
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] => 4167601
[patent_doc_number] => 06019318
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-02-01
[patent_title] => 'Coordinatable system of inclined geosynchronous satellite orbits'
[patent_app_type] => 1
[patent_app_number] => 8/876278
[patent_app_country] => US
[patent_app_date] => 1997-06-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 9
[patent_no_of_words] => 3766
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 309
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/019/06019318.pdf
[firstpage_image] =>[orig_patent_app_number] => 876278
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/876278 | Coordinatable system of inclined geosynchronous satellite orbits | Jun 15, 1997 | Issued |
Array
(
[id] => 3772344
[patent_doc_number] => 05839692
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-11-24
[patent_title] => 'Splayable aircraft nose landing gear'
[patent_app_type] => 1
[patent_app_number] => 8/874689
[patent_app_country] => US
[patent_app_date] => 1997-06-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 4990
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 209
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/839/05839692.pdf
[firstpage_image] =>[orig_patent_app_number] => 874689
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/874689 | Splayable aircraft nose landing gear | Jun 12, 1997 | Issued |
Array
(
[id] => 4098972
[patent_doc_number] => 06045090
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-04-04
[patent_title] => 'Device for reducing the vibrations generated by a lift rotor of a rotary-wing aircraft'
[patent_app_type] => 1
[patent_app_number] => 8/873696
[patent_app_country] => US
[patent_app_date] => 1997-06-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 5
[patent_no_of_words] => 3431
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 211
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/045/06045090.pdf
[firstpage_image] =>[orig_patent_app_number] => 873696
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/873696 | Device for reducing the vibrations generated by a lift rotor of a rotary-wing aircraft | Jun 11, 1997 | Issued |
Array
(
[id] => 3924116
[patent_doc_number] => 05996935
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-12-07
[patent_title] => 'Power plants'
[patent_app_type] => 1
[patent_app_number] => 8/871880
[patent_app_country] => US
[patent_app_date] => 1997-06-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 23
[patent_no_of_words] => 5066
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 158
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/996/05996935.pdf
[firstpage_image] =>[orig_patent_app_number] => 871880
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/871880 | Power plants | Jun 1, 1997 | Issued |
Array
(
[id] => 3721349
[patent_doc_number] => 05697580
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1997-12-16
[patent_title] => 'Infant transporting means for airplanes'
[patent_app_type] => 1
[patent_app_number] => 8/861139
[patent_app_country] => US
[patent_app_date] => 1997-05-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 2
[patent_no_of_words] => 1144
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 40
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/697/05697580.pdf
[firstpage_image] =>[orig_patent_app_number] => 861139
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/861139 | Infant transporting means for airplanes | May 20, 1997 | Issued |
Array
(
[id] => 4034769
[patent_doc_number] => 05931415
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-08-03
[patent_title] => 'Plug-type overwing emergency exit door assembly'
[patent_app_type] => 1
[patent_app_number] => 8/853688
[patent_app_country] => US
[patent_app_date] => 1997-05-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 14
[patent_figures_cnt] => 14
[patent_no_of_words] => 6013
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 300
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/931/05931415.pdf
[firstpage_image] =>[orig_patent_app_number] => 853688
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/853688 | Plug-type overwing emergency exit door assembly | May 8, 1997 | Issued |
Array
(
[id] => 3950165
[patent_doc_number] => 05884873
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-03-23
[patent_title] => 'Suction generator system in an aircraft for maintaining a laminar boundary flow'
[patent_app_type] => 1
[patent_app_number] => 8/851589
[patent_app_country] => US
[patent_app_date] => 1997-05-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 1
[patent_no_of_words] => 2687
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 198
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/884/05884873.pdf
[firstpage_image] =>[orig_patent_app_number] => 851589
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/851589 | Suction generator system in an aircraft for maintaining a laminar boundary flow | May 4, 1997 | Issued |
Array
(
[id] => 4034727
[patent_doc_number] => 05931412
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-08-03
[patent_title] => 'Air balloon containing inert gas'
[patent_app_type] => 1
[patent_app_number] => 8/817885
[patent_app_country] => US
[patent_app_date] => 1997-05-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 2233
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 148
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/931/05931412.pdf
[firstpage_image] =>[orig_patent_app_number] => 817885
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/817885 | Air balloon containing inert gas | Apr 30, 1997 | Issued |
Array
(
[id] => 3791913
[patent_doc_number] => 05853152
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-12-29
[patent_title] => 'Collective detent system for vertical takeoff flight operations'
[patent_app_type] => 1
[patent_app_number] => 8/841096
[patent_app_country] => US
[patent_app_date] => 1997-04-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 11
[patent_no_of_words] => 7472
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 271
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/853/05853152.pdf
[firstpage_image] =>[orig_patent_app_number] => 841096
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/841096 | Collective detent system for vertical takeoff flight operations | Apr 28, 1997 | Issued |
Array
(
[id] => 3775389
[patent_doc_number] => 05779188
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-07-14
[patent_title] => 'Flight device'
[patent_app_type] => 1
[patent_app_number] => 8/844568
[patent_app_country] => US
[patent_app_date] => 1997-04-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
[patent_figures_cnt] => 20
[patent_no_of_words] => 5280
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 160
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/779/05779188.pdf
[firstpage_image] =>[orig_patent_app_number] => 844568
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/844568 | Flight device | Apr 20, 1997 | Issued |
| 08/844485 | IMPROVED INTEGRATED ENVIRONMENTAL & SECONDARY POWER SYSTEM | Apr 17, 1997 | Abandoned |
| 08/844453 | AIRCRAFT LANDING GEAR HAVING AXLE TO BRAKE PLATE INTEGRATION | Apr 17, 1997 | Abandoned |
Array
(
[id] => 3945865
[patent_doc_number] => 05899408
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-05-04
[patent_title] => 'Ornithopter'
[patent_app_type] => 1
[patent_app_number] => 8/826996
[patent_app_country] => US
[patent_app_date] => 1997-04-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 8
[patent_no_of_words] => 3162
[patent_no_of_claims] => 3
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 126
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/899/05899408.pdf
[firstpage_image] =>[orig_patent_app_number] => 826996
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/826996 | Ornithopter | Apr 13, 1997 | Issued |
Array
(
[id] => 4009464
[patent_doc_number] => 05906335
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-05-25
[patent_title] => 'Flight direction control system for blimps'
[patent_app_type] => 1
[patent_app_number] => 8/838609
[patent_app_country] => US
[patent_app_date] => 1997-04-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 15
[patent_no_of_words] => 3192
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 215
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/906/05906335.pdf
[firstpage_image] =>[orig_patent_app_number] => 838609
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/838609 | Flight direction control system for blimps | Apr 9, 1997 | Issued |
Array
(
[id] => 6237225
[patent_doc_number] => 20020043589
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-04-18
[patent_title] => 'LEADING EDGE CHANNEL FOR ENHANCEMENT OF LIFT/DRAG RATIO AND REDUCTION OF SONIC BOOM'
[patent_app_type] => new
[patent_app_number] => 08/833079
[patent_app_country] => US
[patent_app_date] => 1997-04-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 22
[patent_figures_cnt] => 22
[patent_no_of_words] => 9836
[patent_no_of_claims] => 25
[patent_no_of_ind_claims] => 6
[patent_words_short_claim] => 45
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0043/20020043589.pdf
[firstpage_image] =>[orig_patent_app_number] => 08833079
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/833079 | Leading edge channel for enhancement of lift/drag ratio and reduction of sonic boom | Apr 3, 1997 | Issued |
Array
(
[id] => 3914816
[patent_doc_number] => 05979824
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-11-09
[patent_title] => 'Stabilizer fins-inverted for aircraft'
[patent_app_type] => 1
[patent_app_number] => 8/833299
[patent_app_country] => US
[patent_app_date] => 1997-04-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 11
[patent_no_of_words] => 1594
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 6
[patent_words_short_claim] => 100
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/979/05979824.pdf
[firstpage_image] =>[orig_patent_app_number] => 833299
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/833299 | Stabilizer fins-inverted for aircraft | Apr 3, 1997 | Issued |
Array
(
[id] => 4214851
[patent_doc_number] => 06116543
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-09-12
[patent_title] => 'Method and a system for putting a space vehicle into orbit, using thrusters of high specific impulse'
[patent_app_type] => 1
[patent_app_number] => 8/833094
[patent_app_country] => US
[patent_app_date] => 1997-04-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 15
[patent_no_of_words] => 9251
[patent_no_of_claims] => 3
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 237
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/116/06116543.pdf
[firstpage_image] =>[orig_patent_app_number] => 833094
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/833094 | Method and a system for putting a space vehicle into orbit, using thrusters of high specific impulse | Apr 3, 1997 | Issued |
| 08/832874 | AVIATION CRASH SENSOR | Apr 3, 1997 | Abandoned |
Array
(
[id] => 3950130
[patent_doc_number] => 05884870
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-03-23
[patent_title] => 'Device for maintaining the speed of an aircraft within a particular speed range'
[patent_app_type] => 1
[patent_app_number] => 8/829081
[patent_app_country] => US
[patent_app_date] => 1997-03-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 3
[patent_no_of_words] => 3225
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 135
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/884/05884870.pdf
[firstpage_image] =>[orig_patent_app_number] => 829081
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/829081 | Device for maintaining the speed of an aircraft within a particular speed range | Mar 30, 1997 | Issued |
Array
(
[id] => 3957167
[patent_doc_number] => 05915652
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-06-29
[patent_title] => 'Method and apparatus for restraining a cargo barrier net beam assembly'
[patent_app_type] => 1
[patent_app_number] => 8/821787
[patent_app_country] => US
[patent_app_date] => 1997-03-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 8
[patent_no_of_words] => 2256
[patent_no_of_claims] => 3
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[patent_words_short_claim] => 191
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/915/05915652.pdf
[firstpage_image] =>[orig_patent_app_number] => 821787
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/821787 | Method and apparatus for restraining a cargo barrier net beam assembly | Mar 20, 1997 | Issued |