
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] => 3746860
[patent_doc_number] => 05720451
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-02-24
[patent_title] => 'High temperature thrust chamber for spacecraft'
[patent_app_type] => 1
[patent_app_number] => 8/574505
[patent_app_country] => US
[patent_app_date] => 1995-12-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 4
[patent_no_of_words] => 2245
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 88
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/720/05720451.pdf
[firstpage_image] =>[orig_patent_app_number] => 574505
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/574505 | High temperature thrust chamber for spacecraft | Dec 18, 1995 | Issued |
Array
(
[id] => 3945876
[patent_doc_number] => 05899409
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-05-04
[patent_title] => 'Large dimension aircraft'
[patent_app_type] => 1
[patent_app_number] => 8/574364
[patent_app_country] => US
[patent_app_date] => 1995-12-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 13
[patent_no_of_words] => 4149
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 201
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/899/05899409.pdf
[firstpage_image] =>[orig_patent_app_number] => 574364
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/574364 | Large dimension aircraft | Dec 17, 1995 | Issued |
| 08/572814 | MULTI-SERVICE COMMON AIRFRAME-BASED AIRCRAFT | Dec 14, 1995 | Abandoned |
Array
(
[id] => 3714509
[patent_doc_number] => 05669584
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1997-09-23
[patent_title] => 'Space vehicle apparatus including a cellular sandwich with phase change material'
[patent_app_type] => 1
[patent_app_number] => 8/571646
[patent_app_country] => US
[patent_app_date] => 1995-12-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 4
[patent_no_of_words] => 1898
[patent_no_of_claims] => 3
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 121
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/669/05669584.pdf
[firstpage_image] =>[orig_patent_app_number] => 571646
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/571646 | Space vehicle apparatus including a cellular sandwich with phase change material | Dec 12, 1995 | Issued |
Array
(
[id] => 3717536
[patent_doc_number] => 05692705
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1997-12-02
[patent_title] => 'Anti-crash seat with harness for an aircraft'
[patent_app_type] => 1
[patent_app_number] => 8/571654
[patent_app_country] => US
[patent_app_date] => 1995-12-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 10
[patent_no_of_words] => 3491
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 204
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/692/05692705.pdf
[firstpage_image] =>[orig_patent_app_number] => 571654
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/571654 | Anti-crash seat with harness for an aircraft | Dec 12, 1995 | Issued |
Array
(
[id] => 3810239
[patent_doc_number] => 05782432
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-07-21
[patent_title] => 'Apparatus for a variable area nozzle'
[patent_app_type] => 1
[patent_app_number] => 8/571534
[patent_app_country] => US
[patent_app_date] => 1995-12-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 11
[patent_no_of_words] => 5985
[patent_no_of_claims] => 18
[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/05/782/05782432.pdf
[firstpage_image] =>[orig_patent_app_number] => 571534
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/571534 | Apparatus for a variable area nozzle | Dec 12, 1995 | Issued |
Array
(
[id] => 3811939
[patent_doc_number] => 05730393
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-03-24
[patent_title] => 'Aircraft propulsive power unit'
[patent_app_type] => 1
[patent_app_number] => 8/570164
[patent_app_country] => US
[patent_app_date] => 1995-12-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 5
[patent_no_of_words] => 3056
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 262
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/730/05730393.pdf
[firstpage_image] =>[orig_patent_app_number] => 570164
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/570164 | Aircraft propulsive power unit | Dec 10, 1995 | Issued |
Array
(
[id] => 3864173
[patent_doc_number] => 05727756
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-03-17
[patent_title] => 'Modular kite system'
[patent_app_type] => 1
[patent_app_number] => 8/568025
[patent_app_country] => US
[patent_app_date] => 1995-12-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 18
[patent_no_of_words] => 2754
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 118
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/727/05727756.pdf
[firstpage_image] =>[orig_patent_app_number] => 568025
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/568025 | Modular kite system | Dec 5, 1995 | Issued |
Array
(
[id] => 3828507
[patent_doc_number] => 05707028
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-01-13
[patent_title] => 'Cover plate with length compensation'
[patent_app_type] => 1
[patent_app_number] => 8/566785
[patent_app_country] => US
[patent_app_date] => 1995-12-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 2
[patent_no_of_words] => 1640
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 115
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/707/05707028.pdf
[firstpage_image] =>[orig_patent_app_number] => 566785
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/566785 | Cover plate with length compensation | Dec 3, 1995 | Issued |
Array
(
[id] => 3749308
[patent_doc_number] => 05740987
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-04-21
[patent_title] => 'Helicopter cyclic control assembly'
[patent_app_type] => 1
[patent_app_number] => 8/565825
[patent_app_country] => US
[patent_app_date] => 1995-12-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 17
[patent_no_of_words] => 5337
[patent_no_of_claims] => 3
[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/05/740/05740987.pdf
[firstpage_image] =>[orig_patent_app_number] => 565825
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/565825 | Helicopter cyclic control assembly | Nov 30, 1995 | Issued |
Array
(
[id] => 3936334
[patent_doc_number] => 05934618
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-08-10
[patent_title] => 'Passive dynamic structure damage control in a hydraulic ram environment'
[patent_app_type] => 1
[patent_app_number] => 8/566344
[patent_app_country] => US
[patent_app_date] => 1995-12-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 6954
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 66
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/934/05934618.pdf
[firstpage_image] =>[orig_patent_app_number] => 566344
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/566344 | Passive dynamic structure damage control in a hydraulic ram environment | Nov 30, 1995 | Issued |
Array
(
[id] => 3757355
[patent_doc_number] => 05806803
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-09-15
[patent_title] => 'Spacecraft radiator cooling system'
[patent_app_type] => 1
[patent_app_number] => 8/565570
[patent_app_country] => US
[patent_app_date] => 1995-11-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 15
[patent_no_of_words] => 2930
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 127
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/806/05806803.pdf
[firstpage_image] =>[orig_patent_app_number] => 565570
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/565570 | Spacecraft radiator cooling system | Nov 29, 1995 | Issued |
Array
(
[id] => 3750741
[patent_doc_number] => 05772156
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-06-30
[patent_title] => 'Aircraft boundary layer control system with discharge transpiration panel'
[patent_app_type] => 1
[patent_app_number] => 8/566584
[patent_app_country] => US
[patent_app_date] => 1995-11-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 6
[patent_no_of_words] => 4104
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 62
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/772/05772156.pdf
[firstpage_image] =>[orig_patent_app_number] => 566584
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/566584 | Aircraft boundary layer control system with discharge transpiration panel | Nov 29, 1995 | Issued |
Array
(
[id] => 3867393
[patent_doc_number] => 05775639
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-07-07
[patent_title] => 'Thrust reverser with pivoting doors which can move in translation'
[patent_app_type] => 1
[patent_app_number] => 8/544445
[patent_app_country] => US
[patent_app_date] => 1995-11-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 24
[patent_no_of_words] => 7872
[patent_no_of_claims] => 29
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 278
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/775/05775639.pdf
[firstpage_image] =>[orig_patent_app_number] => 544445
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/544445 | Thrust reverser with pivoting doors which can move in translation | Nov 16, 1995 | Issued |
Array
(
[id] => 3673834
[patent_doc_number] => 05695153
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1997-12-09
[patent_title] => 'Launcher system for an unmanned aerial vehicle'
[patent_app_type] => 1
[patent_app_number] => 8/559056
[patent_app_country] => US
[patent_app_date] => 1995-11-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 10
[patent_no_of_words] => 2631
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 109
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/695/05695153.pdf
[firstpage_image] =>[orig_patent_app_number] => 559056
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/559056 | Launcher system for an unmanned aerial vehicle | Nov 15, 1995 | Issued |
Array
(
[id] => 3811896
[patent_doc_number] => 05730390
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-03-24
[patent_title] => 'Reusable spacecraft'
[patent_app_type] => 1
[patent_app_number] => 8/553355
[patent_app_country] => US
[patent_app_date] => 1995-11-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 4011
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 238
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/730/05730390.pdf
[firstpage_image] =>[orig_patent_app_number] => 553355
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/553355 | Reusable spacecraft | Nov 12, 1995 | Issued |
Array
(
[id] => 3825449
[patent_doc_number] => 05743493
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-04-28
[patent_title] => 'Boundary layer control in aerodynamic low drag structures'
[patent_app_type] => 1
[patent_app_number] => 8/522284
[patent_app_country] => US
[patent_app_date] => 1995-10-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 3
[patent_no_of_words] => 2390
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 336
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/743/05743493.pdf
[firstpage_image] =>[orig_patent_app_number] => 522284
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/522284 | Boundary layer control in aerodynamic low drag structures | Oct 30, 1995 | Issued |
Array
(
[id] => 3798688
[patent_doc_number] => 05769363
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-06-23
[patent_title] => 'Aircraft adjustable control stick'
[patent_app_type] => 1
[patent_app_number] => 8/550556
[patent_app_country] => US
[patent_app_date] => 1995-10-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 5
[patent_no_of_words] => 1289
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 85
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/769/05769363.pdf
[firstpage_image] =>[orig_patent_app_number] => 550556
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/550556 | Aircraft adjustable control stick | Oct 30, 1995 | Issued |
| 08/549086 | KITE WITH AN ADJUSTABLE AIRFOIL AND REMOVABLE SURFACE | Oct 26, 1995 | Abandoned |
Array
(
[id] => 3712029
[patent_doc_number] => 05681010
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1997-10-28
[patent_title] => 'Inflatable deployable control structures for aerospace vehicles'
[patent_app_type] => 1
[patent_app_number] => 8/542925
[patent_app_country] => US
[patent_app_date] => 1995-10-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 25
[patent_no_of_words] => 5216
[patent_no_of_claims] => 22
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 165
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/681/05681010.pdf
[firstpage_image] =>[orig_patent_app_number] => 542925
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/542925 | Inflatable deployable control structures for aerospace vehicles | Oct 12, 1995 | Issued |