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] => 7132601
[patent_doc_number] => 20050178926
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-08-18
[patent_title] => 'Disengage device'
[patent_app_type] => utility
[patent_app_number] => 11/038725
[patent_app_country] => US
[patent_app_date] => 2005-01-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 5221
[patent_no_of_claims] => 11
[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/A1/0178/20050178926.pdf
[firstpage_image] =>[orig_patent_app_number] => 11038725
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/038725 | Disengage device for aircraft control | Jan 18, 2005 | Issued |
Array
(
[id] => 858699
[patent_doc_number] => 07370834
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2008-05-13
[patent_title] => 'Apparatus and methods for in-space satellite operations'
[patent_app_type] => utility
[patent_app_number] => 11/039452
[patent_app_country] => US
[patent_app_date] => 2005-01-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 10
[patent_no_of_words] => 6154
[patent_no_of_claims] => 3
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 121
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/370/07370834.pdf
[firstpage_image] =>[orig_patent_app_number] => 11039452
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/039452 | Apparatus and methods for in-space satellite operations | Jan 13, 2005 | Issued |
Array
(
[id] => 6928849
[patent_doc_number] => 20050279881
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-12-22
[patent_title] => 'Airship'
[patent_app_type] => utility
[patent_app_number] => 11/027746
[patent_app_country] => US
[patent_app_date] => 2004-12-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 4238
[patent_no_of_claims] => 19
[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/A1/0279/20050279881.pdf
[firstpage_image] =>[orig_patent_app_number] => 11027746
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/027746 | Airship | Dec 29, 2004 | Issued |
Array
(
[id] => 4654725
[patent_doc_number] => 20080023585
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-01-31
[patent_title] => 'AIRCRAFT WING COMPOSED OF COMPOSITE AND METAL PANELS'
[patent_app_type] => utility
[patent_app_number] => 11/027570
[patent_app_country] => US
[patent_app_date] => 2004-12-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 2259
[patent_no_of_claims] => 28
[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/A1/0023/20080023585.pdf
[firstpage_image] =>[orig_patent_app_number] => 11027570
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/027570 | Aircraft wing composed of composite and metal panels | Dec 28, 2004 | Issued |
Array
(
[id] => 399914
[patent_doc_number] => 07290736
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2007-11-06
[patent_title] => 'Aircraft door'
[patent_app_type] => utility
[patent_app_number] => 11/018640
[patent_app_country] => US
[patent_app_date] => 2004-12-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
[patent_figures_cnt] => 33
[patent_no_of_words] => 4180
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 129
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/290/07290736.pdf
[firstpage_image] =>[orig_patent_app_number] => 11018640
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/018640 | Aircraft door | Dec 20, 2004 | Issued |
Array
(
[id] => 815950
[patent_doc_number] => 07410126
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2008-08-12
[patent_title] => 'Tunable acoustic absorption system for an aircraft cabin'
[patent_app_type] => utility
[patent_app_number] => 11/017241
[patent_app_country] => US
[patent_app_date] => 2004-12-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 6
[patent_no_of_words] => 2762
[patent_no_of_claims] => 24
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 56
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/410/07410126.pdf
[firstpage_image] =>[orig_patent_app_number] => 11017241
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/017241 | Tunable acoustic absorption system for an aircraft cabin | Dec 19, 2004 | Issued |
Array
(
[id] => 795105
[patent_doc_number] => 07429015
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2008-09-30
[patent_title] => 'Acoustic absorption blanket mounting system for an aircraft cabin'
[patent_app_type] => utility
[patent_app_number] => 11/017564
[patent_app_country] => US
[patent_app_date] => 2004-12-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 13
[patent_no_of_words] => 2405
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 46
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/429/07429015.pdf
[firstpage_image] =>[orig_patent_app_number] => 11017564
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/017564 | Acoustic absorption blanket mounting system for an aircraft cabin | Dec 19, 2004 | Issued |
Array
(
[id] => 900563
[patent_doc_number] => 07334759
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2008-02-26
[patent_title] => 'Airplane surface protection film kits'
[patent_app_type] => utility
[patent_app_number] => 11/016309
[patent_app_country] => US
[patent_app_date] => 2004-12-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 2472
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 104
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/334/07334759.pdf
[firstpage_image] =>[orig_patent_app_number] => 11016309
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/016309 | Airplane surface protection film kits | Dec 17, 2004 | Issued |
Array
(
[id] => 5796305
[patent_doc_number] => 20060032982
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-02-16
[patent_title] => 'Method of joining structural elements in an aircraft'
[patent_app_type] => utility
[patent_app_number] => 11/016334
[patent_app_country] => US
[patent_app_date] => 2004-12-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 6156
[patent_no_of_claims] => 22
[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/A1/0032/20060032982.pdf
[firstpage_image] =>[orig_patent_app_number] => 11016334
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/016334 | Method of joining structural elements in an aircraft | Dec 16, 2004 | Issued |
Array
(
[id] => 379477
[patent_doc_number] => 07309046
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2007-12-18
[patent_title] => 'Method for determination of fuselage shape of supersonic aircraft, and fuselage front section shape'
[patent_app_type] => utility
[patent_app_number] => 11/011068
[patent_app_country] => US
[patent_app_date] => 2004-12-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 28
[patent_no_of_words] => 4890
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 113
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/309/07309046.pdf
[firstpage_image] =>[orig_patent_app_number] => 11011068
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/011068 | Method for determination of fuselage shape of supersonic aircraft, and fuselage front section shape | Dec 14, 2004 | Issued |
Array
(
[id] => 440936
[patent_doc_number] => 07255304
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2007-08-14
[patent_title] => 'Tandem motor actuator'
[patent_app_type] => utility
[patent_app_number] => 11/005368
[patent_app_country] => US
[patent_app_date] => 2004-12-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 11
[patent_no_of_words] => 2900
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 132
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/255/07255304.pdf
[firstpage_image] =>[orig_patent_app_number] => 11005368
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/005368 | Tandem motor actuator | Dec 5, 2004 | Issued |
Array
(
[id] => 453230
[patent_doc_number] => 07243611
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2007-07-17
[patent_title] => 'Drinking trough with elongated actuator and method of dispensing water therefrom'
[patent_app_type] => utility
[patent_app_number] => 10/998434
[patent_app_country] => US
[patent_app_date] => 2004-11-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 15
[patent_figures_cnt] => 15
[patent_no_of_words] => 10321
[patent_no_of_claims] => 22
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 139
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/243/07243611.pdf
[firstpage_image] =>[orig_patent_app_number] => 10998434
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/998434 | Drinking trough with elongated actuator and method of dispensing water therefrom | Nov 28, 2004 | Issued |
Array
(
[id] => 6980963
[patent_doc_number] => 20050151031
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-07-14
[patent_title] => 'Aircraft wing structure and a method for decreasing flight speed of the aircraft'
[patent_app_type] => utility
[patent_app_number] => 10/998690
[patent_app_country] => US
[patent_app_date] => 2004-11-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 1462
[patent_no_of_claims] => 17
[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/A1/0151/20050151031.pdf
[firstpage_image] =>[orig_patent_app_number] => 10998690
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/998690 | Aircraft wing structure and a method for decreasing flight speed of the aircraft | Nov 28, 2004 | Issued |
Array
(
[id] => 7139770
[patent_doc_number] => 20050116094
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-06-02
[patent_title] => 'Method making it possible to prevent vibration of a rudder of an aircraft and aircraft using this method'
[patent_app_type] => utility
[patent_app_number] => 10/996454
[patent_app_country] => US
[patent_app_date] => 2004-11-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2190
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0116/20050116094.pdf
[firstpage_image] =>[orig_patent_app_number] => 10996454
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/996454 | Method making it possible to prevent vibration of a rudder of an aircraft and aircraft using this method | Nov 25, 2004 | Issued |
Array
(
[id] => 5745553
[patent_doc_number] => 20060108477
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-05-25
[patent_title] => 'Cargo aircraft'
[patent_app_type] => utility
[patent_app_number] => 10/996799
[patent_app_country] => US
[patent_app_date] => 2004-11-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 16
[patent_figures_cnt] => 16
[patent_no_of_words] => 3885
[patent_no_of_claims] => 21
[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/A1/0108/20060108477.pdf
[firstpage_image] =>[orig_patent_app_number] => 10996799
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/996799 | Cargo aircraft | Nov 22, 2004 | Issued |
Array
(
[id] => 848242
[patent_doc_number] => 07380756
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2008-06-03
[patent_title] => 'Single dielectric barrier aerodynamic plasma actuation'
[patent_app_type] => utility
[patent_app_number] => 10/994029
[patent_app_country] => US
[patent_app_date] => 2004-11-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 19
[patent_figures_cnt] => 43
[patent_no_of_words] => 9981
[patent_no_of_claims] => 24
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 123
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/380/07380756.pdf
[firstpage_image] =>[orig_patent_app_number] => 10994029
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/994029 | Single dielectric barrier aerodynamic plasma actuation | Nov 15, 2004 | Issued |
Array
(
[id] => 7004450
[patent_doc_number] => 20050169763
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-08-04
[patent_title] => 'Helicopter rotor and method of repairing same'
[patent_app_type] => utility
[patent_app_number] => 10/987184
[patent_app_country] => US
[patent_app_date] => 2004-11-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2367
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0169/20050169763.pdf
[firstpage_image] =>[orig_patent_app_number] => 10987184
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/987184 | Helicopter rotor and method of repairing same | Nov 14, 2004 | Issued |
Array
(
[id] => 6957697
[patent_doc_number] => 20050214067
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-09-29
[patent_title] => 'Heat shield'
[patent_app_type] => utility
[patent_app_number] => 10/987995
[patent_app_country] => US
[patent_app_date] => 2004-11-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 22
[patent_figures_cnt] => 22
[patent_no_of_words] => 8240
[patent_no_of_claims] => 22
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0214/20050214067.pdf
[firstpage_image] =>[orig_patent_app_number] => 10987995
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/987995 | Heat shield | Nov 11, 2004 | Issued |
Array
(
[id] => 535536
[patent_doc_number] => 07163179
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2007-01-16
[patent_title] => 'Commercial service platform in space'
[patent_app_type] => utility
[patent_app_number] => 10/987088
[patent_app_country] => US
[patent_app_date] => 2004-11-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
[patent_figures_cnt] => 28
[patent_no_of_words] => 11584
[patent_no_of_claims] => 23
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 95
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/163/07163179.pdf
[firstpage_image] =>[orig_patent_app_number] => 10987088
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/987088 | Commercial service platform in space | Nov 11, 2004 | Issued |
Array
(
[id] => 733253
[patent_doc_number] => 07032860
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2006-04-25
[patent_title] => 'Emergency anti-torque thruster system'
[patent_app_type] => utility
[patent_app_number] => 10/982037
[patent_app_country] => US
[patent_app_date] => 2004-11-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 7285
[patent_no_of_claims] => 24
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 158
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/032/07032860.pdf
[firstpage_image] =>[orig_patent_app_number] => 10982037
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/982037 | Emergency anti-torque thruster system | Nov 4, 2004 | Issued |