
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] => 7267633
[patent_doc_number] => 20040056151
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-03-25
[patent_title] => 'High temperature resistant airfoil apparatus for a hypersonic space vehicle'
[patent_app_type] => new
[patent_app_number] => 10/431414
[patent_app_country] => US
[patent_app_date] => 2003-05-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2431
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 90
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0056/20040056151.pdf
[firstpage_image] =>[orig_patent_app_number] => 10431414
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/431414 | High temperature resistant airfoil apparatus for a hypersonic space vehicle | May 6, 2003 | Abandoned |
Array
(
[id] => 6803277
[patent_doc_number] => 20030230671
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-12-18
[patent_title] => 'Fuel cell powered electric aircraft'
[patent_app_type] => new
[patent_app_number] => 10/431052
[patent_app_country] => US
[patent_app_date] => 2003-05-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 5120
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 41
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0230/20030230671.pdf
[firstpage_image] =>[orig_patent_app_number] => 10431052
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/431052 | Fuel cell powered electric aircraft | May 5, 2003 | Abandoned |
Array
(
[id] => 7318571
[patent_doc_number] => 20040135035
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-07-15
[patent_title] => 'Momentum stabilized launch vehicle upper stage'
[patent_app_type] => new
[patent_app_number] => 10/427111
[patent_app_country] => US
[patent_app_date] => 2003-04-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 5138
[patent_no_of_claims] => 34
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 86
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0135/20040135035.pdf
[firstpage_image] =>[orig_patent_app_number] => 10427111
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/427111 | Momentum stabilized launch vehicle upper stage | Apr 29, 2003 | Issued |
Array
(
[id] => 1096387
[patent_doc_number] => 06817578
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2004-11-16
[patent_title] => 'Enhanced aerial delivery system (EADS) platform'
[patent_app_type] => B1
[patent_app_number] => 10/425147
[patent_app_country] => US
[patent_app_date] => 2003-04-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
[patent_figures_cnt] => 19
[patent_no_of_words] => 5708
[patent_no_of_claims] => 29
[patent_no_of_ind_claims] => 10
[patent_words_short_claim] => 117
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/817/06817578.pdf
[firstpage_image] =>[orig_patent_app_number] => 10425147
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/425147 | Enhanced aerial delivery system (EADS) platform | Apr 27, 2003 | Issued |
Array
(
[id] => 7426695
[patent_doc_number] => 20040007644
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-01-15
[patent_title] => 'Rotor craft'
[patent_app_type] => new
[patent_app_number] => 10/423831
[patent_app_country] => US
[patent_app_date] => 2003-04-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 11
[patent_no_of_words] => 9245
[patent_no_of_claims] => 25
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 14
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0007/20040007644.pdf
[firstpage_image] =>[orig_patent_app_number] => 10423831
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/423831 | Rotor craft | Apr 24, 2003 | Abandoned |
Array
(
[id] => 7337987
[patent_doc_number] => 20040245382
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-12-09
[patent_title] => 'Aircraft which employs hydrogen as fuel'
[patent_app_type] => new
[patent_app_number] => 10/419302
[patent_app_country] => US
[patent_app_date] => 2003-04-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 6756
[patent_no_of_claims] => 2
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 102
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0245/20040245382.pdf
[firstpage_image] =>[orig_patent_app_number] => 10419302
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/419302 | Aircraft which employs hydrogen as fuel | Apr 21, 2003 | Abandoned |
Array
(
[id] => 7432704
[patent_doc_number] => 20040065781
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-04-08
[patent_title] => 'Satellite constellations using nodally-adjusted repeating ground track orbits'
[patent_app_type] => new
[patent_app_number] => 10/420279
[patent_app_country] => US
[patent_app_date] => 2003-04-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 25
[patent_figures_cnt] => 25
[patent_no_of_words] => 8375
[patent_no_of_claims] => 30
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 64
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0065/20040065781.pdf
[firstpage_image] =>[orig_patent_app_number] => 10420279
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/420279 | Satellite constellations using nodally-adjusted repeating ground track orbits | Apr 21, 2003 | Issued |
Array
(
[id] => 7410489
[patent_doc_number] => 20040206853
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-10-21
[patent_title] => 'Apparatus and methods of attaching panels to support structures'
[patent_app_type] => new
[patent_app_number] => 10/418400
[patent_app_country] => US
[patent_app_date] => 2003-04-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 3054
[patent_no_of_claims] => 37
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 88
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0206/20040206853.pdf
[firstpage_image] =>[orig_patent_app_number] => 10418400
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/418400 | Apparatus and methods of attaching panels to support structures | Apr 17, 2003 | Issued |
Array
(
[id] => 7132592
[patent_doc_number] => 20050178924
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-08-18
[patent_title] => 'Perforated skin structure for laminar-flow systems'
[patent_app_type] => utility
[patent_app_number] => 10/511930
[patent_app_country] => US
[patent_app_date] => 2003-04-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 11
[patent_no_of_words] => 8906
[patent_no_of_claims] => 31
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0178/20050178924.pdf
[firstpage_image] =>[orig_patent_app_number] => 10511930
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/511930 | Perforated skin structure for laminar-flow systems | Apr 16, 2003 | Issued |
Array
(
[id] => 1011754
[patent_doc_number] => 06896221
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2005-05-24
[patent_title] => 'Vertical takeoff and landing aircraft'
[patent_app_type] => utility
[patent_app_number] => 10/414874
[patent_app_country] => US
[patent_app_date] => 2003-04-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 13
[patent_no_of_words] => 6609
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 250
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/896/06896221.pdf
[firstpage_image] =>[orig_patent_app_number] => 10414874
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/414874 | Vertical takeoff and landing aircraft | Apr 15, 2003 | Issued |
Array
(
[id] => 670534
[patent_doc_number] => 07090164
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2006-08-15
[patent_title] => 'Method for producing a lift and a horizontal thrust'
[patent_app_type] => utility
[patent_app_number] => 10/511780
[patent_app_country] => US
[patent_app_date] => 2003-04-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 1984
[patent_no_of_claims] => 2
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 148
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/090/07090164.pdf
[firstpage_image] =>[orig_patent_app_number] => 10511780
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/511780 | Method for producing a lift and a horizontal thrust | Apr 13, 2003 | Issued |
Array
(
[id] => 1228000
[patent_doc_number] => 06691948
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2004-02-17
[patent_title] => 'High torque rocket nozzle'
[patent_app_type] => B1
[patent_app_number] => 10/413182
[patent_app_country] => US
[patent_app_date] => 2003-04-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 2
[patent_no_of_words] => 2907
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 64
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/691/06691948.pdf
[firstpage_image] =>[orig_patent_app_number] => 10413182
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/413182 | High torque rocket nozzle | Apr 9, 2003 | Issued |
Array
(
[id] => 1058016
[patent_doc_number] => 06851647
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2005-02-08
[patent_title] => 'Portable catapult launcher for small aircraft'
[patent_app_type] => utility
[patent_app_number] => 10/417377
[patent_app_country] => US
[patent_app_date] => 2003-04-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 16
[patent_figures_cnt] => 22
[patent_no_of_words] => 5207
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 227
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/851/06851647.pdf
[firstpage_image] =>[orig_patent_app_number] => 10417377
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/417377 | Portable catapult launcher for small aircraft | Apr 2, 2003 | Issued |
Array
(
[id] => 7333588
[patent_doc_number] => 20040188563
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-09-30
[patent_title] => 'Efficient cargo liner installation'
[patent_app_type] => new
[patent_app_number] => 10/402508
[patent_app_country] => US
[patent_app_date] => 2003-03-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 5708
[patent_no_of_claims] => 73
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 81
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0188/20040188563.pdf
[firstpage_image] =>[orig_patent_app_number] => 10402508
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/402508 | Efficient cargo liner installation | Mar 26, 2003 | Issued |
Array
(
[id] => 7387607
[patent_doc_number] => 20040016846
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-01-29
[patent_title] => 'Launch vehicle payload carrier and related methods'
[patent_app_type] => new
[patent_app_number] => 10/397499
[patent_app_country] => US
[patent_app_date] => 2003-03-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 22
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[patent_no_of_words] => 5168
[patent_no_of_claims] => 20
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0016/20040016846.pdf
[firstpage_image] =>[orig_patent_app_number] => 10397499
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/397499 | Launch vehicle payload carrier and related methods | Mar 25, 2003 | Issued |
Array
(
[id] => 6702608
[patent_doc_number] => 20030225488
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-12-04
[patent_title] => 'Chemical application and flight guidance control system and method'
[patent_app_type] => new
[patent_app_number] => 10/397040
[patent_app_country] => US
[patent_app_date] => 2003-03-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_no_of_words] => 3453
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 65
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0225/20030225488.pdf
[firstpage_image] =>[orig_patent_app_number] => 10397040
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/397040 | Chemical application and flight guidance control system and method | Mar 24, 2003 | Issued |
Array
(
[id] => 1084610
[patent_doc_number] => 06830222
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2004-12-14
[patent_title] => 'Balloon device for lowering space object orbits'
[patent_app_type] => B1
[patent_app_number] => 10/394477
[patent_app_country] => US
[patent_app_date] => 2003-03-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
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[patent_no_of_words] => 8071
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/830/06830222.pdf
[firstpage_image] =>[orig_patent_app_number] => 10394477
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/394477 | Balloon device for lowering space object orbits | Mar 20, 2003 | Issued |
Array
(
[id] => 7132562
[patent_doc_number] => 20050178911
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-08-18
[patent_title] => 'Triple-fuselage aircraft and families of aircraft of said type'
[patent_app_type] => utility
[patent_app_number] => 10/504318
[patent_app_country] => US
[patent_app_date] => 2003-03-21
[patent_effective_date] => 0000-00-00
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[pdf_file] => publications/A1/0178/20050178911.pdf
[firstpage_image] =>[orig_patent_app_number] => 10504318
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/504318 | Triple-fuselage aircraft and families of aircraft of said type | Mar 20, 2003 | Issued |
Array
(
[id] => 6727532
[patent_doc_number] => 20030183722
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-10-02
[patent_title] => 'Device for controlling the pitch of the blades of a convertible aircraft rotor'
[patent_app_type] => new
[patent_app_number] => 10/392645
[patent_app_country] => US
[patent_app_date] => 2003-03-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0183/20030183722.pdf
[firstpage_image] =>[orig_patent_app_number] => 10392645
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/392645 | Device for controlling the pitch of the blades of a convertible aircraft rotor | Mar 19, 2003 | Issued |
Array
(
[id] => 7419984
[patent_doc_number] => 20040182968
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-09-23
[patent_title] => 'Traction kite harness safety release'
[patent_app_type] => new
[patent_app_number] => 10/391916
[patent_app_country] => US
[patent_app_date] => 2003-03-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
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[patent_no_of_words] => 11259
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0182/20040182968.pdf
[firstpage_image] =>[orig_patent_app_number] => 10391916
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/391916 | Traction kite harness safety release | Mar 18, 2003 | Abandoned |