
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] => 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 |