
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] => 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
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[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
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[patent_no_of_words] => 1944
[patent_no_of_claims] => 19
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[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 |