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] => 81528
[patent_doc_number] => 07740204
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2010-06-22
[patent_title] => 'Propulsion system'
[patent_app_type] => utility
[patent_app_number] => 11/480136
[patent_app_country] => US
[patent_app_date] => 2006-07-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 1154
[patent_no_of_claims] => 3
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 112
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/740/07740204.pdf
[firstpage_image] =>[orig_patent_app_number] => 11480136
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/480136 | Propulsion system | Jul 2, 2006 | Issued |
Array
(
[id] => 5659020
[patent_doc_number] => 20060249616
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-11-09
[patent_title] => 'Payload to Support Track Interface and Fitting Apparatus and Methods'
[patent_app_type] => utility
[patent_app_number] => 11/426848
[patent_app_country] => US
[patent_app_date] => 2006-06-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 12
[patent_no_of_words] => 5834
[patent_no_of_claims] => 27
[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/A1/0249/20060249616.pdf
[firstpage_image] =>[orig_patent_app_number] => 11426848
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/426848 | Payload to support track interface and fitting apparatus and methods | Jun 26, 2006 | Issued |
Array
(
[id] => 181115
[patent_doc_number] => 07651049
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-01-26
[patent_title] => 'Helicopter with an auxiliary lubricating circuit'
[patent_app_type] => utility
[patent_app_number] => 11/454229
[patent_app_country] => US
[patent_app_date] => 2006-06-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 1516
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 188
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/651/07651049.pdf
[firstpage_image] =>[orig_patent_app_number] => 11454229
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/454229 | Helicopter with an auxiliary lubricating circuit | Jun 15, 2006 | Issued |
Array
(
[id] => 5162894
[patent_doc_number] => 20070284474
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-12-13
[patent_title] => 'Wirelessly controlling unmanned aircraft and accessing associated surveillance data'
[patent_app_type] => utility
[patent_app_number] => 11/449927
[patent_app_country] => US
[patent_app_date] => 2006-06-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 6212
[patent_no_of_claims] => 53
[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/A1/0284/20070284474.pdf
[firstpage_image] =>[orig_patent_app_number] => 11449927
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/449927 | Wirelessly controlling unmanned aircraft and accessing associated surveillance data | Jun 8, 2006 | Issued |
Array
(
[id] => 157397
[patent_doc_number] => 07673831
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-03-09
[patent_title] => 'Small unmanned air vehicle system for deploying and towing a sensor in a tow medium and methods related thereto'
[patent_app_type] => utility
[patent_app_number] => 11/422933
[patent_app_country] => US
[patent_app_date] => 2006-06-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 16
[patent_no_of_words] => 4833
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 119
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/673/07673831.pdf
[firstpage_image] =>[orig_patent_app_number] => 11422933
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/422933 | Small unmanned air vehicle system for deploying and towing a sensor in a tow medium and methods related thereto | Jun 7, 2006 | Issued |
Array
(
[id] => 120698
[patent_doc_number] => 07703718
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-04-27
[patent_title] => 'Aircraft cabin arrangement and storage unit'
[patent_app_type] => utility
[patent_app_number] => 11/445324
[patent_app_country] => US
[patent_app_date] => 2006-06-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2318
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 122
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/703/07703718.pdf
[firstpage_image] =>[orig_patent_app_number] => 11445324
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/445324 | Aircraft cabin arrangement and storage unit | Jun 1, 2006 | Issued |
Array
(
[id] => 489065
[patent_doc_number] => 07210651
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2007-05-01
[patent_title] => 'Compact co-axial rotor system for a rotary wing aircraft and a control system therefor'
[patent_app_type] => utility
[patent_app_number] => 11/446352
[patent_app_country] => US
[patent_app_date] => 2006-06-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 11
[patent_no_of_words] => 3043
[patent_no_of_claims] => 23
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 93
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/210/07210651.pdf
[firstpage_image] =>[orig_patent_app_number] => 11446352
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/446352 | Compact co-axial rotor system for a rotary wing aircraft and a control system therefor | Jun 1, 2006 | Issued |
Array
(
[id] => 5605364
[patent_doc_number] => 20060266880
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-11-30
[patent_title] => 'Servo fixing base structure for remote control helicopers'
[patent_app_type] => utility
[patent_app_number] => 11/431854
[patent_app_country] => US
[patent_app_date] => 2006-05-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 1313
[patent_no_of_claims] => 2
[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/A1/0266/20060266880.pdf
[firstpage_image] =>[orig_patent_app_number] => 11431854
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/431854 | Servo fixing base structure for remote control helicopers | May 10, 2006 | Abandoned |
Array
(
[id] => 208505
[patent_doc_number] => 07624941
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2009-12-01
[patent_title] => 'Method of controlling aircraft, missiles, munitions and ground vehicles with plasma actuators'
[patent_app_type] => utility
[patent_app_number] => 11/415535
[patent_app_country] => US
[patent_app_date] => 2006-05-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 5315
[patent_no_of_claims] => 20
[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/07/624/07624941.pdf
[firstpage_image] =>[orig_patent_app_number] => 11415535
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/415535 | Method of controlling aircraft, missiles, munitions and ground vehicles with plasma actuators | May 1, 2006 | Issued |
Array
(
[id] => 888652
[patent_doc_number] => 07344106
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2008-03-18
[patent_title] => 'Vertical take-off and landing aircraft'
[patent_app_type] => utility
[patent_app_number] => 11/380539
[patent_app_country] => US
[patent_app_date] => 2006-04-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
[patent_figures_cnt] => 25
[patent_no_of_words] => 3311
[patent_no_of_claims] => 4
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 580
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/344/07344106.pdf
[firstpage_image] =>[orig_patent_app_number] => 11380539
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/380539 | Vertical take-off and landing aircraft | Apr 26, 2006 | Issued |
Array
(
[id] => 446974
[patent_doc_number] => 07249732
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2007-07-31
[patent_title] => 'Aerodynamically stable, VTOL aircraft'
[patent_app_type] => utility
[patent_app_number] => 11/379963
[patent_app_country] => US
[patent_app_date] => 2006-04-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 29
[patent_figures_cnt] => 104
[patent_no_of_words] => 10738
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 347
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/249/07249732.pdf
[firstpage_image] =>[orig_patent_app_number] => 11379963
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/379963 | Aerodynamically stable, VTOL aircraft | Apr 23, 2006 | Issued |
Array
(
[id] => 5664486
[patent_doc_number] => 20060169836
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-08-03
[patent_title] => 'Apparatus and Method for Lighter-Than-Air Aircraft'
[patent_app_type] => utility
[patent_app_number] => 11/279901
[patent_app_country] => US
[patent_app_date] => 2006-04-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
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[patent_no_of_words] => 6025
[patent_no_of_claims] => 9
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0169/20060169836.pdf
[firstpage_image] =>[orig_patent_app_number] => 11279901
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/279901 | Method for lighter-than-air aircraft | Apr 16, 2006 | Issued |
Array
(
[id] => 547029
[patent_doc_number] => 07469861
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2008-12-30
[patent_title] => 'Seating system and a passenger accommodation unit for a vehicle'
[patent_app_type] => utility
[patent_app_number] => 11/394827
[patent_app_country] => US
[patent_app_date] => 2006-03-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 39
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[patent_no_of_words] => 31729
[patent_no_of_claims] => 24
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 367
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/469/07469861.pdf
[firstpage_image] =>[orig_patent_app_number] => 11394827
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/394827 | Seating system and a passenger accommodation unit for a vehicle | Mar 30, 2006 | Issued |
Array
(
[id] => 5192084
[patent_doc_number] => 20070080566
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-04-12
[patent_title] => 'Seating system and a passenger accommodation unit for a vehicle'
[patent_app_type] => utility
[patent_app_number] => 11/395089
[patent_app_country] => US
[patent_app_date] => 2006-03-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 40
[patent_figures_cnt] => 40
[patent_no_of_words] => 31771
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 3
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0080/20070080566.pdf
[firstpage_image] =>[orig_patent_app_number] => 11395089
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/395089 | Seating system and a passenger accommodation unit for a vehicle | Mar 30, 2006 | Issued |
Array
(
[id] => 5222778
[patent_doc_number] => 20070252044
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-11-01
[patent_title] => 'Satellite active motion damping'
[patent_app_type] => utility
[patent_app_number] => 11/394037
[patent_app_country] => US
[patent_app_date] => 2006-03-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0252/20070252044.pdf
[firstpage_image] =>[orig_patent_app_number] => 11394037
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/394037 | Satellite active motion damping | Mar 28, 2006 | Issued |
Array
(
[id] => 481465
[patent_doc_number] => 07216642
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2007-05-15
[patent_title] => 'Pneumatically launched folding wing glider toy'
[patent_app_type] => utility
[patent_app_number] => 11/392146
[patent_app_country] => US
[patent_app_date] => 2006-03-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 7758
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 171
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/216/07216642.pdf
[firstpage_image] =>[orig_patent_app_number] => 11392146
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/392146 | Pneumatically launched folding wing glider toy | Mar 28, 2006 | Issued |
Array
(
[id] => 5854349
[patent_doc_number] => 20060226282
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-10-12
[patent_title] => 'Deflection system for a gas stream in a nozzle'
[patent_app_type] => utility
[patent_app_number] => 11/386740
[patent_app_country] => US
[patent_app_date] => 2006-03-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_no_of_words] => 2613
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0226/20060226282.pdf
[firstpage_image] =>[orig_patent_app_number] => 11386740
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/386740 | Deflection system for a gas stream in a nozzle | Mar 22, 2006 | Issued |
Array
(
[id] => 119066
[patent_doc_number] => 07708229
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2010-05-04
[patent_title] => 'Circulation controlled airfoil'
[patent_app_type] => utility
[patent_app_number] => 11/387136
[patent_app_country] => US
[patent_app_date] => 2006-03-22
[patent_effective_date] => 0000-00-00
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[pdf_file] => patents/07/708/07708229.pdf
[firstpage_image] =>[orig_patent_app_number] => 11387136
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/387136 | Circulation controlled airfoil | Mar 21, 2006 | Issued |
Array
(
[id] => 5664488
[patent_doc_number] => 20060169838
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-08-03
[patent_title] => 'Method of enhancing the movement of dangerous goods'
[patent_app_type] => utility
[patent_app_number] => 11/371722
[patent_app_country] => US
[patent_app_date] => 2006-03-09
[patent_effective_date] => 0000-00-00
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[pdf_file] => publications/A1/0169/20060169838.pdf
[firstpage_image] =>[orig_patent_app_number] => 11371722
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/371722 | Method of enhancing the movement of dangerous goods | Mar 8, 2006 | Abandoned |
Array
(
[id] => 5128930
[patent_doc_number] => 20070205327
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-09-06
[patent_title] => 'Aircraft sensor pod assembly'
[patent_app_type] => utility
[patent_app_number] => 11/368838
[patent_app_country] => US
[patent_app_date] => 2006-03-06
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0205/20070205327.pdf
[firstpage_image] =>[orig_patent_app_number] => 11368838
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/368838 | Aircraft sensor pod assembly | Mar 5, 2006 | Issued |