
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] => 6747846
[patent_doc_number] => 20030042366
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-03-06
[patent_title] => 'Kite structure'
[patent_app_type] => new
[patent_app_number] => 10/042139
[patent_app_country] => US
[patent_app_date] => 2002-01-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 8224
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 101
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0042/20030042366.pdf
[firstpage_image] =>[orig_patent_app_number] => 10042139
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/042139 | Kite structure | Jan 10, 2002 | Abandoned |
Array
(
[id] => 5782617
[patent_doc_number] => 20020158166
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-10-31
[patent_title] => 'Device for precaution skyjacking and system'
[patent_app_type] => new
[patent_app_number] => 10/029951
[patent_app_country] => US
[patent_app_date] => 2001-12-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 5069
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 82
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0158/20020158166.pdf
[firstpage_image] =>[orig_patent_app_number] => 10029951
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/029951 | Device for precaution skyjacking and system | Dec 30, 2001 | Abandoned |
| 09/980637 | Method on regulating the air flow around the windmill wing and device for use in such method | Dec 27, 2001 | Abandoned |
Array
(
[id] => 1437813
[patent_doc_number] => 06494407
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2002-12-17
[patent_title] => 'Joint on a spacecraft'
[patent_app_type] => B2
[patent_app_number] => 10/013841
[patent_app_country] => US
[patent_app_date] => 2001-12-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 1
[patent_no_of_words] => 1109
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 172
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/494/06494407.pdf
[firstpage_image] =>[orig_patent_app_number] => 10013841
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/013841 | Joint on a spacecraft | Dec 12, 2001 | Issued |
Array
(
[id] => 1358776
[patent_doc_number] => 06557802
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2003-05-06
[patent_title] => 'Device for separation of a plurality of axially arranged satellites'
[patent_app_type] => B2
[patent_app_number] => 10/012566
[patent_app_country] => US
[patent_app_date] => 2001-12-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 4
[patent_no_of_words] => 1505
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 66
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/557/06557802.pdf
[firstpage_image] =>[orig_patent_app_number] => 10012566
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/012566 | Device for separation of a plurality of axially arranged satellites | Dec 11, 2001 | Issued |
Array
(
[id] => 1354981
[patent_doc_number] => 06561456
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2003-05-13
[patent_title] => 'Vertical/short take-off and landing aircraft'
[patent_app_type] => B1
[patent_app_number] => 10/010649
[patent_app_country] => US
[patent_app_date] => 2001-12-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 16
[patent_no_of_words] => 5672
[patent_no_of_claims] => 25
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 117
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/561/06561456.pdf
[firstpage_image] =>[orig_patent_app_number] => 10010649
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/010649 | Vertical/short take-off and landing aircraft | Dec 5, 2001 | Issued |
Array
(
[id] => 1193974
[patent_doc_number] => 06726154
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-04-27
[patent_title] => 'Reusable space access launch vehicle system'
[patent_app_type] => B2
[patent_app_number] => 10/000430
[patent_app_country] => US
[patent_app_date] => 2001-11-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 1327
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 45
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/726/06726154.pdf
[firstpage_image] =>[orig_patent_app_number] => 10000430
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/000430 | Reusable space access launch vehicle system | Nov 29, 2001 | Issued |
Array
(
[id] => 1286625
[patent_doc_number] => 06629673
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2003-10-07
[patent_title] => 'Adaptable solid-hybrid rocket for crew escape and orbital injection propulsion'
[patent_app_type] => B2
[patent_app_number] => 09/996532
[patent_app_country] => US
[patent_app_date] => 2001-11-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 1921
[patent_no_of_claims] => 21
[patent_no_of_ind_claims] => 6
[patent_words_short_claim] => 89
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/629/06629673.pdf
[firstpage_image] =>[orig_patent_app_number] => 09996532
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/996532 | Adaptable solid-hybrid rocket for crew escape and orbital injection propulsion | Nov 27, 2001 | Issued |
Array
(
[id] => 6568982
[patent_doc_number] => 20020084382
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-07-04
[patent_title] => 'Aircraft deicer'
[patent_app_type] => new
[patent_app_number] => 09/995242
[patent_app_country] => US
[patent_app_date] => 2001-11-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 2069
[patent_no_of_claims] => 33
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 37
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0084/20020084382.pdf
[firstpage_image] =>[orig_patent_app_number] => 09995242
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/995242 | Aircraft deicer | Nov 26, 2001 | Abandoned |
Array
(
[id] => 1228019
[patent_doc_number] => 06691955
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-02-17
[patent_title] => 'Spacecraft having a momentum wheel configuration that prevents zero wheel speeds'
[patent_app_type] => B2
[patent_app_number] => 09/995017
[patent_app_country] => US
[patent_app_date] => 2001-11-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 4
[patent_no_of_words] => 2114
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 4
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/691/06691955.pdf
[firstpage_image] =>[orig_patent_app_number] => 09995017
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/995017 | Spacecraft having a momentum wheel configuration that prevents zero wheel speeds | Nov 26, 2001 | Issued |
Array
(
[id] => 6569010
[patent_doc_number] => 20020084384
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-07-04
[patent_title] => 'Kite control systems'
[patent_app_type] => new
[patent_app_number] => 09/990758
[patent_app_country] => US
[patent_app_date] => 2001-11-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 12
[patent_no_of_words] => 15606
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0084/20020084384.pdf
[firstpage_image] =>[orig_patent_app_number] => 09990758
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/990758 | Kite control systems | Nov 15, 2001 | Issued |
Array
(
[id] => 6348337
[patent_doc_number] => 20020056788
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-05-16
[patent_title] => 'One-piece closed-shape structure and method of forming same'
[patent_app_type] => new
[patent_app_number] => 09/987612
[patent_app_country] => US
[patent_app_date] => 2001-11-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 66
[patent_figures_cnt] => 66
[patent_no_of_words] => 17856
[patent_no_of_claims] => 67
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0056/20020056788.pdf
[firstpage_image] =>[orig_patent_app_number] => 09987612
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/987612 | One-piece closed-shape structure and method of forming same | Nov 14, 2001 | Issued |
Array
(
[id] => 6955480
[patent_doc_number] => 20050211850
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-09-29
[patent_title] => 'TWO-SIDED DEPLOYABLE THERMAL RADIATOR SYSTEM AND METHOD'
[patent_app_type] => utility
[patent_app_number] => 10/007256
[patent_app_country] => US
[patent_app_date] => 2001-11-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0211/20050211850.pdf
[firstpage_image] =>[orig_patent_app_number] => 10007256
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/007256 | Two-sided deployable thermal radiator system and method | Nov 10, 2001 | Issued |
Array
(
[id] => 1595035
[patent_doc_number] => 06474601
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-11-05
[patent_title] => 'Warren portal identification and tunnel resident disgorger system'
[patent_app_type] => B1
[patent_app_number] => 10/004241
[patent_app_country] => US
[patent_app_date] => 2001-11-02
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/474/06474601.pdf
[firstpage_image] =>[orig_patent_app_number] => 10004241
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/004241 | Warren portal identification and tunnel resident disgorger system | Nov 1, 2001 | Issued |
Array
(
[id] => 6854060
[patent_doc_number] => 20030127561
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-07-10
[patent_title] => 'Wing airfoil'
[patent_app_type] => new
[patent_app_number] => 09/982972
[patent_app_country] => US
[patent_app_date] => 2001-10-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
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[patent_no_of_words] => 3720
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0127/20030127561.pdf
[firstpage_image] =>[orig_patent_app_number] => 09982972
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/982972 | Wing airfoil | Oct 21, 2001 | Issued |
Array
(
[id] => 1299710
[patent_doc_number] => 06616097
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2003-09-09
[patent_title] => 'Reconfigurable reconnaissance pod system'
[patent_app_type] => B2
[patent_app_number] => 09/977461
[patent_app_country] => US
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[pdf_file] => patents/06/616/06616097.pdf
[firstpage_image] =>[orig_patent_app_number] => 09977461
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/977461 | Reconfigurable reconnaissance pod system | Oct 14, 2001 | Issued |
Array
(
[id] => 251853
[patent_doc_number] => 07578483
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2009-08-25
[patent_title] => 'Conformable skin element system for active vortex control'
[patent_app_type] => utility
[patent_app_number] => 09/975507
[patent_app_country] => US
[patent_app_date] => 2001-10-12
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/578/07578483.pdf
[firstpage_image] =>[orig_patent_app_number] => 09975507
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/975507 | Conformable skin element system for active vortex control | Oct 11, 2001 | Issued |
Array
(
[id] => 1446612
[patent_doc_number] => 06454220
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-09-24
[patent_title] => 'Evacuation slide with toe end center support member'
[patent_app_type] => B1
[patent_app_number] => 09/976479
[patent_app_country] => US
[patent_app_date] => 2001-10-11
[patent_effective_date] => 0000-00-00
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[pdf_file] => patents/06/454/06454220.pdf
[firstpage_image] =>[orig_patent_app_number] => 09976479
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/976479 | Evacuation slide with toe end center support member | Oct 10, 2001 | Issued |
Array
(
[id] => 1334948
[patent_doc_number] => 06581881
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2003-06-24
[patent_title] => 'METHOD FOR PLACING PAYLOAD IN ORBIT BY MULTIFUNCTIONAL LAUNCH VEHICLE OF COMBINED SCHEME WITH CRUISE LIQUID ROCKET ENGINE SYSTEM (LRES), MULTIFUNCTIONAL LAUNCH VEHICLE OF COMBINED SCHEME WITH CRUISE LRES AND METHOD FOR REFINING IT'
[patent_app_type] => B2
[patent_app_number] => 09/972006
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[pdf_file] => patents/06/581/06581881.pdf
[firstpage_image] =>[orig_patent_app_number] => 09972006
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/972006 | METHOD FOR PLACING PAYLOAD IN ORBIT BY MULTIFUNCTIONAL LAUNCH VEHICLE OF COMBINED SCHEME WITH CRUISE LIQUID ROCKET ENGINE SYSTEM (LRES), MULTIFUNCTIONAL LAUNCH VEHICLE OF COMBINED SCHEME WITH CRUISE LRES AND METHOD FOR REFINING IT | Oct 8, 2001 | Issued |
Array
(
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[patent_issue_date] => 2002-09-10
[patent_title] => 'Aircraft weapons bay high frequency acoustic suppression apparatus'
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[patent_app_number] => 09/973175
[patent_app_country] => US
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[firstpage_image] =>[orig_patent_app_number] => 09973175
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/973175 | Aircraft weapons bay high frequency acoustic suppression apparatus | Oct 4, 2001 | Issued |