Search

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 numberTitle of the applicationFiling DateStatus
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 [patent_no_of_ind_claims] => 2 [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
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