
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] => 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 |