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] => 5981662 [patent_doc_number] => 20020096601 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2002-07-25 [patent_title] => 'Large thermal protection system panel' [patent_app_type] => new [patent_app_number] => 09/769118 [patent_app_country] => US [patent_app_date] => 2001-01-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2629 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 71 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0096/20020096601.pdf [firstpage_image] =>[orig_patent_app_number] => 09769118 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/769118
Large thermal protection system panel Jan 23, 2001 Issued
Array ( [id] => 6576721 [patent_doc_number] => 20020040950 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2002-04-11 [patent_title] => 'System and method for spacecraft attitude control' [patent_app_type] => new [patent_app_number] => 09/905179 [patent_app_country] => US [patent_app_date] => 2001-01-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 11294 [patent_no_of_claims] => 24 [patent_no_of_ind_claims] => 8 [patent_words_short_claim] => 114 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0040/20020040950.pdf [firstpage_image] =>[orig_patent_app_number] => 09905179 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/905179
System and method for spacecraft attitude control Jan 22, 2001 Issued
Array ( [id] => 1571093 [patent_doc_number] => 06467730 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2002-10-22 [patent_title] => 'Aircraft airfoil leading edge member equipped with a de-icing device' [patent_app_type] => B2 [patent_app_number] => 09/760715 [patent_app_country] => US [patent_app_date] => 2001-01-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 3 [patent_no_of_words] => 2246 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 139 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/467/06467730.pdf [firstpage_image] =>[orig_patent_app_number] => 09760715 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/760715
Aircraft airfoil leading edge member equipped with a de-icing device Jan 16, 2001 Issued
Array ( [id] => 6890109 [patent_doc_number] => 20010007340 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2001-07-12 [patent_title] => 'Redundant energy storage device having momentum wheels' [patent_app_type] => new-utility [patent_app_number] => 09/753610 [patent_app_country] => US [patent_app_date] => 2001-01-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 1 [patent_no_of_words] => 3279 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 24 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0007/20010007340.pdf [firstpage_image] =>[orig_patent_app_number] => 09753610 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/753610
Redundant energy storage device having momentum wheels Jan 3, 2001 Issued
Array ( [id] => 7641520 [patent_doc_number] => 06394387 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-05-28 [patent_title] => 'Rotor shaft support and drive arrangement' [patent_app_type] => B1 [patent_app_number] => 09/742010 [patent_app_country] => US [patent_app_date] => 2000-12-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2327 [patent_no_of_claims] => 30 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 68 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/394/06394387.pdf [firstpage_image] =>[orig_patent_app_number] => 09742010 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/742010
Rotor shaft support and drive arrangement Dec 21, 2000 Issued
Array ( [id] => 5825714 [patent_doc_number] => 20020066827 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2002-06-06 [patent_title] => 'Radome deicer' [patent_app_type] => new [patent_app_number] => 09/730201 [patent_app_country] => US [patent_app_date] => 2000-12-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 2485 [patent_no_of_claims] => 38 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 47 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0066/20020066827.pdf [firstpage_image] =>[orig_patent_app_number] => 09730201 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/730201
Radome deicer Dec 4, 2000 Issued
Array ( [id] => 1446611 [patent_doc_number] => 06454219 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-09-24 [patent_title] => 'Aircraft wing and method for reducing airframe-generated noise' [patent_app_type] => B1 [patent_app_number] => 09/729518 [patent_app_country] => US [patent_app_date] => 2000-12-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 8 [patent_no_of_words] => 3004 [patent_no_of_claims] => 24 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 97 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/454/06454219.pdf [firstpage_image] =>[orig_patent_app_number] => 09729518 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/729518
Aircraft wing and method for reducing airframe-generated noise Dec 3, 2000 Issued
Array ( [id] => 5825728 [patent_doc_number] => 20020066830 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2002-06-06 [patent_title] => 'Vibrational air mover (V. A. M. )' [patent_app_type] => new [patent_app_number] => 09/727735 [patent_app_country] => US [patent_app_date] => 2000-12-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 1383 [patent_no_of_claims] => 4 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 132 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0066/20020066830.pdf [firstpage_image] =>[orig_patent_app_number] => 09727735 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/727735
Vibrational air mover (V. A. M. ) Dec 3, 2000 Abandoned
Array ( [id] => 1299700 [patent_doc_number] => 06616094 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2003-09-09 [patent_title] => 'Lifting platform' [patent_app_type] => B2 [patent_app_number] => 09/728602 [patent_app_country] => US [patent_app_date] => 2000-12-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 28 [patent_no_of_words] => 26791 [patent_no_of_claims] => 40 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 104 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/616/06616094.pdf [firstpage_image] =>[orig_patent_app_number] => 09728602 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/728602
Lifting platform Nov 30, 2000 Issued
90/005863 APPARATUS AND METHOD FOR DEICING AIRCRAFT Nov 20, 2000 Issued
Array ( [id] => 1525587 [patent_doc_number] => 06478258 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-11-12 [patent_title] => 'Spacecraft multiple loop heat pipe thermal system for internal equipment panel applications' [patent_app_type] => B1 [patent_app_number] => 09/718181 [patent_app_country] => US [patent_app_date] => 2000-11-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 3 [patent_no_of_words] => 1078 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 75 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/478/06478258.pdf [firstpage_image] =>[orig_patent_app_number] => 09718181 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/718181
Spacecraft multiple loop heat pipe thermal system for internal equipment panel applications Nov 20, 2000 Issued
90/005860 APPARATUS AND METHOD FOR DEICING AIRCRAFT Nov 16, 2000 Issued
09/700414 Heat shield Nov 14, 2000 Abandoned
Array ( [id] => 1334835 [patent_doc_number] => 06581870 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2003-06-24 [patent_title] => 'Method and apparatus for reducing pressure and temperature on the front of a missile at ultrasonic speed' [patent_app_type] => B1 [patent_app_number] => 09/707915 [patent_app_country] => US [patent_app_date] => 2000-11-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 7 [patent_no_of_words] => 1350 [patent_no_of_claims] => 5 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 92 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/581/06581870.pdf [firstpage_image] =>[orig_patent_app_number] => 09707915 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/707915
Method and apparatus for reducing pressure and temperature on the front of a missile at ultrasonic speed Nov 7, 2000 Issued
Array ( [id] => 1446584 [patent_doc_number] => 06454207 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-09-24 [patent_title] => 'Flap support mechanism and a flap-equipped rotor blade' [patent_app_type] => B1 [patent_app_number] => 09/702809 [patent_app_country] => US [patent_app_date] => 2000-11-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 10 [patent_no_of_words] => 4904 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 91 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/454/06454207.pdf [firstpage_image] =>[orig_patent_app_number] => 09702809 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/702809
Flap support mechanism and a flap-equipped rotor blade Oct 31, 2000 Issued
Array ( [id] => 1290559 [patent_doc_number] => 06626400 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2003-09-30 [patent_title] => 'Parachute deployment system and method' [patent_app_type] => B1 [patent_app_number] => 09/691517 [patent_app_country] => US [patent_app_date] => 2000-10-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 12 [patent_no_of_words] => 4951 [patent_no_of_claims] => 63 [patent_no_of_ind_claims] => 7 [patent_words_short_claim] => 169 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/626/06626400.pdf [firstpage_image] =>[orig_patent_app_number] => 09691517 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/691517
Parachute deployment system and method Oct 17, 2000 Issued
Array ( [id] => 1461166 [patent_doc_number] => 06392213 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-05-21 [patent_title] => 'Flyer assembly' [patent_app_type] => B1 [patent_app_number] => 09/690000 [patent_app_country] => US [patent_app_date] => 2000-10-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 13 [patent_figures_cnt] => 18 [patent_no_of_words] => 6584 [patent_no_of_claims] => 29 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 102 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/392/06392213.pdf [firstpage_image] =>[orig_patent_app_number] => 09690000 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/690000
Flyer assembly Oct 11, 2000 Issued
Array ( [id] => 7641517 [patent_doc_number] => 06394390 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-05-28 [patent_title] => 'Hook cable support assembly' [patent_app_type] => B1 [patent_app_number] => 09/689100 [patent_app_country] => US [patent_app_date] => 2000-10-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 8 [patent_no_of_words] => 3717 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 12 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/394/06394390.pdf [firstpage_image] =>[orig_patent_app_number] => 09689100 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/689100
Hook cable support assembly Oct 11, 2000 Issued
Array ( [id] => 1571072 [patent_doc_number] => 06467723 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-10-22 [patent_title] => 'Active vibration control system for helicopter with improved actustor placement' [patent_app_type] => B1 [patent_app_number] => 09/686009 [patent_app_country] => US [patent_app_date] => 2000-10-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 9 [patent_no_of_words] => 4122 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 127 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/467/06467723.pdf [firstpage_image] =>[orig_patent_app_number] => 09686009 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/686009
Active vibration control system for helicopter with improved actustor placement Oct 9, 2000 Issued
Array ( [id] => 1595030 [patent_doc_number] => 06474600 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-11-05 [patent_title] => 'Aircraft fuselage having a rear-end opening for cargo dispatch' [patent_app_type] => B1 [patent_app_number] => 09/647710 [patent_app_country] => US [patent_app_date] => 2000-10-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 5 [patent_no_of_words] => 1955 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 139 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/474/06474600.pdf [firstpage_image] =>[orig_patent_app_number] => 09647710 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/647710
Aircraft fuselage having a rear-end opening for cargo dispatch Oct 3, 2000 Issued
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