
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] => 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
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[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
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[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
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[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
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[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
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[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'
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[patent_app_number] => 10/304236
[patent_app_country] => US
[patent_app_date] => 2002-11-25
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[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
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[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
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[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
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[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
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[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'
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[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
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[patent_kind] => B2
[patent_issue_date] => 2005-02-15
[patent_title] => 'Solid oxide regenerative fuel cell for airplane power generation and storage'
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[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
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[patent_kind] => B2
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[patent_title] => 'Pressure rate of change sensitive latching method and apparatus'
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[patent_app_number] => 10/300681
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[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 |