
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] => 3673890
[patent_doc_number] => 05695157
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1997-12-09
[patent_title] => 'Device for assistance in the piloting of an aircraft at the landing stage'
[patent_app_type] => 1
[patent_app_number] => 8/542326
[patent_app_country] => US
[patent_app_date] => 1995-10-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 1
[patent_no_of_words] => 1124
[patent_no_of_claims] => 4
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 131
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/695/05695157.pdf
[firstpage_image] =>[orig_patent_app_number] => 542326
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/542326 | Device for assistance in the piloting of an aircraft at the landing stage | Oct 11, 1995 | Issued |
| 08/533486 | INFANT TRANSPORTING MEANS FOR AIRPLANES | Sep 24, 1995 | Abandoned |
Array
(
[id] => 3811923
[patent_doc_number] => 05730392
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-03-24
[patent_title] => 'Adjustable fairing for thrust reversers'
[patent_app_type] => 1
[patent_app_number] => 8/532176
[patent_app_country] => US
[patent_app_date] => 1995-09-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 6
[patent_no_of_words] => 1662
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 125
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/730/05730392.pdf
[firstpage_image] =>[orig_patent_app_number] => 532176
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/532176 | Adjustable fairing for thrust reversers | Sep 21, 1995 | Issued |
Array
(
[id] => 3673862
[patent_doc_number] => 05695155
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1997-12-09
[patent_title] => 'Resonator-based, surface-condition sensor'
[patent_app_type] => 1
[patent_app_number] => 8/531876
[patent_app_country] => US
[patent_app_date] => 1995-09-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 12
[patent_no_of_words] => 3634
[patent_no_of_claims] => 24
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 128
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/695/05695155.pdf
[firstpage_image] =>[orig_patent_app_number] => 531876
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/531876 | Resonator-based, surface-condition sensor | Sep 20, 1995 | Issued |
Array
(
[id] => 3643800
[patent_doc_number] => 05657946
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1997-08-19
[patent_title] => 'Static vent units'
[patent_app_type] => 1
[patent_app_number] => 8/528156
[patent_app_country] => US
[patent_app_date] => 1995-09-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 7
[patent_no_of_words] => 2581
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 176
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/657/05657946.pdf
[firstpage_image] =>[orig_patent_app_number] => 528156
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/528156 | Static vent units | Sep 12, 1995 | Issued |
Array
(
[id] => 3713523
[patent_doc_number] => 05702067
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1997-12-30
[patent_title] => 'Method and apparatus for determining the angular momentum vector of a satellite'
[patent_app_type] => 1
[patent_app_number] => 8/526566
[patent_app_country] => US
[patent_app_date] => 1995-09-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 1
[patent_no_of_words] => 3930
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 223
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/702/05702067.pdf
[firstpage_image] =>[orig_patent_app_number] => 526566
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/526566 | Method and apparatus for determining the angular momentum vector of a satellite | Sep 10, 1995 | Issued |
Array
(
[id] => 3721362
[patent_doc_number] => 05697581
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1997-12-16
[patent_title] => 'Towplate and method of delivering cargo'
[patent_app_type] => 1
[patent_app_number] => 8/521674
[patent_app_country] => US
[patent_app_date] => 1995-08-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 19
[patent_no_of_words] => 6309
[patent_no_of_claims] => 22
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 81
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/697/05697581.pdf
[firstpage_image] =>[orig_patent_app_number] => 521674
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/521674 | Towplate and method of delivering cargo | Aug 30, 1995 | Issued |
Array
(
[id] => 3649762
[patent_doc_number] => 05624088
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1997-04-29
[patent_title] => 'Spacecraft structure and method'
[patent_app_type] => 1
[patent_app_number] => 8/521366
[patent_app_country] => US
[patent_app_date] => 1995-08-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 17
[patent_no_of_words] => 5184
[patent_no_of_claims] => 3
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 232
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/624/05624088.pdf
[firstpage_image] =>[orig_patent_app_number] => 521366
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/521366 | Spacecraft structure and method | Aug 30, 1995 | Issued |
Array
(
[id] => 3797351
[patent_doc_number] => 05788191
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-08-04
[patent_title] => 'Half-plow vortex generators for rotor blades for reducing blade-vortex interaction noise'
[patent_app_type] => 1
[patent_app_number] => 8/517026
[patent_app_country] => US
[patent_app_date] => 1995-08-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 7
[patent_no_of_words] => 5199
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 259
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/788/05788191.pdf
[firstpage_image] =>[orig_patent_app_number] => 517026
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/517026 | Half-plow vortex generators for rotor blades for reducing blade-vortex interaction noise | Aug 17, 1995 | Issued |
Array
(
[id] => 3732443
[patent_doc_number] => 05716027
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-02-10
[patent_title] => 'Retrofit luggage bin assemblies compatible with existing aircraft bin supports'
[patent_app_type] => 1
[patent_app_number] => 8/516908
[patent_app_country] => US
[patent_app_date] => 1995-08-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 11
[patent_no_of_words] => 6468
[patent_no_of_claims] => 22
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 89
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/716/05716027.pdf
[firstpage_image] =>[orig_patent_app_number] => 516908
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/516908 | Retrofit luggage bin assemblies compatible with existing aircraft bin supports | Aug 17, 1995 | Issued |
Array
(
[id] => 3683782
[patent_doc_number] => 05676312
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1997-10-14
[patent_title] => 'Seal for a variable geometry nozzle'
[patent_app_type] => 1
[patent_app_number] => 8/516827
[patent_app_country] => US
[patent_app_date] => 1995-08-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 5
[patent_no_of_words] => 2378
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 371
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/676/05676312.pdf
[firstpage_image] =>[orig_patent_app_number] => 516827
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/516827 | Seal for a variable geometry nozzle | Aug 17, 1995 | Issued |
Array
(
[id] => 3515140
[patent_doc_number] => 05540406
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1996-07-30
[patent_title] => 'Hydrofoils and airfoils'
[patent_app_type] => 1
[patent_app_number] => 8/507811
[patent_app_country] => US
[patent_app_date] => 1995-07-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 8
[patent_no_of_words] => 3989
[patent_no_of_claims] => 24
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 183
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/540/05540406.pdf
[firstpage_image] =>[orig_patent_app_number] => 507811
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/507811 | Hydrofoils and airfoils | Jul 25, 1995 | Issued |
Array
(
[id] => 3726392
[patent_doc_number] => 05785280
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-07-28
[patent_title] => 'Hybrid solar panel array'
[patent_app_type] => 1
[patent_app_number] => 8/504484
[patent_app_country] => US
[patent_app_date] => 1995-07-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 24
[patent_no_of_words] => 4494
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 110
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/785/05785280.pdf
[firstpage_image] =>[orig_patent_app_number] => 504484
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/504484 | Hybrid solar panel array | Jul 19, 1995 | Issued |
Array
(
[id] => 3842554
[patent_doc_number] => 05791599
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-08-11
[patent_title] => 'System for increasing the aerodynamic and hydrodynamic efficiency of a vehicle in motion'
[patent_app_type] => 1
[patent_app_number] => 8/504056
[patent_app_country] => US
[patent_app_date] => 1995-07-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 14
[patent_no_of_words] => 8483
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 6
[patent_words_short_claim] => 113
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/791/05791599.pdf
[firstpage_image] =>[orig_patent_app_number] => 504056
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/504056 | System for increasing the aerodynamic and hydrodynamic efficiency of a vehicle in motion | Jul 17, 1995 | Issued |
Array
(
[id] => 3693147
[patent_doc_number] => 05653405
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1997-08-05
[patent_title] => 'Balloon venting valves'
[patent_app_type] => 1
[patent_app_number] => 8/501905
[patent_app_country] => US
[patent_app_date] => 1995-07-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 4
[patent_no_of_words] => 1993
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 179
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/653/05653405.pdf
[firstpage_image] =>[orig_patent_app_number] => 501905
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/501905 | Balloon venting valves | Jul 12, 1995 | Issued |
Array
(
[id] => 3881325
[patent_doc_number] => 05749546
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-05-12
[patent_title] => 'Method and apparatus for reducing airframe aerosound'
[patent_app_type] => 1
[patent_app_number] => 8/501246
[patent_app_country] => US
[patent_app_date] => 1995-07-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 18
[patent_no_of_words] => 3533
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 157
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/749/05749546.pdf
[firstpage_image] =>[orig_patent_app_number] => 501246
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/501246 | Method and apparatus for reducing airframe aerosound | Jul 9, 1995 | Issued |
Array
(
[id] => 1580735
[patent_doc_number] => 06357672
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-03-19
[patent_title] => 'Sealing means for a multi-axis nozzle'
[patent_app_type] => B1
[patent_app_number] => 08/499100
[patent_app_country] => US
[patent_app_date] => 1995-07-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 4
[patent_no_of_words] => 1655
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 253
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/357/06357672.pdf
[firstpage_image] =>[orig_patent_app_number] => 08499100
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/499100 | Sealing means for a multi-axis nozzle | Jul 5, 1995 | Issued |
Array
(
[id] => 3648740
[patent_doc_number] => 05655735
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1997-08-12
[patent_title] => 'Post transition momentum management'
[patent_app_type] => 1
[patent_app_number] => 8/497776
[patent_app_country] => US
[patent_app_date] => 1995-07-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 3322
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 7
[patent_words_short_claim] => 110
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/655/05655735.pdf
[firstpage_image] =>[orig_patent_app_number] => 497776
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/497776 | Post transition momentum management | Jul 2, 1995 | Issued |
Array
(
[id] => 3821918
[patent_doc_number] => 05711496
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-01-27
[patent_title] => 'STOL aircraft and wing slat actuating mechanism for same'
[patent_app_type] => 1
[patent_app_number] => 8/497725
[patent_app_country] => US
[patent_app_date] => 1995-06-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 6
[patent_no_of_words] => 4208
[patent_no_of_claims] => 4
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 179
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/711/05711496.pdf
[firstpage_image] =>[orig_patent_app_number] => 497725
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/497725 | STOL aircraft and wing slat actuating mechanism for same | Jun 29, 1995 | Issued |
| 08/433495 | FLIGHT DEVICE | Jun 27, 1995 | Abandoned |