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] => 5599355 [patent_doc_number] => 20060289699 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-12-28 [patent_title] => 'CONTAINER APPARATUS FOR OBJECT TO BE DROPPED' [patent_app_type] => utility [patent_app_number] => 10/408272 [patent_app_country] => US [patent_app_date] => 2003-04-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 4503 [patent_no_of_claims] => 3 [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/A1/0289/20060289699.pdf [firstpage_image] =>[orig_patent_app_number] => 10408272 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/408272
Container apparatus for object to be dropped Apr 6, 2003 Issued
Array ( [id] => 6803274 [patent_doc_number] => 20030230668 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2003-12-18 [patent_title] => 'Helicopter electric connecting unit, and helicopter equipped with such a connecting unit' [patent_app_type] => new [patent_app_number] => 10/407942 [patent_app_country] => US [patent_app_date] => 2003-04-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 1314 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 95 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0230/20030230668.pdf [firstpage_image] =>[orig_patent_app_number] => 10407942 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/407942
Helicopter electric connecting unit, and helicopter equipped with such a connecting unit Apr 6, 2003 Issued
Array ( [id] => 7439956 [patent_doc_number] => 20040195462 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-10-07 [patent_title] => 'SURFACE PLASMA DISCHARGE FOR CONTROLLING LEADING EDGE CONTAMINATION AND CROSSFLOW INSTABILITIES FOR LAMINAR FLOW' [patent_app_type] => new [patent_app_number] => 10/406940 [patent_app_country] => US [patent_app_date] => 2003-04-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 3294 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 12 [patent_words_short_claim] => 2 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0195/20040195462.pdf [firstpage_image] =>[orig_patent_app_number] => 10406940 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/406940
Surface plasma discharge for controlling leading edge contamination and crossflow instabilities for laminar flow Apr 2, 2003 Issued
Array ( [id] => 1120308 [patent_doc_number] => 06793171 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2004-09-21 [patent_title] => 'Method and system for flying an aircraft' [patent_app_type] => B1 [patent_app_number] => 10/406047 [patent_app_country] => US [patent_app_date] => 2003-04-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 4 [patent_no_of_words] => 2751 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 97 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/793/06793171.pdf [firstpage_image] =>[orig_patent_app_number] => 10406047 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/406047
Method and system for flying an aircraft Apr 1, 2003 Issued
Array ( [id] => 7455306 [patent_doc_number] => 20040118971 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-06-24 [patent_title] => 'TAIL BOOM SADDLE FOR MAINTAINING HELICOPTOR MAIN ROTOR BLADES IN A STOWED CONFIGURATION FOR HELICOPTER STOWAGE AND TRANSPORT' [patent_app_type] => new [patent_app_number] => 10/405780 [patent_app_country] => US [patent_app_date] => 2003-04-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 5833 [patent_no_of_claims] => 29 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 294 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0118/20040118971.pdf [firstpage_image] =>[orig_patent_app_number] => 10405780 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/405780
Tail boom saddle for maintaining helicoptor main rotor blades in a stowed configuration for helicopter stowage and transport Mar 31, 2003 Issued
Array ( [id] => 1149793 [patent_doc_number] => 06761332 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2004-07-13 [patent_title] => 'Multi-functional galley system' [patent_app_type] => B1 [patent_app_number] => 10/404856 [patent_app_country] => US [patent_app_date] => 2003-04-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 4332 [patent_no_of_claims] => 52 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 103 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/761/06761332.pdf [firstpage_image] =>[orig_patent_app_number] => 10404856 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/404856
Multi-functional galley system Mar 31, 2003 Issued
Array ( [id] => 753985 [patent_doc_number] => 07014147 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2006-03-21 [patent_title] => 'Anti hijacking system' [patent_app_type] => utility [patent_app_number] => 10/397563 [patent_app_country] => US [patent_app_date] => 2003-03-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 5 [patent_no_of_words] => 1369 [patent_no_of_claims] => 3 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 118 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/014/07014147.pdf [firstpage_image] =>[orig_patent_app_number] => 10397563 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/397563
Anti hijacking system Mar 26, 2003 Issued
Array ( [id] => 7387603 [patent_doc_number] => 20040016845 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-01-29 [patent_title] => 'Integrated and/or modular high-speed aircraft' [patent_app_type] => new [patent_app_number] => 10/394550 [patent_app_country] => US [patent_app_date] => 2003-03-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 20 [patent_figures_cnt] => 20 [patent_no_of_words] => 9698 [patent_no_of_claims] => 90 [patent_no_of_ind_claims] => 10 [patent_words_short_claim] => 103 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0016/20040016845.pdf [firstpage_image] =>[orig_patent_app_number] => 10394550 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/394550
Integrated and/or modular high-speed aircraft Mar 20, 2003 Issued
Array ( [id] => 6770903 [patent_doc_number] => 20030216843 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2003-11-20 [patent_title] => 'AirSafety system' [patent_app_type] => new [patent_app_number] => 10/394081 [patent_app_country] => US [patent_app_date] => 2003-03-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 1087 [patent_no_of_claims] => 3 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 28 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0216/20030216843.pdf [firstpage_image] =>[orig_patent_app_number] => 10394081 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/394081
AirSafety system Mar 20, 2003 Abandoned
Array ( [id] => 721088 [patent_doc_number] => 07044422 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2006-05-16 [patent_title] => 'Gyrostabilized self propelled aircraft' [patent_app_type] => utility [patent_app_number] => 10/390222 [patent_app_country] => US [patent_app_date] => 2003-03-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 17 [patent_figures_cnt] => 23 [patent_no_of_words] => 9489 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 228 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/044/07044422.pdf [firstpage_image] =>[orig_patent_app_number] => 10390222 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/390222
Gyrostabilized self propelled aircraft Mar 16, 2003 Issued
Array ( [id] => 1120319 [patent_doc_number] => 06793177 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2004-09-21 [patent_title] => 'Active drag and thrust modulation system and method' [patent_app_type] => B2 [patent_app_number] => 10/386992 [patent_app_country] => US [patent_app_date] => 2003-03-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 13 [patent_figures_cnt] => 42 [patent_no_of_words] => 17482 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 57 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/793/06793177.pdf [firstpage_image] =>[orig_patent_app_number] => 10386992 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/386992
Active drag and thrust modulation system and method Mar 11, 2003 Issued
Array ( [id] => 653563 [patent_doc_number] => 07108225 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2006-09-19 [patent_title] => 'More aerodynamic wheel fairings for small airplanes' [patent_app_type] => utility [patent_app_number] => 10/385360 [patent_app_country] => US [patent_app_date] => 2003-03-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 6764 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 125 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/108/07108225.pdf [firstpage_image] =>[orig_patent_app_number] => 10385360 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/385360
More aerodynamic wheel fairings for small airplanes Mar 10, 2003 Issued
Array ( [id] => 1061425 [patent_doc_number] => 06848652 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2005-02-01 [patent_title] => 'Aircraft heater' [patent_app_type] => utility [patent_app_number] => 10/376004 [patent_app_country] => US [patent_app_date] => 2003-02-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 8 [patent_no_of_words] => 3170 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 84 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/848/06848652.pdf [firstpage_image] =>[orig_patent_app_number] => 10376004 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/376004
Aircraft heater Feb 27, 2003 Issued
Array ( [id] => 6827470 [patent_doc_number] => 20030178528 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2003-09-25 [patent_title] => 'Rotary-wing aircraft rotor with constant velocity drive' [patent_app_type] => new [patent_app_number] => 10/378003 [patent_app_country] => US [patent_app_date] => 2003-02-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 10138 [patent_no_of_claims] => 22 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 430 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0178/20030178528.pdf [firstpage_image] =>[orig_patent_app_number] => 10378003 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/378003
Rotary-wing aircraft rotor with constant velocity drive Feb 27, 2003 Issued
Array ( [id] => 7304744 [patent_doc_number] => 20040140403 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-07-22 [patent_title] => 'Asymetric gravitational wave propulsion system' [patent_app_type] => new [patent_app_number] => 10/363287 [patent_app_country] => US [patent_app_date] => 2003-02-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 1811 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 69 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0140/20040140403.pdf [firstpage_image] =>[orig_patent_app_number] => 10363287 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/363287
Asymetric gravitational wave propulsion system Feb 26, 2003 Abandoned
Array ( [id] => 7367742 [patent_doc_number] => 20040026564 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-02-12 [patent_title] => 'METHOD AND APPARATUS FOR FOLDING/UNFOLDING THE BLADES OF A ROTARY-WING AIRCRAFT ROTOR' [patent_app_type] => new [patent_app_number] => 10/375707 [patent_app_country] => US [patent_app_date] => 2003-02-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 13325 [patent_no_of_claims] => 30 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 153 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0026/20040026564.pdf [firstpage_image] =>[orig_patent_app_number] => 10375707 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/375707
Method and apparatus for folding/unfolding the blades of a rotary-wing aircraft rotor Feb 26, 2003 Issued
Array ( [id] => 1166874 [patent_doc_number] => 06745981 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2004-06-08 [patent_title] => 'Aircraft sensor pod assembly' [patent_app_type] => B1 [patent_app_number] => 10/373459 [patent_app_country] => US [patent_app_date] => 2003-02-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 1608 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 204 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/745/06745981.pdf [firstpage_image] =>[orig_patent_app_number] => 10373459 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/373459
Aircraft sensor pod assembly Feb 24, 2003 Issued
Array ( [id] => 7446669 [patent_doc_number] => 20040164203 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-08-26 [patent_title] => 'Vertical take-off and landing aircraft' [patent_app_type] => new [patent_app_number] => 10/371704 [patent_app_country] => US [patent_app_date] => 2003-02-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 5678 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 48 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0164/20040164203.pdf [firstpage_image] =>[orig_patent_app_number] => 10371704 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/371704
Vertical take-off and landing aircraft Feb 20, 2003 Abandoned
Array ( [id] => 7446683 [patent_doc_number] => 20040164205 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-08-26 [patent_title] => 'Deployable spacecraft mount for electric propulsion' [patent_app_type] => new [patent_app_number] => 10/371838 [patent_app_country] => US [patent_app_date] => 2003-02-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 11 [patent_no_of_words] => 4302 [patent_no_of_claims] => 24 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 59 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0164/20040164205.pdf [firstpage_image] =>[orig_patent_app_number] => 10371838 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/371838
Deployable spacecraft mount for electric propulsion Feb 20, 2003 Issued
Array ( [id] => 7432627 [patent_doc_number] => 20040065772 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-04-08 [patent_title] => 'High-lift, low-drag, stall-resistant airfoil' [patent_app_type] => new [patent_app_number] => 10/370740 [patent_app_country] => US [patent_app_date] => 2003-02-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 13 [patent_figures_cnt] => 13 [patent_no_of_words] => 5728 [patent_no_of_claims] => 68 [patent_no_of_ind_claims] => 6 [patent_words_short_claim] => 146 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0065/20040065772.pdf [firstpage_image] =>[orig_patent_app_number] => 10370740 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/370740
High-lift, low-drag, stall-resistant airfoil Feb 20, 2003 Issued
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