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] => 4333642 [patent_doc_number] => 06290186 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 2001-09-18 [patent_title] => 'Planar hoytether failure resistant multiline tether' [patent_app_type] => 1 [patent_app_number] => 9/657418 [patent_app_country] => US [patent_app_date] => 2000-09-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 28 [patent_figures_cnt] => 54 [patent_no_of_words] => 21089 [patent_no_of_claims] => 4 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 41 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/290/06290186.pdf [firstpage_image] =>[orig_patent_app_number] => 657418 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/657418
Planar hoytether failure resistant multiline tether Sep 7, 2000 Issued
Array ( [id] => 1296837 [patent_doc_number] => 06619587 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2003-09-16 [patent_title] => 'Aircraft noise reduction apparatus' [patent_app_type] => B1 [patent_app_number] => 09/655347 [patent_app_country] => US [patent_app_date] => 2000-09-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 10 [patent_no_of_words] => 4409 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 7 [patent_words_short_claim] => 94 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/619/06619587.pdf [firstpage_image] =>[orig_patent_app_number] => 09655347 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/655347
Aircraft noise reduction apparatus Sep 4, 2000 Issued
Array ( [id] => 1555335 [patent_doc_number] => 06435453 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-08-20 [patent_title] => 'High speed rotor aircraft' [patent_app_type] => B1 [patent_app_number] => 09/641364 [patent_app_country] => US [patent_app_date] => 2000-08-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 18 [patent_no_of_words] => 5866 [patent_no_of_claims] => 7 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 182 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/435/06435453.pdf [firstpage_image] =>[orig_patent_app_number] => 09641364 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/641364
High speed rotor aircraft Aug 17, 2000 Issued
Array ( [id] => 4254709 [patent_doc_number] => 06322023 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 2001-11-27 [patent_title] => 'Evolvable propulsion module' [patent_app_type] => 1 [patent_app_number] => 9/635607 [patent_app_country] => US [patent_app_date] => 2000-08-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 19 [patent_no_of_words] => 8142 [patent_no_of_claims] => 36 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 155 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/322/06322023.pdf [firstpage_image] =>[orig_patent_app_number] => 635607 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/635607
Evolvable propulsion module Aug 9, 2000 Issued
Array ( [id] => 1159872 [patent_doc_number] => 06752358 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2004-06-22 [patent_title] => 'Laminar flow control system and suction panel for use therewith' [patent_app_type] => B1 [patent_app_number] => 09/601884 [patent_app_country] => US [patent_app_date] => 2000-08-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 10 [patent_no_of_words] => 2721 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 5 [patent_words_short_claim] => 103 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/752/06752358.pdf [firstpage_image] =>[orig_patent_app_number] => 09601884 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/601884
Laminar flow control system and suction panel for use therewith Aug 8, 2000 Issued
Array ( [id] => 1538873 [patent_doc_number] => 06371408 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-04-16 [patent_title] => 'Helicopter tail rotor authority altitude compensator' [patent_app_type] => B1 [patent_app_number] => 09/632041 [patent_app_country] => US [patent_app_date] => 2000-08-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 24 [patent_no_of_words] => 3501 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 355 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/371/06371408.pdf [firstpage_image] =>[orig_patent_app_number] => 09632041 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/632041
Helicopter tail rotor authority altitude compensator Aug 2, 2000 Issued
Array ( [id] => 1473722 [patent_doc_number] => 06450444 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-09-17 [patent_title] => 'Fin lock system' [patent_app_type] => B1 [patent_app_number] => 09/631149 [patent_app_country] => US [patent_app_date] => 2000-08-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 7 [patent_no_of_words] => 1398 [patent_no_of_claims] => 7 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 52 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/450/06450444.pdf [firstpage_image] =>[orig_patent_app_number] => 09631149 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/631149
Fin lock system Aug 1, 2000 Issued
Array ( [id] => 1401040 [patent_doc_number] => 06511021 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2003-01-28 [patent_title] => 'Thermal control system for controlling temperature in spacecraft' [patent_app_type] => B1 [patent_app_number] => 09/630184 [patent_app_country] => US [patent_app_date] => 2000-08-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 6 [patent_no_of_words] => 1617 [patent_no_of_claims] => 7 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 180 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/511/06511021.pdf [firstpage_image] =>[orig_patent_app_number] => 09630184 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/630184
Thermal control system for controlling temperature in spacecraft Jul 31, 2000 Issued
Array ( [id] => 4253261 [patent_doc_number] => 06244540 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 2001-06-12 [patent_title] => 'Method of calculating oxygen required and system for monitoring oxygen supply and/or calculating flight level after emergency cabin decompression' [patent_app_type] => 1 [patent_app_number] => 9/630212 [patent_app_country] => US [patent_app_date] => 2000-08-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 15 [patent_figures_cnt] => 15 [patent_no_of_words] => 6770 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 129 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/244/06244540.pdf [firstpage_image] =>[orig_patent_app_number] => 630212 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/630212
Method of calculating oxygen required and system for monitoring oxygen supply and/or calculating flight level after emergency cabin decompression Jul 31, 2000 Issued
09/601268 Flying object with a rotational effect Jul 28, 2000 Abandoned
Array ( [id] => 1514376 [patent_doc_number] => 06499700 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-12-31 [patent_title] => 'Attachment device for a cryogenic satellite tank' [patent_app_type] => B1 [patent_app_number] => 09/621760 [patent_app_country] => US [patent_app_date] => 2000-07-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 3313 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 157 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/499/06499700.pdf [firstpage_image] =>[orig_patent_app_number] => 09621760 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/621760
Attachment device for a cryogenic satellite tank Jul 20, 2000 Issued
Array ( [id] => 1096367 [patent_doc_number] => 06817569 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2004-11-16 [patent_title] => 'Guidance seeker system with optically triggered diverter elements' [patent_app_type] => B1 [patent_app_number] => 09/619949 [patent_app_country] => US [patent_app_date] => 2000-07-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 9 [patent_no_of_words] => 3176 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 131 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/817/06817569.pdf [firstpage_image] =>[orig_patent_app_number] => 09619949 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/619949
Guidance seeker system with optically triggered diverter elements Jul 19, 2000 Issued
Array ( [id] => 4329186 [patent_doc_number] => 06213432 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 2001-04-10 [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] => 9/619281 [patent_app_country] => US [patent_app_date] => 2000-07-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 15 [patent_no_of_words] => 9250 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 39 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/213/06213432.pdf [firstpage_image] =>[orig_patent_app_number] => 619281 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/619281
Method and a system for putting a space vehicle into orbit, using thrusters of high specific impulse Jul 18, 2000 Issued
Array ( [id] => 1345084 [patent_doc_number] => 06572055 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2003-06-03 [patent_title] => 'Hydrostatic sidestick coupling' [patent_app_type] => B1 [patent_app_number] => 09/616479 [patent_app_country] => US [patent_app_date] => 2000-07-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 12 [patent_no_of_words] => 6492 [patent_no_of_claims] => 28 [patent_no_of_ind_claims] => 6 [patent_words_short_claim] => 153 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/572/06572055.pdf [firstpage_image] =>[orig_patent_app_number] => 09616479 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/616479
Hydrostatic sidestick coupling Jul 13, 2000 Issued
09/615843 Method and apparatus for imparting unidirectional motion to an object in space Jul 12, 2000 Abandoned
Array ( [id] => 4312935 [patent_doc_number] => 06311927 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 2001-11-06 [patent_title] => 'Emergency landing gear extension system using pyrotechnic operated high pressure bottle' [patent_app_type] => 1 [patent_app_number] => 9/613740 [patent_app_country] => US [patent_app_date] => 2000-07-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 1 [patent_no_of_words] => 1180 [patent_no_of_claims] => 5 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 86 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/311/06311927.pdf [firstpage_image] =>[orig_patent_app_number] => 613740 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/613740
Emergency landing gear extension system using pyrotechnic operated high pressure bottle Jul 10, 2000 Issued
Array ( [id] => 1560991 [patent_doc_number] => 06375127 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-04-23 [patent_title] => 'Active control surface modal system for aircraft buffet and gust load alleviation and flutter suppression' [patent_app_type] => B1 [patent_app_number] => 09/612058 [patent_app_country] => US [patent_app_date] => 2000-07-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 12 [patent_no_of_words] => 4749 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 229 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/375/06375127.pdf [firstpage_image] =>[orig_patent_app_number] => 09612058 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/612058
Active control surface modal system for aircraft buffet and gust load alleviation and flutter suppression Jul 6, 2000 Issued
Array ( [id] => 479128 [patent_doc_number] => 07219861 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2007-05-22 [patent_title] => 'Guidance system for radio-controlled aircraft' [patent_app_type] => utility [patent_app_number] => 09/611177 [patent_app_country] => US [patent_app_date] => 2000-07-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 7 [patent_no_of_words] => 5748 [patent_no_of_claims] => 23 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 87 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/219/07219861.pdf [firstpage_image] =>[orig_patent_app_number] => 09611177 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/611177
Guidance system for radio-controlled aircraft Jul 5, 2000 Issued
Array ( [id] => 1480807 [patent_doc_number] => 06364248 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-04-02 [patent_title] => 'Articulated nose missile control actuation system' [patent_app_type] => B1 [patent_app_number] => 09/610924 [patent_app_country] => US [patent_app_date] => 2000-07-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 4 [patent_no_of_words] => 3537 [patent_no_of_claims] => 31 [patent_no_of_ind_claims] => 5 [patent_words_short_claim] => 46 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/364/06364248.pdf [firstpage_image] =>[orig_patent_app_number] => 09610924 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/610924
Articulated nose missile control actuation system Jul 5, 2000 Issued
Array ( [id] => 1538861 [patent_doc_number] => 06371407 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-04-16 [patent_title] => 'Mechanism for vectoring exhaust flow' [patent_app_type] => B1 [patent_app_number] => 09/609484 [patent_app_country] => US [patent_app_date] => 2000-07-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 11 [patent_no_of_words] => 1944 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 71 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/371/06371407.pdf [firstpage_image] =>[orig_patent_app_number] => 09609484 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/609484
Mechanism for vectoring exhaust flow Jul 4, 2000 Issued
Menu