Search

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 numberTitle of the applicationFiling DateStatus
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 [patent_figures_cnt] => 11 [patent_no_of_words] => 7112 [patent_no_of_claims] => 5 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 112 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_figures_cnt] => 7 [patent_no_of_words] => 3617 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 137 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_figures_cnt] => 5 [patent_no_of_words] => 4548 [patent_no_of_claims] => 15 [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/A1/0145/20050145750.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 [patent_figures_cnt] => 7 [patent_no_of_words] => 5349 [patent_no_of_claims] => 3 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 72 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 2097 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 11 [patent_words_short_claim] => 35 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_figures_cnt] => 4 [patent_no_of_words] => 842 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 84 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_figures_cnt] => 10 [patent_no_of_words] => 3909 [patent_no_of_claims] => 25 [patent_no_of_ind_claims] => 7 [patent_words_short_claim] => 108 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 8 [patent_no_of_words] => 3825 [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] => patent [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 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 4356 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 120 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [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 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 2 [patent_no_of_words] => 469 [patent_no_of_claims] => 2 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 171 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [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 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2003-10-09 [patent_title] => 'Aircraft with electric flight controls provided with a fuselage able to deform and vibrate' [patent_app_type] => new [patent_app_number] => 10/336730 [patent_app_country] => US [patent_app_date] => 2003-01-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 3098 [patent_no_of_claims] => 7 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 237 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0189/20030189129.pdf [firstpage_image] =>[orig_patent_app_number] => 10336730 [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' [patent_app_type] => B1 [patent_app_number] => 10/336117 [patent_app_country] => US [patent_app_date] => 2003-01-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 13 [patent_no_of_words] => 4754 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 92 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/685/06685143.pdf [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 [patent_country] => US [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 [patent_app_country] => US [patent_app_date] => 2003-01-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 7 [patent_no_of_words] => 3833 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 77 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/866/06866233.pdf [firstpage_image] =>[orig_patent_app_number] => 10336113 [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 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-07-01 [patent_title] => 'Hybrid solid oxide fuel cell aircraft auxiliary power unit' [patent_app_type] => new [patent_app_number] => 10/334480 [patent_app_country] => US [patent_app_date] => 2002-12-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 2513 [patent_no_of_claims] => 34 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 75 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0124/20040124308.pdf [firstpage_image] =>[orig_patent_app_number] => 10334480 [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 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2003-12-30 [patent_title] => 'Apparatus, method and system for fluid-motion-powered modulation of a retroreflector for remote position sensing' [patent_app_type] => B1 [patent_app_number] => 10/331810 [patent_app_country] => US [patent_app_date] => 2002-12-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 11 [patent_no_of_words] => 6370 [patent_no_of_claims] => 39 [patent_no_of_ind_claims] => 6 [patent_words_short_claim] => 60 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/669/06669145.pdf [firstpage_image] =>[orig_patent_app_number] => 10331810 [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 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2004-10-26 [patent_title] => 'Autonomous payload recovery system' [patent_app_type] => B1 [patent_app_number] => 10/331009 [patent_app_country] => US [patent_app_date] => 2002-12-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 6 [patent_no_of_words] => 4696 [patent_no_of_claims] => 35 [patent_no_of_ind_claims] => 6 [patent_words_short_claim] => 64 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/808/06808144.pdf [firstpage_image] =>[orig_patent_app_number] => 10331009 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/331009
Autonomous payload recovery system Dec 25, 2002 Issued
Array ( [id] => 7455375 [patent_doc_number] => 20040118978 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-06-24 [patent_title] => 'Helicopter rotor and method of repairing same' [patent_app_type] => new [patent_app_number] => 10/326995 [patent_app_country] => US [patent_app_date] => 2002-12-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 1387 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 25 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0118/20040118978.pdf [firstpage_image] =>[orig_patent_app_number] => 10326995 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/326995
Helicopter rotor and method of repairing same Dec 23, 2002 Abandoned
Array ( [id] => 1260620 [patent_doc_number] => 06659404 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2003-12-09 [patent_title] => 'Overboard venting inflation system and control valve therefor' [patent_app_type] => B1 [patent_app_number] => 10/328557 [patent_app_country] => US [patent_app_date] => 2002-12-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 6 [patent_no_of_words] => 2141 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 290 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/659/06659404.pdf [firstpage_image] =>[orig_patent_app_number] => 10328557 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/328557
Overboard venting inflation system and control valve therefor Dec 22, 2002 Issued
Array ( [id] => 1048606 [patent_doc_number] => 06860450 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2005-03-01 [patent_title] => 'Apparatus and method for folding helicopter rotor blades for storage and transport of helicopter' [patent_app_type] => utility [patent_app_number] => 10/329250 [patent_app_country] => US [patent_app_date] => 2002-12-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 13 [patent_figures_cnt] => 20 [patent_no_of_words] => 13507 [patent_no_of_claims] => 25 [patent_no_of_ind_claims] => 8 [patent_words_short_claim] => 217 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/860/06860450.pdf [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
Menu