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] => 5019219
[patent_doc_number] => 20070145184
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-06-28
[patent_title] => 'Device and system for assistance within interception by an aircraft of a flight path segment'
[patent_app_type] => utility
[patent_app_number] => 11/636439
[patent_app_country] => US
[patent_app_date] => 2006-12-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 5413
[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/A1/0145/20070145184.pdf
[firstpage_image] =>[orig_patent_app_number] => 11636439
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/636439 | Device and system for assistance within interception by an aircraft of a flight path segment | Dec 10, 2006 | Issued |
Array
(
[id] => 273344
[patent_doc_number] => 07559508
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2009-07-14
[patent_title] => 'Propellant depot in space'
[patent_app_type] => utility
[patent_app_number] => 11/608221
[patent_app_country] => US
[patent_app_date] => 2006-12-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 14
[patent_figures_cnt] => 36
[patent_no_of_words] => 11873
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 59
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/559/07559508.pdf
[firstpage_image] =>[orig_patent_app_number] => 11608221
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/608221 | Propellant depot in space | Dec 6, 2006 | Issued |
Array
(
[id] => 194988
[patent_doc_number] => 07637453
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2009-12-29
[patent_title] => 'Aircraft spiraling mechanism with jet assistance - A'
[patent_app_type] => utility
[patent_app_number] => 11/605310
[patent_app_country] => US
[patent_app_date] => 2006-11-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 12
[patent_no_of_words] => 3248
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 231
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/637/07637453.pdf
[firstpage_image] =>[orig_patent_app_number] => 11605310
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/605310 | Aircraft spiraling mechanism with jet assistance - A | Nov 28, 2006 | Issued |
Array
(
[id] => 110329
[patent_doc_number] => 07712702
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-05-11
[patent_title] => 'Methods and apparatuses for launching unmanned aircraft, including releasably gripping aircraft during launch and breaking subsequent grip motion'
[patent_app_type] => utility
[patent_app_number] => 11/603810
[patent_app_country] => US
[patent_app_date] => 2006-11-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 15
[patent_no_of_words] => 6874
[patent_no_of_claims] => 25
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 103
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/712/07712702.pdf
[firstpage_image] =>[orig_patent_app_number] => 11603810
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/603810 | Methods and apparatuses for launching unmanned aircraft, including releasably gripping aircraft during launch and breaking subsequent grip motion | Nov 20, 2006 | Issued |
Array
(
[id] => 870017
[patent_doc_number] => 07360741
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2008-04-22
[patent_title] => 'Methods and apparatuses for launching unmanned aircraft, including releasably gripping aircraft during launch and breaking subsequent grip motion'
[patent_app_type] => utility
[patent_app_number] => 11/603815
[patent_app_country] => US
[patent_app_date] => 2006-11-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 15
[patent_no_of_words] => 6890
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 86
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/360/07360741.pdf
[firstpage_image] =>[orig_patent_app_number] => 11603815
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/603815 | Methods and apparatuses for launching unmanned aircraft, including releasably gripping aircraft during launch and breaking subsequent grip motion | Nov 20, 2006 | Issued |
Array
(
[id] => 194801
[patent_doc_number] => 07635104
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2009-12-22
[patent_title] => 'Aircraft spiraling mechanism with jet assistance—B'
[patent_app_type] => utility
[patent_app_number] => 11/601804
[patent_app_country] => US
[patent_app_date] => 2006-11-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 11
[patent_no_of_words] => 3042
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 127
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/635/07635104.pdf
[firstpage_image] =>[orig_patent_app_number] => 11601804
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/601804 | Aircraft spiraling mechanism with jet assistance—B | Nov 19, 2006 | Issued |
Array
(
[id] => 5213495
[patent_doc_number] => 20070102575
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-05-10
[patent_title] => 'Aircraft attitude control configuration'
[patent_app_type] => utility
[patent_app_number] => 11/595525
[patent_app_country] => US
[patent_app_date] => 2006-11-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 11
[patent_no_of_words] => 12580
[patent_no_of_claims] => 22
[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/A1/0102/20070102575.pdf
[firstpage_image] =>[orig_patent_app_number] => 11595525
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/595525 | Aircraft attitude control configuration | Nov 8, 2006 | Issued |
Array
(
[id] => 573473
[patent_doc_number] => 07445179
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2008-11-04
[patent_title] => 'Engine assembly for aircraft'
[patent_app_type] => utility
[patent_app_number] => 11/527622
[patent_app_country] => US
[patent_app_date] => 2006-09-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 4369
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 22
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/445/07445179.pdf
[firstpage_image] =>[orig_patent_app_number] => 11527622
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/527622 | Engine assembly for aircraft | Sep 26, 2006 | Issued |
Array
(
[id] => 5168637
[patent_doc_number] => 20070069068
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-03-29
[patent_title] => 'Engine suspension pylon for aircraft'
[patent_app_type] => utility
[patent_app_number] => 11/525025
[patent_app_country] => US
[patent_app_date] => 2006-09-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 3084
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0069/20070069068.pdf
[firstpage_image] =>[orig_patent_app_number] => 11525025
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/525025 | Engine suspension pylon for aircraft | Sep 21, 2006 | Issued |
Array
(
[id] => 438291
[patent_doc_number] => 07258306
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2007-08-21
[patent_title] => 'Thermal deformation determination for payload pointing using space-based beacon'
[patent_app_type] => utility
[patent_app_number] => 11/533165
[patent_app_country] => US
[patent_app_date] => 2006-09-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2947
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 107
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/258/07258306.pdf
[firstpage_image] =>[orig_patent_app_number] => 11533165
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/533165 | Thermal deformation determination for payload pointing using space-based beacon | Sep 18, 2006 | Issued |
Array
(
[id] => 815955
[patent_doc_number] => 07410131
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2008-08-12
[patent_title] => 'Pulsed detonation engines for reaction control systems'
[patent_app_type] => utility
[patent_app_number] => 11/532163
[patent_app_country] => US
[patent_app_date] => 2006-09-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 11
[patent_no_of_words] => 5097
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 66
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/410/07410131.pdf
[firstpage_image] =>[orig_patent_app_number] => 11532163
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/532163 | Pulsed detonation engines for reaction control systems | Sep 14, 2006 | Issued |
Array
(
[id] => 5092714
[patent_doc_number] => 20070114323
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-05-24
[patent_title] => 'Method of Synchronizing Fin Fold-Out on a Fin-Stabilized Artillery Shell, and an Artillery Shell Designed in Accordance Therewith'
[patent_app_type] => utility
[patent_app_number] => 11/530520
[patent_app_country] => US
[patent_app_date] => 2006-09-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 3324
[patent_no_of_claims] => 3
[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/A1/0114/20070114323.pdf
[firstpage_image] =>[orig_patent_app_number] => 11530520
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/530520 | Method of synchronizing fin fold-out on a fin-stabilized artillery shell, and an artillery shell designed in accordance therewith | Sep 10, 2006 | Issued |
Array
(
[id] => 4723680
[patent_doc_number] => 20080203221
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-08-28
[patent_title] => 'JAM TOLERANT ELECTROMECHANICAL ACTUATION SYSTEMS AND METHODS OF OPERATION'
[patent_app_type] => utility
[patent_app_number] => 11/469531
[patent_app_country] => US
[patent_app_date] => 2006-09-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 22
[patent_figures_cnt] => 22
[patent_no_of_words] => 9576
[patent_no_of_claims] => 23
[patent_no_of_ind_claims] => 4
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0203/20080203221.pdf
[firstpage_image] =>[orig_patent_app_number] => 11469531
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/469531 | Jam tolerant electromechanical actuation systems and methods of operation | Aug 31, 2006 | Issued |
Array
(
[id] => 903917
[patent_doc_number] => 07331546
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2008-02-19
[patent_title] => 'Bendable wing for micro air vehicle'
[patent_app_type] => utility
[patent_app_number] => 11/510013
[patent_app_country] => US
[patent_app_date] => 2006-08-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 10
[patent_no_of_words] => 2919
[patent_no_of_claims] => 24
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 149
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/331/07331546.pdf
[firstpage_image] =>[orig_patent_app_number] => 11510013
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/510013 | Bendable wing for micro air vehicle | Aug 24, 2006 | Issued |
Array
(
[id] => 5425591
[patent_doc_number] => 20090084901
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-04-02
[patent_title] => 'PIVOTABLE PYLON FOR EXTERNAL CARRIAGE OF AIRCRAFT STORES'
[patent_app_type] => utility
[patent_app_number] => 11/502239
[patent_app_country] => US
[patent_app_date] => 2006-08-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 3001
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 2
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0084/20090084901.pdf
[firstpage_image] =>[orig_patent_app_number] => 11502239
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/502239 | Pivotable pylon for external carriage of aircraft stores | Aug 9, 2006 | Issued |
Array
(
[id] => 4648540
[patent_doc_number] => 20080035795
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-02-14
[patent_title] => 'Illuminated flying kite'
[patent_app_type] => utility
[patent_app_number] => 11/501532
[patent_app_country] => US
[patent_app_date] => 2006-08-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2382
[patent_no_of_claims] => 20
[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/A1/0035/20080035795.pdf
[firstpage_image] =>[orig_patent_app_number] => 11501532
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/501532 | Illuminated flying kite | Aug 7, 2006 | Abandoned |
Array
(
[id] => 208515
[patent_doc_number] => 07624951
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2009-12-01
[patent_title] => 'Aircraft with antennas mounted on the tops and bottoms of aerodynamic-surface extensions'
[patent_app_type] => utility
[patent_app_number] => 11/499223
[patent_app_country] => US
[patent_app_date] => 2006-08-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 21
[patent_no_of_words] => 6318
[patent_no_of_claims] => 18
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[patent_words_short_claim] => 145
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/624/07624951.pdf
[firstpage_image] =>[orig_patent_app_number] => 11499223
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/499223 | Aircraft with antennas mounted on the tops and bottoms of aerodynamic-surface extensions | Aug 3, 2006 | Issued |
Array
(
[id] => 4566844
[patent_doc_number] => 07832689
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-11-16
[patent_title] => 'Element for generating a fluid dynamic force'
[patent_app_type] => utility
[patent_app_number] => 11/995440
[patent_app_country] => US
[patent_app_date] => 2006-07-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
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[pdf_file] => patents/07/832/07832689.pdf
[firstpage_image] =>[orig_patent_app_number] => 11995440
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/995440 | Element for generating a fluid dynamic force | Jul 12, 2006 | Issued |
Array
(
[id] => 40210
[patent_doc_number] => 07780117
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-08-24
[patent_title] => 'Aircraft engine nacelle ice protection system'
[patent_app_type] => utility
[patent_app_number] => 11/456629
[patent_app_country] => US
[patent_app_date] => 2006-07-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/780/07780117.pdf
[firstpage_image] =>[orig_patent_app_number] => 11456629
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/456629 | Aircraft engine nacelle ice protection system | Jul 10, 2006 | Issued |
Array
(
[id] => 306469
[patent_doc_number] => 07530532
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2009-05-12
[patent_title] => 'Counterweight based rocket launch platform'
[patent_app_type] => utility
[patent_app_number] => 11/480120
[patent_app_country] => US
[patent_app_date] => 2006-07-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 3
[patent_no_of_words] => 1483
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 104
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/530/07530532.pdf
[firstpage_image] =>[orig_patent_app_number] => 11480120
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/480120 | Counterweight based rocket launch platform | Jul 2, 2006 | Issued |