
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] => 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
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[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
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[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
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[patent_no_of_words] => 2544
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[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
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[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
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[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
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[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
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[patent_no_of_words] => 2005
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[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
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[patent_no_of_words] => 4765
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[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
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[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
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[rel_patent_id] =>[rel_patent_doc_number] =>) 09/881790 | Controlled spin projectile | Jun 13, 2001 | Issued |
Array
(
[id] => 6364994
[patent_doc_number] => 20020117585
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[patent_title] => 'Apparatus for determining attitude of artificaial satellite'
[patent_app_type] => new
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[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
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[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
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[patent_title] => 'Aircraft control lever vernier'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 09/872371 | Aircraft control lever vernier | May 31, 2001 | Issued |
Array
(
[id] => 1499439
[patent_doc_number] => 06464166
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[patent_title] => 'Ducted fan vehicles particularly useful as VTOL aircraft'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 09/865678 | Ducted fan vehicles particularly useful as VTOL aircraft | May 28, 2001 | Issued |
Array
(
[id] => 1508797
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[patent_issue_date] => 2002-10-29
[patent_title] => 'Method for deploying a parachute on a drone'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 09/865106 | Method for deploying a parachute on a drone | May 23, 2001 | Issued |
Array
(
[id] => 1449503
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[patent_title] => 'Precision guidance system for aircraft launched bombs'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 09/862843 | Precision guidance system for aircraft launched bombs | May 22, 2001 | Issued |
Array
(
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Array
(
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[patent_title] => 'Rotor control with negative collective in high speed auto-rotation'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 09/862566 | Rotor control with negative collective in high speed auto-rotation | May 21, 2001 | Abandoned |