
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] => 1336102
[patent_doc_number] => 06578667
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2003-06-17
[patent_title] => 'Thrust reverser blocker door access platform'
[patent_app_type] => B2
[patent_app_number] => 09/791442
[patent_app_country] => US
[patent_app_date] => 2001-02-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 9
[patent_no_of_words] => 1826
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 58
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/578/06578667.pdf
[firstpage_image] =>[orig_patent_app_number] => 09791442
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/791442 | Thrust reverser blocker door access platform | Feb 22, 2001 | Issued |
Array
(
[id] => 1019511
[patent_doc_number] => 06886777
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2005-05-03
[patent_title] => 'Coaxial helicopter'
[patent_app_type] => utility
[patent_app_number] => 09/782941
[patent_app_country] => US
[patent_app_date] => 2001-02-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
[patent_figures_cnt] => 17
[patent_no_of_words] => 10663
[patent_no_of_claims] => 27
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 57
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/886/06886777.pdf
[firstpage_image] =>[orig_patent_app_number] => 09782941
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/782941 | Coaxial helicopter | Feb 13, 2001 | Issued |
Array
(
[id] => 6903287
[patent_doc_number] => 20050098682
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-05-12
[patent_title] => 'Light weight helicopter'
[patent_app_type] => utility
[patent_app_number] => 10/380904
[patent_app_country] => US
[patent_app_date] => 2001-02-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 3203
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0098/20050098682.pdf
[firstpage_image] =>[orig_patent_app_number] => 10380904
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/380904 | Light weight helicopter | Feb 6, 2001 | Abandoned |
Array
(
[id] => 1217318
[patent_doc_number] => 06702233
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2004-03-09
[patent_title] => 'Airfoil anti-icing assembly and method'
[patent_app_type] => B1
[patent_app_number] => 09/778178
[patent_app_country] => US
[patent_app_date] => 2001-02-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 10
[patent_no_of_words] => 3818
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 6
[patent_words_short_claim] => 156
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/702/06702233.pdf
[firstpage_image] =>[orig_patent_app_number] => 09778178
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/778178 | Airfoil anti-icing assembly and method | Feb 6, 2001 | Issued |
Array
(
[id] => 1541511
[patent_doc_number] => 06443392
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2002-09-03
[patent_title] => 'Monolithic structure with redundant load paths'
[patent_app_type] => B2
[patent_app_number] => 09/778359
[patent_app_country] => US
[patent_app_date] => 2001-02-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 9
[patent_no_of_words] => 3210
[patent_no_of_claims] => 3
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 179
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/443/06443392.pdf
[firstpage_image] =>[orig_patent_app_number] => 09778359
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/778359 | Monolithic structure with redundant load paths | Feb 6, 2001 | Issued |
Array
(
[id] => 1347443
[patent_doc_number] => 06568636
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2003-05-27
[patent_title] => 'Buffer stop assembly'
[patent_app_type] => B2
[patent_app_number] => 09/778640
[patent_app_country] => US
[patent_app_date] => 2001-02-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 3318
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 6
[patent_words_short_claim] => 68
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/568/06568636.pdf
[firstpage_image] =>[orig_patent_app_number] => 09778640
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/778640 | Buffer stop assembly | Feb 6, 2001 | Issued |
Array
(
[id] => 1555350
[patent_doc_number] => 06435457
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-08-20
[patent_title] => 'Thruster systems for spacecraft station changing, station keeping and momentum dumping'
[patent_app_type] => B1
[patent_app_number] => 09/769936
[patent_app_country] => US
[patent_app_date] => 2001-01-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 6
[patent_no_of_words] => 4040
[patent_no_of_claims] => 28
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 301
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/435/06435457.pdf
[firstpage_image] =>[orig_patent_app_number] => 09769936
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/769936 | Thruster systems for spacecraft station changing, station keeping and momentum dumping | Jan 24, 2001 | Issued |
Array
(
[id] => 1449523
[patent_doc_number] => 06460809
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-10-08
[patent_title] => 'Spacecraft methods and systems for autonomous correction of star tracker charge-transfer-efficiency errors'
[patent_app_type] => B1
[patent_app_number] => 09/769637
[patent_app_country] => US
[patent_app_date] => 2001-01-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 13
[patent_no_of_words] => 5296
[patent_no_of_claims] => 24
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 282
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/460/06460809.pdf
[firstpage_image] =>[orig_patent_app_number] => 09769637
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/769637 | Spacecraft methods and systems for autonomous correction of star tracker charge-transfer-efficiency errors | Jan 24, 2001 | Issued |
Array
(
[id] => 1525582
[patent_doc_number] => 06478255
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-11-12
[patent_title] => 'Crash energy absorbing glareshield and method of protecting against head injury in aircraft crashes'
[patent_app_type] => B1
[patent_app_number] => 09/765849
[patent_app_country] => US
[patent_app_date] => 2001-01-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 4
[patent_no_of_words] => 1542
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 75
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/478/06478255.pdf
[firstpage_image] =>[orig_patent_app_number] => 09765849
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/765849 | Crash energy absorbing glareshield and method of protecting against head injury in aircraft crashes | Jan 18, 2001 | Issued |
Array
(
[id] => 6300030
[patent_doc_number] => 20020092948
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-07-18
[patent_title] => 'Apparatus and method for reducing jet engine noise'
[patent_app_type] => new
[patent_app_number] => 09/761335
[patent_app_country] => US
[patent_app_date] => 2001-01-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2912
[patent_no_of_claims] => 2
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 95
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0092/20020092948.pdf
[firstpage_image] =>[orig_patent_app_number] => 09761335
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/761335 | Apparatus and method for reducing jet engine noise | Jan 15, 2001 | Abandoned |
Array
(
[id] => 1331888
[patent_doc_number] => 06589017
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2003-07-08
[patent_title] => 'Aircraft airfoil assembly and method'
[patent_app_type] => B1
[patent_app_number] => 09/752239
[patent_app_country] => US
[patent_app_date] => 2001-01-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 10
[patent_no_of_words] => 2131
[patent_no_of_claims] => 4
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 284
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/589/06589017.pdf
[firstpage_image] =>[orig_patent_app_number] => 09752239
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/752239 | Aircraft airfoil assembly and method | Jan 1, 2001 | Issued |
| 09/720876 | SPIRAL AND CYLINDRICAL WING TIP | Jan 1, 2001 | Abandoned |
Array
(
[id] => 6569027
[patent_doc_number] => 20020084385
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-07-04
[patent_title] => 'Spacecraft attack and distress ejectable recorder'
[patent_app_type] => new
[patent_app_number] => 09/752175
[patent_app_country] => US
[patent_app_date] => 2000-12-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[patent_no_of_words] => 2296
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0084/20020084385.pdf
[firstpage_image] =>[orig_patent_app_number] => 09752175
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/752175 | Spacecraft attack and distress ejectable recorder | Dec 28, 2000 | Issued |
Array
(
[id] => 7039975
[patent_doc_number] => 20010005000
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2001-06-28
[patent_title] => 'Opening reinforcement for aerostat envelope'
[patent_app_type] => new-utility
[patent_app_number] => 09/742543
[patent_app_country] => US
[patent_app_date] => 2000-12-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
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[patent_no_of_words] => 2039
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0005/20010005000.pdf
[firstpage_image] =>[orig_patent_app_number] => 09742543
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/742543 | Opening reinforcement for aerostat envelope | Dec 21, 2000 | Issued |
Array
(
[id] => 1371403
[patent_doc_number] => 06543717
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2003-04-08
[patent_title] => 'Compact optimal and modulatable thrust device for controlling aerospace vehicles'
[patent_app_type] => B1
[patent_app_number] => 09/720210
[patent_app_country] => US
[patent_app_date] => 2000-12-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[patent_no_of_words] => 2750
[patent_no_of_claims] => 12
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/543/06543717.pdf
[firstpage_image] =>[orig_patent_app_number] => 09720210
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/720210 | Compact optimal and modulatable thrust device for controlling aerospace vehicles | Dec 21, 2000 | Issued |
Array
(
[id] => 6885821
[patent_doc_number] => 20010019090
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2001-09-06
[patent_title] => 'High pressure spray system'
[patent_app_type] => new
[patent_app_number] => 09/741745
[patent_app_country] => US
[patent_app_date] => 2000-12-19
[patent_effective_date] => 0000-00-00
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[pdf_file] => publications/A1/0019/20010019090.pdf
[firstpage_image] =>[orig_patent_app_number] => 09741745
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/741745 | High pressure spray system | Dec 18, 2000 | Abandoned |
Array
(
[id] => 1591015
[patent_doc_number] => 06491255
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-12-10
[patent_title] => 'Crashworthy external auxiliary fuel tank for aircraft'
[patent_app_type] => B1
[patent_app_number] => 09/738125
[patent_app_country] => US
[patent_app_date] => 2000-12-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
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[patent_no_of_words] => 2726
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/491/06491255.pdf
[firstpage_image] =>[orig_patent_app_number] => 09738125
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/738125 | Crashworthy external auxiliary fuel tank for aircraft | Dec 14, 2000 | Issued |
Array
(
[id] => 1443854
[patent_doc_number] => 06367741
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2002-04-09
[patent_title] => 'Flight control system for a rotary-wing aircraft, particularly for a helicopter'
[patent_app_type] => B2
[patent_app_number] => 09/734641
[patent_app_country] => US
[patent_app_date] => 2000-12-13
[patent_effective_date] => 0000-00-00
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[pdf_file] => patents/06/367/06367741.pdf
[firstpage_image] =>[orig_patent_app_number] => 09734641
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/734641 | Flight control system for a rotary-wing aircraft, particularly for a helicopter | Dec 12, 2000 | Issued |
Array
(
[id] => 1485590
[patent_doc_number] => 06428381
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-08-06
[patent_title] => 'Flying device which rotates as it travels through the air'
[patent_app_type] => B1
[patent_app_number] => 09/734263
[patent_app_country] => US
[patent_app_date] => 2000-12-11
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[pdf_file] => patents/06/428/06428381.pdf
[firstpage_image] =>[orig_patent_app_number] => 09734263
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/734263 | Flying device which rotates as it travels through the air | Dec 10, 2000 | Issued |
Array
(
[id] => 6300029
[patent_doc_number] => 20020092947
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-07-18
[patent_title] => 'Aircraft with elliptical Winglets'
[patent_app_type] => new
[patent_app_number] => 09/734347
[patent_app_country] => US
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[pdf_file] => publications/A1/0092/20020092947.pdf
[firstpage_image] =>[orig_patent_app_number] => 09734347
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/734347 | Aircraft with elliptical winglets | Dec 10, 2000 | Issued |