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] => 7193934
[patent_doc_number] => 20050050790
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-03-10
[patent_title] => 'Collapsible umbrella fishing rig'
[patent_app_type] => utility
[patent_app_number] => 10/306731
[patent_app_country] => US
[patent_app_date] => 2002-11-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 3917
[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/A1/0050/20050050790.pdf
[firstpage_image] =>[orig_patent_app_number] => 10306731
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/306731 | Collapsible umbrella fishing rig | Nov 28, 2002 | Abandoned |
Array
(
[id] => 306255
[patent_doc_number] => 07530318
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2009-05-12
[patent_title] => 'Method and system for producing a potential over a body'
[patent_app_type] => utility
[patent_app_number] => 10/496494
[patent_app_country] => US
[patent_app_date] => 2002-11-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 1
[patent_no_of_words] => 3286
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 95
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/530/07530318.pdf
[firstpage_image] =>[orig_patent_app_number] => 10496494
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/496494 | Method and system for producing a potential over a body | Nov 28, 2002 | Issued |
Array
(
[id] => 7450198
[patent_doc_number] => 20040099767
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-05-27
[patent_title] => 'Flexible hydraulic latch'
[patent_app_type] => new
[patent_app_number] => 10/302539
[patent_app_country] => US
[patent_app_date] => 2002-11-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 1706
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 38
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0099/20040099767.pdf
[firstpage_image] =>[orig_patent_app_number] => 10302539
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/302539 | Flexible hydraulic latch | Nov 21, 2002 | Issued |
Array
(
[id] => 670541
[patent_doc_number] => 07090170
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2006-08-15
[patent_title] => 'In-orbit satellite sensor alignment determination'
[patent_app_type] => utility
[patent_app_number] => 10/302388
[patent_app_country] => US
[patent_app_date] => 2002-11-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 2558
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 123
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/090/07090170.pdf
[firstpage_image] =>[orig_patent_app_number] => 10302388
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/302388 | In-orbit satellite sensor alignment determination | Nov 21, 2002 | Issued |
Array
(
[id] => 7450176
[patent_doc_number] => 20040099764
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-05-27
[patent_title] => 'Aircraft and detonative engine incorporating pulse detonation engines'
[patent_app_type] => new
[patent_app_number] => 10/065815
[patent_app_country] => US
[patent_app_date] => 2002-11-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 3430
[patent_no_of_claims] => 31
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 39
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0099/20040099764.pdf
[firstpage_image] =>[orig_patent_app_number] => 10065815
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/065815 | Aircraft and detonative engine incorporating pulse detonation engines | Nov 21, 2002 | Issued |
Array
(
[id] => 7122616
[patent_doc_number] => 20050014445
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-01-20
[patent_title] => 'Remote-controlled flying craft, in particular for aerial photography'
[patent_app_type] => utility
[patent_app_number] => 10/495339
[patent_app_country] => US
[patent_app_date] => 2002-11-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 2405
[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/A1/0014/20050014445.pdf
[firstpage_image] =>[orig_patent_app_number] => 10495339
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/495339 | Remote-controlled flying craft, in particular for aerial photography | Nov 13, 2002 | Abandoned |
Array
(
[id] => 1190651
[patent_doc_number] => 06729582
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-05-04
[patent_title] => 'Method for making a support base plate for an artificial satellite on a dispenser platform for a plurality of such satellites'
[patent_app_type] => B2
[patent_app_number] => 10/203644
[patent_app_country] => US
[patent_app_date] => 2002-11-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 8
[patent_no_of_words] => 2257
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 181
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/729/06729582.pdf
[firstpage_image] =>[orig_patent_app_number] => 10203644
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/203644 | Method for making a support base plate for an artificial satellite on a dispenser platform for a plurality of such satellites | Nov 6, 2002 | Issued |
Array
(
[id] => 1238586
[patent_doc_number] => 06682022
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-01-27
[patent_title] => 'Boundary layer control of aerodynamic airfoils'
[patent_app_type] => B2
[patent_app_number] => 10/286865
[patent_app_country] => US
[patent_app_date] => 2002-11-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 9
[patent_no_of_words] => 4301
[patent_no_of_claims] => 29
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 154
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/682/06682022.pdf
[firstpage_image] =>[orig_patent_app_number] => 10286865
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/286865 | Boundary layer control of aerodynamic airfoils | Nov 3, 2002 | Issued |
Array
(
[id] => 7119678
[patent_doc_number] => 20050011507
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-01-20
[patent_title] => 'Projectile firing device using liquified gas propellant'
[patent_app_type] => utility
[patent_app_number] => 10/494490
[patent_app_country] => US
[patent_app_date] => 2002-11-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 12
[patent_no_of_words] => 4802
[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/A1/0011/20050011507.pdf
[firstpage_image] =>[orig_patent_app_number] => 10494490
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/494490 | Projectile firing device using liquified gas propellant | Oct 31, 2002 | Issued |
Array
(
[id] => 6789510
[patent_doc_number] => 20030084854
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-05-08
[patent_title] => 'Drinking trough and method of converting same'
[patent_app_type] => new
[patent_app_number] => 10/282788
[patent_app_country] => US
[patent_app_date] => 2002-10-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 6922
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 73
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0084/20030084854.pdf
[firstpage_image] =>[orig_patent_app_number] => 10282788
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/282788 | Drinking through and method of converting same | Oct 28, 2002 | Issued |
Array
(
[id] => 1243674
[patent_doc_number] => 06676086
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2004-01-13
[patent_title] => 'Tandem kite device'
[patent_app_type] => B1
[patent_app_number] => 10/285878
[patent_app_country] => US
[patent_app_date] => 2002-10-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 1078
[patent_no_of_claims] => 4
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 217
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/676/06676086.pdf
[firstpage_image] =>[orig_patent_app_number] => 10285878
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/285878 | Tandem kite device | Oct 24, 2002 | Issued |
Array
(
[id] => 6666592
[patent_doc_number] => 20030111575
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-06-19
[patent_title] => 'Pneumatic driven propeller related vehicles'
[patent_app_type] => new
[patent_app_number] => 10/277844
[patent_app_country] => US
[patent_app_date] => 2002-10-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[patent_no_of_words] => 2689
[patent_no_of_claims] => 19
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0111/20030111575.pdf
[firstpage_image] =>[orig_patent_app_number] => 10277844
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/277844 | Pneumatic driven propeller related vehicles | Oct 22, 2002 | Issued |
Array
(
[id] => 1187745
[patent_doc_number] => 06732973
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2004-05-11
[patent_title] => 'Stabilizer for a propeller related vehicle'
[patent_app_type] => B1
[patent_app_number] => 10/277691
[patent_app_country] => US
[patent_app_date] => 2002-10-23
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[patent_drawing_sheets_cnt] => 2
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/732/06732973.pdf
[firstpage_image] =>[orig_patent_app_number] => 10277691
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/277691 | Stabilizer for a propeller related vehicle | Oct 22, 2002 | Issued |
Array
(
[id] => 1136385
[patent_doc_number] => 06776376
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-08-17
[patent_title] => 'Flight control surface actuation system'
[patent_app_type] => B2
[patent_app_number] => 10/274024
[patent_app_country] => US
[patent_app_date] => 2002-10-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
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[patent_no_of_words] => 2371
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/776/06776376.pdf
[firstpage_image] =>[orig_patent_app_number] => 10274024
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/274024 | Flight control surface actuation system | Oct 17, 2002 | Issued |
Array
(
[id] => 1286612
[patent_doc_number] => 06629671
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2003-10-07
[patent_title] => 'Airline seat parachute'
[patent_app_type] => B1
[patent_app_number] => 10/273106
[patent_app_country] => US
[patent_app_date] => 2002-10-18
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[pdf_file] => patents/06/629/06629671.pdf
[firstpage_image] =>[orig_patent_app_number] => 10273106
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/273106 | Airline seat parachute | Oct 17, 2002 | Issued |
Array
(
[id] => 1126581
[patent_doc_number] => 06786457
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-09-07
[patent_title] => 'Geometric morphing wing with layers'
[patent_app_type] => B2
[patent_app_number] => 10/268558
[patent_app_country] => US
[patent_app_date] => 2002-10-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/786/06786457.pdf
[firstpage_image] =>[orig_patent_app_number] => 10268558
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/268558 | Geometric morphing wing with layers | Oct 9, 2002 | Issued |
Array
(
[id] => 7058742
[patent_doc_number] => 20050001101
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-01-06
[patent_title] => 'Surface optical reflector, for a space craft such as a geostationary satellite'
[patent_app_type] => utility
[patent_app_number] => 10/491633
[patent_app_country] => US
[patent_app_date] => 2002-09-30
[patent_effective_date] => 0000-00-00
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[pdf_file] => publications/A1/0001/20050001101.pdf
[firstpage_image] =>[orig_patent_app_number] => 10491633
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/491633 | Surface optical reflector, for space craft such as a geostationary satellite | Sep 29, 2002 | Issued |
Array
(
[id] => 1277835
[patent_doc_number] => 06637700
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2003-10-28
[patent_title] => 'Spacecraft protected by a coating including pyroelectric/ferroelectric particles, and the coating material'
[patent_app_type] => B2
[patent_app_number] => 10/262115
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[pdf_file] => patents/06/637/06637700.pdf
[firstpage_image] =>[orig_patent_app_number] => 10262115
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/262115 | Spacecraft protected by a coating including pyroelectric/ferroelectric particles, and the coating material | Sep 29, 2002 | Issued |
Array
(
[id] => 4673150
[patent_doc_number] => 20080210778
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-09-04
[patent_title] => 'Aircraft engine exhaust shroud'
[patent_app_type] => utility
[patent_app_number] => 10/265097
[patent_app_country] => US
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[pdf_file] => publications/A1/0210/20080210778.pdf
[firstpage_image] =>[orig_patent_app_number] => 10265097
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/265097 | Aircraft engine exhaust shroud | Sep 24, 2002 | Issued |
Array
(
[id] => 1120311
[patent_doc_number] => 06793174
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-09-21
[patent_title] => 'Pulsejet augmentor powered VTOL aircraft'
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[patent_app_number] => 10/245145
[patent_app_country] => US
[patent_app_date] => 2002-09-16
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/793/06793174.pdf
[firstpage_image] =>[orig_patent_app_number] => 10245145
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/245145 | Pulsejet augmentor powered VTOL aircraft | Sep 15, 2002 | Issued |