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] => 992859
[patent_doc_number] => 06915984
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2005-07-12
[patent_title] => 'Apparatus and method for mounting a cascade support ring to a thrust reverser'
[patent_app_type] => utility
[patent_app_number] => 10/779184
[patent_app_country] => US
[patent_app_date] => 2004-02-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 2910
[patent_no_of_claims] => 30
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 61
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/915/06915984.pdf
[firstpage_image] =>[orig_patent_app_number] => 10779184
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/779184 | Apparatus and method for mounting a cascade support ring to a thrust reverser | Feb 12, 2004 | Issued |
Array
(
[id] => 7349672
[patent_doc_number] => 20040248497
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-12-09
[patent_title] => 'Pneumatically launched folding wing glider toy'
[patent_app_type] => new
[patent_app_number] => 10/776812
[patent_app_country] => US
[patent_app_date] => 2004-02-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 11
[patent_no_of_words] => 7802
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 51
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0248/20040248497.pdf
[firstpage_image] =>[orig_patent_app_number] => 10776812
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/776812 | Pneumatically launched folding wing glider toy | Feb 10, 2004 | Issued |
Array
(
[id] => 7190600
[patent_doc_number] => 20050040288
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-02-24
[patent_title] => 'Aircraft medical unit'
[patent_app_type] => utility
[patent_app_number] => 10/775827
[patent_app_country] => US
[patent_app_date] => 2004-02-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 6728
[patent_no_of_claims] => 27
[patent_no_of_ind_claims] => 2
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0040/20050040288.pdf
[firstpage_image] =>[orig_patent_app_number] => 10775827
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/775827 | Aircraft medical unit | Feb 9, 2004 | Abandoned |
Array
(
[id] => 313922
[patent_doc_number] => 07523888
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2009-04-28
[patent_title] => 'Seating system and a passenger accommodation unit for a vehicle'
[patent_app_type] => utility
[patent_app_number] => 10/774244
[patent_app_country] => US
[patent_app_date] => 2004-02-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 39
[patent_figures_cnt] => 48
[patent_no_of_words] => 31688
[patent_no_of_claims] => 45
[patent_no_of_ind_claims] => 6
[patent_words_short_claim] => 214
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/523/07523888.pdf
[firstpage_image] =>[orig_patent_app_number] => 10774244
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/774244 | Seating system and a passenger accommodation unit for a vehicle | Feb 5, 2004 | Issued |
Array
(
[id] => 618748
[patent_doc_number] => 07140576
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2006-11-28
[patent_title] => 'Inflatable wing with manifold'
[patent_app_type] => utility
[patent_app_number] => 10/773652
[patent_app_country] => US
[patent_app_date] => 2004-02-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 5
[patent_no_of_words] => 3503
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 112
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/140/07140576.pdf
[firstpage_image] =>[orig_patent_app_number] => 10773652
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/773652 | Inflatable wing with manifold | Feb 5, 2004 | Issued |
Array
(
[id] => 653573
[patent_doc_number] => 07108232
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2006-09-19
[patent_title] => 'Helicopter force-feel and stability augmentation system with parallel servo-actuator'
[patent_app_type] => utility
[patent_app_number] => 10/772990
[patent_app_country] => US
[patent_app_date] => 2004-02-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 6266
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 175
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/108/07108232.pdf
[firstpage_image] =>[orig_patent_app_number] => 10772990
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/772990 | Helicopter force-feel and stability augmentation system with parallel servo-actuator | Feb 4, 2004 | Issued |
Array
(
[id] => 287986
[patent_doc_number] => 07546982
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2009-06-16
[patent_title] => 'Shuttle thermal integrity detection system'
[patent_app_type] => utility
[patent_app_number] => 10/773511
[patent_app_country] => US
[patent_app_date] => 2004-02-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 3483
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 62
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/546/07546982.pdf
[firstpage_image] =>[orig_patent_app_number] => 10773511
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/773511 | Shuttle thermal integrity detection system | Feb 4, 2004 | Issued |
Array
(
[id] => 950696
[patent_doc_number] => 06959895
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2005-11-01
[patent_title] => 'Dual wing-pair air vehicle'
[patent_app_type] => utility
[patent_app_number] => 10/774653
[patent_app_country] => US
[patent_app_date] => 2004-02-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 10
[patent_no_of_words] => 4945
[patent_no_of_claims] => 37
[patent_no_of_ind_claims] => 6
[patent_words_short_claim] => 120
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/959/06959895.pdf
[firstpage_image] =>[orig_patent_app_number] => 10774653
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/774653 | Dual wing-pair air vehicle | Feb 3, 2004 | Issued |
Array
(
[id] => 667556
[patent_doc_number] => 07093791
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2006-08-22
[patent_title] => 'Aircraft spiralling mechanism—c'
[patent_app_type] => utility
[patent_app_number] => 10/762267
[patent_app_country] => US
[patent_app_date] => 2004-01-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 11
[patent_no_of_words] => 2917
[patent_no_of_claims] => 20
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/093/07093791.pdf
[firstpage_image] =>[orig_patent_app_number] => 10762267
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/762267 | Aircraft spiralling mechanism—c | Jan 22, 2004 | Issued |
Array
(
[id] => 733254
[patent_doc_number] => 07032861
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2006-04-25
[patent_title] => 'Quiet vertical takeoff and landing aircraft using ducted, magnetic induction air-impeller rotors'
[patent_app_type] => utility
[patent_app_number] => 10/763973
[patent_app_country] => US
[patent_app_date] => 2004-01-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 29
[patent_figures_cnt] => 94
[patent_no_of_words] => 10696
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 285
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/032/07032861.pdf
[firstpage_image] =>[orig_patent_app_number] => 10763973
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/763973 | Quiet vertical takeoff and landing aircraft using ducted, magnetic induction air-impeller rotors | Jan 21, 2004 | Issued |
Array
(
[id] => 7153979
[patent_doc_number] => 20050082433
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-04-21
[patent_title] => 'Cockpit door of aircraft'
[patent_app_type] => utility
[patent_app_number] => 10/759252
[patent_app_country] => US
[patent_app_date] => 2004-01-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 19
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[patent_no_of_words] => 2888
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0082/20050082433.pdf
[firstpage_image] =>[orig_patent_app_number] => 10759252
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/759252 | Cockpit door of aircraft | Jan 19, 2004 | Issued |
Array
(
[id] => 7218758
[patent_doc_number] => 20040155144
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-08-12
[patent_title] => 'Aircraft spiralling mechanism - B'
[patent_app_type] => new
[patent_app_number] => 10/759090
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[patent_effective_date] => 0000-00-00
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[pdf_file] => publications/A1/0155/20040155144.pdf
[firstpage_image] =>[orig_patent_app_number] => 10759090
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/759090 | Aircraft spiralling mechanism - B | Jan 19, 2004 | Issued |
Array
(
[id] => 481275
[patent_doc_number] => 07216581
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2007-05-15
[patent_title] => 'Piston locking actuator'
[patent_app_type] => utility
[patent_app_number] => 10/758887
[patent_app_country] => US
[patent_app_date] => 2004-01-16
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[pdf_file] => patents/07/216/07216581.pdf
[firstpage_image] =>[orig_patent_app_number] => 10758887
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/758887 | Piston locking actuator | Jan 15, 2004 | Issued |
Array
(
[id] => 1090165
[patent_doc_number] => 06824095
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-11-30
[patent_title] => 'VSTOL vehicle'
[patent_app_type] => B2
[patent_app_number] => 10/757482
[patent_app_country] => US
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/824/06824095.pdf
[firstpage_image] =>[orig_patent_app_number] => 10757482
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/757482 | VSTOL vehicle | Jan 14, 2004 | Issued |
Array
(
[id] => 535497
[patent_doc_number] => 07163176
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2007-01-16
[patent_title] => '2-D projectile trajectory correction system and method'
[patent_app_type] => utility
[patent_app_number] => 10/758522
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[pdf_file] => patents/07/163/07163176.pdf
[firstpage_image] =>[orig_patent_app_number] => 10758522
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/758522 | 2-D projectile trajectory correction system and method | Jan 14, 2004 | Issued |
Array
(
[id] => 745710
[patent_doc_number] => 07021587
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2006-04-04
[patent_title] => 'Dual channel fail-safe system and method for adjusting aircraft trim'
[patent_app_type] => utility
[patent_app_number] => 10/753884
[patent_app_country] => US
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/021/07021587.pdf
[firstpage_image] =>[orig_patent_app_number] => 10753884
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/753884 | Dual channel fail-safe system and method for adjusting aircraft trim | Jan 6, 2004 | Issued |
Array
(
[id] => 7114234
[patent_doc_number] => 20050067534
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-03-31
[patent_title] => 'Method and apparatus for supplying orbital space platforms using payload canisters via intermediate orbital rendezvous and docking'
[patent_app_type] => utility
[patent_app_number] => 10/748527
[patent_app_country] => US
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[pdf_file] => publications/A1/0067/20050067534.pdf
[firstpage_image] =>[orig_patent_app_number] => 10748527
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/748527 | Method and apparatus for supplying orbital space platforms using payload canisters via intermediate orbital rendezvous and docking | Dec 28, 2003 | Issued |
Array
(
[id] => 7362302
[patent_doc_number] => 20040217233
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-11-04
[patent_title] => 'Aerostat deployment apparatus'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 10/736932 | Aerostat deployment apparatus | Dec 15, 2003 | Issued |
Array
(
[id] => 7094461
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[patent_title] => 'Apparatus and method for aerodynamic wing'
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[firstpage_image] =>[orig_patent_app_number] => 10736925
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/736925 | Apparatus and method for aerodynamic wing | Dec 15, 2003 | Issued |
Array
(
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[patent_title] => 'Dynamic baselining in current modulation-based communication'
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[pdf_file] => publications/A1/0011/20050011389.pdf
[firstpage_image] =>[orig_patent_app_number] => 10736166
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/736166 | Dynamic baselining in current modulation-based communication | Dec 12, 2003 | Issued |