
Galen L. Barefoot
Examiner (ID: 7830)
| Most Active Art Unit | 3105 |
| Art Unit(s) | 3104, 3644, 3643, 3107, 3105, 3613, 3641, 2506 |
| Total Applications | 2920 |
| Issued Applications | 2553 |
| Pending Applications | 115 |
| Abandoned Applications | 252 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 7413706
[patent_doc_number] => 20040159742
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-08-19
[patent_title] => 'ATTACHMENT APPARATUS FOR INJECTED-MOLDED CANOPIES'
[patent_app_type] => new
[patent_app_number] => 10/366949
[patent_app_country] => US
[patent_app_date] => 2003-02-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 2643
[patent_no_of_claims] => 24
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 32
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0159/20040159742.pdf
[firstpage_image] =>[orig_patent_app_number] => 10366949
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/366949 | Attachment apparatus for injected-molded canopies | Feb 12, 2003 | Issued |
Array
(
[id] => 6704223
[patent_doc_number] => 20030150957
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-08-14
[patent_title] => 'Adaptable kite/airfoil'
[patent_app_type] => new
[patent_app_number] => 10/361957
[patent_app_country] => US
[patent_app_date] => 2003-02-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
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[patent_no_of_words] => 7112
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[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0150/20030150957.pdf
[firstpage_image] =>[orig_patent_app_number] => 10361957
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/361957 | Adaptable kite/airfoil | Feb 9, 2003 | Issued |
Array
(
[id] => 6845256
[patent_doc_number] => 20030164423
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-09-04
[patent_title] => 'Aircraft landing gear having an independent low-noise fairing system'
[patent_app_type] => new
[patent_app_number] => 10/360638
[patent_app_country] => US
[patent_app_date] => 2003-02-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[patent_no_of_words] => 3617
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0164/20030164423.pdf
[firstpage_image] =>[orig_patent_app_number] => 10360638
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/360638 | Aircraft landing gear having an independent low-noise fairing system | Feb 9, 2003 | Issued |
Array
(
[id] => 7072484
[patent_doc_number] => 20050145750
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-07-07
[patent_title] => 'Flying body for firing from a tube with over-calibre stabilisers'
[patent_app_type] => utility
[patent_app_number] => 10/504116
[patent_app_country] => US
[patent_app_date] => 2003-02-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_no_of_words] => 4548
[patent_no_of_claims] => 15
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0145/20050145750.pdf
[firstpage_image] =>[orig_patent_app_number] => 10504116
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/504116 | Flying body for firing from a tube with over-caliber stabilizers | Feb 5, 2003 | Issued |
Array
(
[id] => 1173944
[patent_doc_number] => 06736354
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-05-18
[patent_title] => 'Airplane fuel supply system and airplane wing pipeline assembly method'
[patent_app_type] => B2
[patent_app_number] => 10/356616
[patent_app_country] => US
[patent_app_date] => 2003-02-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/736/06736354.pdf
[firstpage_image] =>[orig_patent_app_number] => 10356616
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/356616 | Airplane fuel supply system and airplane wing pipeline assembly method | Feb 2, 2003 | Issued |
Array
(
[id] => 7259281
[patent_doc_number] => 20040149859
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-08-05
[patent_title] => 'AIRCRAFT'
[patent_app_type] => new
[patent_app_number] => 10/355974
[patent_app_country] => US
[patent_app_date] => 2003-01-31
[patent_effective_date] => 0000-00-00
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[patent_no_of_words] => 2097
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0149/20040149859.pdf
[firstpage_image] =>[orig_patent_app_number] => 10355974
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/355974 | Aircraft | Jan 30, 2003 | Issued |
Array
(
[id] => 1093387
[patent_doc_number] => 06820840
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-11-23
[patent_title] => 'Hydrogen powered toy rocket utilizing hydrogen from the electrolysis of water'
[patent_app_type] => B2
[patent_app_number] => 10/348830
[patent_app_country] => US
[patent_app_date] => 2003-01-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_no_of_words] => 842
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/820/06820840.pdf
[firstpage_image] =>[orig_patent_app_number] => 10348830
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/348830 | Hydrogen powered toy rocket utilizing hydrogen from the electrolysis of water | Jan 21, 2003 | Issued |
Array
(
[id] => 7304740
[patent_doc_number] => 20040140399
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-07-22
[patent_title] => 'METHOD AND APPARATUS FOR MINIMIZING SOLAR ARRAY SUN TRACKING DISTURBANCE BY NORTH AND SOUTH SOLAR ARRAY WING CANCELLATION'
[patent_app_type] => new
[patent_app_number] => 10/348663
[patent_app_country] => US
[patent_app_date] => 2003-01-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
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[patent_no_of_words] => 3909
[patent_no_of_claims] => 25
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0140/20040140399.pdf
[firstpage_image] =>[orig_patent_app_number] => 10348663
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/348663 | Method and apparatus for minimizing solar array sun tracking disturbance by north and south solar array wing cancellation | Jan 20, 2003 | Issued |
Array
(
[id] => 7967557
[patent_doc_number] => 06679457
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2004-01-20
[patent_title] => 'Reaction wheel system with vernier control rotor'
[patent_app_type] => B1
[patent_app_number] => 10/341753
[patent_app_country] => US
[patent_app_date] => 2003-01-13
[patent_effective_date] => 0000-00-00
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[pdf_file] => patents/06/679/06679457.pdf
[firstpage_image] =>[orig_patent_app_number] => 10341753
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/341753 | Reaction wheel system with vernier control rotor | Jan 12, 2003 | Issued |
Array
(
[id] => 7318570
[patent_doc_number] => 20040135034
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-07-15
[patent_title] => 'FLYWHEEL PROGNOSTIC HEALTH AND FAULT MANAGEMENT SYSTEM AND METHOD'
[patent_app_type] => new
[patent_app_number] => 10/340480
[patent_app_country] => US
[patent_app_date] => 2003-01-10
[patent_effective_date] => 0000-00-00
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[pdf_file] => publications/A1/0135/20040135034.pdf
[firstpage_image] =>[orig_patent_app_number] => 10340480
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/340480 | Flywheel prognostic health and fault management system and method | Jan 9, 2003 | Issued |
Array
(
[id] => 750173
[patent_doc_number] => 07017862
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2006-03-28
[patent_title] => 'Wake vortex visualizer for an aircraft'
[patent_app_type] => utility
[patent_app_number] => 10/893696
[patent_app_country] => US
[patent_app_date] => 2003-01-08
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[pdf_file] => patents/07/017/07017862.pdf
[firstpage_image] =>[orig_patent_app_number] => 10893696
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/893696 | Wake vortex visualizer for an aircraft | Jan 7, 2003 | Issued |
Array
(
[id] => 6863603
[patent_doc_number] => 20030189129
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[patent_kind] => A1
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[patent_title] => 'Aircraft with electric flight controls provided with a fuselage able to deform and vibrate'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 10/336730 | Aircraft with electric flight controls provided with a fuselage able to deform and vibrate | Jan 5, 2003 | Issued |
Array
(
[id] => 1235656
[patent_doc_number] => 06685143
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2004-02-03
[patent_title] => 'Aircraft and missile forebody flow control device and method of controlling flow'
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[patent_app_number] => 10/336117
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[firstpage_image] =>[orig_patent_app_number] => 10336117
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/336117 | Aircraft and missile forebody flow control device and method of controlling flow | Jan 2, 2003 | Issued |
Array
(
[id] => 1042304
[patent_doc_number] => 06866233
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[patent_kind] => B2
[patent_issue_date] => 2005-03-15
[patent_title] => 'Reconfigurable porous technology for fluid flow control and method of controlling flow'
[patent_app_type] => utility
[patent_app_number] => 10/336113
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[rel_patent_id] =>[rel_patent_doc_number] =>) 10/336113 | Reconfigurable porous technology for fluid flow control and method of controlling flow | Jan 2, 2003 | Issued |
Array
(
[id] => 7295617
[patent_doc_number] => 20040124308
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[patent_title] => 'Hybrid solid oxide fuel cell aircraft auxiliary power unit'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 10/334480 | Hybrid solid oxide fuel cell aircraft auxiliary power unit | Dec 30, 2002 | Issued |
Array
(
[id] => 1251533
[patent_doc_number] => 06669145
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[patent_title] => 'Apparatus, method and system for fluid-motion-powered modulation of a retroreflector for remote position sensing'
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[patent_app_number] => 10/331810
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[rel_patent_id] =>[rel_patent_doc_number] =>) 10/331810 | Apparatus, method and system for fluid-motion-powered modulation of a retroreflector for remote position sensing | Dec 29, 2002 | Issued |
Array
(
[id] => 1105048
[patent_doc_number] => 06808144
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[patent_title] => 'Autonomous payload recovery system'
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Array
(
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[rel_patent_id] =>[rel_patent_doc_number] =>) 10/326995 | Helicopter rotor and method of repairing same | Dec 23, 2002 | Abandoned |
Array
(
[id] => 1260620
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[patent_title] => 'Overboard venting inflation system and control valve therefor'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 10/328557 | Overboard venting inflation system and control valve therefor | Dec 22, 2002 | Issued |
Array
(
[id] => 1048606
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[patent_title] => 'Apparatus and method for folding helicopter rotor blades for storage and transport of helicopter'
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[firstpage_image] =>[orig_patent_app_number] => 10329250
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/329250 | Apparatus and method for folding helicopter rotor blades for storage and transport of helicopter | Dec 22, 2002 | Issued |