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] => 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 (“hum”) 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 [patent_figures_cnt] => 13 [patent_no_of_words] => 3530 [patent_no_of_claims] => 21 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 254 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_no_of_claims] => 4 [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/A1/0116/20050116091.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
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