patent_app_country] => US [patent_app_date] => 2004-04-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 5 [patent_no_of_words] => 4096 [patent_no_of_claims] => 21 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 118 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/270/07270302.pdf [firstpage_image] =>[orig_patent_app_number] => 10829358 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/829358
Scalable thermal control system for spacecraft mounted instrumentation Apr 21, 2004 Issued
Array ( [id] => 6923265 [patent_doc_number] => 20050236520 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-10-27 [patent_title] => 'Flying amphibious SUV' [patent_app_type] => utility [patent_app_number] => 10/828777 [patent_app_country] => US [patent_app_date] => 2004-04-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 2312 [patent_no_of_claims] => 12 [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/A1/0236/20050236520.pdf [firstpage_image] =>[orig_patent_app_number] => 10828777 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/828777
Flying amphibious SUV Apr 21, 2004 Issued
Array ( [id] => 704664 [patent_doc_number] => 07059570 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2006-06-13 [patent_title] => 'Aerial delivery device' [patent_app_type] => utility [patent_app_number] => 10/709186 [patent_app_country] => US [patent_app_date] => 2004-04-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 17 [patent_no_of_words] => 5465 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 88 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/059/07059570.pdf [firstpage_image] =>[orig_patent_app_number] => 10709186 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/709186
Aerial delivery device Apr 19, 2004 Issued
Array ( [id] => 396506 [patent_doc_number] => 07293737 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2007-11-13 [patent_title] => 'Co-cured stringers and associated mandrel and fabrication method' [patent_app_type] => utility [patent_app_number] => 10/830291 [patent_app_country] => US [patent_app_date] => 2004-04-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 3756 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 60 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/293/07293737.pdf [firstpage_image] =>[orig_patent_app_number] => 10830291 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/830291
Co-cured stringers and associated mandrel and fabrication method Apr 19, 2004 Issued
Array ( [id] => 977580 [patent_doc_number] => 06929219 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2005-08-16 [patent_title] => 'Derivative aircraft and methods for their manufacture' [patent_app_type] => utility [patent_app_number] => 10/827460 [patent_app_country] => US [patent_app_date] => 2004-04-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 10 [patent_no_of_words] => 5667 [patent_no_of_claims] => 29 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 125 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/929/06929219.pdf [firstpage_image] =>[orig_patent_app_number] => 10827460 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/827460
Derivative aircraft and methods for their manufacture Apr 18, 2004 Issued
Array ( [id] => 660813 [patent_doc_number] => 07100872 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2006-09-05 [patent_title] => 'Lavatory fast pack system and method' [patent_app_type] => utility [patent_app_number] => 10/825906 [patent_app_country] => US [patent_app_date] => 2004-04-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 6 [patent_no_of_words] => 2376 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 61 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/100/07100872.pdf [firstpage_image] =>[orig_patent_app_number] => 10825906 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/825906
Lavatory fast pack system and method Apr 14, 2004 Issued
Array ( [id] => 7337962 [patent_doc_number] => 20040245376 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-12-09 [patent_title] => 'Rotor and aircraft passively stable in hover' [patent_app_type] => new [patent_app_number] => 10/824492 [patent_app_country] => US [patent_app_date] => 2004-04-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 7429 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 35 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0245/20040245376.pdf [firstpage_image] =>[orig_patent_app_number] => 10824492 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/824492
Rotor and aircraft passively stable in hover Apr 14, 2004 Issued
Array ( [id] => 6963638 [patent_doc_number] => 20050230535 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-10-20 [patent_title] => 'Immersible unmanned air vehicle and system for launch, recovery, and re-launch at sea' [patent_app_type] => utility [patent_app_number] => 10/823434 [patent_app_country] => US [patent_app_date] => 2004-04-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 2759 [patent_no_of_claims] => 21 [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/A1/0230/20050230535.pdf [firstpage_image] =>[orig_patent_app_number] => 10823434 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/823434
Immersible unmanned air vehicle and system for launch, recovery, and re-launch at sea Apr 12, 2004 Issued
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