
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] => 6819932
[patent_doc_number] => 20030218093
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-11-27
[patent_title] => 'TRANSMISSION FOR A COAXIAL COUNTER ROTATING ROTOR SYSTEM'
[patent_app_type] => new
[patent_app_number] => 10/153970
[patent_app_country] => US
[patent_app_date] => 2002-05-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 2791
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 47
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0218/20030218093.pdf
[firstpage_image] =>[orig_patent_app_number] => 10153970
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/153970 | Transmission for a coaxial counter rotating rotor system | May 22, 2002 | Issued |
Array
(
[id] => 799848
[patent_doc_number] => 07424988
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2008-09-16
[patent_title] => 'Use of aerodynamic forces to assist in the control and positioning of aircraft control surfaces and variable geometry systems'
[patent_app_type] => utility
[patent_app_number] => 10/482314
[patent_app_country] => US
[patent_app_date] => 2002-05-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 7052
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 191
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/424/07424988.pdf
[firstpage_image] =>[orig_patent_app_number] => 10482314
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/482314 | Use of aerodynamic forces to assist in the control and positioning of aircraft control surfaces and variable geometry systems | May 22, 2002 | Issued |
Array
(
[id] => 1051849
[patent_doc_number] => 06857602
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2005-02-22
[patent_title] => 'Environmental control system and method of using the same'
[patent_app_type] => utility
[patent_app_number] => 10/152907
[patent_app_country] => US
[patent_app_date] => 2002-05-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 17
[patent_no_of_words] => 12151
[patent_no_of_claims] => 49
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 101
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/857/06857602.pdf
[firstpage_image] =>[orig_patent_app_number] => 10152907
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/152907 | Environmental control system and method of using the same | May 21, 2002 | Issued |
Array
(
[id] => 6723328
[patent_doc_number] => 20030205640
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-11-06
[patent_title] => 'HYPERSONIC WAVERIDER VARIABLE LEADING EDGE FLAPS'
[patent_app_type] => new
[patent_app_number] => 10/138610
[patent_app_country] => US
[patent_app_date] => 2002-05-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 2120
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 120
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0205/20030205640.pdf
[firstpage_image] =>[orig_patent_app_number] => 10138610
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/138610 | Hypersonic waverider variable leading edge flaps | May 2, 2002 | Issued |
Array
(
[id] => 1316107
[patent_doc_number] => 06601801
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2003-08-05
[patent_title] => 'Gapped trailing-edge control surface for an airfoil'
[patent_app_type] => B1
[patent_app_number] => 10/131109
[patent_app_country] => US
[patent_app_date] => 2002-04-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 13
[patent_no_of_words] => 4001
[patent_no_of_claims] => 25
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 247
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/601/06601801.pdf
[firstpage_image] =>[orig_patent_app_number] => 10131109
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/131109 | Gapped trailing-edge control surface for an airfoil | Apr 23, 2002 | Issued |
Array
(
[id] => 1277849
[patent_doc_number] => 06637702
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2003-10-28
[patent_title] => 'Nested beam deployable solar array'
[patent_app_type] => B1
[patent_app_number] => 10/128421
[patent_app_country] => US
[patent_app_date] => 2002-04-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 4705
[patent_no_of_claims] => 22
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 60
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/637/06637702.pdf
[firstpage_image] =>[orig_patent_app_number] => 10128421
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/128421 | Nested beam deployable solar array | Apr 23, 2002 | Issued |
Array
(
[id] => 636233
[patent_doc_number] => 07124982
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2006-10-24
[patent_title] => 'Device for bracing a shell in an aircraft fuselage'
[patent_app_type] => utility
[patent_app_number] => 10/479663
[patent_app_country] => US
[patent_app_date] => 2002-04-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 8
[patent_no_of_words] => 977
[patent_no_of_claims] => 2
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 168
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/124/07124982.pdf
[firstpage_image] =>[orig_patent_app_number] => 10479663
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/479663 | Device for bracing a shell in an aircraft fuselage | Apr 22, 2002 | Issued |
Array
(
[id] => 1145791
[patent_doc_number] => 06766979
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-07-27
[patent_title] => 'Guidance seeker system with optically triggered diverter elements'
[patent_app_type] => B2
[patent_app_number] => 10/123459
[patent_app_country] => US
[patent_app_date] => 2002-04-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 9
[patent_no_of_words] => 3212
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 189
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/766/06766979.pdf
[firstpage_image] =>[orig_patent_app_number] => 10123459
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/123459 | Guidance seeker system with optically triggered diverter elements | Apr 15, 2002 | Issued |
Array
(
[id] => 1013649
[patent_doc_number] => 06892988
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2005-05-17
[patent_title] => 'Cylindrical wing tip with helical slot'
[patent_app_type] => utility
[patent_app_number] => 10/474879
[patent_app_country] => US
[patent_app_date] => 2002-04-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 4521
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 69
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/892/06892988.pdf
[firstpage_image] =>[orig_patent_app_number] => 10474879
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/474879 | Cylindrical wing tip with helical slot | Apr 8, 2002 | Issued |
Array
(
[id] => 1019520
[patent_doc_number] => 06886782
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2005-05-03
[patent_title] => 'System for supplying an aircraft with cool air'
[patent_app_type] => utility
[patent_app_number] => 10/121475
[patent_app_country] => US
[patent_app_date] => 2002-04-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 2
[patent_no_of_words] => 1992
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 74
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/886/06886782.pdf
[firstpage_image] =>[orig_patent_app_number] => 10121475
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/121475 | System for supplying an aircraft with cool air | Apr 7, 2002 | Issued |
Array
(
[id] => 1277841
[patent_doc_number] => 06637701
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2003-10-28
[patent_title] => 'Gimbaled ion thruster arrangement for high efficiency stationkeeping'
[patent_app_type] => B1
[patent_app_number] => 10/114472
[patent_app_country] => US
[patent_app_date] => 2002-04-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 7
[patent_no_of_words] => 4503
[patent_no_of_claims] => 30
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 117
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/637/06637701.pdf
[firstpage_image] =>[orig_patent_app_number] => 10114472
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/114472 | Gimbaled ion thruster arrangement for high efficiency stationkeeping | Apr 2, 2002 | Issued |
Array
(
[id] => 6533941
[patent_doc_number] => 20020162916
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-11-07
[patent_title] => 'Fast evacuation device for aircraft'
[patent_app_type] => new
[patent_app_number] => 10/112727
[patent_app_country] => US
[patent_app_date] => 2002-04-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_no_of_words] => 4856
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0162/20020162916.pdf
[firstpage_image] =>[orig_patent_app_number] => 10112727
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/112727 | Fast evacuation device for aircraft | Apr 1, 2002 | Issued |
Array
(
[id] => 6727529
[patent_doc_number] => 20030183719
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-10-02
[patent_title] => 'AIRCRAFT FERRYING SYSTEM AND METHOD THEREOF'
[patent_app_type] => new
[patent_app_number] => 10/112144
[patent_app_country] => US
[patent_app_date] => 2002-04-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[patent_no_of_words] => 3060
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0183/20030183719.pdf
[firstpage_image] =>[orig_patent_app_number] => 10112144
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/112144 | Aircraft ferrying system and method thereof | Mar 31, 2002 | Issued |
Array
(
[id] => 6727538
[patent_doc_number] => 20030183728
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-10-02
[patent_title] => 'Aircraft control surface controller and associated method'
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[patent_app_number] => 10/112815
[patent_app_country] => US
[patent_app_date] => 2002-03-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[patent_no_of_words] => 6117
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0183/20030183728.pdf
[firstpage_image] =>[orig_patent_app_number] => 10112815
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/112815 | Aircraft control surface controller and associated method | Mar 28, 2002 | Abandoned |
Array
(
[id] => 792368
[patent_doc_number] => 06981671
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2006-01-03
[patent_title] => 'Airframe structure-integrated capacitor'
[patent_app_type] => utility
[patent_app_number] => 10/109396
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[patent_app_date] => 2002-03-28
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/981/06981671.pdf
[firstpage_image] =>[orig_patent_app_number] => 10109396
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/109396 | Airframe structure-integrated capacitor | Mar 27, 2002 | Issued |
Array
(
[id] => 1341453
[patent_doc_number] => 06575404
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2003-06-10
[patent_title] => 'Air intake and flying device, particularly a missile, equipped with such an air intake'
[patent_app_type] => B2
[patent_app_number] => 10/106209
[patent_app_country] => US
[patent_app_date] => 2002-03-27
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/575/06575404.pdf
[firstpage_image] =>[orig_patent_app_number] => 10106209
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/106209 | Air intake and flying device, particularly a missile, equipped with such an air intake | Mar 26, 2002 | Issued |
Array
(
[id] => 7030601
[patent_doc_number] => 20050029402
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-02-10
[patent_title] => 'Aircraft configuration with improved aerodynamic performance'
[patent_app_type] => utility
[patent_app_number] => 10/491327
[patent_app_country] => US
[patent_app_date] => 2002-03-27
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0029/20050029402.pdf
[firstpage_image] =>[orig_patent_app_number] => 10491327
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/491327 | Aircraft configuration with improved aerodynamic performance | Mar 26, 2002 | Issued |
Array
(
[id] => 696520
[patent_doc_number] => 07066431
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2006-06-27
[patent_title] => 'Turbulent flow drag reduction'
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[patent_app_number] => 10/474006
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[pdf_file] => patents/07/066/07066431.pdf
[firstpage_image] =>[orig_patent_app_number] => 10474006
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/474006 | Turbulent flow drag reduction | Mar 25, 2002 | Issued |
Array
(
[id] => 750174
[patent_doc_number] => 07017863
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[patent_kind] => B2
[patent_issue_date] => 2006-03-28
[patent_title] => 'Turbulent flow drag reduction'
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[pdf_file] => patents/07/017/07017863.pdf
[firstpage_image] =>[orig_patent_app_number] => 10474008
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/474008 | Turbulent flow drag reduction | Mar 25, 2002 | Issued |
Array
(
[id] => 6153596
[patent_doc_number] => 20020145076
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-10-10
[patent_title] => 'AIRCRAFT'
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[patent_app_number] => 10/105334
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0145/20020145076.pdf
[firstpage_image] =>[orig_patent_app_number] => 10105334
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/105334 | AIRCRAFT | Mar 25, 2002 | Abandoned |