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] => 1381766 [patent_doc_number] => 06530542 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2003-03-11 [patent_title] => 'Rotary wing aircraft with electric pitch control' [patent_app_type] => B2 [patent_app_number] => 09/901901 [patent_app_country] => US [patent_app_date] => 2001-07-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 5 [patent_no_of_words] => 4628 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 355 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/530/06530542.pdf [firstpage_image] =>[orig_patent_app_number] => 09901901 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/901901
Rotary wing aircraft with electric pitch control Jul 10, 2001 Issued
Array ( [id] => 6986574 [patent_doc_number] => 20010036406 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2001-11-01 [patent_title] => 'Fluid flow straightening techniques' [patent_app_type] => new [patent_app_number] => 09/901287 [patent_app_country] => US [patent_app_date] => 2001-07-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 3368 [patent_no_of_claims] => 27 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 29 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0036/20010036406.pdf [firstpage_image] =>[orig_patent_app_number] => 09901287 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/901287
Fluid flow straightening techniques Jul 8, 2001 Issued
Array ( [id] => 6634295 [patent_doc_number] => 20030006341 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2003-01-09 [patent_title] => 'Method and apparatus for damping vibration' [patent_app_type] => new [patent_app_number] => 09/899600 [patent_app_country] => US [patent_app_date] => 2001-07-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 5197 [patent_no_of_claims] => 27 [patent_no_of_ind_claims] => 5 [patent_words_short_claim] => 108 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0006/20030006341.pdf [firstpage_image] =>[orig_patent_app_number] => 09899600 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/899600
Method and apparatus for damping vibration Jul 4, 2001 Issued
Array ( [id] => 6269091 [patent_doc_number] => 20020104926 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2002-08-08 [patent_title] => 'Arrangement for the electrical operation of a door of an aircraft' [patent_app_type] => new [patent_app_number] => 09/895923 [patent_app_country] => US [patent_app_date] => 2001-06-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 3890 [patent_no_of_claims] => 24 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 66 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0104/20020104926.pdf [firstpage_image] =>[orig_patent_app_number] => 09895923 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/895923
Arrangement for the electrical operation of a door of an aircraft Jun 27, 2001 Abandoned
Array ( [id] => 5798349 [patent_doc_number] => 20020008174 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2002-01-24 [patent_title] => 'Eyepiece-support arm assembly device on an aircraft such as a rotary aircraft' [patent_app_type] => new [patent_app_number] => 09/888601 [patent_app_country] => US [patent_app_date] => 2001-06-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 2544 [patent_no_of_claims] => 7 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 20 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0008/20020008174.pdf [firstpage_image] =>[orig_patent_app_number] => 09888601 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/888601
Eyepiece-support arm assembly device on an aircraft such as a rotary aircraft Jun 25, 2001 Issued
Array ( [id] => 6313602 [patent_doc_number] => 20020194771 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2002-12-26 [patent_title] => 'MULTI-CARRIER PHEROMONE CARRYING SUBSTRATE DISPENSER, APPARATUS DISTRIBUTION SYSTEM' [patent_app_type] => new [patent_app_number] => 09/888877 [patent_app_country] => US [patent_app_date] => 2001-06-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 5245 [patent_no_of_claims] => 27 [patent_no_of_ind_claims] => 9 [patent_words_short_claim] => 44 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0194/20020194771.pdf [firstpage_image] =>[orig_patent_app_number] => 09888877 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/888877
Multi-carrier pheromone carrying substrate dispenser, apparatus distribution system Jun 22, 2001 Issued
Array ( [id] => 1544909 [patent_doc_number] => 06398158 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-06-04 [patent_title] => 'High altitude low flying platform hull' [patent_app_type] => B1 [patent_app_number] => 09/888416 [patent_app_country] => US [patent_app_date] => 2001-06-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 5113 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 159 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/398/06398158.pdf [firstpage_image] =>[orig_patent_app_number] => 09888416 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/888416
High altitude low flying platform hull Jun 21, 2001 Issued
Array ( [id] => 1591010 [patent_doc_number] => 06491254 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-12-10 [patent_title] => 'Environment control system for aircraft having interior condensation problem reduction, cabin air quality improvement, fire suppression and fire venting functions' [patent_app_type] => B1 [patent_app_number] => 09/857220 [patent_app_country] => US [patent_app_date] => 2001-06-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 14 [patent_figures_cnt] => 14 [patent_no_of_words] => 11264 [patent_no_of_claims] => 77 [patent_no_of_ind_claims] => 7 [patent_words_short_claim] => 104 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/491/06491254.pdf [firstpage_image] =>[orig_patent_app_number] => 09857220 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/857220
Environment control system for aircraft having interior condensation problem reduction, cabin air quality improvement, fire suppression and fire venting functions Jun 19, 2001 Issued
Array ( [id] => 1514371 [patent_doc_number] => 06499697 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-12-31 [patent_title] => 'Deployable flexible airlock' [patent_app_type] => B1 [patent_app_number] => 09/884401 [patent_app_country] => US [patent_app_date] => 2001-06-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 4 [patent_no_of_words] => 2005 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 5 [patent_words_short_claim] => 81 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/499/06499697.pdf [firstpage_image] =>[orig_patent_app_number] => 09884401 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/884401
Deployable flexible airlock Jun 17, 2001 Issued
Array ( [id] => 1503075 [patent_doc_number] => 06439504 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-08-27 [patent_title] => 'System and method for sustaining electric power during a momentary power interruption in an electric thrust reverser actuation system' [patent_app_type] => B1 [patent_app_number] => 09/882905 [patent_app_country] => US [patent_app_date] => 2001-06-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 4765 [patent_no_of_claims] => 38 [patent_no_of_ind_claims] => 6 [patent_words_short_claim] => 115 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/439/06439504.pdf [firstpage_image] =>[orig_patent_app_number] => 09882905 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/882905
System and method for sustaining electric power during a momentary power interruption in an electric thrust reverser actuation system Jun 14, 2001 Issued
Array ( [id] => 6137478 [patent_doc_number] => 20020000491 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2002-01-03 [patent_title] => 'Modular trim paneling and outfitting system for an aircraft passenger cabin interior' [patent_app_type] => new [patent_app_number] => 09/882877 [patent_app_country] => US [patent_app_date] => 2001-06-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 19 [patent_figures_cnt] => 19 [patent_no_of_words] => 8178 [patent_no_of_claims] => 28 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 139 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0000/20020000491.pdf [firstpage_image] =>[orig_patent_app_number] => 09882877 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/882877
Modular trim paneling and outfitting system for an aircraft passenger cabin interior Jun 14, 2001 Issued
Array ( [id] => 6491872 [patent_doc_number] => 20020190156 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2002-12-19 [patent_title] => 'Controlled spin projectile' [patent_app_type] => new [patent_app_number] => 09/881790 [patent_app_country] => US [patent_app_date] => 2001-06-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 14 [patent_figures_cnt] => 14 [patent_no_of_words] => 4704 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 52 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0190/20020190156.pdf [firstpage_image] =>[orig_patent_app_number] => 09881790 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/881790
Controlled spin projectile Jun 13, 2001 Issued
Array ( [id] => 6364994 [patent_doc_number] => 20020117585 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2002-08-29 [patent_title] => 'Apparatus for determining attitude of artificaial satellite' [patent_app_type] => new [patent_app_number] => 09/879918 [patent_app_country] => US [patent_app_date] => 2001-06-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 5169 [patent_no_of_claims] => 4 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 204 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0117/20020117585.pdf [firstpage_image] =>[orig_patent_app_number] => 09879918 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/879918
Apparatus for determining attitude of artificial satellite Jun 13, 2001 Issued
Array ( [id] => 1483880 [patent_doc_number] => 06427942 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2002-08-06 [patent_title] => 'Stiffness de-coupled skid landing gear' [patent_app_type] => B2 [patent_app_number] => 09/877428 [patent_app_country] => US [patent_app_date] => 2001-06-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 14 [patent_figures_cnt] => 29 [patent_no_of_words] => 11234 [patent_no_of_claims] => 64 [patent_no_of_ind_claims] => 18 [patent_words_short_claim] => 78 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/427/06427942.pdf [firstpage_image] =>[orig_patent_app_number] => 09877428 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/877428
Stiffness de-coupled skid landing gear Jun 7, 2001 Issued
Array ( [id] => 1531406 [patent_doc_number] => 06488239 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2002-12-03 [patent_title] => 'Aircraft control lever vernier' [patent_app_type] => B2 [patent_app_number] => 09/872371 [patent_app_country] => US [patent_app_date] => 2001-06-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 1744 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 62 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/488/06488239.pdf [firstpage_image] =>[orig_patent_app_number] => 09872371 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/872371
Aircraft control lever vernier May 31, 2001 Issued
Array ( [id] => 1499439 [patent_doc_number] => 06464166 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-10-15 [patent_title] => 'Ducted fan vehicles particularly useful as VTOL aircraft' [patent_app_type] => B1 [patent_app_number] => 09/865678 [patent_app_country] => US [patent_app_date] => 2001-05-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 16 [patent_no_of_words] => 3322 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 146 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/464/06464166.pdf [firstpage_image] =>[orig_patent_app_number] => 09865678 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/865678
Ducted fan vehicles particularly useful as VTOL aircraft May 28, 2001 Issued
Array ( [id] => 1508797 [patent_doc_number] => 06471160 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2002-10-29 [patent_title] => 'Method for deploying a parachute on a drone' [patent_app_type] => B2 [patent_app_number] => 09/865106 [patent_app_country] => US [patent_app_date] => 2001-05-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 1 [patent_no_of_words] => 2036 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 181 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/471/06471160.pdf [firstpage_image] =>[orig_patent_app_number] => 09865106 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/865106
Method for deploying a parachute on a drone May 23, 2001 Issued
Array ( [id] => 1449503 [patent_doc_number] => 06460801 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-10-08 [patent_title] => 'Precision guidance system for aircraft launched bombs' [patent_app_type] => B1 [patent_app_number] => 09/862843 [patent_app_country] => US [patent_app_date] => 2001-05-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 13 [patent_figures_cnt] => 18 [patent_no_of_words] => 3944 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 125 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/460/06460801.pdf [firstpage_image] =>[orig_patent_app_number] => 09862843 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/862843
Precision guidance system for aircraft launched bombs May 22, 2001 Issued
Array ( [id] => 5933175 [patent_doc_number] => 20020060269 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2002-05-23 [patent_title] => 'Lift-providing unit for levitating a platform' [patent_app_type] => new [patent_app_number] => 09/973679 [patent_app_country] => US [patent_app_date] => 2001-05-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 4222 [patent_no_of_claims] => 25 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 34 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0060/20020060269.pdf [firstpage_image] =>[orig_patent_app_number] => 09973679 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/973679
Lift-providing unit for levitating a platform May 22, 2001 Abandoned
Array ( [id] => 5948281 [patent_doc_number] => 20020005455 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2002-01-17 [patent_title] => 'Rotor control with negative collective in high speed auto-rotation' [patent_app_type] => new [patent_app_number] => 09/862566 [patent_app_country] => US [patent_app_date] => 2001-05-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 4093 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 97 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0005/20020005455.pdf [firstpage_image] =>[orig_patent_app_number] => 09862566 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/862566
Rotor control with negative collective in high speed auto-rotation May 21, 2001 Abandoned
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