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] => 5745555
[patent_doc_number] => 20060108479
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-05-25
[patent_title] => 'Winged spacecraft'
[patent_app_type] => utility
[patent_app_number] => 10/515777
[patent_app_country] => US
[patent_app_date] => 2004-03-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 1198
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0108/20060108479.pdf
[firstpage_image] =>[orig_patent_app_number] => 10515777
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/515777 | Winged spacecraft | Mar 28, 2004 | Issued |
Array
(
[id] => 858697
[patent_doc_number] => 07370832
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2008-05-13
[patent_title] => 'Payload to support track interface and fitting apparatus and methods'
[patent_app_type] => utility
[patent_app_number] => 10/811522
[patent_app_country] => US
[patent_app_date] => 2004-03-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 27
[patent_no_of_words] => 5880
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 286
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/370/07370832.pdf
[firstpage_image] =>[orig_patent_app_number] => 10811522
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/811522 | Payload to support track interface and fitting apparatus and methods | Mar 28, 2004 | Issued |
Array
(
[id] => 434726
[patent_doc_number] => 07261256
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2007-08-28
[patent_title] => 'Variable-duct support assembly'
[patent_app_type] => utility
[patent_app_number] => 10/708864
[patent_app_country] => US
[patent_app_date] => 2004-03-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 15
[patent_no_of_words] => 3195
[patent_no_of_claims] => 22
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 135
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/261/07261256.pdf
[firstpage_image] =>[orig_patent_app_number] => 10708864
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/708864 | Variable-duct support assembly | Mar 28, 2004 | Issued |
Array
(
[id] => 532776
[patent_doc_number] => 07165745
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2007-01-23
[patent_title] => 'Methods and apparatuses for launching unmanned aircraft, including releasably gripping aircraft during launch and braking subsequent grip motion'
[patent_app_type] => utility
[patent_app_number] => 10/808725
[patent_app_country] => US
[patent_app_date] => 2004-03-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 15
[patent_no_of_words] => 6907
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 144
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/165/07165745.pdf
[firstpage_image] =>[orig_patent_app_number] => 10808725
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/808725 | Methods and apparatuses for launching unmanned aircraft, including releasably gripping aircraft during launch and braking subsequent grip motion | Mar 23, 2004 | Issued |
Array
(
[id] => 656306
[patent_doc_number] => 07104507
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2006-09-12
[patent_title] => 'Very safe manned rocket and method of entertaining'
[patent_app_type] => utility
[patent_app_number] => 10/801829
[patent_app_country] => US
[patent_app_date] => 2004-03-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 11
[patent_no_of_words] => 16786
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 142
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/104/07104507.pdf
[firstpage_image] =>[orig_patent_app_number] => 10801829
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/801829 | Very safe manned rocket and method of entertaining | Mar 16, 2004 | Issued |
Array
(
[id] => 647510
[patent_doc_number] => 07114684
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2006-10-03
[patent_title] => 'Method, apparatus, and computer program product for safe exit maneuver from dimensionally extended rotating space vehicle'
[patent_app_type] => utility
[patent_app_number] => 10/802021
[patent_app_country] => US
[patent_app_date] => 2004-03-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 7163
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 206
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/114/07114684.pdf
[firstpage_image] =>[orig_patent_app_number] => 10802021
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/802021 | Method, apparatus, and computer program product for safe exit maneuver from dimensionally extended rotating space vehicle | Mar 15, 2004 | Issued |
Array
(
[id] => 7264869
[patent_doc_number] => 20040242405
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-12-02
[patent_title] => 'Construction methods in space'
[patent_app_type] => new
[patent_app_number] => 10/489638
[patent_app_country] => US
[patent_app_date] => 2004-03-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 28326
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 20
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0242/20040242405.pdf
[firstpage_image] =>[orig_patent_app_number] => 10489638
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/489638 | Construction methods in space | Mar 15, 2004 | Abandoned |
Array
(
[id] => 446977
[patent_doc_number] => 07249734
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2007-07-31
[patent_title] => 'Aerodynamic vehicle having a variable geometry, co-planar, joined wing'
[patent_app_type] => utility
[patent_app_number] => 10/801750
[patent_app_country] => US
[patent_app_date] => 2004-03-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 5
[patent_no_of_words] => 4021
[patent_no_of_claims] => 30
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 129
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/249/07249734.pdf
[firstpage_image] =>[orig_patent_app_number] => 10801750
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/801750 | Aerodynamic vehicle having a variable geometry, co-planar, joined wing | Mar 15, 2004 | Issued |
Array
(
[id] => 6949542
[patent_doc_number] => 20050224636
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-10-13
[patent_title] => 'Animal-scaring device and method of employing same'
[patent_app_type] => utility
[patent_app_number] => 10/799804
[patent_app_country] => US
[patent_app_date] => 2004-03-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 1849
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0224/20050224636.pdf
[firstpage_image] =>[orig_patent_app_number] => 10799804
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/799804 | Animal-scaring device and method of employing same | Mar 11, 2004 | Issued |
Array
(
[id] => 1039323
[patent_doc_number] => 06869045
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2005-03-22
[patent_title] => 'Helicopter tail section and retrofit method'
[patent_app_type] => utility
[patent_app_number] => 10/799508
[patent_app_country] => US
[patent_app_date] => 2004-03-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 8
[patent_no_of_words] => 2074
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 177
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/869/06869045.pdf
[firstpage_image] =>[orig_patent_app_number] => 10799508
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/799508 | Helicopter tail section and retrofit method | Mar 10, 2004 | Issued |
Array
(
[id] => 6949545
[patent_doc_number] => 20050224639
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-10-13
[patent_title] => 'Venting for thermal aircraft'
[patent_app_type] => utility
[patent_app_number] => 10/798842
[patent_app_country] => US
[patent_app_date] => 2004-03-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 6740
[patent_no_of_claims] => 29
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0224/20050224639.pdf
[firstpage_image] =>[orig_patent_app_number] => 10798842
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/798842 | Venting for thermal aircraft | Mar 10, 2004 | Abandoned |
Array
(
[id] => 413804
[patent_doc_number] => 07278611
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2007-10-09
[patent_title] => 'Pulsed detonation engines for reaction control systems'
[patent_app_type] => utility
[patent_app_number] => 10/796279
[patent_app_country] => US
[patent_app_date] => 2004-03-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 11
[patent_no_of_words] => 5082
[patent_no_of_claims] => 41
[patent_no_of_ind_claims] => 6
[patent_words_short_claim] => 72
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/278/07278611.pdf
[firstpage_image] =>[orig_patent_app_number] => 10796279
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/796279 | Pulsed detonation engines for reaction control systems | Mar 9, 2004 | Issued |
Array
(
[id] => 660815
[patent_doc_number] => 07100873
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2006-09-05
[patent_title] => 'Hanger assembly for aircraft'
[patent_app_type] => utility
[patent_app_number] => 10/797681
[patent_app_country] => US
[patent_app_date] => 2004-03-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 2768
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 278
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/100/07100873.pdf
[firstpage_image] =>[orig_patent_app_number] => 10797681
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/797681 | Hanger assembly for aircraft | Mar 4, 2004 | Issued |
10/794444 | Flying motorcycle | Mar 4, 2004 | Abandoned |
Array
(
[id] => 5616737
[patent_doc_number] => 20060186269
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-08-24
[patent_title] => 'Adaptive compliant wing and rotor system'
[patent_app_type] => utility
[patent_app_number] => 10/548053
[patent_app_country] => US
[patent_app_date] => 2004-03-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 23
[patent_figures_cnt] => 23
[patent_no_of_words] => 7830
[patent_no_of_claims] => 23
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0186/20060186269.pdf
[firstpage_image] =>[orig_patent_app_number] => 10548053
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/548053 | Adaptive compliant wing and rotor system | Mar 2, 2004 | Issued |
Array
(
[id] => 643450
[patent_doc_number] => 07118076
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2006-10-10
[patent_title] => 'Satellite comprising means for transferring heat from a shelf supporting equipment to radiator panels'
[patent_app_type] => utility
[patent_app_number] => 10/787131
[patent_app_country] => US
[patent_app_date] => 2004-02-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 1987
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 75
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/118/07118076.pdf
[firstpage_image] =>[orig_patent_app_number] => 10787131
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/787131 | Satellite comprising means for transferring heat from a shelf supporting equipment to radiator panels | Feb 26, 2004 | Issued |
Array
(
[id] => 7359885
[patent_doc_number] => 20040216691
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-11-04
[patent_title] => 'Automatic cat grooming, feeding, and litterbox apparatus'
[patent_app_type] => new
[patent_app_number] => 10/789255
[patent_app_country] => US
[patent_app_date] => 2004-02-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 30
[patent_figures_cnt] => 30
[patent_no_of_words] => 5392
[patent_no_of_claims] => 50
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 39
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0216/20040216691.pdf
[firstpage_image] =>[orig_patent_app_number] => 10789255
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/789255 | Automatic cat grooming, feeding, and litterbox apparatus | Feb 26, 2004 | Issued |
Array
(
[id] => 503897
[patent_doc_number] => 07195209
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2007-03-27
[patent_title] => 'Aircraft high-lift system with overload protection'
[patent_app_type] => utility
[patent_app_number] => 10/788160
[patent_app_country] => US
[patent_app_date] => 2004-02-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 2
[patent_no_of_words] => 1196
[patent_no_of_claims] => 19
[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/07/195/07195209.pdf
[firstpage_image] =>[orig_patent_app_number] => 10788160
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/788160 | Aircraft high-lift system with overload protection | Feb 25, 2004 | Issued |
Array
(
[id] => 480921
[patent_doc_number] => 07216474
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2007-05-15
[patent_title] => 'Integrated air inlet system for multi-propulsion aircraft engines'
[patent_app_type] => utility
[patent_app_number] => 10/784482
[patent_app_country] => US
[patent_app_date] => 2004-02-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 8
[patent_no_of_words] => 3792
[patent_no_of_claims] => 23
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 145
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/216/07216474.pdf
[firstpage_image] =>[orig_patent_app_number] => 10784482
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/784482 | Integrated air inlet system for multi-propulsion aircraft engines | Feb 18, 2004 | Issued |
Array
(
[id] => 7406145
[patent_doc_number] => 20040227033
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-11-18
[patent_title] => 'Turboprop carrier structure and an assembly including such a carrier structure'
[patent_app_type] => new
[patent_app_number] => 10/780639
[patent_app_country] => US
[patent_app_date] => 2004-02-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 4508
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 195
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0227/20040227033.pdf
[firstpage_image] =>[orig_patent_app_number] => 10780639
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/780639 | Turboprop carrier structure and an assembly including such a carrier structure | Feb 18, 2004 | Issued |