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] => 3856963 [patent_doc_number] => 05823471 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-10-20 [patent_title] => 'System for controlling a control surface articulated to a structure of a vehicle' [patent_app_type] => 1 [patent_app_number] => 8/688095 [patent_app_country] => US [patent_app_date] => 1996-07-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 5 [patent_no_of_words] => 3589 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 307 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/823/05823471.pdf [firstpage_image] =>[orig_patent_app_number] => 688095 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/688095
System for controlling a control surface articulated to a structure of a vehicle Jul 28, 1996 Issued
Array ( [id] => 3867407 [patent_doc_number] => 05775640 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-07-07 [patent_title] => 'Landing installation for landing a tethered balloon' [patent_app_type] => 1 [patent_app_number] => 8/663074 [patent_app_country] => US [patent_app_date] => 1996-06-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 6 [patent_no_of_words] => 4984 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 186 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/775/05775640.pdf [firstpage_image] =>[orig_patent_app_number] => 663074 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/663074
Landing installation for landing a tethered balloon Jun 18, 1996 Issued
Array ( [id] => 3766445 [patent_doc_number] => 05820073 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-10-13 [patent_title] => 'Helicopter having a balanced torque transmission and no tail rotor' [patent_app_type] => 1 [patent_app_number] => 8/664595 [patent_app_country] => US [patent_app_date] => 1996-06-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 3 [patent_no_of_words] => 1613 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 76 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/820/05820073.pdf [firstpage_image] =>[orig_patent_app_number] => 664595 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/664595
Helicopter having a balanced torque transmission and no tail rotor Jun 16, 1996 Issued
Array ( [id] => 3792764 [patent_doc_number] => 05810290 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-09-22 [patent_title] => 'Vehicle seating rows, particularly airplane passenger seating rows' [patent_app_type] => 1 [patent_app_number] => 8/660234 [patent_app_country] => US [patent_app_date] => 1996-06-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 3796 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 229 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/810/05810290.pdf [firstpage_image] =>[orig_patent_app_number] => 660234 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/660234
Vehicle seating rows, particularly airplane passenger seating rows Jun 6, 1996 Issued
Array ( [id] => 3874508 [patent_doc_number] => 05722617 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-03-03 [patent_title] => 'Adjustable safety seat for a vehicle such as an aircraft' [patent_app_type] => 1 [patent_app_number] => 8/659195 [patent_app_country] => US [patent_app_date] => 1996-06-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 3 [patent_no_of_words] => 4082 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 157 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/722/05722617.pdf [firstpage_image] =>[orig_patent_app_number] => 659195 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/659195
Adjustable safety seat for a vehicle such as an aircraft Jun 5, 1996 Issued
Array ( [id] => 3861304 [patent_doc_number] => 05803409 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-09-08 [patent_title] => 'Method and apparatus for reducing the drag of flows over surfaces' [patent_app_type] => 1 [patent_app_number] => 8/659306 [patent_app_country] => US [patent_app_date] => 1996-06-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 11 [patent_no_of_words] => 5594 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 6 [patent_words_short_claim] => 68 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/803/05803409.pdf [firstpage_image] =>[orig_patent_app_number] => 659306 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/659306
Method and apparatus for reducing the drag of flows over surfaces Jun 5, 1996 Issued
Array ( [id] => 3775467 [patent_doc_number] => 05779194 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-07-14 [patent_title] => 'Joint for a cantilever arm on a satellite' [patent_app_type] => 1 [patent_app_number] => 8/655684 [patent_app_country] => US [patent_app_date] => 1996-06-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 6 [patent_no_of_words] => 2494 [patent_no_of_claims] => 7 [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/05/779/05779194.pdf [firstpage_image] =>[orig_patent_app_number] => 655684 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/655684
Joint for a cantilever arm on a satellite Jun 2, 1996 Issued
Array ( [id] => 3873240 [patent_doc_number] => 05713539 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-02-03 [patent_title] => 'Apparatus for locking aircraft controls' [patent_app_type] => 1 [patent_app_number] => 8/653894 [patent_app_country] => US [patent_app_date] => 1996-05-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 3 [patent_no_of_words] => 4065 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 269 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/713/05713539.pdf [firstpage_image] =>[orig_patent_app_number] => 653894 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/653894
Apparatus for locking aircraft controls May 27, 1996 Issued
Array ( [id] => 3755351 [patent_doc_number] => 05755405 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-05-26 [patent_title] => 'Parachute promotion' [patent_app_type] => 1 [patent_app_number] => 8/653015 [patent_app_country] => US [patent_app_date] => 1996-05-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 5 [patent_no_of_words] => 1623 [patent_no_of_claims] => 26 [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/05/755/05755405.pdf [firstpage_image] =>[orig_patent_app_number] => 653015 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/653015
Parachute promotion May 23, 1996 Issued
Array ( [id] => 3772384 [patent_doc_number] => 05839695 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-11-24 [patent_title] => 'Cruciform parachute design' [patent_app_type] => 1 [patent_app_number] => 8/650946 [patent_app_country] => US [patent_app_date] => 1996-05-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 5 [patent_no_of_words] => 5472 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 89 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/839/05839695.pdf [firstpage_image] =>[orig_patent_app_number] => 650946 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/650946
Cruciform parachute design May 19, 1996 Issued
Array ( [id] => 3797267 [patent_doc_number] => 05788185 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-08-04 [patent_title] => 'Aircraft seat having improved user lumbar load characteristics during a crash event' [patent_app_type] => 1 [patent_app_number] => 8/649575 [patent_app_country] => US [patent_app_date] => 1996-05-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 10 [patent_no_of_words] => 3600 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 229 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/788/05788185.pdf [firstpage_image] =>[orig_patent_app_number] => 649575 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/649575
Aircraft seat having improved user lumbar load characteristics during a crash event May 16, 1996 Issued
Array ( [id] => 3772416 [patent_doc_number] => 05839697 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-11-24 [patent_title] => 'Method and apparatus for turn coordination gain as a function of flap position' [patent_app_type] => 1 [patent_app_number] => 8/645616 [patent_app_country] => US [patent_app_date] => 1996-05-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 10 [patent_no_of_words] => 2872 [patent_no_of_claims] => 7 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 85 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/839/05839697.pdf [firstpage_image] =>[orig_patent_app_number] => 645616 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/645616
Method and apparatus for turn coordination gain as a function of flap position May 13, 1996 Issued
Array ( [id] => 3746831 [patent_doc_number] => 05720449 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-02-24 [patent_title] => 'Thrust reverser with doors for aircraft engine, equipped with safety systems preventing the untimely opening of the doors' [patent_app_type] => 1 [patent_app_number] => 8/638595 [patent_app_country] => US [patent_app_date] => 1996-04-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 2514 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 29 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/720/05720449.pdf [firstpage_image] =>[orig_patent_app_number] => 638595 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/638595
Thrust reverser with doors for aircraft engine, equipped with safety systems preventing the untimely opening of the doors Apr 28, 1996 Issued
Array ( [id] => 3982962 [patent_doc_number] => 05857646 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1999-01-12 [patent_title] => 'Aircraft de-icing and recovery system' [patent_app_type] => 1 [patent_app_number] => 8/634954 [patent_app_country] => US [patent_app_date] => 1996-04-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 3 [patent_no_of_words] => 1588 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 99 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/857/05857646.pdf [firstpage_image] =>[orig_patent_app_number] => 634954 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/634954
Aircraft de-icing and recovery system Apr 18, 1996 Issued
Array ( [id] => 3912924 [patent_doc_number] => 05927653 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1999-07-27 [patent_title] => 'Two-stage reusable earth-to-orbit aerospace vehicle and transport system' [patent_app_type] => 1 [patent_app_number] => 8/632786 [patent_app_country] => US [patent_app_date] => 1996-04-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 26 [patent_figures_cnt] => 35 [patent_no_of_words] => 16956 [patent_no_of_claims] => 57 [patent_no_of_ind_claims] => 8 [patent_words_short_claim] => 541 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/927/05927653.pdf [firstpage_image] =>[orig_patent_app_number] => 632786 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/632786
Two-stage reusable earth-to-orbit aerospace vehicle and transport system Apr 16, 1996 Issued
08/632031 AIRCRAFT LANDING GEAR HAVING AXLE TO BRAKE PLATE INTEGRATION Apr 9, 1996 Abandoned
Array ( [id] => 3818843 [patent_doc_number] => 05813629 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-09-29 [patent_title] => 'Airplane stretcher system' [patent_app_type] => 1 [patent_app_number] => 8/631734 [patent_app_country] => US [patent_app_date] => 1996-04-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 16 [patent_no_of_words] => 3644 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 234 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/813/05813629.pdf [firstpage_image] =>[orig_patent_app_number] => 631734 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/631734
Airplane stretcher system Apr 9, 1996 Issued
Array ( [id] => 3870885 [patent_doc_number] => 05797563 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-08-25 [patent_title] => 'System for increasing the aerodynamic and hydrodynamic efficiency of a vehicle in motion' [patent_app_type] => 1 [patent_app_number] => 8/625914 [patent_app_country] => US [patent_app_date] => 1996-04-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 14 [patent_figures_cnt] => 21 [patent_no_of_words] => 12967 [patent_no_of_claims] => 29 [patent_no_of_ind_claims] => 6 [patent_words_short_claim] => 139 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/797/05797563.pdf [firstpage_image] =>[orig_patent_app_number] => 625914 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/625914
System for increasing the aerodynamic and hydrodynamic efficiency of a vehicle in motion Mar 31, 1996 Issued
Array ( [id] => 3792779 [patent_doc_number] => 05810291 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-09-22 [patent_title] => 'Continuous moldline technology system' [patent_app_type] => 1 [patent_app_number] => 8/616485 [patent_app_country] => US [patent_app_date] => 1996-03-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 14 [patent_no_of_words] => 1701 [patent_no_of_claims] => 21 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 54 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/810/05810291.pdf [firstpage_image] =>[orig_patent_app_number] => 616485 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/616485
Continuous moldline technology system Mar 18, 1996 Issued
08/578545 OPERATING AIRCRAFT Mar 13, 1996 Abandoned
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