
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] => 3945977
[patent_doc_number] => 05899415
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-05-04
[patent_title] => 'Personnel guided aerial delivery device'
[patent_app_type] => 1
[patent_app_number] => 8/818495
[patent_app_country] => US
[patent_app_date] => 1997-03-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 15
[patent_no_of_words] => 4966
[patent_no_of_claims] => 29
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 119
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/899/05899415.pdf
[firstpage_image] =>[orig_patent_app_number] => 818495
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/818495 | Personnel guided aerial delivery device | Mar 13, 1997 | Issued |
Array
(
[id] => 4217562
[patent_doc_number] => 06142416
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-11-07
[patent_title] => 'Hydraulic failsafe system and method for an axisymmetric vectoring nozzle'
[patent_app_type] => 1
[patent_app_number] => 8/818051
[patent_app_country] => US
[patent_app_date] => 1997-03-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 7
[patent_no_of_words] => 6028
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 183
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/142/06142416.pdf
[firstpage_image] =>[orig_patent_app_number] => 818051
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/818051 | Hydraulic failsafe system and method for an axisymmetric vectoring nozzle | Mar 13, 1997 | Issued |
Array
(
[id] => 3979745
[patent_doc_number] => 05918832
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-07-06
[patent_title] => 'Wing design using a high-lift center section, augmented by all-moving wing tips and tails'
[patent_app_type] => 1
[patent_app_number] => 8/818582
[patent_app_country] => US
[patent_app_date] => 1997-03-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 5
[patent_no_of_words] => 4197
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 179
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/918/05918832.pdf
[firstpage_image] =>[orig_patent_app_number] => 818582
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/818582 | Wing design using a high-lift center section, augmented by all-moving wing tips and tails | Mar 13, 1997 | Issued |
Array
(
[id] => 1588786
[patent_doc_number] => 06382565
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-05-07
[patent_title] => 'Satellite spin reorientation using a single degree of freedom momentum storage device'
[patent_app_type] => B1
[patent_app_number] => 08/816728
[patent_app_country] => US
[patent_app_date] => 1997-03-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 8448
[patent_no_of_claims] => 23
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 78
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/382/06382565.pdf
[firstpage_image] =>[orig_patent_app_number] => 08816728
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/816728 | Satellite spin reorientation using a single degree of freedom momentum storage device | Mar 12, 1997 | Issued |
Array
(
[id] => 3810627
[patent_doc_number] => 05758846
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-06-02
[patent_title] => 'Satellite spin inversion using a single degree of freedom momentum storage device'
[patent_app_type] => 1
[patent_app_number] => 8/816727
[patent_app_country] => US
[patent_app_date] => 1997-03-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 8128
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 209
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/758/05758846.pdf
[firstpage_image] =>[orig_patent_app_number] => 816727
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/816727 | Satellite spin inversion using a single degree of freedom momentum storage device | Mar 12, 1997 | Issued |
Array
(
[id] => 3912862
[patent_doc_number] => 05927649
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-07-27
[patent_title] => 'Suspendible carrier for carrying multiple cargo loads by helicopter'
[patent_app_type] => 1
[patent_app_number] => 8/813197
[patent_app_country] => US
[patent_app_date] => 1997-03-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 4181
[patent_no_of_claims] => 25
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 225
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/927/05927649.pdf
[firstpage_image] =>[orig_patent_app_number] => 813197
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/813197 | Suspendible carrier for carrying multiple cargo loads by helicopter | Mar 6, 1997 | Issued |
Array
(
[id] => 3978063
[patent_doc_number] => 05909859
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-06-08
[patent_title] => 'Multi-rotor kite glider'
[patent_app_type] => 1
[patent_app_number] => 8/812684
[patent_app_country] => US
[patent_app_date] => 1997-03-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 6
[patent_no_of_words] => 4304
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 131
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/909/05909859.pdf
[firstpage_image] =>[orig_patent_app_number] => 812684
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/812684 | Multi-rotor kite glider | Mar 5, 1997 | Issued |
Array
(
[id] => 3974462
[patent_doc_number] => 05890680
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-04-06
[patent_title] => 'Device at the adapter of a launcher and a satellite carried by the adapter'
[patent_app_type] => 1
[patent_app_number] => 8/796688
[patent_app_country] => US
[patent_app_date] => 1997-03-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 2
[patent_no_of_words] => 643
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 131
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/890/05890680.pdf
[firstpage_image] =>[orig_patent_app_number] => 796688
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/796688 | Device at the adapter of a launcher and a satellite carried by the adapter | Mar 3, 1997 | Issued |
Array
(
[id] => 4192797
[patent_doc_number] => 06027074
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-02-22
[patent_title] => 'Reinforced elastomer panel'
[patent_app_type] => 1
[patent_app_number] => 8/807295
[patent_app_country] => US
[patent_app_date] => 1997-02-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 26
[patent_no_of_words] => 2699
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 154
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/027/06027074.pdf
[firstpage_image] =>[orig_patent_app_number] => 807295
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/807295 | Reinforced elastomer panel | Feb 26, 1997 | Issued |
Array
(
[id] => 4392205
[patent_doc_number] => 06264141
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2001-07-24
[patent_title] => 'Aircraft decompression protection panel'
[patent_app_type] => 1
[patent_app_number] => 8/802582
[patent_app_country] => US
[patent_app_date] => 1997-02-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 5
[patent_no_of_words] => 1688
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 91
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/264/06264141.pdf
[firstpage_image] =>[orig_patent_app_number] => 802582
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/802582 | Aircraft decompression protection panel | Feb 18, 1997 | Issued |
Array
(
[id] => 4391463
[patent_doc_number] => 06237872
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2001-05-29
[patent_title] => 'Aircraft cabin environment'
[patent_app_type] => 1
[patent_app_number] => 8/801799
[patent_app_country] => US
[patent_app_date] => 1997-02-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 20
[patent_no_of_words] => 6661
[patent_no_of_claims] => 28
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 226
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/237/06237872.pdf
[firstpage_image] =>[orig_patent_app_number] => 801799
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/801799 | Aircraft cabin environment | Feb 13, 1997 | Issued |
| 08/722081 | AIRCRAFT LANDING GEAR DRIVE SYSTEM | Jan 21, 1997 | Abandoned |
Array
(
[id] => 4108159
[patent_doc_number] => 06126115
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-10-03
[patent_title] => 'Apparatus for retaining and releasing a payload'
[patent_app_type] => 1
[patent_app_number] => 8/781359
[patent_app_country] => US
[patent_app_date] => 1997-01-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 8
[patent_no_of_words] => 4436
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 114
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/126/06126115.pdf
[firstpage_image] =>[orig_patent_app_number] => 781359
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/781359 | Apparatus for retaining and releasing a payload | Jan 20, 1997 | Issued |
Array
(
[id] => 4127491
[patent_doc_number] => 06029928
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-02-29
[patent_title] => 'Space launch vehicles configured as gliders and towed to launch altitude by conventional aircraft'
[patent_app_type] => 1
[patent_app_number] => 8/782769
[patent_app_country] => US
[patent_app_date] => 1997-01-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 15
[patent_no_of_words] => 5926
[patent_no_of_claims] => 40
[patent_no_of_ind_claims] => 19
[patent_words_short_claim] => 36
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/029/06029928.pdf
[firstpage_image] =>[orig_patent_app_number] => 782769
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/782769 | Space launch vehicles configured as gliders and towed to launch altitude by conventional aircraft | Jan 12, 1997 | Issued |
Array
(
[id] => 4021062
[patent_doc_number] => 05855341
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-01-05
[patent_title] => 'Method of controlling a plurality of satellites'
[patent_app_type] => 1
[patent_app_number] => 8/780394
[patent_app_country] => US
[patent_app_date] => 1997-01-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 3480
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 6
[patent_words_short_claim] => 102
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/855/05855341.pdf
[firstpage_image] =>[orig_patent_app_number] => 780394
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/780394 | Method of controlling a plurality of satellites | Jan 7, 1997 | Issued |
Array
(
[id] => 3911618
[patent_doc_number] => 05913493
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-06-22
[patent_title] => 'Seaplane hull'
[patent_app_type] => 1
[patent_app_number] => 8/750882
[patent_app_country] => US
[patent_app_date] => 1996-12-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 11
[patent_no_of_words] => 4219
[patent_no_of_claims] => 13
[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/05/913/05913493.pdf
[firstpage_image] =>[orig_patent_app_number] => 750882
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/750882 | Seaplane hull | Dec 16, 1996 | Issued |
Array
(
[id] => 3822084
[patent_doc_number] => 05845880
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-12-08
[patent_title] => 'Hall effect plasma thruster'
[patent_app_type] => 1
[patent_app_number] => 8/763692
[patent_app_country] => US
[patent_app_date] => 1996-12-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 6
[patent_no_of_words] => 3851
[patent_no_of_claims] => 21
[patent_no_of_ind_claims] => 7
[patent_words_short_claim] => 202
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/845/05845880.pdf
[firstpage_image] =>[orig_patent_app_number] => 763692
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/763692 | Hall effect plasma thruster | Dec 8, 1996 | Issued |
Array
(
[id] => 3864163
[patent_doc_number] => 05727755
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-03-17
[patent_title] => 'Aircraft engines with a controllable outer casing'
[patent_app_type] => 1
[patent_app_number] => 8/759305
[patent_app_country] => US
[patent_app_date] => 1996-12-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 15
[patent_figures_cnt] => 15
[patent_no_of_words] => 8387
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 279
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/727/05727755.pdf
[firstpage_image] =>[orig_patent_app_number] => 759305
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/759305 | Aircraft engines with a controllable outer casing | Dec 1, 1996 | Issued |
Array
(
[id] => 4053821
[patent_doc_number] => 05895015
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-04-20
[patent_title] => 'Automatic flap'
[patent_app_type] => 1
[patent_app_number] => 8/757994
[patent_app_country] => US
[patent_app_date] => 1996-11-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 7
[patent_no_of_words] => 1179
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 180
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/895/05895015.pdf
[firstpage_image] =>[orig_patent_app_number] => 757994
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/757994 | Automatic flap | Nov 26, 1996 | Issued |
| 08/755822 | STOL/VTOL AIRCRAFT WITH IMPROVED CONTROL DURING TRANSITION | Nov 25, 1996 | Abandoned |