
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] => 4707907
[patent_doc_number] => 20080296433
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-12-04
[patent_title] => 'LIGHTWEIGHT STRUCTURAL COMPONENT IN PARTICULAR FOR AIRCRAFT AND METHOD FOR ITS PRODUCTION'
[patent_app_type] => utility
[patent_app_number] => 12/192706
[patent_app_country] => US
[patent_app_date] => 2008-08-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 15
[patent_figures_cnt] => 15
[patent_no_of_words] => 15799
[patent_no_of_claims] => 132
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0296/20080296433.pdf
[firstpage_image] =>[orig_patent_app_number] => 12192706
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/192706 | LIGHTWEIGHT STRUCTURAL COMPONENT IN PARTICULAR FOR AIRCRAFT AND METHOD FOR ITS PRODUCTION | Aug 14, 2008 | Abandoned |
Array
(
[id] => 5518338
[patent_doc_number] => 20090026319
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-01-29
[patent_title] => 'Aerial delivery system'
[patent_app_type] => utility
[patent_app_number] => 12/222485
[patent_app_country] => US
[patent_app_date] => 2008-08-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 23
[patent_figures_cnt] => 23
[patent_no_of_words] => 9707
[patent_no_of_claims] => 25
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0026/20090026319.pdf
[firstpage_image] =>[orig_patent_app_number] => 12222485
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/222485 | Aerial delivery system | Aug 10, 2008 | Abandoned |
Array
(
[id] => 6244361
[patent_doc_number] => 20100024305
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-02-04
[patent_title] => 'TRANSLATING DOOR CENTERING SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 12/185201
[patent_app_country] => US
[patent_app_date] => 2008-08-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 5262
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0024/20100024305.pdf
[firstpage_image] =>[orig_patent_app_number] => 12185201
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/185201 | Translating door centering system | Aug 3, 2008 | Issued |
Array
(
[id] => 8304515
[patent_doc_number] => 08226042
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2012-07-24
[patent_title] => 'Spin control system for a suspended object that is to be deployed in or recovered from water'
[patent_app_type] => utility
[patent_app_number] => 12/220432
[patent_app_country] => US
[patent_app_date] => 2008-07-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 4
[patent_no_of_words] => 1843
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 213
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12220432
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/220432 | Spin control system for a suspended object that is to be deployed in or recovered from water | Jul 13, 2008 | Issued |
Array
(
[id] => 4883675
[patent_doc_number] => 20080258007
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-10-23
[patent_title] => 'ATTACHING PANELS TO SUPPORT STRUCTURES IN AN AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 12/145748
[patent_app_country] => US
[patent_app_date] => 2008-06-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 3107
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0258/20080258007.pdf
[firstpage_image] =>[orig_patent_app_number] => 12145748
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/145748 | Attaching panels to support structures in an aircraft | Jun 24, 2008 | Issued |
Array
(
[id] => 8801043
[patent_doc_number] => 08439312
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-05-14
[patent_title] => 'System and methods for simultaneous momentum dumping and orbit control'
[patent_app_type] => utility
[patent_app_number] => 12/141832
[patent_app_country] => US
[patent_app_date] => 2008-06-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 7786
[patent_no_of_claims] => 22
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12141832
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/141832 | System and methods for simultaneous momentum dumping and orbit control | Jun 17, 2008 | Issued |
Array
(
[id] => 8211241
[patent_doc_number] => 08191828
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-06-05
[patent_title] => 'Methods and apparatus for aerial recovery of flying apparatus'
[patent_app_type] => utility
[patent_app_number] => 12/120065
[patent_app_country] => US
[patent_app_date] => 2008-05-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 11
[patent_no_of_words] => 4238
[patent_no_of_claims] => 20
[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/08/191/08191828.pdf
[firstpage_image] =>[orig_patent_app_number] => 12120065
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/120065 | Methods and apparatus for aerial recovery of flying apparatus | May 12, 2008 | Issued |
Array
(
[id] => 5461373
[patent_doc_number] => 20090321573
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-12-31
[patent_title] => 'Rotor/wing dual mode hub fairing system'
[patent_app_type] => utility
[patent_app_number] => 12/151801
[patent_app_country] => US
[patent_app_date] => 2008-05-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 3922
[patent_no_of_claims] => 17
[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/A1/0321/20090321573.pdf
[firstpage_image] =>[orig_patent_app_number] => 12151801
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/151801 | Rotor/wing dual mode hub fairing system | May 8, 2008 | Issued |
Array
(
[id] => 8350653
[patent_doc_number] => 08245981
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-08-21
[patent_title] => 'Ice shed reduction for leading edge structures'
[patent_app_type] => utility
[patent_app_number] => 12/112733
[patent_app_country] => US
[patent_app_date] => 2008-04-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 15
[patent_no_of_words] => 1980
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 75
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12112733
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/112733 | Ice shed reduction for leading edge structures | Apr 29, 2008 | Issued |
Array
(
[id] => 8025473
[patent_doc_number] => 08141816
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-03-27
[patent_title] => 'AFT inlet duct mounted door actuator'
[patent_app_type] => utility
[patent_app_number] => 12/112711
[patent_app_country] => US
[patent_app_date] => 2008-04-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 6
[patent_no_of_words] => 3132
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 214
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/141/08141816.pdf
[firstpage_image] =>[orig_patent_app_number] => 12112711
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/112711 | AFT inlet duct mounted door actuator | Apr 29, 2008 | Issued |
Array
(
[id] => 5555359
[patent_doc_number] => 20090266936
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-10-29
[patent_title] => 'AIRCRAFT FUSELAGE STRUCTURAL COMPONENTS AND METHODS OF MAKING SAME'
[patent_app_type] => utility
[patent_app_number] => 12/111825
[patent_app_country] => US
[patent_app_date] => 2008-04-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 2313
[patent_no_of_claims] => 21
[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/A1/0266/20090266936.pdf
[firstpage_image] =>[orig_patent_app_number] => 12111825
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/111825 | AIRCRAFT FUSELAGE STRUCTURAL COMPONENTS AND METHODS OF MAKING SAME | Apr 28, 2008 | Abandoned |
Array
(
[id] => 4856253
[patent_doc_number] => 20080265103
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-10-30
[patent_title] => 'AEROFOIL'
[patent_app_type] => utility
[patent_app_number] => 12/107816
[patent_app_country] => US
[patent_app_date] => 2008-04-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 2330
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 3
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[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0265/20080265103.pdf
[firstpage_image] =>[orig_patent_app_number] => 12107816
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/107816 | Aerofoil with leading edge projection | Apr 22, 2008 | Issued |
Array
(
[id] => 4723686
[patent_doc_number] => 20080203227
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-08-28
[patent_title] => 'AIRCRAFT PASSENGER ACCOMMODATION UNIT WITH DEPLOYABLE BED'
[patent_app_type] => utility
[patent_app_number] => 12/107345
[patent_app_country] => US
[patent_app_date] => 2008-04-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
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[patent_no_of_words] => 3164
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0203/20080203227.pdf
[firstpage_image] =>[orig_patent_app_number] => 12107345
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/107345 | Aircraft passenger accommodation unit with deployable bed | Apr 21, 2008 | Issued |
Array
(
[id] => 5334286
[patent_doc_number] => 20090050750
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-02-26
[patent_title] => 'Airborne Manipulator System'
[patent_app_type] => utility
[patent_app_number] => 12/104432
[patent_app_country] => US
[patent_app_date] => 2008-04-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
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[patent_no_of_words] => 4573
[patent_no_of_claims] => 20
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0050/20090050750.pdf
[firstpage_image] =>[orig_patent_app_number] => 12104432
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/104432 | Airborne manipulator system | Apr 15, 2008 | Issued |
Array
(
[id] => 4789247
[patent_doc_number] => 20080290220
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-11-27
[patent_title] => 'Unloading and loading of aircraft'
[patent_app_type] => utility
[patent_app_number] => 12/081455
[patent_app_country] => US
[patent_app_date] => 2008-04-16
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[pdf_file] => publications/A1/0290/20080290220.pdf
[firstpage_image] =>[orig_patent_app_number] => 12081455
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/081455 | Unloading and loading of aircraft | Apr 15, 2008 | Issued |
Array
(
[id] => 5293581
[patent_doc_number] => 20090008507
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-01-08
[patent_title] => 'AIRCRAFT WING'
[patent_app_type] => utility
[patent_app_number] => 12/058482
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[patent_effective_date] => 0000-00-00
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[pdf_file] => publications/A1/0008/20090008507.pdf
[firstpage_image] =>[orig_patent_app_number] => 12058482
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/058482 | AIRCRAFT WING | Mar 27, 2008 | Abandoned |
Array
(
[id] => 5307315
[patent_doc_number] => 20090014596
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-01-15
[patent_title] => 'LONG ENDURANCE AIRCRAFT HAVING MORPHING WING CONFIGURED TO CHANGE SHAPE'
[patent_app_type] => utility
[patent_app_number] => 12/058466
[patent_app_country] => US
[patent_app_date] => 2008-03-28
[patent_effective_date] => 0000-00-00
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[pdf_file] => publications/A1/0014/20090014596.pdf
[firstpage_image] =>[orig_patent_app_number] => 12058466
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/058466 | LONG ENDURANCE AIRCRAFT HAVING MORPHING WING CONFIGURED TO CHANGE SHAPE | Mar 27, 2008 | Abandoned |
Array
(
[id] => 8150754
[patent_doc_number] => 08167237
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-05-01
[patent_title] => 'Mounting system for a gas turbine engine'
[patent_app_type] => utility
[patent_app_number] => 12/052769
[patent_app_country] => US
[patent_app_date] => 2008-03-21
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/167/08167237.pdf
[firstpage_image] =>[orig_patent_app_number] => 12052769
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/052769 | Mounting system for a gas turbine engine | Mar 20, 2008 | Issued |
Array
(
[id] => 5401157
[patent_doc_number] => 20090236470
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-09-24
[patent_title] => 'LAUNCH AND CAPTURE SYSTEMS FOR VERTICAL TAKE-OFF AND LANDING (VTOL) VEHICLES'
[patent_app_type] => utility
[patent_app_number] => 12/051552
[patent_app_country] => US
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[pdf_file] => publications/A1/0236/20090236470.pdf
[firstpage_image] =>[orig_patent_app_number] => 12051552
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/051552 | Launch and capture systems for vertical take-off and landing (VTOL) vehicles | Mar 18, 2008 | Issued |
Array
(
[id] => 4925008
[patent_doc_number] => 20080164371
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-07-10
[patent_title] => 'SYSTEM AND METHOD FOR CONVERTING A PASSENGER AIRCRAFT TO A CARGO AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 12/051291
[patent_app_country] => US
[patent_app_date] => 2008-03-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0164/20080164371.pdf
[firstpage_image] =>[orig_patent_app_number] => 12051291
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/051291 | SYSTEM AND METHOD FOR CONVERTING A PASSENGER AIRCRAFT TO A CARGO AIRCRAFT | Mar 18, 2008 | Abandoned |