
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] => 716879
[patent_doc_number] => 07048229
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2006-05-23
[patent_title] => 'Low sonic boom inlet for supersonic aircraft'
[patent_app_type] => utility
[patent_app_number] => 09/966551
[patent_app_country] => US
[patent_app_date] => 2001-09-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 14
[patent_figures_cnt] => 26
[patent_no_of_words] => 5267
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/048/07048229.pdf
[firstpage_image] =>[orig_patent_app_number] => 09966551
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/966551 | Low sonic boom inlet for supersonic aircraft | Sep 25, 2001 | Issued |
Array
(
[id] => 7379285
[patent_doc_number] => 20040035980
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-02-26
[patent_title] => 'Seats that convert to sleeper bunks'
[patent_app_type] => new
[patent_app_number] => 10/380654
[patent_app_country] => US
[patent_app_date] => 2003-03-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
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[patent_no_of_words] => 5880
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[pdf_file] => publications/A1/0035/20040035980.pdf
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[rel_patent_id] =>[rel_patent_doc_number] =>) 10/380654 | Seats that convert to sleeper bunks | Sep 18, 2001 | Issued |
Array
(
[id] => 7967563
[patent_doc_number] => 06679455
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-01-20
[patent_title] => 'Pointing device and an onboard pointing system'
[patent_app_type] => B2
[patent_app_number] => 09/954416
[patent_app_country] => US
[patent_app_date] => 2001-09-17
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[patent_drawing_sheets_cnt] => 5
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[rel_patent_id] =>[rel_patent_doc_number] =>) 09/954416 | Pointing device and an onboard pointing system | Sep 16, 2001 | Issued |
Array
(
[id] => 980871
[patent_doc_number] => 06926228
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2005-08-09
[patent_title] => 'Method and arrangement for extending the range of fire of a fin-stabilized artillery missile'
[patent_app_type] => utility
[patent_app_number] => 10/363636
[patent_app_country] => US
[patent_app_date] => 2001-08-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
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[patent_no_of_words] => 1416
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[pdf_file] => patents/06/926/06926228.pdf
[firstpage_image] =>[orig_patent_app_number] => 10363636
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/363636 | Method and arrangement for extending the range of fire of a fin-stabilized artillery missile | Aug 23, 2001 | Issued |
Array
(
[id] => 5718348
[patent_doc_number] => 20060071120
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-04-06
[patent_title] => 'Canard fin unit'
[patent_app_type] => utility
[patent_app_number] => 10/362825
[patent_app_country] => US
[patent_app_date] => 2001-08-24
[patent_effective_date] => 0000-00-00
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[pdf_file] => publications/A1/0071/20060071120.pdf
[firstpage_image] =>[orig_patent_app_number] => 10362825
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/362825 | Canard fin unit | Aug 23, 2001 | Issued |
Array
(
[id] => 6845257
[patent_doc_number] => 20030164424
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-09-04
[patent_title] => 'Seaplane with retractable twin floats'
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[patent_app_number] => 10/362436
[patent_app_country] => US
[patent_app_date] => 2003-02-20
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[pdf_file] => publications/A1/0164/20030164424.pdf
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[rel_patent_id] =>[rel_patent_doc_number] =>) 10/362436 | Seaplane with retractable twin floats | Aug 21, 2001 | Issued |
Array
(
[id] => 1454368
[patent_doc_number] => 06390413
[patent_country] => US
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[patent_issue_date] => 2002-05-21
[patent_title] => 'Years two thousand of new safety helicopter'
[patent_app_type] => B1
[patent_app_number] => 09/947037
[patent_app_country] => US
[patent_app_date] => 2001-08-21
[patent_effective_date] => 0000-00-00
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[pdf_file] => patents/06/390/06390413.pdf
[firstpage_image] =>[orig_patent_app_number] => 09947037
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/947037 | Years two thousand of new safety helicopter | Aug 20, 2001 | Issued |
Array
(
[id] => 6733233
[patent_doc_number] => 20030010868
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-01-16
[patent_title] => 'ORBIT TRANSFER VEHICLE WITH SUPPORT SERVICES'
[patent_app_type] => new
[patent_app_number] => 09/925206
[patent_app_country] => US
[patent_app_date] => 2001-08-09
[patent_effective_date] => 0000-00-00
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[patent_no_of_words] => 4040
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[pdf_file] => publications/A1/0010/20030010868.pdf
[firstpage_image] =>[orig_patent_app_number] => 09925206
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/925206 | Orbit transfer vehicle with support services | Aug 8, 2001 | Issued |
Array
(
[id] => 6491913
[patent_doc_number] => 20020190160
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-12-19
[patent_title] => 'AEROBRAKING ORBIT TRANSFER VEHICLE'
[patent_app_type] => new
[patent_app_number] => 09/925207
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[rel_patent_id] =>[rel_patent_doc_number] =>) 09/925207 | Aerobraking orbit transfer vehicle | Aug 8, 2001 | Issued |
Array
(
[id] => 1337330
[patent_doc_number] => 06578797
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2003-06-17
[patent_title] => 'Kite altitude measuring apparatus'
[patent_app_type] => B2
[patent_app_number] => 09/922212
[patent_app_country] => US
[patent_app_date] => 2001-08-06
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[pdf_file] => patents/06/578/06578797.pdf
[firstpage_image] =>[orig_patent_app_number] => 09922212
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/922212 | Kite altitude measuring apparatus | Aug 5, 2001 | Issued |
Array
(
[id] => 1334964
[patent_doc_number] => 06581883
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[patent_kind] => B2
[patent_issue_date] => 2003-06-24
[patent_title] => 'Extendable/retractable bi-fold solar array'
[patent_app_type] => B2
[patent_app_number] => 09/905544
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[pdf_file] => patents/06/581/06581883.pdf
[firstpage_image] =>[orig_patent_app_number] => 09905544
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/905544 | Extendable/retractable bi-fold solar array | Jul 12, 2001 | Issued |
Array
(
[id] => 1577086
[patent_doc_number] => 06422511
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-07-23
[patent_title] => 'Support system for ground testing an aircraft'
[patent_app_type] => B1
[patent_app_number] => 09/898840
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[firstpage_image] =>[orig_patent_app_number] => 09898840
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/898840 | Support system for ground testing an aircraft | Jul 4, 2001 | Issued |
Array
(
[id] => 6137494
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[patent_title] => 'Linear actuation device for spacecraft and solar generator unfolding systems'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 09/894138 | Linear actuation device for spacecraft and solar generator unfolding systems | Jun 28, 2001 | Issued |
Array
(
[id] => 1253777
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[patent_issue_date] => 2003-12-23
[patent_title] => 'Blended wing and multiple-body airplane configuration'
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Array
(
[id] => 6646040
[patent_doc_number] => 20030075643
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[patent_issue_date] => 2003-04-24
[patent_title] => 'FUEL CELL POWERED ELECTRIC AIRCRAFT'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 09/938877 | Fuel cell powered electric aircraft | Jun 23, 2001 | Issued |
| 09/868943 | ADJUSTABLE BLADE PROFILE OF THE ROTOR BLADE OF A ROTARY WING AIRCRAFT | Jun 20, 2001 | Abandoned |
Array
(
[id] => 6880161
[patent_doc_number] => 20010031448
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[patent_title] => 'Method of technical education employing flying objects and flying objects used therefor'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 09/883392 | Method of technical education employing flying objects and flying objects used therefor | Jun 18, 2001 | Abandoned |
Array
(
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[patent_title] => 'Phase change material thermal control for electric propulsion'
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Array
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Array
(
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