
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] => 4122428
[patent_doc_number] => 06059233
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-05-09
[patent_title] => 'Method and a system for launching satellites on non-coplanar orbits, making the use of gravitational assistance from the moon'
[patent_app_type] => 1
[patent_app_number] => 9/000896
[patent_app_country] => US
[patent_app_date] => 1997-12-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 7
[patent_no_of_words] => 5276
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 391
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/059/06059233.pdf
[firstpage_image] =>[orig_patent_app_number] => 000896
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/000896 | Method and a system for launching satellites on non-coplanar orbits, making the use of gravitational assistance from the moon | Dec 29, 1997 | Issued |
Array
(
[id] => 4150187
[patent_doc_number] => 06138947
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-10-31
[patent_title] => 'Active noise control system for a defined volume'
[patent_app_type] => 1
[patent_app_number] => 8/997435
[patent_app_country] => US
[patent_app_date] => 1997-12-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 2954
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 154
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/138/06138947.pdf
[firstpage_image] =>[orig_patent_app_number] => 997435
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/997435 | Active noise control system for a defined volume | Dec 22, 1997 | Issued |
Array
(
[id] => 4134459
[patent_doc_number] => 06105900
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-08-22
[patent_title] => 'Active noise control system for a helicopter gearbox mount'
[patent_app_type] => 1
[patent_app_number] => 8/996955
[patent_app_country] => US
[patent_app_date] => 1997-12-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 3176
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 202
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/105/06105900.pdf
[firstpage_image] =>[orig_patent_app_number] => 996955
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/996955 | Active noise control system for a helicopter gearbox mount | Dec 22, 1997 | Issued |
Array
(
[id] => 3913264
[patent_doc_number] => 05971325
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-10-26
[patent_title] => 'Compensation for rotorcraft pitch axis control saturation'
[patent_app_type] => 1
[patent_app_number] => 8/996692
[patent_app_country] => US
[patent_app_date] => 1997-12-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 10
[patent_no_of_words] => 4030
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 112
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/971/05971325.pdf
[firstpage_image] =>[orig_patent_app_number] => 996692
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/996692 | Compensation for rotorcraft pitch axis control saturation | Dec 22, 1997 | Issued |
Array
(
[id] => 4175016
[patent_doc_number] => 06042055
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-03-28
[patent_title] => 'Structural joint to accomodate large thermally-induced displacements'
[patent_app_type] => 1
[patent_app_number] => 8/994798
[patent_app_country] => US
[patent_app_date] => 1997-12-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 16
[patent_no_of_words] => 2075
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 173
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/042/06042055.pdf
[firstpage_image] =>[orig_patent_app_number] => 994798
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/994798 | Structural joint to accomodate large thermally-induced displacements | Dec 18, 1997 | Issued |
Array
(
[id] => 4102430
[patent_doc_number] => 06070834
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-06-06
[patent_title] => 'Aerodynamic body with internal actuating drives'
[patent_app_type] => 1
[patent_app_number] => 8/994682
[patent_app_country] => US
[patent_app_date] => 1997-12-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 4
[patent_no_of_words] => 1254
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 134
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/070/06070834.pdf
[firstpage_image] =>[orig_patent_app_number] => 994682
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/994682 | Aerodynamic body with internal actuating drives | Dec 18, 1997 | Issued |
Array
(
[id] => 4126908
[patent_doc_number] => 06015116
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-01-18
[patent_title] => 'Fuel efficient methods for satellite stationkeeping and momentum dumping'
[patent_app_type] => 1
[patent_app_number] => 8/989184
[patent_app_country] => US
[patent_app_date] => 1997-12-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 12
[patent_no_of_words] => 5992
[patent_no_of_claims] => 28
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 139
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/015/06015116.pdf
[firstpage_image] =>[orig_patent_app_number] => 989184
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/989184 | Fuel efficient methods for satellite stationkeeping and momentum dumping | Dec 10, 1997 | Issued |
Array
(
[id] => 4272185
[patent_doc_number] => 06234427
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2001-05-22
[patent_title] => 'Solar array regulation and spacecraft pointing using flywheel energy storage with programmable voltage control'
[patent_app_type] => 1
[patent_app_number] => 8/988055
[patent_app_country] => US
[patent_app_date] => 1997-12-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 4
[patent_no_of_words] => 3848
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 96
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/234/06234427.pdf
[firstpage_image] =>[orig_patent_app_number] => 988055
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/988055 | Solar array regulation and spacecraft pointing using flywheel energy storage with programmable voltage control | Dec 9, 1997 | Issued |
Array
(
[id] => 3907676
[patent_doc_number] => 05944283
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-08-31
[patent_title] => 'Crashworthy landing gear shock'
[patent_app_type] => 1
[patent_app_number] => 8/985892
[patent_app_country] => US
[patent_app_date] => 1997-12-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 16
[patent_no_of_words] => 4900
[patent_no_of_claims] => 24
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 149
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/944/05944283.pdf
[firstpage_image] =>[orig_patent_app_number] => 985892
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/985892 | Crashworthy landing gear shock | Dec 4, 1997 | Issued |
Array
(
[id] => 3920748
[patent_doc_number] => 05988566
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-11-23
[patent_title] => 'Aircraft window construction'
[patent_app_type] => 1
[patent_app_number] => 8/985093
[patent_app_country] => US
[patent_app_date] => 1997-12-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 6
[patent_no_of_words] => 3182
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 241
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/988/05988566.pdf
[firstpage_image] =>[orig_patent_app_number] => 985093
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/985093 | Aircraft window construction | Dec 3, 1997 | Issued |
| 08/984895 | CATHODE CURRENT SHARING APPARATUS AND METHOD THEREFOR | Dec 3, 1997 | Abandoned |
Array
(
[id] => 4338732
[patent_doc_number] => 06199801
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2001-03-13
[patent_title] => 'Whole-spacecraft passive isolation devices'
[patent_app_type] => 1
[patent_app_number] => 8/980790
[patent_app_country] => US
[patent_app_date] => 1997-12-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2356
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 103
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/199/06199801.pdf
[firstpage_image] =>[orig_patent_app_number] => 980790
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/980790 | Whole-spacecraft passive isolation devices | Nov 30, 1997 | Issued |
Array
(
[id] => 4161567
[patent_doc_number] => 06036141
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-03-14
[patent_title] => 'Jet thruster for helicopter antitorque and yaw control system'
[patent_app_type] => 1
[patent_app_number] => 8/964397
[patent_app_country] => US
[patent_app_date] => 1997-11-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 7
[patent_no_of_words] => 3047
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 207
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/036/06036141.pdf
[firstpage_image] =>[orig_patent_app_number] => 964397
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/964397 | Jet thruster for helicopter antitorque and yaw control system | Nov 5, 1997 | Issued |
| 08/965685 | PARTIALLY BUOYANT AERIAL VEHICLE | Nov 5, 1997 | Abandoned |
Array
(
[id] => 4026496
[patent_doc_number] => 05967463
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-10-19
[patent_title] => 'Air foil having valve'
[patent_app_type] => 1
[patent_app_number] => 8/961898
[patent_app_country] => US
[patent_app_date] => 1997-10-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 16
[patent_no_of_words] => 5149
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 58
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/967/05967463.pdf
[firstpage_image] =>[orig_patent_app_number] => 961898
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/961898 | Air foil having valve | Oct 30, 1997 | Issued |
Array
(
[id] => 4172038
[patent_doc_number] => 06152405
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-11-28
[patent_title] => 'Lift body having a variable camber'
[patent_app_type] => 1
[patent_app_number] => 8/954198
[patent_app_country] => US
[patent_app_date] => 1997-10-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 8
[patent_no_of_words] => 3152
[patent_no_of_claims] => 55
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 192
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/152/06152405.pdf
[firstpage_image] =>[orig_patent_app_number] => 954198
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/954198 | Lift body having a variable camber | Oct 19, 1997 | Issued |
Array
(
[id] => 502888
[patent_doc_number] => 07198230
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2007-04-03
[patent_title] => 'Method and system for maximizing satellite constellation coverage'
[patent_app_type] => utility
[patent_app_number] => 08/949988
[patent_app_country] => US
[patent_app_date] => 1997-10-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 8
[patent_no_of_words] => 2258
[patent_no_of_claims] => 21
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 122
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/198/07198230.pdf
[firstpage_image] =>[orig_patent_app_number] => 08949988
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/949988 | Method and system for maximizing satellite constellation coverage | Oct 13, 1997 | Issued |
Array
(
[id] => 4167560
[patent_doc_number] => 06019315
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-02-01
[patent_title] => 'Aircraft door structure with an air flow system'
[patent_app_type] => 1
[patent_app_number] => 8/942591
[patent_app_country] => US
[patent_app_date] => 1997-10-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 3
[patent_no_of_words] => 1669
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 174
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/019/06019315.pdf
[firstpage_image] =>[orig_patent_app_number] => 942591
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/942591 | Aircraft door structure with an air flow system | Oct 1, 1997 | Issued |
Array
(
[id] => 4135646
[patent_doc_number] => 06102331
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-08-15
[patent_title] => 'Operation of airports'
[patent_app_type] => 1
[patent_app_number] => 8/941485
[patent_app_country] => US
[patent_app_date] => 1997-10-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 13
[patent_no_of_words] => 4127
[patent_no_of_claims] => 26
[patent_no_of_ind_claims] => 7
[patent_words_short_claim] => 77
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/102/06102331.pdf
[firstpage_image] =>[orig_patent_app_number] => 941485
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/941485 | Operation of airports | Sep 30, 1997 | Issued |
Array
(
[id] => 3924134
[patent_doc_number] => 05996936
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-12-07
[patent_title] => 'Fluidic throat exhaust nozzle'
[patent_app_type] => 1
[patent_app_number] => 8/939384
[patent_app_country] => US
[patent_app_date] => 1997-09-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 5
[patent_no_of_words] => 2900
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 78
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/996/05996936.pdf
[firstpage_image] =>[orig_patent_app_number] => 939384
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/939384 | Fluidic throat exhaust nozzle | Sep 28, 1997 | Issued |