
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 |
|---|---|---|---|
| 09/457783 | OVERHEAD ACCOMMODATIONS FOR AIRCRAFT | Dec 8, 1999 | Abandoned |
Array
(
[id] => 4366870
[patent_doc_number] => 06293495
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2001-09-25
[patent_title] => 'Pivoting door thrust reverser system for turbofan aircraft jet engine'
[patent_app_type] => 1
[patent_app_number] => 9/456783
[patent_app_country] => US
[patent_app_date] => 1999-12-08
[patent_effective_date] => 0000-00-00
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[patent_figures_cnt] => 10
[patent_no_of_words] => 4025
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[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/293/06293495.pdf
[firstpage_image] =>[orig_patent_app_number] => 456783
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/456783 | Pivoting door thrust reverser system for turbofan aircraft jet engine | Dec 7, 1999 | Issued |
Array
(
[id] => 4289744
[patent_doc_number] => 06325332
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2001-12-04
[patent_title] => 'Coordinatable system of inclined geosynchronous satellite orbits'
[patent_app_type] => 1
[patent_app_number] => 9/444199
[patent_app_country] => US
[patent_app_date] => 1999-11-19
[patent_effective_date] => 0000-00-00
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[pdf_file] => patents/06/325/06325332.pdf
[firstpage_image] =>[orig_patent_app_number] => 444199
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/444199 | Coordinatable system of inclined geosynchronous satellite orbits | Nov 18, 1999 | Issued |
Array
(
[id] => 4351297
[patent_doc_number] => 06286790
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2001-09-11
[patent_title] => 'Aerofoil having a slat with flexible data link'
[patent_app_type] => 1
[patent_app_number] => 9/428533
[patent_app_country] => US
[patent_app_date] => 1999-10-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[pdf_file] => patents/06/286/06286790.pdf
[firstpage_image] =>[orig_patent_app_number] => 428533
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/428533 | Aerofoil having a slat with flexible data link | Oct 27, 1999 | Issued |
Array
(
[id] => 4333625
[patent_doc_number] => 06290185
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2001-09-18
[patent_title] => 'Solar thermal rocket'
[patent_app_type] => 1
[patent_app_number] => 9/427844
[patent_app_country] => US
[patent_app_date] => 1999-10-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
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[firstpage_image] =>[orig_patent_app_number] => 427844
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/427844 | Solar thermal rocket | Oct 25, 1999 | Issued |
Array
(
[id] => 4344189
[patent_doc_number] => 06173922
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2001-01-16
[patent_title] => 'Failure resistant multiline tether'
[patent_app_type] => 1
[patent_app_number] => 9/403033
[patent_app_country] => US
[patent_app_date] => 1999-10-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 28
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[pdf_file] => patents/06/173/06173922.pdf
[firstpage_image] =>[orig_patent_app_number] => 403033
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/403033 | Failure resistant multiline tether | Oct 21, 1999 | Issued |
Array
(
[id] => 4333485
[patent_doc_number] => 06290175
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2001-09-18
[patent_title] => 'Bin extension for a vehicle'
[patent_app_type] => 1
[patent_app_number] => 9/422113
[patent_app_country] => US
[patent_app_date] => 1999-10-20
[patent_effective_date] => 0000-00-00
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[pdf_file] => patents/06/290/06290175.pdf
[firstpage_image] =>[orig_patent_app_number] => 422113
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/422113 | Bin extension for a vehicle | Oct 19, 1999 | Issued |
Array
(
[id] => 4333598
[patent_doc_number] => 06290183
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2001-09-18
[patent_title] => 'Three-axis, six degree-of-freedom, whole-spacecraft passive vibration isolation system'
[patent_app_type] => 1
[patent_app_number] => 9/420843
[patent_app_country] => US
[patent_app_date] => 1999-10-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[pdf_file] => patents/06/290/06290183.pdf
[firstpage_image] =>[orig_patent_app_number] => 420843
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/420843 | Three-axis, six degree-of-freedom, whole-spacecraft passive vibration isolation system | Oct 18, 1999 | Issued |
Array
(
[id] => 4284645
[patent_doc_number] => 06250584
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2001-06-26
[patent_title] => 'Missile fin locking mechanism'
[patent_app_type] => 1
[patent_app_number] => 9/419544
[patent_app_country] => US
[patent_app_date] => 1999-10-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[pdf_file] => patents/06/250/06250584.pdf
[firstpage_image] =>[orig_patent_app_number] => 419544
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/419544 | Missile fin locking mechanism | Oct 17, 1999 | Issued |
Array
(
[id] => 4391492
[patent_doc_number] => 06237874
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2001-05-29
[patent_title] => 'Zoned aircraft de-icing system and method'
[patent_app_type] => 1
[patent_app_number] => 9/419466
[patent_app_country] => US
[patent_app_date] => 1999-10-15
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[patent_drawing_sheets_cnt] => 30
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[pdf_file] => patents/06/237/06237874.pdf
[firstpage_image] =>[orig_patent_app_number] => 419466
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/419466 | Zoned aircraft de-icing system and method | Oct 14, 1999 | Issued |
Array
(
[id] => 4326013
[patent_doc_number] => 06283413
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2001-09-04
[patent_title] => 'Rotary flyer'
[patent_app_type] => 1
[patent_app_number] => 9/399553
[patent_app_country] => US
[patent_app_date] => 1999-09-20
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[pdf_file] => patents/06/283/06283413.pdf
[firstpage_image] =>[orig_patent_app_number] => 399553
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/399553 | Rotary flyer | Sep 19, 1999 | Issued |
Array
(
[id] => 4364444
[patent_doc_number] => 06260800
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2001-07-17
[patent_title] => 'Aircraft power plant with two air intake fans'
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[patent_app_number] => 9/399178
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[pdf_file] => patents/06/260/06260800.pdf
[firstpage_image] =>[orig_patent_app_number] => 399178
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/399178 | Aircraft power plant with two air intake fans | Sep 19, 1999 | Issued |
Array
(
[id] => 1540065
[patent_doc_number] => 06371681
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-04-16
[patent_title] => 'Anti-rotation clip'
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[patent_app_number] => 09/400513
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[firstpage_image] =>[orig_patent_app_number] => 09400513
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/400513 | Anti-rotation clip | Sep 19, 1999 | Issued |
Array
(
[id] => 4365027
[patent_doc_number] => 06276632
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2001-08-21
[patent_title] => 'Axi-symmetric mixed compression inlet with variable geometry centerbody'
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[patent_app_number] => 9/397393
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[pdf_file] => patents/06/276/06276632.pdf
[firstpage_image] =>[orig_patent_app_number] => 397393
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/397393 | Axi-symmetric mixed compression inlet with variable geometry centerbody | Sep 15, 1999 | Issued |
Array
(
[id] => 4366830
[patent_doc_number] => 06293492
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2001-09-25
[patent_title] => 'Coaxial twin-rotor type helicopter'
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[patent_app_number] => 9/387493
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[pdf_file] => patents/06/293/06293492.pdf
[firstpage_image] =>[orig_patent_app_number] => 387493
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/387493 | Coaxial twin-rotor type helicopter | Aug 31, 1999 | Issued |
Array
(
[id] => 4310075
[patent_doc_number] => 06318671
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[patent_issue_date] => 2001-11-20
[patent_title] => 'Variable position and modular luggage storage system for an aircraft passenger cabin'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 09/388134 | Variable position and modular luggage storage system for an aircraft passenger cabin | Aug 31, 1999 | Issued |
Array
(
[id] => 1120313
[patent_doc_number] => 06793175
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[patent_issue_date] => 2004-09-21
[patent_title] => 'Supersonic external-compression diffuser and method for designing same'
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[pdf_file] => patents/06/793/06793175.pdf
[firstpage_image] =>[orig_patent_app_number] => 09382437
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/382437 | Supersonic external-compression diffuser and method for designing same | Aug 24, 1999 | Issued |
Array
(
[id] => 4391597
[patent_doc_number] => 06227497
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2001-05-08
[patent_title] => 'Adaptively positioned solar array'
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[patent_app_number] => 9/378564
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[firstpage_image] =>[orig_patent_app_number] => 378564
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/378564 | Adaptively positioned solar array | Aug 18, 1999 | Issued |
Array
(
[id] => 4068235
[patent_doc_number] => 06131857
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[firstpage_image] =>[orig_patent_app_number] => 371784
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/371784 | Miniature spacecraft | Aug 9, 1999 | Issued |
Array
(
[id] => 4404567
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[firstpage_image] =>[orig_patent_app_number] => 371663
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/371663 | Rotary engine and helicopter application | Aug 9, 1999 | Issued |