
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] => 4108179
[patent_doc_number] => 06126116
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-10-03
[patent_title] => 'Coordinatable system of inclined eccentric geosynchronous orbits'
[patent_app_type] => 1
[patent_app_number] => 9/119680
[patent_app_country] => US
[patent_app_date] => 1998-07-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 13
[patent_no_of_words] => 4626
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 309
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/126/06126116.pdf
[firstpage_image] =>[orig_patent_app_number] => 119680
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/119680 | Coordinatable system of inclined eccentric geosynchronous orbits | Jul 20, 1998 | Issued |
Array
(
[id] => 4135720
[patent_doc_number] => 06102336
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-08-15
[patent_title] => 'Passive device for stabilizing the direction in which a spacecraft points'
[patent_app_type] => 1
[patent_app_number] => 9/100252
[patent_app_country] => US
[patent_app_date] => 1998-06-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 12
[patent_no_of_words] => 2401
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 115
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/102/06102336.pdf
[firstpage_image] =>[orig_patent_app_number] => 100252
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/100252 | Passive device for stabilizing the direction in which a spacecraft points | Jun 18, 1998 | Issued |
Array
(
[id] => 4304164
[patent_doc_number] => 06247669
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2001-06-19
[patent_title] => 'Airfoil low ice adhesion surface'
[patent_app_type] => 1
[patent_app_number] => 9/098809
[patent_app_country] => US
[patent_app_date] => 1998-06-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 4471
[patent_no_of_claims] => 26
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 97
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/247/06247669.pdf
[firstpage_image] =>[orig_patent_app_number] => 098809
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/098809 | Airfoil low ice adhesion surface | Jun 16, 1998 | Issued |
Array
(
[id] => 4192810
[patent_doc_number] => 06027075
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-02-22
[patent_title] => 'Systems and methods for modifying ice adhesion strength'
[patent_app_type] => 1
[patent_app_number] => 9/094779
[patent_app_country] => US
[patent_app_date] => 1998-06-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 24
[patent_figures_cnt] => 42
[patent_no_of_words] => 17468
[patent_no_of_claims] => 27
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 84
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/027/06027075.pdf
[firstpage_image] =>[orig_patent_app_number] => 094779
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/094779 | Systems and methods for modifying ice adhesion strength | Jun 14, 1998 | Issued |
| 09/080187 | SYSTEM FOR MONITORING OXYGEN SUPPLY | May 17, 1998 | Abandoned |
Array
(
[id] => 4218194
[patent_doc_number] => 06073880
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-06-13
[patent_title] => 'Integrated missile fin deployment system'
[patent_app_type] => 1
[patent_app_number] => 9/080483
[patent_app_country] => US
[patent_app_date] => 1998-05-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 11
[patent_no_of_words] => 2968
[patent_no_of_claims] => 23
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 171
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/073/06073880.pdf
[firstpage_image] =>[orig_patent_app_number] => 080483
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/080483 | Integrated missile fin deployment system | May 17, 1998 | Issued |
Array
(
[id] => 4172024
[patent_doc_number] => 06152404
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-11-28
[patent_title] => 'Apparatus for influencing a wing root airflow in an aircraft'
[patent_app_type] => 1
[patent_app_number] => 9/078292
[patent_app_country] => US
[patent_app_date] => 1998-05-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 14
[patent_no_of_words] => 3499
[patent_no_of_claims] => 24
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 152
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/152/06152404.pdf
[firstpage_image] =>[orig_patent_app_number] => 078292
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/078292 | Apparatus for influencing a wing root airflow in an aircraft | May 12, 1998 | Issued |
Array
(
[id] => 4122388
[patent_doc_number] => 06059230
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-05-09
[patent_title] => 'Expandable aircraft door'
[patent_app_type] => 1
[patent_app_number] => 9/075099
[patent_app_country] => US
[patent_app_date] => 1998-05-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 6
[patent_no_of_words] => 4510
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 112
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/059/06059230.pdf
[firstpage_image] =>[orig_patent_app_number] => 075099
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/075099 | Expandable aircraft door | May 7, 1998 | Issued |
Array
(
[id] => 4108113
[patent_doc_number] => 06126112
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-10-03
[patent_title] => 'Advertising placard'
[patent_app_type] => 1
[patent_app_number] => 9/069444
[patent_app_country] => US
[patent_app_date] => 1998-04-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 5
[patent_no_of_words] => 3586
[patent_no_of_claims] => 17
[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/06/126/06126112.pdf
[firstpage_image] =>[orig_patent_app_number] => 069444
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/069444 | Advertising placard | Apr 28, 1998 | Issued |
Array
(
[id] => 4018527
[patent_doc_number] => 05941478
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-08-24
[patent_title] => 'STOL/VTOL free wing aircraft with modular wing and tail'
[patent_app_type] => 1
[patent_app_number] => 9/066980
[patent_app_country] => US
[patent_app_date] => 1998-04-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 8
[patent_no_of_words] => 3817
[patent_no_of_claims] => 24
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 143
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/941/05941478.pdf
[firstpage_image] =>[orig_patent_app_number] => 066980
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/066980 | STOL/VTOL free wing aircraft with modular wing and tail | Apr 27, 1998 | Issued |
Array
(
[id] => 4087997
[patent_doc_number] => 06050525
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-04-18
[patent_title] => 'Asymmetric open rosette constellations'
[patent_app_type] => 1
[patent_app_number] => 9/069090
[patent_app_country] => US
[patent_app_date] => 1998-04-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 6724
[patent_no_of_claims] => 55
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 304
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/050/06050525.pdf
[firstpage_image] =>[orig_patent_app_number] => 069090
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/069090 | Asymmetric open rosette constellations | Apr 27, 1998 | Issued |
Array
(
[id] => 4344248
[patent_doc_number] => 06173925
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2001-01-16
[patent_title] => 'Skin-rib structure'
[patent_app_type] => 1
[patent_app_number] => 9/061067
[patent_app_country] => US
[patent_app_date] => 1998-04-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 3
[patent_no_of_words] => 2817
[patent_no_of_claims] => 22
[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/06/173/06173925.pdf
[firstpage_image] =>[orig_patent_app_number] => 061067
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/061067 | Skin-rib structure | Apr 15, 1998 | Issued |
Array
(
[id] => 4257017
[patent_doc_number] => 06279852
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2001-08-28
[patent_title] => 'Drive system for a propeller driven transport aircraft'
[patent_app_type] => 1
[patent_app_number] => 9/061092
[patent_app_country] => US
[patent_app_date] => 1998-04-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 1996
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 215
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/279/06279852.pdf
[firstpage_image] =>[orig_patent_app_number] => 061092
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/061092 | Drive system for a propeller driven transport aircraft | Apr 15, 1998 | Issued |
Array
(
[id] => 4388311
[patent_doc_number] => 06231005
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2001-05-15
[patent_title] => 'Device for the individual control of the rotor blades of the rotary wing structures of aircraft with multiple swashplates'
[patent_app_type] => 1
[patent_app_number] => 9/055997
[patent_app_country] => US
[patent_app_date] => 1998-04-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 15
[patent_figures_cnt] => 20
[patent_no_of_words] => 18759
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 388
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/231/06231005.pdf
[firstpage_image] =>[orig_patent_app_number] => 055997
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/055997 | Device for the individual control of the rotor blades of the rotary wing structures of aircraft with multiple swashplates | Apr 6, 1998 | Issued |
Array
(
[id] => 4114007
[patent_doc_number] => 06119982
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-09-19
[patent_title] => 'Pre-loaded stores ejection ram system and method'
[patent_app_type] => 1
[patent_app_number] => 9/054787
[patent_app_country] => US
[patent_app_date] => 1998-04-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 6
[patent_no_of_words] => 2989
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 96
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/119/06119982.pdf
[firstpage_image] =>[orig_patent_app_number] => 054787
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/054787 | Pre-loaded stores ejection ram system and method | Apr 2, 1998 | Issued |
Array
(
[id] => 4404618
[patent_doc_number] => 06193193
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2001-02-27
[patent_title] => 'Evolvable propulsion module'
[patent_app_type] => 1
[patent_app_number] => 9/053178
[patent_app_country] => US
[patent_app_date] => 1998-04-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
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[patent_no_of_words] => 8143
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/193/06193193.pdf
[firstpage_image] =>[orig_patent_app_number] => 053178
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/053178 | Evolvable propulsion module | Mar 31, 1998 | Issued |
Array
(
[id] => 4165263
[patent_doc_number] => 06149104
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-11-21
[patent_title] => 'Structural layout for spacecraft including specialized compartment configuration'
[patent_app_type] => 1
[patent_app_number] => 9/053188
[patent_app_country] => US
[patent_app_date] => 1998-04-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 19
[patent_no_of_words] => 8143
[patent_no_of_claims] => 43
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 81
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/149/06149104.pdf
[firstpage_image] =>[orig_patent_app_number] => 053188
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/053188 | Structural layout for spacecraft including specialized compartment configuration | Mar 31, 1998 | Issued |
Array
(
[id] => 4126894
[patent_doc_number] => 06015115
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-01-18
[patent_title] => 'Inflatable structures to control aircraft'
[patent_app_type] => 1
[patent_app_number] => 9/047695
[patent_app_country] => US
[patent_app_date] => 1998-03-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 11
[patent_no_of_words] => 2840
[patent_no_of_claims] => 16
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[patent_words_short_claim] => 136
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/015/06015115.pdf
[firstpage_image] =>[orig_patent_app_number] => 047695
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/047695 | Inflatable structures to control aircraft | Mar 24, 1998 | Issued |
Array
(
[id] => 4216151
[patent_doc_number] => 06164596
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-12-26
[patent_title] => 'Designs of and methodology for inward or outward, and partially inward or outward turning flow hypersonic air-breathing and rocket-based-combined-cycle vehicles'
[patent_app_type] => 1
[patent_app_number] => 9/048080
[patent_app_country] => US
[patent_app_date] => 1998-03-25
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/164/06164596.pdf
[firstpage_image] =>[orig_patent_app_number] => 048080
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/048080 | Designs of and methodology for inward or outward, and partially inward or outward turning flow hypersonic air-breathing and rocket-based-combined-cycle vehicles | Mar 24, 1998 | Issued |
Array
(
[id] => 4351236
[patent_doc_number] => 06286786
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2001-09-11
[patent_title] => 'Remotely controlled aircraft'
[patent_app_type] => 1
[patent_app_number] => 9/045994
[patent_app_country] => US
[patent_app_date] => 1998-03-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/286/06286786.pdf
[firstpage_image] =>[orig_patent_app_number] => 045994
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/045994 | Remotely controlled aircraft | Mar 22, 1998 | Issued |