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] => 7328494 [patent_doc_number] => 20040129830 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-07-08 [patent_title] => 'Tail boom saddle for maintaining helicoptor main rotor blades in a stowed configuration for helicoptor stowage and transport' [patent_app_type] => new [patent_app_number] => 10/328567 [patent_app_country] => US [patent_app_date] => 2002-12-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 5800 [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/A1/0129/20040129830.pdf [firstpage_image] =>[orig_patent_app_number] => 10328567 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/328567
Tail boom saddle for maintaining helicoptor main rotor blades in a stowed configuration for helicoptor stowage and transport Dec 22, 2002 Abandoned
Array ( [id] => 1029580 [patent_doc_number] => 06877696 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2005-04-12 [patent_title] => 'Evacuation slide with leading edge spoiler' [patent_app_type] => utility [patent_app_number] => 10/324713 [patent_app_country] => US [patent_app_date] => 2002-12-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 6 [patent_no_of_words] => 1623 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 7 [patent_words_short_claim] => 167 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/877/06877696.pdf [firstpage_image] =>[orig_patent_app_number] => 10324713 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/324713
Evacuation slide with leading edge spoiler Dec 18, 2002 Issued
Array ( [id] => 973928 [patent_doc_number] => 06932302 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2005-08-23 [patent_title] => 'Reusable launch system' [patent_app_type] => utility [patent_app_number] => 10/325522 [patent_app_country] => US [patent_app_date] => 2002-12-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 10 [patent_no_of_words] => 7478 [patent_no_of_claims] => 40 [patent_no_of_ind_claims] => 5 [patent_words_short_claim] => 201 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/932/06932302.pdf [firstpage_image] =>[orig_patent_app_number] => 10325522 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/325522
Reusable launch system Dec 18, 2002 Issued
Array ( [id] => 6655515 [patent_doc_number] => 20030132347 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2003-07-17 [patent_title] => 'Emergency opening cylinder of a passenger door for an airplane, a door system and a method of modifying a door system' [patent_app_type] => new [patent_app_number] => 10/319808 [patent_app_country] => US [patent_app_date] => 2002-12-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 2380 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 104 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0132/20030132347.pdf [firstpage_image] =>[orig_patent_app_number] => 10319808 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/319808
Emergency opening cylinder of a passenger door for an airplane, a door system and a method of modifying a door system Dec 15, 2002 Issued
Array ( [id] => 6708804 [patent_doc_number] => 20030168553 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2003-09-11 [patent_title] => 'Decompression unit for equalizing an explosive air pressure' [patent_app_type] => new [patent_app_number] => 10/311608 [patent_app_country] => US [patent_app_date] => 2002-12-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 4288 [patent_no_of_claims] => 7 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 51 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0168/20030168553.pdf [firstpage_image] =>[orig_patent_app_number] => 10311608 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/311608
Decompression unit for equalizing an explosive air pressure Dec 15, 2002 Issued
Array ( [id] => 6626081 [patent_doc_number] => 20030102411 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2003-06-05 [patent_title] => 'System for varying a surface contour' [patent_app_type] => new [patent_app_number] => 10/316661 [patent_app_country] => US [patent_app_date] => 2002-12-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 4572 [patent_no_of_claims] => 39 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 117 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0102/20030102411.pdf [firstpage_image] =>[orig_patent_app_number] => 10316661 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/316661
System for varying a surface contour Dec 9, 2002 Abandoned
Array ( [id] => 1072802 [patent_doc_number] => 06837464 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2005-01-04 [patent_title] => 'Lox-compatible composite tank for aerospace applications' [patent_app_type] => utility [patent_app_number] => 10/316131 [patent_app_country] => US [patent_app_date] => 2002-12-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 19 [patent_no_of_words] => 5393 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 11 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/837/06837464.pdf [firstpage_image] =>[orig_patent_app_number] => 10316131 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/316131
Lox-compatible composite tank for aerospace applications Dec 9, 2002 Issued
Array ( [id] => 6807156 [patent_doc_number] => 20030197095 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2003-10-23 [patent_title] => 'Steerable parachute control system and method' [patent_app_type] => new [patent_app_number] => 10/315466 [patent_app_country] => US [patent_app_date] => 2002-12-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 6100 [patent_no_of_claims] => 30 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 32 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0197/20030197095.pdf [firstpage_image] =>[orig_patent_app_number] => 10315466 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/315466
Steerable parachute control system and method Dec 8, 2002 Issued
Array ( [id] => 696503 [patent_doc_number] => 07066426 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2006-06-27 [patent_title] => 'Multimodal, deployable vehicle' [patent_app_type] => utility [patent_app_number] => 10/315686 [patent_app_country] => US [patent_app_date] => 2002-12-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 2 [patent_no_of_words] => 1821 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 181 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/066/07066426.pdf [firstpage_image] =>[orig_patent_app_number] => 10315686 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/315686
Multimodal, deployable vehicle Dec 8, 2002 Issued
Array ( [id] => 1220613 [patent_doc_number] => 06698690 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2004-03-02 [patent_title] => 'Impact resistant door containing resealable panels' [patent_app_type] => B2 [patent_app_number] => 10/310217 [patent_app_country] => US [patent_app_date] => 2002-12-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 20 [patent_figures_cnt] => 26 [patent_no_of_words] => 6193 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 79 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/698/06698690.pdf [firstpage_image] =>[orig_patent_app_number] => 10310217 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/310217
Impact resistant door containing resealable panels Dec 3, 2002 Issued
Array ( [id] => 1245986 [patent_doc_number] => 06672540 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2004-01-06 [patent_title] => 'Actuator for aircraft stabilizers with a failure responsive lock control mechanism' [patent_app_type] => B1 [patent_app_number] => 10/308527 [patent_app_country] => US [patent_app_date] => 2002-12-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 12 [patent_no_of_words] => 8068 [patent_no_of_claims] => 42 [patent_no_of_ind_claims] => 6 [patent_words_short_claim] => 482 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/672/06672540.pdf [firstpage_image] =>[orig_patent_app_number] => 10308527 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/308527
Actuator for aircraft stabilizers with a failure responsive lock control mechanism Dec 2, 2002 Issued
Array ( [id] => 1251531 [patent_doc_number] => 06669143 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2003-12-30 [patent_title] => 'Non-encroaching aircraft passenger seat' [patent_app_type] => B1 [patent_app_number] => 10/305849 [patent_app_country] => US [patent_app_date] => 2002-11-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 3179 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 146 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/669/06669143.pdf [firstpage_image] =>[orig_patent_app_number] => 10305849 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/305849
Non-encroaching aircraft passenger seat Nov 26, 2002 Issued
Array ( [id] => 1251532 [patent_doc_number] => 06669144 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2003-12-30 [patent_title] => 'Access apparatus' [patent_app_type] => B2 [patent_app_number] => 10/304064 [patent_app_country] => US [patent_app_date] => 2002-11-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 12 [patent_no_of_words] => 2758 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 81 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/669/06669144.pdf [firstpage_image] =>[orig_patent_app_number] => 10304064 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/304064
Access apparatus Nov 25, 2002 Issued
Array ( [id] => 6653546 [patent_doc_number] => 20030131982 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2003-07-17 [patent_title] => 'Method and system of thermal protection' [patent_app_type] => new [patent_app_number] => 10/304236 [patent_app_country] => US [patent_app_date] => 2002-11-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 3392 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 158 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0131/20030131982.pdf [firstpage_image] =>[orig_patent_app_number] => 10304236 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/304236
Method and system of thermal protection Nov 24, 2002 Issued
Array ( [id] => 1197523 [patent_doc_number] => 06722610 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2004-04-20 [patent_title] => 'Method, system, and computer program product for controlling maneuverable wheels on a vehicle' [patent_app_type] => B1 [patent_app_number] => 10/303552 [patent_app_country] => US [patent_app_date] => 2002-11-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 8521 [patent_no_of_claims] => 33 [patent_no_of_ind_claims] => 9 [patent_words_short_claim] => 85 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/722/06722610.pdf [firstpage_image] =>[orig_patent_app_number] => 10303552 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/303552
Method, system, and computer program product for controlling maneuverable wheels on a vehicle Nov 24, 2002 Issued
Array ( [id] => 1116956 [patent_doc_number] => 06796526 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2004-09-28 [patent_title] => 'Augmenting flight control surface actuation system and method' [patent_app_type] => B2 [patent_app_number] => 10/303521 [patent_app_country] => US [patent_app_date] => 2002-11-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 3 [patent_no_of_words] => 5050 [patent_no_of_claims] => 24 [patent_no_of_ind_claims] => 7 [patent_words_short_claim] => 107 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/796/06796526.pdf [firstpage_image] =>[orig_patent_app_number] => 10303521 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/303521
Augmenting flight control surface actuation system and method Nov 24, 2002 Issued
Array ( [id] => 1260598 [patent_doc_number] => 06659399 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2003-12-09 [patent_title] => 'Compact linear split sleeves for accurate rigging in confined space' [patent_app_type] => B1 [patent_app_number] => 10/303472 [patent_app_country] => US [patent_app_date] => 2002-11-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 8 [patent_no_of_words] => 2375 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 278 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/659/06659399.pdf [firstpage_image] =>[orig_patent_app_number] => 10303472 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/303472
Compact linear split sleeves for accurate rigging in confined space Nov 24, 2002 Issued
Array ( [id] => 1123081 [patent_doc_number] => 06789769 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2004-09-14 [patent_title] => 'Flexible airflow separator to reduce aerodynamic noise generated by a leading edge slat of an aircraft wing' [patent_app_type] => B2 [patent_app_number] => 10/302454 [patent_app_country] => US [patent_app_date] => 2002-11-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 9 [patent_no_of_words] => 6384 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 186 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/789/06789769.pdf [firstpage_image] =>[orig_patent_app_number] => 10302454 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/302454
Flexible airflow separator to reduce aerodynamic noise generated by a leading edge slat of an aircraft wing Nov 21, 2002 Issued
Array ( [id] => 1055064 [patent_doc_number] => 06854688 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2005-02-15 [patent_title] => 'Solid oxide regenerative fuel cell for airplane power generation and storage' [patent_app_type] => utility [patent_app_number] => 10/299863 [patent_app_country] => US [patent_app_date] => 2002-11-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 12 [patent_no_of_words] => 7545 [patent_no_of_claims] => 45 [patent_no_of_ind_claims] => 8 [patent_words_short_claim] => 26 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/854/06854688.pdf [firstpage_image] =>[orig_patent_app_number] => 10299863 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/299863
Solid oxide regenerative fuel cell for airplane power generation and storage Nov 19, 2002 Issued
Array ( [id] => 1166879 [patent_doc_number] => 06745982 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2004-06-08 [patent_title] => 'Pressure rate of change sensitive latching method and apparatus' [patent_app_type] => B2 [patent_app_number] => 10/300681 [patent_app_country] => US [patent_app_date] => 2002-11-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 12 [patent_no_of_words] => 4637 [patent_no_of_claims] => 37 [patent_no_of_ind_claims] => 9 [patent_words_short_claim] => 83 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/745/06745982.pdf [firstpage_image] =>[orig_patent_app_number] => 10300681 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/300681
Pressure rate of change sensitive latching method and apparatus Nov 18, 2002 Issued
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