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] => 6780996
[patent_doc_number] => 20030062443
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-04-03
[patent_title] => 'VTOL personal aircraft'
[patent_app_type] => new
[patent_app_number] => 10/114754
[patent_app_country] => US
[patent_app_date] => 2002-04-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 12
[patent_no_of_words] => 10725
[patent_no_of_claims] => 67
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 87
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0062/20030062443.pdf
[firstpage_image] =>[orig_patent_app_number] => 10114754
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/114754 | VTOL personal aircraft | Apr 1, 2002 | Abandoned |
Array
(
[id] => 1260576
[patent_doc_number] => 06659393
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2003-12-09
[patent_title] => 'Retarding and lock apparatus and method for retardation and interlocking of elements'
[patent_app_type] => B1
[patent_app_number] => 09/980948
[patent_app_country] => US
[patent_app_date] => 2002-03-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 13
[patent_no_of_words] => 2194
[patent_no_of_claims] => 13
[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/06/659/06659393.pdf
[firstpage_image] =>[orig_patent_app_number] => 09980948
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/980948 | Retarding and lock apparatus and method for retardation and interlocking of elements | Mar 28, 2002 | Issued |
Array
(
[id] => 6646024
[patent_doc_number] => 20030075641
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-04-24
[patent_title] => 'RADAR-GUIDED MISSILE PROGRAMMABLE DIGITAL PREDETECTION SIGNAL PROCESSOR'
[patent_app_type] => new
[patent_app_number] => 10/108477
[patent_app_country] => US
[patent_app_date] => 2002-03-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 4819
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 135
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0075/20030075641.pdf
[firstpage_image] =>[orig_patent_app_number] => 10108477
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/108477 | Radar-guided missile programmable digital predetection signal processor | Mar 26, 2002 | Issued |
Array
(
[id] => 6794588
[patent_doc_number] => 20030173461
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-09-18
[patent_title] => 'Spaceshuttle forked observatory'
[patent_app_type] => new
[patent_app_number] => 10/100728
[patent_app_country] => US
[patent_app_date] => 2002-03-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 456
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 30
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0173/20030173461.pdf
[firstpage_image] =>[orig_patent_app_number] => 10100728
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/100728 | Spaceshuttle forked observatory | Mar 17, 2002 | Abandoned |
Array
(
[id] => 6794590
[patent_doc_number] => 20030173463
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-09-18
[patent_title] => 'Spaceshuttle double observatory'
[patent_app_type] => new
[patent_app_number] => 10/100730
[patent_app_country] => US
[patent_app_date] => 2002-03-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 704
[patent_no_of_claims] => 3
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 38
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0173/20030173463.pdf
[firstpage_image] =>[orig_patent_app_number] => 10100730
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/100730 | Spaceshuttle double observatory | Mar 17, 2002 | Abandoned |
Array
(
[id] => 6794593
[patent_doc_number] => 20030173466
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-09-18
[patent_title] => 'Spaceshuttle observatory'
[patent_app_type] => new
[patent_app_number] => 10/100733
[patent_app_country] => US
[patent_app_date] => 2002-03-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 823
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 23
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0173/20030173466.pdf
[firstpage_image] =>[orig_patent_app_number] => 10100733
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/100733 | Spaceshuttle observatory | Mar 17, 2002 | Abandoned |
Array
(
[id] => 6413800
[patent_doc_number] => 20020125367
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-09-12
[patent_title] => 'Combination fixed and rotating wing aircraft, land vehicle and water craft'
[patent_app_type] => new
[patent_app_number] => 10/096747
[patent_app_country] => US
[patent_app_date] => 2002-03-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 1754
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 205
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0125/20020125367.pdf
[firstpage_image] =>[orig_patent_app_number] => 10096747
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/096747 | Combination fixed and rotating wing aircraft, land vehicle and water craft | Mar 11, 2002 | Abandoned |
Array
(
[id] => 1271371
[patent_doc_number] => 06644598
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2003-11-11
[patent_title] => 'Modification of fluid flow about bodies and surfaces through virtual aero-shaping of airfoils with synthetic jet actuators'
[patent_app_type] => B2
[patent_app_number] => 10/094194
[patent_app_country] => US
[patent_app_date] => 2002-03-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 30
[patent_no_of_words] => 8770
[patent_no_of_claims] => 36
[patent_no_of_ind_claims] => 9
[patent_words_short_claim] => 104
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/644/06644598.pdf
[firstpage_image] =>[orig_patent_app_number] => 10094194
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/094194 | Modification of fluid flow about bodies and surfaces through virtual aero-shaping of airfoils with synthetic jet actuators | Mar 7, 2002 | Issued |
Array
(
[id] => 6413826
[patent_doc_number] => 20020125370
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-09-12
[patent_title] => 'System driving the displaceable fairing of a turbojet-engine thrust reverser'
[patent_app_type] => new
[patent_app_number] => 10/092881
[patent_app_country] => US
[patent_app_date] => 2002-03-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 3257
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 233
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0125/20020125370.pdf
[firstpage_image] =>[orig_patent_app_number] => 10092881
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/092881 | System driving the displaceable fairing of a turbojet-engine thrust reverser | Mar 7, 2002 | Issued |
Array
(
[id] => 5782614
[patent_doc_number] => 20020158164
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-10-31
[patent_title] => 'Cockpit for light airplanes'
[patent_app_type] => new
[patent_app_number] => 10/084760
[patent_app_country] => US
[patent_app_date] => 2002-02-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 1204
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 64
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0158/20020158164.pdf
[firstpage_image] =>[orig_patent_app_number] => 10084760
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/084760 | Cockpit for light airplanes | Feb 21, 2002 | Abandoned |
Array
(
[id] => 1268827
[patent_doc_number] => 06648433
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2003-11-18
[patent_title] => 'Spiralling missileB'
[patent_app_type] => B2
[patent_app_number] => 10/067964
[patent_app_country] => US
[patent_app_date] => 2002-02-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 2390
[patent_no_of_claims] => 34
[patent_no_of_ind_claims] => 17
[patent_words_short_claim] => 31
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/648/06648433.pdf
[firstpage_image] =>[orig_patent_app_number] => 10067964
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/067964 | Spiralling missileB | Feb 7, 2002 | Issued |
Array
(
[id] => 1210120
[patent_doc_number] => 06708928
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-03-23
[patent_title] => 'Variable spacer for a separation system of a launch vehicle'
[patent_app_type] => B2
[patent_app_number] => 10/060439
[patent_app_country] => US
[patent_app_date] => 2002-01-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 7
[patent_no_of_words] => 3848
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 106
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/708/06708928.pdf
[firstpage_image] =>[orig_patent_app_number] => 10060439
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/060439 | Variable spacer for a separation system of a launch vehicle | Jan 29, 2002 | Issued |
Array
(
[id] => 6364964
[patent_doc_number] => 20020117580
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-08-29
[patent_title] => '2-D projectile trajectory corrector'
[patent_app_type] => new
[patent_app_number] => 10/060078
[patent_app_country] => US
[patent_app_date] => 2002-01-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 5398
[patent_no_of_claims] => 60
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 32
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0117/20020117580.pdf
[firstpage_image] =>[orig_patent_app_number] => 10060078
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/060078 | 2-D projectile trajectory corrector | Jan 28, 2002 | Issued |
Array
(
[id] => 5981659
[patent_doc_number] => 20020096600
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-07-25
[patent_title] => 'Aircraft and watercraft adapted to float on main wing'
[patent_app_type] => new
[patent_app_number] => 10/050591
[patent_app_country] => US
[patent_app_date] => 2002-01-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 3724
[patent_no_of_claims] => 30
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 58
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0096/20020096600.pdf
[firstpage_image] =>[orig_patent_app_number] => 10050591
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/050591 | Aircraft and watercraft adapted to float on main wing | Jan 17, 2002 | Abandoned |
Array
(
[id] => 1525589
[patent_doc_number] => 06478259
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2002-11-12
[patent_title] => 'Spacecraft protected by a coating including pyroelectric/ferroelectric particles, and the coating material'
[patent_app_type] => B2
[patent_app_number] => 10/051672
[patent_app_country] => US
[patent_app_date] => 2002-01-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 9
[patent_no_of_words] => 7439
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/478/06478259.pdf
[firstpage_image] =>[orig_patent_app_number] => 10051672
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/051672 | Spacecraft protected by a coating including pyroelectric/ferroelectric particles, and the coating material | Jan 15, 2002 | Issued |
Array
(
[id] => 6545847
[patent_doc_number] => 20020193914
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-12-19
[patent_title] => 'Remote control powered parafoil aircraft'
[patent_app_type] => new
[patent_app_number] => 10/045777
[patent_app_country] => US
[patent_app_date] => 2002-01-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 2535
[patent_no_of_claims] => 38
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 105
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0193/20020193914.pdf
[firstpage_image] =>[orig_patent_app_number] => 10045777
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/045777 | Remote control powered parafoil aircraft | Jan 10, 2002 | Abandoned |
09/914047 | Foldable/collapsible structures | Jan 8, 2002 | Abandoned |
Array
(
[id] => 1149825
[patent_doc_number] => 06761336
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-07-13
[patent_title] => 'Aircraft tailstrike avoidance system'
[patent_app_type] => B2
[patent_app_number] => 10/043401
[patent_app_country] => US
[patent_app_date] => 2002-01-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 13
[patent_no_of_words] => 6351
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 2
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[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/761/06761336.pdf
[firstpage_image] =>[orig_patent_app_number] => 10043401
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/043401 | Aircraft tailstrike avoidance system | Jan 7, 2002 | Issued |
Array
(
[id] => 6569047
[patent_doc_number] => 20020084386
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-07-04
[patent_title] => 'Inflatable airfoils, and elevated and propulsion driven vehicles'
[patent_app_type] => new
[patent_app_number] => 10/035856
[patent_app_country] => US
[patent_app_date] => 2002-01-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 38
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0084/20020084386.pdf
[firstpage_image] =>[orig_patent_app_number] => 10035856
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/035856 | Inflatable airfoils, and elevated and propulsion driven vehicles | Jan 3, 2002 | Issued |
Array
(
[id] => 1329489
[patent_doc_number] => 06588702
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2003-07-08
[patent_title] => 'Lighter-than-air device having a flexible usable surface'
[patent_app_type] => B2
[patent_app_number] => 10/028736
[patent_app_country] => US
[patent_app_date] => 2001-12-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/588/06588702.pdf
[firstpage_image] =>[orig_patent_app_number] => 10028736
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/028736 | Lighter-than-air device having a flexible usable surface | Dec 27, 2001 | Issued |