
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] => 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 |