Edwin L Swinehart
Examiner (ID: 13684, Phone: (571)272-6688 , Office: P/3617 )
Most Active Art Unit | 3617 |
Art Unit(s) | 3617, 3612, 3105, 3102, 2899 |
Total Applications | 3741 |
Issued Applications | 2973 |
Pending Applications | 88 |
Abandoned Applications | 680 |
Applications
Application number | Title of the application | Filing Date | Status |
---|---|---|---|
Array
(
[id] => 7444263
[patent_doc_number] => 20040050997
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-03-18
[patent_title] => 'Apparatus and method for selectively locking a fin assembly'
[patent_app_type] => new
[patent_app_number] => 10/244323
[patent_app_country] => US
[patent_app_date] => 2002-09-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 2532
[patent_no_of_claims] => 44
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 29
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0050/20040050997.pdf
[firstpage_image] =>[orig_patent_app_number] => 10244323
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/244323 | Apparatus and method for selectivity locking a fin assembly | Sep 15, 2002 | Issued |
Array
(
[id] => 1019510
[patent_doc_number] => 06886776
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2005-05-03
[patent_title] => 'VTOL personal aircraft'
[patent_app_type] => utility
[patent_app_number] => 10/242036
[patent_app_country] => US
[patent_app_date] => 2002-09-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 25
[patent_figures_cnt] => 37
[patent_no_of_words] => 14769
[patent_no_of_claims] => 62
[patent_no_of_ind_claims] => 7
[patent_words_short_claim] => 184
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/886/06886776.pdf
[firstpage_image] =>[orig_patent_app_number] => 10242036
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/242036 | VTOL personal aircraft | Sep 10, 2002 | Issued |
Array
(
[id] => 1253771
[patent_doc_number] => 06666402
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2003-12-23
[patent_title] => '2-D projectile trajectory corrector'
[patent_app_type] => B2
[patent_app_number] => 10/237503
[patent_app_country] => US
[patent_app_date] => 2002-09-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 12
[patent_no_of_words] => 5369
[patent_no_of_claims] => 26
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 100
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/666/06666402.pdf
[firstpage_image] =>[orig_patent_app_number] => 10237503
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/237503 | 2-D projectile trajectory corrector | Sep 8, 2002 | Issued |
Array
(
[id] => 6747247
[patent_doc_number] => 20030041767
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-03-06
[patent_title] => 'Power supplies for projectiles and other devices'
[patent_app_type] => new
[patent_app_number] => 10/235997
[patent_app_country] => US
[patent_app_date] => 2002-09-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 7263
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 36
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0041/20030041767.pdf
[firstpage_image] =>[orig_patent_app_number] => 10235997
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/235997 | Power supplies for projectiles and other devices | Sep 4, 2002 | Issued |
Array
(
[id] => 977567
[patent_doc_number] => 06929215
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2005-08-16
[patent_title] => 'Rotor system for helicopters'
[patent_app_type] => utility
[patent_app_number] => 10/488317
[patent_app_country] => US
[patent_app_date] => 2002-09-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 19
[patent_figures_cnt] => 19
[patent_no_of_words] => 5419
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 7
[patent_words_short_claim] => 110
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/929/06929215.pdf
[firstpage_image] =>[orig_patent_app_number] => 10488317
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/488317 | Rotor system for helicopters | Sep 3, 2002 | Issued |
Array
(
[id] => 7130030
[patent_doc_number] => 20040041059
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-03-04
[patent_title] => 'Device for projectile control'
[patent_app_type] => new
[patent_app_number] => 10/235019
[patent_app_country] => US
[patent_app_date] => 2002-09-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 1726
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 88
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0041/20040041059.pdf
[firstpage_image] =>[orig_patent_app_number] => 10235019
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/235019 | Device for projectile control | Sep 2, 2002 | Abandoned |
Array
(
[id] => 960610
[patent_doc_number] => 06951322
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2005-10-04
[patent_title] => 'Personal aircraft device'
[patent_app_type] => utility
[patent_app_number] => 10/227528
[patent_app_country] => US
[patent_app_date] => 2002-08-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 15
[patent_figures_cnt] => 43
[patent_no_of_words] => 11373
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 163
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/951/06951322.pdf
[firstpage_image] =>[orig_patent_app_number] => 10227528
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/227528 | Personal aircraft device | Aug 25, 2002 | Issued |
Array
(
[id] => 6680812
[patent_doc_number] => 20030116676
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-06-26
[patent_title] => 'STEERABLE POWER TUG FOR SMALL AIRCRAFT'
[patent_app_type] => new
[patent_app_number] => 10/226574
[patent_app_country] => US
[patent_app_date] => 2002-08-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 20
[patent_figures_cnt] => 20
[patent_no_of_words] => 3432
[patent_no_of_claims] => 24
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 141
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0116/20030116676.pdf
[firstpage_image] =>[orig_patent_app_number] => 10226574
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/226574 | Steerable power tug for small aircraft | Aug 22, 2002 | Issued |
Array
(
[id] => 1388226
[patent_doc_number] => 06527223
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2003-03-04
[patent_title] => 'Platform-type airship'
[patent_app_type] => B1
[patent_app_number] => 10/212632
[patent_app_country] => US
[patent_app_date] => 2002-08-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 4848
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 259
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/527/06527223.pdf
[firstpage_image] =>[orig_patent_app_number] => 10212632
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/212632 | Platform-type airship | Aug 4, 2002 | Issued |
Array
(
[id] => 6316449
[patent_doc_number] => 20020195518
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-12-26
[patent_title] => 'Combination fixed and rotating wing aircraft and land vehicle'
[patent_app_type] => new
[patent_app_number] => 10/208076
[patent_app_country] => US
[patent_app_date] => 2002-07-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 1580
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 115
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0195/20020195518.pdf
[firstpage_image] =>[orig_patent_app_number] => 10208076
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/208076 | Combination fixed and rotating wing aircraft and land vehicle | Jul 28, 2002 | Abandoned |
Array
(
[id] => 7403141
[patent_doc_number] => 20040262455
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-12-30
[patent_title] => 'FUEL INERTING SYSTEM'
[patent_app_type] => new
[patent_app_number] => 10/182277
[patent_app_country] => US
[patent_app_date] => 2002-07-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
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[patent_no_of_words] => 1795
[patent_no_of_claims] => 12
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0262/20040262455.pdf
[firstpage_image] =>[orig_patent_app_number] => 10182277
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/182277 | Fuel inerting system | Jul 25, 2002 | Issued |
Array
(
[id] => 1231525
[patent_doc_number] => 06688553
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-02-10
[patent_title] => 'Inflatable airfoils, and elevated and propulsion driven vehicles'
[patent_app_type] => B2
[patent_app_number] => 10/200348
[patent_app_country] => US
[patent_app_date] => 2002-07-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 37
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[pdf_file] => patents/06/688/06688553.pdf
[firstpage_image] =>[orig_patent_app_number] => 10200348
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/200348 | Inflatable airfoils, and elevated and propulsion driven vehicles | Jul 22, 2002 | Issued |
Array
(
[id] => 6854066
[patent_doc_number] => 20030127567
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-07-10
[patent_title] => 'Inflatable airfoils, and elevated and propulsion driven vehicles'
[patent_app_type] => new
[patent_app_number] => 10/200456
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[pdf_file] => publications/A1/0127/20030127567.pdf
[firstpage_image] =>[orig_patent_app_number] => 10200456
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/200456 | Inflatable airfoils, and elevated and propulsion driven vehicles | Jul 22, 2002 | Issued |
Array
(
[id] => 7347780
[patent_doc_number] => 20040011918
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-01-22
[patent_title] => 'Aviation ground power unit connection system and method incorporating same'
[patent_app_type] => new
[patent_app_number] => 10/199657
[patent_app_country] => US
[patent_app_date] => 2002-07-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_no_of_words] => 1719
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0011/20040011918.pdf
[firstpage_image] =>[orig_patent_app_number] => 10199657
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/199657 | Aviation ground power unit connection system and method incorporating same | Jul 18, 2002 | Issued |
Array
(
[id] => 1260584
[patent_doc_number] => 06659395
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2003-12-09
[patent_title] => 'Propellers and propeller related vehicles'
[patent_app_type] => B2
[patent_app_number] => 10/189681
[patent_app_country] => US
[patent_app_date] => 2002-07-08
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[pdf_file] => patents/06/659/06659395.pdf
[firstpage_image] =>[orig_patent_app_number] => 10189681
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/189681 | Propellers and propeller related vehicles | Jul 7, 2002 | Issued |
Array
(
[id] => 1051845
[patent_doc_number] => 06857601
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2005-02-22
[patent_title] => 'Airship system'
[patent_app_type] => utility
[patent_app_number] => 10/189796
[patent_app_country] => US
[patent_app_date] => 2002-07-03
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/857/06857601.pdf
[firstpage_image] =>[orig_patent_app_number] => 10189796
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/189796 | Airship system | Jul 2, 2002 | Issued |
Array
(
[id] => 1132349
[patent_doc_number] => 06779456
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-08-24
[patent_title] => 'Initiator with a bridgewire configured in an enhanced heat-sinking relationship'
[patent_app_type] => B2
[patent_app_number] => 10/188010
[patent_app_country] => US
[patent_app_date] => 2002-07-01
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/779/06779456.pdf
[firstpage_image] =>[orig_patent_app_number] => 10188010
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/188010 | Initiator with a bridgewire configured in an enhanced heat-sinking relationship | Jun 30, 2002 | Issued |
Array
(
[id] => 6491878
[patent_doc_number] => 20020190157
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-12-19
[patent_title] => 'Small-sized radio-controlled flying device'
[patent_app_type] => new
[patent_app_number] => 10/168588
[patent_app_country] => US
[patent_app_date] => 2002-06-24
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[pdf_file] => publications/A1/0190/20020190157.pdf
[firstpage_image] =>[orig_patent_app_number] => 10168588
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/168588 | Small-sized radio-controlled flying device | Jun 23, 2002 | Issued |
Array
(
[id] => 6738100
[patent_doc_number] => 20030155468
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-08-21
[patent_title] => 'Constellation of spacecraft, and broadcasting method using said constellation'
[patent_app_type] => new
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[patent_app_date] => 2002-06-21
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[pdf_file] => publications/A1/0155/20030155468.pdf
[firstpage_image] =>[orig_patent_app_number] => 10176936
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/176936 | Constellation of spacecraft, and broadcasting method using said constellation | Jun 20, 2002 | Issued |
Array
(
[id] => 6316458
[patent_doc_number] => 20020195521
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-12-26
[patent_title] => 'Aeroplane spiralling mechanism - 2'
[patent_app_type] => new
[patent_app_number] => 10/173634
[patent_app_country] => US
[patent_app_date] => 2002-06-19
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0195/20020195521.pdf
[firstpage_image] =>[orig_patent_app_number] => 10173634
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/173634 | Aeroplane spiralling mechanism - 2 | Jun 18, 2002 | Abandoned |