
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] => 7338004
[patent_doc_number] => 20040245390
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-12-09
[patent_title] => 'Emergency oxygen supply system for an aircraft'
[patent_app_type] => new
[patent_app_number] => 10/850655
[patent_app_country] => US
[patent_app_date] => 2004-05-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2325
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 110
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0245/20040245390.pdf
[firstpage_image] =>[orig_patent_app_number] => 10850655
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/850655 | Emergency oxygen supply system for an aircraft | May 20, 2004 | Abandoned |
Array
(
[id] => 7337964
[patent_doc_number] => 20040245377
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-12-09
[patent_title] => 'Helicopter'
[patent_app_type] => new
[patent_app_number] => 10/849132
[patent_app_country] => US
[patent_app_date] => 2004-05-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 4057
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 38
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0245/20040245377.pdf
[firstpage_image] =>[orig_patent_app_number] => 10849132
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/849132 | Helicopter having a fusilage section and a tail section coupled thereto | May 19, 2004 | Issued |
Array
(
[id] => 4737000
[patent_doc_number] => 20080230652
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-09-25
[patent_title] => 'COMPOSITE BARREL SECTIONS FOR AIRCRAFT FUSELAGES AND OTHER STRUCTURES, AND METHODS AND SYSTEMS FOR MANUFACTURING SUCH BARREL SECTIONS'
[patent_app_type] => utility
[patent_app_number] => 10/851381
[patent_app_country] => US
[patent_app_date] => 2004-05-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 12
[patent_no_of_words] => 7642
[patent_no_of_claims] => 50
[patent_no_of_ind_claims] => 13
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0230/20080230652.pdf
[firstpage_image] =>[orig_patent_app_number] => 10851381
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/851381 | Composite barrel sections for aircraft fuselages and other structures, and methods and systems for manufacturing such barrel sections | May 19, 2004 | Issued |
Array
(
[id] => 436138
[patent_doc_number] => 07262395
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2007-08-28
[patent_title] => 'Expendable sonobuoy flight kit with aerodynamically assisted sonobuoy separation'
[patent_app_type] => utility
[patent_app_number] => 10/848131
[patent_app_country] => US
[patent_app_date] => 2004-05-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 3935
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 173
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/262/07262395.pdf
[firstpage_image] =>[orig_patent_app_number] => 10848131
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/848131 | Expendable sonobuoy flight kit with aerodynamically assisted sonobuoy separation | May 18, 2004 | Issued |
Array
(
[id] => 7212863
[patent_doc_number] => 20050253021
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-11-17
[patent_title] => 'Operational ground support system'
[patent_app_type] => utility
[patent_app_number] => 10/847739
[patent_app_country] => US
[patent_app_date] => 2004-05-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 22
[patent_figures_cnt] => 22
[patent_no_of_words] => 10329
[patent_no_of_claims] => 40
[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/A1/0253/20050253021.pdf
[firstpage_image] =>[orig_patent_app_number] => 10847739
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/847739 | Operational ground support system | May 16, 2004 | Abandoned |
Array
(
[id] => 7212827
[patent_doc_number] => 20050253016
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-11-17
[patent_title] => 'Structural mode shape alignment'
[patent_app_type] => utility
[patent_app_number] => 10/846861
[patent_app_country] => US
[patent_app_date] => 2004-05-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 3967
[patent_no_of_claims] => 21
[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/A1/0253/20050253016.pdf
[firstpage_image] =>[orig_patent_app_number] => 10846861
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/846861 | Structural mode shape alignment | May 13, 2004 | Issued |
Array
(
[id] => 5087820
[patent_doc_number] => 20070227459
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-10-04
[patent_title] => 'Fish acclimation transfer line'
[patent_app_type] => utility
[patent_app_number] => 10/845428
[patent_app_country] => US
[patent_app_date] => 2004-05-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 3054
[patent_no_of_claims] => 5
[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/A1/0227/20070227459.pdf
[firstpage_image] =>[orig_patent_app_number] => 10845428
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/845428 | Fish acclimation transfer line | May 11, 2004 | Abandoned |
Array
(
[id] => 716880
[patent_doc_number] => 07048230
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2006-05-23
[patent_title] => 'Laminar flow nacelle for an aircraft engine'
[patent_app_type] => utility
[patent_app_number] => 10/842446
[patent_app_country] => US
[patent_app_date] => 2004-05-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 6
[patent_no_of_words] => 2732
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 169
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/048/07048230.pdf
[firstpage_image] =>[orig_patent_app_number] => 10842446
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/842446 | Laminar flow nacelle for an aircraft engine | May 10, 2004 | Issued |
Array
(
[id] => 450470
[patent_doc_number] => 07246773
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2007-07-24
[patent_title] => 'Low power, pulsed, electro-thermal ice protection system'
[patent_app_type] => utility
[patent_app_number] => 10/840736
[patent_app_country] => US
[patent_app_date] => 2004-05-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 15
[patent_no_of_words] => 10535
[patent_no_of_claims] => 23
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 161
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/246/07246773.pdf
[firstpage_image] =>[orig_patent_app_number] => 10840736
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/840736 | Low power, pulsed, electro-thermal ice protection system | May 5, 2004 | Issued |
Array
(
[id] => 5832034
[patent_doc_number] => 20060243864
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-11-02
[patent_title] => 'UNITIZED ROTARY ACTUATOR HINGE FITTING'
[patent_app_type] => utility
[patent_app_number] => 10/838959
[patent_app_country] => US
[patent_app_date] => 2004-05-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2838
[patent_no_of_claims] => 20
[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/A1/0243/20060243864.pdf
[firstpage_image] =>[orig_patent_app_number] => 10838959
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/838959 | Unitized rotary actuator hinge fitting | May 3, 2004 | Issued |
Array
(
[id] => 424314
[patent_doc_number] => 07270295
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2007-09-18
[patent_title] => 'Solar thermal aircraft'
[patent_app_type] => utility
[patent_app_number] => 10/835665
[patent_app_country] => US
[patent_app_date] => 2004-04-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 21
[patent_no_of_words] => 8592
[patent_no_of_claims] => 96
[patent_no_of_ind_claims] => 6
[patent_words_short_claim] => 30
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/270/07270295.pdf
[firstpage_image] =>[orig_patent_app_number] => 10835665
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/835665 | Solar thermal aircraft | Apr 29, 2004 | Issued |
Array
(
[id] => 7066852
[patent_doc_number] => 20050242234
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-11-03
[patent_title] => 'Lifters, methods of flight control and maneuver load alleviation'
[patent_app_type] => utility
[patent_app_number] => 10/837464
[patent_app_country] => US
[patent_app_date] => 2004-04-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 6230
[patent_no_of_claims] => 43
[patent_no_of_ind_claims] => 9
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0242/20050242234.pdf
[firstpage_image] =>[orig_patent_app_number] => 10837464
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/837464 | Lifters, methods of flight control and maneuver load alleviation | Apr 28, 2004 | Abandoned |
Array
(
[id] => 424321
[patent_doc_number] => 07270302
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2007-09-18
[patent_title] => 'Scalable thermal control system for spacecraft mounted instrumentation'
[patent_app_type] => utility
[patent_app_number] => 10/829358
[patent_app_country] => US
[patent_app_date] => 2004-04-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 5
[patent_no_of_words] => 4096
[patent_no_of_claims] => 21
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 118
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/270/07270302.pdf
[firstpage_image] =>[orig_patent_app_number] => 10829358
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/829358 | Scalable thermal control system for spacecraft mounted instrumentation | Apr 21, 2004 | Issued |
Array
(
[id] => 6923265
[patent_doc_number] => 20050236520
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-10-27
[patent_title] => 'Flying amphibious SUV'
[patent_app_type] => utility
[patent_app_number] => 10/828777
[patent_app_country] => US
[patent_app_date] => 2004-04-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 2312
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 1
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[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0236/20050236520.pdf
[firstpage_image] =>[orig_patent_app_number] => 10828777
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/828777 | Flying amphibious SUV | Apr 21, 2004 | Issued |
Array
(
[id] => 704664
[patent_doc_number] => 07059570
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2006-06-13
[patent_title] => 'Aerial delivery device'
[patent_app_type] => utility
[patent_app_number] => 10/709186
[patent_app_country] => US
[patent_app_date] => 2004-04-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
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[patent_no_of_words] => 5465
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/059/07059570.pdf
[firstpage_image] =>[orig_patent_app_number] => 10709186
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/709186 | Aerial delivery device | Apr 19, 2004 | Issued |
Array
(
[id] => 396506
[patent_doc_number] => 07293737
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2007-11-13
[patent_title] => 'Co-cured stringers and associated mandrel and fabrication method'
[patent_app_type] => utility
[patent_app_number] => 10/830291
[patent_app_country] => US
[patent_app_date] => 2004-04-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 3756
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 60
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/293/07293737.pdf
[firstpage_image] =>[orig_patent_app_number] => 10830291
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/830291 | Co-cured stringers and associated mandrel and fabrication method | Apr 19, 2004 | Issued |
Array
(
[id] => 977580
[patent_doc_number] => 06929219
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2005-08-16
[patent_title] => 'Derivative aircraft and methods for their manufacture'
[patent_app_type] => utility
[patent_app_number] => 10/827460
[patent_app_country] => US
[patent_app_date] => 2004-04-19
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/929/06929219.pdf
[firstpage_image] =>[orig_patent_app_number] => 10827460
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/827460 | Derivative aircraft and methods for their manufacture | Apr 18, 2004 | Issued |
Array
(
[id] => 660813
[patent_doc_number] => 07100872
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2006-09-05
[patent_title] => 'Lavatory fast pack system and method'
[patent_app_type] => utility
[patent_app_number] => 10/825906
[patent_app_country] => US
[patent_app_date] => 2004-04-15
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/100/07100872.pdf
[firstpage_image] =>[orig_patent_app_number] => 10825906
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/825906 | Lavatory fast pack system and method | Apr 14, 2004 | Issued |
Array
(
[id] => 7337962
[patent_doc_number] => 20040245376
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-12-09
[patent_title] => 'Rotor and aircraft passively stable in hover'
[patent_app_type] => new
[patent_app_number] => 10/824492
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0245/20040245376.pdf
[firstpage_image] =>[orig_patent_app_number] => 10824492
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/824492 | Rotor and aircraft passively stable in hover | Apr 14, 2004 | Issued |
Array
(
[id] => 6963638
[patent_doc_number] => 20050230535
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-10-20
[patent_title] => 'Immersible unmanned air vehicle and system for launch, recovery, and re-launch at sea'
[patent_app_type] => utility
[patent_app_number] => 10/823434
[patent_app_country] => US
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0230/20050230535.pdf
[firstpage_image] =>[orig_patent_app_number] => 10823434
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/823434 | Immersible unmanned air vehicle and system for launch, recovery, and re-launch at sea | Apr 12, 2004 | Issued |