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] => 1251536
[patent_doc_number] => 06669148
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2003-12-30
[patent_title] => 'Method and apparatus for supplying orbital space platforms using payload canisters via intermediate orbital rendezvous and docking'
[patent_app_type] => B2
[patent_app_number] => 10/093971
[patent_app_country] => US
[patent_app_date] => 2002-03-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
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[patent_no_of_words] => 5214
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/669/06669148.pdf
[firstpage_image] =>[orig_patent_app_number] => 10093971
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/093971 | Method and apparatus for supplying orbital space platforms using payload canisters via intermediate orbital rendezvous and docking | Mar 6, 2002 | Issued |
Array
(
[id] => 6708807
[patent_doc_number] => 20030168556
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-09-11
[patent_title] => 'Variable area wing aircraft and method'
[patent_app_type] => new
[patent_app_number] => 10/090616
[patent_app_country] => US
[patent_app_date] => 2002-03-06
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0168/20030168556.pdf
[firstpage_image] =>[orig_patent_app_number] => 10090616
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/090616 | Variable area wing aircraft and method | Mar 5, 2002 | Issued |
Array
(
[id] => 1126565
[patent_doc_number] => 06786450
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2004-09-07
[patent_title] => 'Rapidly-convertible roadable aircraft'
[patent_app_type] => B1
[patent_app_number] => 10/082994
[patent_app_country] => US
[patent_app_date] => 2002-02-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
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[patent_no_of_words] => 3638
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[pdf_file] => patents/06/786/06786450.pdf
[firstpage_image] =>[orig_patent_app_number] => 10082994
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/082994 | Rapidly-convertible roadable aircraft | Feb 25, 2002 | Issued |
Array
(
[id] => 1347523
[patent_doc_number] => 06564691
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2003-05-20
[patent_title] => 'Semi-automatic gas-operated shotgun'
[patent_app_type] => B2
[patent_app_number] => 10/071140
[patent_app_country] => US
[patent_app_date] => 2002-02-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 18
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[patent_no_of_words] => 5339
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[pdf_file] => patents/06/564/06564691.pdf
[firstpage_image] =>[orig_patent_app_number] => 10071140
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/071140 | Semi-automatic gas-operated shotgun | Feb 5, 2002 | Issued |
Array
(
[id] => 6785638
[patent_doc_number] => 20030136877
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-07-24
[patent_title] => 'Aircraft with means for at least reducing impact against a ground'
[patent_app_type] => new
[patent_app_number] => 10/054191
[patent_app_country] => US
[patent_app_date] => 2002-01-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_no_of_words] => 1041
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[pdf_file] => publications/A1/0136/20030136877.pdf
[firstpage_image] =>[orig_patent_app_number] => 10054191
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/054191 | Aircraft with means for at least reducing impact against a ground | Jan 23, 2002 | Abandoned |
Array
(
[id] => 1316072
[patent_doc_number] => 06601796
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2003-08-05
[patent_title] => 'Device for attachment of an engine onto an aircraft nacelle stub'
[patent_app_type] => B2
[patent_app_number] => 10/052439
[patent_app_country] => US
[patent_app_date] => 2002-01-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[patent_no_of_words] => 3454
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[pdf_file] => patents/06/601/06601796.pdf
[firstpage_image] =>[orig_patent_app_number] => 10052439
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/052439 | Device for attachment of an engine onto an aircraft nacelle stub | Jan 22, 2002 | Issued |
Array
(
[id] => 1403695
[patent_doc_number] => 06508437
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2003-01-21
[patent_title] => 'Launch lock for spacecraft payloads'
[patent_app_type] => B1
[patent_app_number] => 10/050066
[patent_app_country] => US
[patent_app_date] => 2002-01-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
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[patent_no_of_words] => 1123
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/508/06508437.pdf
[firstpage_image] =>[orig_patent_app_number] => 10050066
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/050066 | Launch lock for spacecraft payloads | Jan 14, 2002 | Issued |
Array
(
[id] => 1296839
[patent_doc_number] => 06619588
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2003-09-16
[patent_title] => 'Installation of single passenger interface unit and method thereof'
[patent_app_type] => B2
[patent_app_number] => 10/047746
[patent_app_country] => US
[patent_app_date] => 2002-01-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_no_of_words] => 1932
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/619/06619588.pdf
[firstpage_image] =>[orig_patent_app_number] => 10047746
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/047746 | Installation of single passenger interface unit and method thereof | Jan 13, 2002 | Issued |
Array
(
[id] => 1281014
[patent_doc_number] => 06634601
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2003-10-21
[patent_title] => 'Attitude sensor for spacecraft'
[patent_app_type] => B2
[patent_app_number] => 10/044145
[patent_app_country] => US
[patent_app_date] => 2002-01-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
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[pdf_file] => patents/06/634/06634601.pdf
[firstpage_image] =>[orig_patent_app_number] => 10044145
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/044145 | Attitude sensor for spacecraft | Jan 10, 2002 | Issued |
Array
(
[id] => 6520655
[patent_doc_number] => 20020109047
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-08-15
[patent_title] => 'De-orbit instrument package'
[patent_app_type] => new
[patent_app_number] => 10/022858
[patent_app_country] => US
[patent_app_date] => 2001-12-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_no_of_words] => 3022
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[pdf_file] => publications/A1/0109/20020109047.pdf
[firstpage_image] =>[orig_patent_app_number] => 10022858
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/022858 | De-orbit instrument package | Dec 19, 2001 | Abandoned |
Array
(
[id] => 1224651
[patent_doc_number] => 06695262
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-02-24
[patent_title] => 'Spacecraft methods and structures for enhanced service-attitude accuracy'
[patent_app_type] => B2
[patent_app_number] => 10/013137
[patent_app_country] => US
[patent_app_date] => 2001-12-07
[patent_effective_date] => 0000-00-00
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[pdf_file] => patents/06/695/06695262.pdf
[firstpage_image] =>[orig_patent_app_number] => 10013137
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/013137 | Spacecraft methods and structures for enhanced service-attitude accuracy | Dec 6, 2001 | Issued |
Array
(
[id] => 1410862
[patent_doc_number] => 06502790
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2003-01-07
[patent_title] => 'Inclined non-uniform planar spaced constellation of satellites'
[patent_app_type] => B1
[patent_app_number] => 09/988781
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[pdf_file] => patents/06/502/06502790.pdf
[firstpage_image] =>[orig_patent_app_number] => 09988781
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/988781 | Inclined non-uniform planar spaced constellation of satellites | Nov 19, 2001 | Issued |
Array
(
[id] => 6858816
[patent_doc_number] => 20030089824
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-05-15
[patent_title] => 'ACOUSTIC TREATED THRUST REVERSER BULLNOSE FAIRING ASSEMBLY'
[patent_app_type] => new
[patent_app_number] => 10/035964
[patent_app_country] => US
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[pdf_file] => publications/A1/0089/20030089824.pdf
[firstpage_image] =>[orig_patent_app_number] => 10035964
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/035964 | Acoustic treated thrust reverser bullnose fairing assembly | Nov 8, 2001 | Issued |
Array
(
[id] => 1233898
[patent_doc_number] => 06684547
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-02-03
[patent_title] => 'Firearm recoil dampening assembly'
[patent_app_type] => B2
[patent_app_number] => 10/001042
[patent_app_country] => US
[patent_app_date] => 2001-10-31
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[pdf_file] => patents/06/684/06684547.pdf
[firstpage_image] =>[orig_patent_app_number] => 10001042
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/001042 | Firearm recoil dampening assembly | Oct 30, 2001 | Issued |
Array
(
[id] => 1344062
[patent_doc_number] => 06568310
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2003-05-27
[patent_title] => 'Lightweight armored panels and doors'
[patent_app_type] => B2
[patent_app_number] => 10/002584
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[pdf_file] => patents/06/568/06568310.pdf
[firstpage_image] =>[orig_patent_app_number] => 10002584
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/002584 | Lightweight armored panels and doors | Oct 24, 2001 | Issued |
Array
(
[id] => 1393896
[patent_doc_number] => 06510641
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2003-01-28
[patent_title] => 'Trigger and firing pin locking system'
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[pdf_file] => patents/06/510/06510641.pdf
[firstpage_image] =>[orig_patent_app_number] => 09978712
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/978712 | Trigger and firing pin locking system | Oct 15, 2001 | Issued |
Array
(
[id] => 1495641
[patent_doc_number] => 06484618
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-11-26
[patent_title] => 'Marine countermeasures launch assembly'
[patent_app_type] => B1
[patent_app_number] => 09/968387
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[pdf_file] => patents/06/484/06484618.pdf
[firstpage_image] =>[orig_patent_app_number] => 09968387
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/968387 | Marine countermeasures launch assembly | Sep 30, 2001 | Issued |
Array
(
[id] => 1271340
[patent_doc_number] => 06644590
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[patent_issue_date] => 2003-11-11
[patent_title] => 'Active system and method for vibration and noise reduction'
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Array
(
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[patent_title] => 'SLING ATTACHMENT HARDWARE FOR FIREARMS'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 09/950994 | Sling attachment hardware for firearms | Sep 12, 2001 | Issued |
Array
(
[id] => 6776023
[patent_doc_number] => 20030047103
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[patent_title] => 'Externally accessible thermal ground plane for tactical missiles'
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[pdf_file] => publications/A1/0047/20030047103.pdf
[firstpage_image] =>[orig_patent_app_number] => 09950893
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/950893 | Externally accessible thermal ground plane for tactical missiles | Sep 9, 2001 | Issued |