Jean F Duverne
Examiner (ID: 1480, Phone: (571)272-2091 , Office: P/2833 )
Most Active Art Unit | 2833 |
Art Unit(s) | 2833, 2839 |
Total Applications | 3066 |
Issued Applications | 2687 |
Pending Applications | 115 |
Abandoned Applications | 263 |
Applications
Application number | Title of the application | Filing Date | Status |
---|---|---|---|
Array
(
[id] => 997875
[patent_doc_number] => 06910404
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2005-06-28
[patent_title] => 'Gun bolt locking mechanism'
[patent_app_type] => utility
[patent_app_number] => 10/436238
[patent_app_country] => US
[patent_app_date] => 2003-05-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 15
[patent_figures_cnt] => 18
[patent_no_of_words] => 5374
[patent_no_of_claims] => 29
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 108
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/910/06910404.pdf
[firstpage_image] =>[orig_patent_app_number] => 10436238
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/436238 | Gun bolt locking mechanism | May 12, 2003 | Issued |
Array
(
[id] => 6872694
[patent_doc_number] => 20030192991
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-10-16
[patent_title] => 'Switchable electrochromic devices for use in aircraft transparency windows'
[patent_app_type] => new
[patent_app_number] => 10/436214
[patent_app_country] => US
[patent_app_date] => 2003-05-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 8977
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 203
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0192/20030192991.pdf
[firstpage_image] =>[orig_patent_app_number] => 10436214
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/436214 | Switchable electrochromic devices for use in aircraft transparency windows | May 11, 2003 | Issued |
Array
(
[id] => 1086312
[patent_doc_number] => 06826864
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2004-12-07
[patent_title] => 'Forward mounting rails'
[patent_app_type] => B1
[patent_app_number] => 10/249702
[patent_app_country] => US
[patent_app_date] => 2003-05-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 860
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 131
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/826/06826864.pdf
[firstpage_image] =>[orig_patent_app_number] => 10249702
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/249702 | Forward mounting rails | Apr 30, 2003 | Issued |
Array
(
[id] => 7359556
[patent_doc_number] => 20040216634
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-11-04
[patent_title] => 'LOW SHOCK SEPARATION BOLT'
[patent_app_type] => new
[patent_app_number] => 10/426089
[patent_app_country] => US
[patent_app_date] => 2003-04-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2776
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 7
[patent_words_short_claim] => 3
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0216/20040216634.pdf
[firstpage_image] =>[orig_patent_app_number] => 10426089
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/426089 | Low shock separation bolt | Apr 28, 2003 | Issued |
Array
(
[id] => 5877767
[patent_doc_number] => 20060027700
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-02-09
[patent_title] => 'LIGHTNING STRIKE MITIGATION SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 10/424435
[patent_app_country] => US
[patent_app_date] => 2003-04-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 1994
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 7
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0027/20060027700.pdf
[firstpage_image] =>[orig_patent_app_number] => 10424435
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/424435 | Lightning strike mitigation system | Apr 27, 2003 | Issued |
Array
(
[id] => 7291493
[patent_doc_number] => 20040211864
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-10-28
[patent_title] => 'Efficient communications utilizing highly inclined, highly elliptic orbits'
[patent_app_type] => new
[patent_app_number] => 10/423749
[patent_app_country] => US
[patent_app_date] => 2003-04-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 12857
[patent_no_of_claims] => 30
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 87
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0211/20040211864.pdf
[firstpage_image] =>[orig_patent_app_number] => 10423749
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/423749 | Efficient communications utilizing highly inclined, highly elliptic orbits | Apr 24, 2003 | Abandoned |
Array
(
[id] => 7291489
[patent_doc_number] => 20040211862
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-10-28
[patent_title] => 'Unmanned aerial vehicle with integrated wing battery'
[patent_app_type] => new
[patent_app_number] => 10/423187
[patent_app_country] => US
[patent_app_date] => 2003-04-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 3025
[patent_no_of_claims] => 21
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 2
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0211/20040211862.pdf
[firstpage_image] =>[orig_patent_app_number] => 10423187
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/423187 | Unmanned aerial vehicle with integrated wing battery | Apr 24, 2003 | Abandoned |
Array
(
[id] => 1102298
[patent_doc_number] => 06811120
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2004-11-02
[patent_title] => 'Modular spar tunnel'
[patent_app_type] => B1
[patent_app_number] => 10/414390
[patent_app_country] => US
[patent_app_date] => 2003-04-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 1493
[patent_no_of_claims] => 5
[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/06/811/06811120.pdf
[firstpage_image] =>[orig_patent_app_number] => 10414390
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/414390 | Modular spar tunnel | Apr 14, 2003 | Issued |
Array
(
[id] => 7381647
[patent_doc_number] => 20040020394
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-02-05
[patent_title] => 'Ordnance firing system'
[patent_app_type] => new
[patent_app_number] => 10/413771
[patent_app_country] => US
[patent_app_date] => 2003-04-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 10374
[patent_no_of_claims] => 22
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 25
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0020/20040020394.pdf
[firstpage_image] =>[orig_patent_app_number] => 10413771
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/413771 | Ordnance firing system | Apr 14, 2003 | Issued |
Array
(
[id] => 6767934
[patent_doc_number] => 20030213874
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-11-20
[patent_title] => 'Combined propulsion system intended for a spacecraft'
[patent_app_type] => new
[patent_app_number] => 10/389990
[patent_app_country] => US
[patent_app_date] => 2003-03-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 2635
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 117
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0213/20030213874.pdf
[firstpage_image] =>[orig_patent_app_number] => 10389990
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/389990 | Combined propulsion system intended for a spacecraft | Mar 17, 2003 | Issued |
Array
(
[id] => 7173418
[patent_doc_number] => 20040200925
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-10-14
[patent_title] => 'Cavitating oil hyperspace energy generator'
[patent_app_type] => new
[patent_app_number] => 10/372557
[patent_app_country] => US
[patent_app_date] => 2003-02-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 25
[patent_figures_cnt] => 25
[patent_no_of_words] => 6483
[patent_no_of_claims] => 3
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 40
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0200/20040200925.pdf
[firstpage_image] =>[orig_patent_app_number] => 10372557
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/372557 | Cavitating oil hyperspace energy generator | Feb 20, 2003 | Abandoned |
Array
(
[id] => 1041794
[patent_doc_number] => 06865978
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2005-03-15
[patent_title] => 'Well perforating gun'
[patent_app_type] => utility
[patent_app_number] => 10/370142
[patent_app_country] => US
[patent_app_date] => 2003-02-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 20
[patent_figures_cnt] => 27
[patent_no_of_words] => 7908
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 75
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/865/06865978.pdf
[firstpage_image] =>[orig_patent_app_number] => 10370142
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/370142 | Well perforating gun | Feb 17, 2003 | Issued |
Array
(
[id] => 7379963
[patent_doc_number] => 20040020092
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-02-05
[patent_title] => 'Firearm with fixed cartridge magazine top'
[patent_app_type] => new
[patent_app_number] => 10/358418
[patent_app_country] => US
[patent_app_date] => 2003-02-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
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[patent_no_of_words] => 7204
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0020/20040020092.pdf
[firstpage_image] =>[orig_patent_app_number] => 10358418
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/358418 | Firearm with fixed cartridge magazine top | Feb 3, 2003 | Issued |
Array
(
[id] => 6704226
[patent_doc_number] => 20030150960
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-08-14
[patent_title] => 'Spacecraft methods and structures with beacon-receiving field-of-view matched to beacon station window'
[patent_app_type] => new
[patent_app_number] => 10/356032
[patent_app_country] => US
[patent_app_date] => 2003-01-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_no_of_words] => 3908
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0150/20030150960.pdf
[firstpage_image] =>[orig_patent_app_number] => 10356032
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/356032 | Spacecraft methods and structures with beacon-receiving field-of-view matched to beacon station window | Jan 29, 2003 | Issued |
Array
(
[id] => 6698471
[patent_doc_number] => 20030221351
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-12-04
[patent_title] => 'FIREARM SAFETY DEVICE'
[patent_app_type] => new
[patent_app_number] => 10/248533
[patent_app_country] => US
[patent_app_date] => 2003-01-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0221/20030221351.pdf
[firstpage_image] =>[orig_patent_app_number] => 10248533
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/248533 | Firearm safety device | Jan 26, 2003 | Issued |
Array
(
[id] => 1156872
[patent_doc_number] => 06755374
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2004-06-29
[patent_title] => 'Anti-Torque and yaw-control system for a rotary-wing aircraft'
[patent_app_type] => B1
[patent_app_number] => 10/353162
[patent_app_country] => US
[patent_app_date] => 2003-01-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
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[patent_no_of_claims] => 37
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/755/06755374.pdf
[firstpage_image] =>[orig_patent_app_number] => 10353162
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/353162 | Anti-Torque and yaw-control system for a rotary-wing aircraft | Jan 26, 2003 | Issued |
Array
(
[id] => 1144335
[patent_doc_number] => 06766744
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2004-07-27
[patent_title] => 'Incendiary device'
[patent_app_type] => B1
[patent_app_number] => 10/341924
[patent_app_country] => US
[patent_app_date] => 2003-01-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/766/06766744.pdf
[firstpage_image] =>[orig_patent_app_number] => 10341924
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/341924 | Incendiary device | Jan 13, 2003 | Issued |
Array
(
[id] => 7295621
[patent_doc_number] => 20040124311
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-07-01
[patent_title] => 'Structural attach method for thin fairings'
[patent_app_type] => new
[patent_app_number] => 10/334452
[patent_app_country] => US
[patent_app_date] => 2002-12-31
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0124/20040124311.pdf
[firstpage_image] =>[orig_patent_app_number] => 10334452
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/334452 | Structural attach method for thin fairings | Dec 30, 2002 | Issued |
Array
(
[id] => 1029579
[patent_doc_number] => 06877695
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2005-04-12
[patent_title] => 'Hinge cover integration into door seal edges'
[patent_app_type] => utility
[patent_app_number] => 10/318439
[patent_app_country] => US
[patent_app_date] => 2002-12-13
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/877/06877695.pdf
[firstpage_image] =>[orig_patent_app_number] => 10318439
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/318439 | Hinge cover integration into door seal edges | Dec 12, 2002 | Issued |
Array
(
[id] => 1128492
[patent_doc_number] => 06782650
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-08-31
[patent_title] => 'Nodular nickel boron coating'
[patent_app_type] => B2
[patent_app_number] => 10/316108
[patent_app_country] => US
[patent_app_date] => 2002-12-11
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/782/06782650.pdf
[firstpage_image] =>[orig_patent_app_number] => 10316108
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/316108 | Nodular nickel boron coating | Dec 10, 2002 | Issued |