
Galen L. Barefoot
Examiner (ID: 15606)
| Most Active Art Unit | 3105 |
| Art Unit(s) | 3613, 3641, 3107, 2506, 3644, 3104, 3105, 3643 |
| Total Applications | 2920 |
| Issued Applications | 2553 |
| Pending Applications | 115 |
| Abandoned Applications | 252 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 1116964
[patent_doc_number] => 06796530
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-09-28
[patent_title] => 'Method and apparatus for providing pneumatic energy to an ejector'
[patent_app_type] => B2
[patent_app_number] => 10/299126
[patent_app_country] => US
[patent_app_date] => 2002-11-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 4340
[patent_no_of_claims] => 35
[patent_no_of_ind_claims] => 6
[patent_words_short_claim] => 23
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/796/06796530.pdf
[firstpage_image] =>[orig_patent_app_number] => 10299126
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/299126 | Method and apparatus for providing pneumatic energy to an ejector | Nov 17, 2002 | Issued |
Array
(
[id] => 970822
[patent_doc_number] => 06935594
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2005-08-30
[patent_title] => 'Composite components with integral protective casings'
[patent_app_type] => utility
[patent_app_number] => 10/293852
[patent_app_country] => US
[patent_app_date] => 2002-11-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 4
[patent_no_of_words] => 4625
[patent_no_of_claims] => 20
[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/06/935/06935594.pdf
[firstpage_image] =>[orig_patent_app_number] => 10293852
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/293852 | Composite components with integral protective casings | Nov 11, 2002 | Issued |
Array
(
[id] => 1045242
[patent_doc_number] => 06863245
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2005-03-08
[patent_title] => 'Aerodynamic profile with an adjustable flap'
[patent_app_type] => utility
[patent_app_number] => 10/291750
[patent_app_country] => US
[patent_app_date] => 2002-11-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 6
[patent_no_of_words] => 4258
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 7
[patent_words_short_claim] => 172
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/863/06863245.pdf
[firstpage_image] =>[orig_patent_app_number] => 10291750
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/291750 | Aerodynamic profile with an adjustable flap | Nov 11, 2002 | Issued |
Array
(
[id] => 1048608
[patent_doc_number] => 06860452
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2005-03-01
[patent_title] => 'Aircraft flight surface control system'
[patent_app_type] => utility
[patent_app_number] => 10/288902
[patent_app_country] => US
[patent_app_date] => 2002-11-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
[patent_figures_cnt] => 13
[patent_no_of_words] => 8593
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 97
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/860/06860452.pdf
[firstpage_image] =>[orig_patent_app_number] => 10288902
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/288902 | Aircraft flight surface control system | Nov 5, 2002 | Issued |
Array
(
[id] => 1090187
[patent_doc_number] => 06824108
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-11-30
[patent_title] => 'Active drag modulation system and method'
[patent_app_type] => B2
[patent_app_number] => 10/287379
[patent_app_country] => US
[patent_app_date] => 2002-11-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 10
[patent_no_of_words] => 5894
[patent_no_of_claims] => 26
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 90
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/824/06824108.pdf
[firstpage_image] =>[orig_patent_app_number] => 10287379
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/287379 | Active drag modulation system and method | Nov 3, 2002 | Issued |
Array
(
[id] => 1169501
[patent_doc_number] => 06742745
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-06-01
[patent_title] => 'Autonomous satellite docking system'
[patent_app_type] => B2
[patent_app_number] => 10/286192
[patent_app_country] => US
[patent_app_date] => 2002-11-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 14
[patent_no_of_words] => 2835
[patent_no_of_claims] => 4
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 77
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/742/06742745.pdf
[firstpage_image] =>[orig_patent_app_number] => 10286192
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/286192 | Autonomous satellite docking system | Oct 31, 2002 | Issued |
Array
(
[id] => 1090190
[patent_doc_number] => 06824109
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-11-30
[patent_title] => 'Lift adjusting device for aircraft'
[patent_app_type] => B2
[patent_app_number] => 10/283524
[patent_app_country] => US
[patent_app_date] => 2002-10-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 6
[patent_no_of_words] => 7435
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 131
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/824/06824109.pdf
[firstpage_image] =>[orig_patent_app_number] => 10283524
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/283524 | Lift adjusting device for aircraft | Oct 29, 2002 | Issued |
Array
(
[id] => 1163230
[patent_doc_number] => 06749154
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2004-06-15
[patent_title] => 'Aircraft advertising system'
[patent_app_type] => B1
[patent_app_number] => 10/282808
[patent_app_country] => US
[patent_app_date] => 2002-10-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 7
[patent_no_of_words] => 2398
[patent_no_of_claims] => 1
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 253
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/749/06749154.pdf
[firstpage_image] =>[orig_patent_app_number] => 10282808
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/282808 | Aircraft advertising system | Oct 28, 2002 | Issued |
Array
(
[id] => 7158869
[patent_doc_number] => 20040075020
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-04-22
[patent_title] => 'METHOD AND APPARATUS FOR CONTROLLING AIRCRAFT DEVICES WITH MULTIPLE ACTUATORS'
[patent_app_type] => new
[patent_app_number] => 10/282792
[patent_app_country] => US
[patent_app_date] => 2002-10-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 3905
[patent_no_of_claims] => 60
[patent_no_of_ind_claims] => 7
[patent_words_short_claim] => 118
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0075/20040075020.pdf
[firstpage_image] =>[orig_patent_app_number] => 10282792
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/282792 | Method and apparatus for controlling aircraft devices with multiple actuators | Oct 27, 2002 | Issued |
Array
(
[id] => 7370673
[patent_doc_number] => 20040079835
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-04-29
[patent_title] => 'Control system for alleviating a gust load on an aircraft wing'
[patent_app_type] => new
[patent_app_number] => 10/280512
[patent_app_country] => US
[patent_app_date] => 2002-10-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 7598
[patent_no_of_claims] => 30
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 66
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0079/20040079835.pdf
[firstpage_image] =>[orig_patent_app_number] => 10280512
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/280512 | Control system for alleviating a gust load on an aircraft wing | Oct 24, 2002 | Issued |
Array
(
[id] => 7967577
[patent_doc_number] => 06679452
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2004-01-20
[patent_title] => 'Aircraft landing gear support assemblies and associated methods of installation'
[patent_app_type] => B1
[patent_app_number] => 10/278633
[patent_app_country] => US
[patent_app_date] => 2002-10-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_no_of_words] => 4168
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/679/06679452.pdf
[firstpage_image] =>[orig_patent_app_number] => 10278633
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/278633 | Aircraft landing gear support assemblies and associated methods of installation | Oct 21, 2002 | Issued |
Array
(
[id] => 1154893
[patent_doc_number] => 06758439
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-07-06
[patent_title] => 'Apparatuses and methods for attaching engine nacelles to aircraft'
[patent_app_type] => B2
[patent_app_number] => 10/278382
[patent_app_country] => US
[patent_app_date] => 2002-10-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_no_of_words] => 4614
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[pdf_file] => patents/06/758/06758439.pdf
[firstpage_image] =>[orig_patent_app_number] => 10278382
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/278382 | Apparatuses and methods for attaching engine nacelles to aircraft | Oct 21, 2002 | Issued |
Array
(
[id] => 7158905
[patent_doc_number] => 20040075025
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-04-22
[patent_title] => 'AIRCRAFT WITH MULTIPURPOSE LOWER DECKS AND ASSOCIATED METHODS OF MANUFACTURE'
[patent_app_type] => new
[patent_app_number] => 10/278717
[patent_app_country] => US
[patent_app_date] => 2002-10-22
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[pdf_file] => publications/A1/0075/20040075025.pdf
[firstpage_image] =>[orig_patent_app_number] => 10278717
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/278717 | Aircraft with multipurpose lower decks and associated methods of manufacture | Oct 21, 2002 | Issued |
Array
(
[id] => 7158912
[patent_doc_number] => 20040075027
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-04-22
[patent_title] => 'Method and apparatus for liquid containment, such as for aircraft fuel vessels'
[patent_app_type] => new
[patent_app_number] => 10/278585
[patent_app_country] => US
[patent_app_date] => 2002-10-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0075/20040075027.pdf
[firstpage_image] =>[orig_patent_app_number] => 10278585
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/278585 | Method and apparatus for liquid containment, such as for aircraft fuel vessels | Oct 21, 2002 | Issued |
Array
(
[id] => 1260593
[patent_doc_number] => 06659397
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2003-12-09
[patent_title] => 'Control system for ornithopter'
[patent_app_type] => B1
[patent_app_number] => 10/273692
[patent_app_country] => US
[patent_app_date] => 2002-10-18
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[pdf_file] => patents/06/659/06659397.pdf
[firstpage_image] =>[orig_patent_app_number] => 10273692
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/273692 | Control system for ornithopter | Oct 17, 2002 | Issued |
Array
(
[id] => 6988463
[patent_doc_number] => 20050087653
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-04-28
[patent_title] => 'Parachute (survival air guard)'
[patent_app_type] => utility
[patent_app_number] => 10/492501
[patent_app_country] => US
[patent_app_date] => 2002-10-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 19
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0087/20050087653.pdf
[firstpage_image] =>[orig_patent_app_number] => 10492501
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/492501 | Parachute (survival air guard) | Oct 3, 2002 | Abandoned |
Array
(
[id] => 7432620
[patent_doc_number] => 20040065771
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-04-08
[patent_title] => 'Aircraft wheels having vanes'
[patent_app_type] => new
[patent_app_number] => 10/263427
[patent_app_country] => US
[patent_app_date] => 2002-10-03
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[pdf_file] => publications/A1/0065/20040065771.pdf
[firstpage_image] =>[orig_patent_app_number] => 10263427
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/263427 | Aircraft wheels having vanes | Oct 2, 2002 | Abandoned |
Array
(
[id] => 1228006
[patent_doc_number] => 06691950
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-02-17
[patent_title] => 'Device and system for the automatic control of a helicopter'
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[pdf_file] => patents/06/691/06691950.pdf
[firstpage_image] =>[orig_patent_app_number] => 10256072
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/256072 | Device and system for the automatic control of a helicopter | Sep 26, 2002 | Issued |
Array
(
[id] => 6671722
[patent_doc_number] => 20030057325
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[patent_kind] => A1
[patent_issue_date] => 2003-03-27
[patent_title] => 'Manually disassembled and readily shippable miniature, unmanned aircraft with data handling capability'
[patent_app_type] => new
[patent_app_number] => 10/255182
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[firstpage_image] =>[orig_patent_app_number] => 10255182
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/255182 | Manually disassembled and readily shippable miniature, unmanned aircraft with data handling capability | Sep 25, 2002 | Issued |
Array
(
[id] => 677833
[patent_doc_number] => 07083139
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2006-08-01
[patent_title] => 'Method for guiding a rocket'
[patent_app_type] => utility
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/083/07083139.pdf
[firstpage_image] =>[orig_patent_app_number] => 10490951
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/490951 | Method for guiding a rocket | Sep 22, 2002 | Issued |