
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] => 7439865
[patent_doc_number] => 20040195448
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-10-07
[patent_title] => 'Environmental control system'
[patent_app_type] => new
[patent_app_number] => 10/724094
[patent_app_country] => US
[patent_app_date] => 2003-12-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 1400
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 113
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0195/20040195448.pdf
[firstpage_image] =>[orig_patent_app_number] => 10724094
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/724094 | Environmental control system | Nov 30, 2003 | Abandoned |
Array
(
[id] => 7058734
[patent_doc_number] => 20050001093
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-01-06
[patent_title] => 'Impact resistant structure for the helicopter and energy absorber used for the same'
[patent_app_type] => utility
[patent_app_number] => 10/724186
[patent_app_country] => US
[patent_app_date] => 2003-12-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 18
[patent_figures_cnt] => 18
[patent_no_of_words] => 4707
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0001/20050001093.pdf
[firstpage_image] =>[orig_patent_app_number] => 10724186
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/724186 | Impact resistant structure for the helicopter and energy absorber used for the same | Nov 30, 2003 | Issued |
Array
(
[id] => 1096369
[patent_doc_number] => 06817570
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-11-16
[patent_title] => 'Ducted fan vehicles particularly useful as VTOL aircraft'
[patent_app_type] => B2
[patent_app_number] => 10/479149
[patent_app_country] => US
[patent_app_date] => 2003-11-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 20
[patent_no_of_words] => 4421
[patent_no_of_claims] => 2
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 244
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/817/06817570.pdf
[firstpage_image] =>[orig_patent_app_number] => 10479149
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/479149 | Ducted fan vehicles particularly useful as VTOL aircraft | Nov 27, 2003 | Issued |
Array
(
[id] => 6936312
[patent_doc_number] => 20050109873
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-05-26
[patent_title] => 'Method and apparatus for stowing and deploying control surfaces of a guided air vehicle'
[patent_app_type] => utility
[patent_app_number] => 10/720400
[patent_app_country] => US
[patent_app_date] => 2003-11-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 4213
[patent_no_of_claims] => 20
[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/A1/0109/20050109873.pdf
[firstpage_image] =>[orig_patent_app_number] => 10720400
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/720400 | Method and apparatus for stowing and deploying control surfaces of a guided air vehicle | Nov 23, 2003 | Issued |
Array
(
[id] => 7396135
[patent_doc_number] => 20040104306
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-06-03
[patent_title] => 'Aircraft cockpit window'
[patent_app_type] => new
[patent_app_number] => 10/722020
[patent_app_country] => US
[patent_app_date] => 2003-11-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 6311
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 85
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0104/20040104306.pdf
[firstpage_image] =>[orig_patent_app_number] => 10722020
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/722020 | Aircraft cockpit window | Nov 23, 2003 | Issued |
Array
(
[id] => 7008195
[patent_doc_number] => 20050061911
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-03-24
[patent_title] => 'Air cycle air conditioning with adaptive ram heat exchanger'
[patent_app_type] => utility
[patent_app_number] => 10/716313
[patent_app_country] => US
[patent_app_date] => 2003-11-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 1679
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0061/20050061911.pdf
[firstpage_image] =>[orig_patent_app_number] => 10716313
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/716313 | Air cycle air conditioning with adaptive ram heat exchanger | Nov 17, 2003 | Issued |
Array
(
[id] => 933244
[patent_doc_number] => 06976656
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2005-12-20
[patent_title] => 'Method for controlling the flight of an aircraft'
[patent_app_type] => utility
[patent_app_number] => 10/714959
[patent_app_country] => US
[patent_app_date] => 2003-11-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 4
[patent_no_of_words] => 3069
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 83
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/976/06976656.pdf
[firstpage_image] =>[orig_patent_app_number] => 10714959
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/714959 | Method for controlling the flight of an aircraft | Nov 17, 2003 | Issued |
Array
(
[id] => 1016656
[patent_doc_number] => 06889936
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2005-05-10
[patent_title] => 'Apparatus and methods for increasing useable space within aircraft lavatories'
[patent_app_type] => utility
[patent_app_number] => 10/715309
[patent_app_country] => US
[patent_app_date] => 2003-11-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 20
[patent_figures_cnt] => 24
[patent_no_of_words] => 4703
[patent_no_of_claims] => 27
[patent_no_of_ind_claims] => 6
[patent_words_short_claim] => 116
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/889/06889936.pdf
[firstpage_image] =>[orig_patent_app_number] => 10715309
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/715309 | Apparatus and methods for increasing useable space within aircraft lavatories | Nov 16, 2003 | Issued |
Array
(
[id] => 7139771
[patent_doc_number] => 20050116095
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-06-02
[patent_title] => 'ENHANCED RUDDER CONTROL SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 10/714744
[patent_app_country] => US
[patent_app_date] => 2003-11-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 8211
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 9
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0116/20050116095.pdf
[firstpage_image] =>[orig_patent_app_number] => 10714744
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/714744 | Enhanced rudder control system | Nov 16, 2003 | Issued |
Array
(
[id] => 7218823
[patent_doc_number] => 20040155155
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-08-12
[patent_title] => 'Inertial reference system for an aircraft'
[patent_app_type] => new
[patent_app_number] => 10/713016
[patent_app_country] => US
[patent_app_date] => 2003-11-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 3148
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 56
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0155/20040155155.pdf
[firstpage_image] =>[orig_patent_app_number] => 10713016
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/713016 | Inertial reference system for an aircraft | Nov 16, 2003 | Issued |
Array
(
[id] => 1055063
[patent_doc_number] => 06854687
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2005-02-15
[patent_title] => 'Nacelle integration with reflexed wing for sonic boom reduction'
[patent_app_type] => utility
[patent_app_number] => 10/713515
[patent_app_country] => US
[patent_app_date] => 2003-11-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 21
[patent_no_of_words] => 6057
[patent_no_of_claims] => 21
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 94
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/854/06854687.pdf
[firstpage_image] =>[orig_patent_app_number] => 10713515
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/713515 | Nacelle integration with reflexed wing for sonic boom reduction | Nov 10, 2003 | Issued |
Array
(
[id] => 7458302
[patent_doc_number] => 20040094668
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-05-20
[patent_title] => 'Aircraft seat footrest system and method'
[patent_app_type] => new
[patent_app_number] => 10/703703
[patent_app_country] => US
[patent_app_date] => 2003-11-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 1679
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 39
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0094/20040094668.pdf
[firstpage_image] =>[orig_patent_app_number] => 10703703
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/703703 | Aircraft seat footrest system and method | Nov 6, 2003 | Issued |
Array
(
[id] => 605465
[patent_doc_number] => 07152828
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2006-12-26
[patent_title] => 'Method and apparatus for the hookup of unmanned/manned (“hum”) multi purpose vehicles with each other'
[patent_app_type] => utility
[patent_app_number] => 10/701209
[patent_app_country] => US
[patent_app_date] => 2003-11-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 21
[patent_no_of_words] => 3777
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 184
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/152/07152828.pdf
[firstpage_image] =>[orig_patent_app_number] => 10701209
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/701209 | Method and apparatus for the hookup of unmanned/manned (“humâ€) multi purpose vehicles with each other | Oct 31, 2003 | Issued |
Array
(
[id] => 1090161
[patent_doc_number] => 06824092
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2004-11-30
[patent_title] => 'Aircraft tail configuration for sonic boom reduction'
[patent_app_type] => B1
[patent_app_number] => 10/696795
[patent_app_country] => US
[patent_app_date] => 2003-10-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 24
[patent_figures_cnt] => 25
[patent_no_of_words] => 9052
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 116
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/824/06824092.pdf
[firstpage_image] =>[orig_patent_app_number] => 10696795
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/696795 | Aircraft tail configuration for sonic boom reduction | Oct 29, 2003 | Issued |
Array
(
[id] => 7101203
[patent_doc_number] => 20050103929
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-05-19
[patent_title] => 'SUPERSONIC AIRCRAFT WITH CHANNEL RELIEF CONTROL'
[patent_app_type] => utility
[patent_app_number] => 10/696796
[patent_app_country] => US
[patent_app_date] => 2003-10-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 20
[patent_figures_cnt] => 20
[patent_no_of_words] => 5534
[patent_no_of_claims] => 21
[patent_no_of_ind_claims] => 20
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0103/20050103929.pdf
[firstpage_image] =>[orig_patent_app_number] => 10696796
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/696796 | Supersonic aircraft with channel relief control | Oct 29, 2003 | Issued |
Array
(
[id] => 995497
[patent_doc_number] => 06913226
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2005-07-05
[patent_title] => 'Methods and systems for redundant control and/or failure detection'
[patent_app_type] => utility
[patent_app_number] => 10/697383
[patent_app_country] => US
[patent_app_date] => 2003-10-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 5
[patent_no_of_words] => 5218
[patent_no_of_claims] => 32
[patent_no_of_ind_claims] => 9
[patent_words_short_claim] => 137
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/913/06913226.pdf
[firstpage_image] =>[orig_patent_app_number] => 10697383
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/697383 | Methods and systems for redundant control and/or failure detection | Oct 29, 2003 | Issued |
Array
(
[id] => 7101212
[patent_doc_number] => 20050103938
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-05-19
[patent_title] => 'PILOT DIRECTOR LIGHT UTILIZING LIGHT EMITTING DIODE (LED) TECHNOLOGY'
[patent_app_type] => utility
[patent_app_number] => 10/694185
[patent_app_country] => US
[patent_app_date] => 2003-10-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 12
[patent_no_of_words] => 4930
[patent_no_of_claims] => 24
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0103/20050103938.pdf
[firstpage_image] =>[orig_patent_app_number] => 10694185
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/694185 | Pilot director light utilizing light emitting diode (LED) technology | Oct 27, 2003 | Issued |
Array
(
[id] => 962874
[patent_doc_number] => 06948685
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2005-09-27
[patent_title] => 'Locking device with solenoid release pin'
[patent_app_type] => utility
[patent_app_number] => 10/695500
[patent_app_country] => US
[patent_app_date] => 2003-10-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
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[patent_no_of_words] => 3530
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/948/06948685.pdf
[firstpage_image] =>[orig_patent_app_number] => 10695500
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/695500 | Locking device with solenoid release pin | Oct 26, 2003 | Issued |
Array
(
[id] => 7139767
[patent_doc_number] => 20050116091
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-06-02
[patent_title] => 'High-altitude launching of rockets lifted by helium devices and platforms with rotatable wings'
[patent_app_type] => utility
[patent_app_number] => 10/692057
[patent_app_country] => US
[patent_app_date] => 2003-10-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 11071
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0116/20050116091.pdf
[firstpage_image] =>[orig_patent_app_number] => 10692057
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/692057 | High-altitude launching of rockets lifted by helium devices and platforms with rotatable wings | Oct 22, 2003 | Issued |
Array
(
[id] => 7153977
[patent_doc_number] => 20050082432
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-04-21
[patent_title] => 'STRUCTURAL COCKPIT WINDOW AND METHOD OF MAKING SAME'
[patent_app_type] => utility
[patent_app_number] => 10/690101
[patent_app_country] => US
[patent_app_date] => 2003-10-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 1685
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0082/20050082432.pdf
[firstpage_image] =>[orig_patent_app_number] => 10690101
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/690101 | Structural cockpit window and method of making same | Oct 20, 2003 | Issued |