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] => 6237226
[patent_doc_number] => 20020043590
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-04-18
[patent_title] => 'Subdermally-reinforced elastomeric transitions'
[patent_app_type] => new
[patent_app_number] => 09/943271
[patent_app_country] => US
[patent_app_date] => 2001-08-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 3836
[patent_no_of_claims] => 28
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 90
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0043/20020043590.pdf
[firstpage_image] =>[orig_patent_app_number] => 09943271
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/943271 | Subdermally-reinforced elastomeric transitions | Aug 29, 2001 | Issued |
Array
(
[id] => 1243663
[patent_doc_number] => 06676075
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-01-13
[patent_title] => 'Airplane hard landing indication system'
[patent_app_type] => B2
[patent_app_number] => 09/943539
[patent_app_country] => US
[patent_app_date] => 2001-08-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 7
[patent_no_of_words] => 2316
[patent_no_of_claims] => 4
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 69
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/676/06676075.pdf
[firstpage_image] =>[orig_patent_app_number] => 09943539
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/943539 | Airplane hard landing indication system | Aug 29, 2001 | Issued |
Array
(
[id] => 1271349
[patent_doc_number] => 06644593
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2003-11-11
[patent_title] => 'Aircraft seat mounted passenger interface'
[patent_app_type] => B2
[patent_app_number] => 09/941497
[patent_app_country] => US
[patent_app_date] => 2001-08-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 3
[patent_no_of_words] => 2013
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 107
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/644/06644593.pdf
[firstpage_image] =>[orig_patent_app_number] => 09941497
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/941497 | Aircraft seat mounted passenger interface | Aug 28, 2001 | Issued |
Array
(
[id] => 6348333
[patent_doc_number] => 20020056787
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-05-16
[patent_title] => 'Aircraft supplemental air heater'
[patent_app_type] => new
[patent_app_number] => 09/932394
[patent_app_country] => US
[patent_app_date] => 2001-08-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 4389
[patent_no_of_claims] => 28
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 87
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0056/20020056787.pdf
[firstpage_image] =>[orig_patent_app_number] => 09932394
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/932394 | Aircraft supplemental air heater | Aug 16, 2001 | Issued |
Array
(
[id] => 6836406
[patent_doc_number] => 20030033746
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-02-20
[patent_title] => 'Live well cooling and aeration system'
[patent_app_type] => new
[patent_app_number] => 09/930363
[patent_app_country] => US
[patent_app_date] => 2001-08-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 2595
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 69
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0033/20030033746.pdf
[firstpage_image] =>[orig_patent_app_number] => 09930363
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/930363 | Live well cooling and aeration system | Aug 15, 2001 | Abandoned |
Array
(
[id] => 1400726
[patent_doc_number] => 06513753
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2003-02-04
[patent_title] => 'Transmission support structure for a rotary wing aircraft'
[patent_app_type] => B1
[patent_app_number] => 09/930340
[patent_app_country] => US
[patent_app_date] => 2001-08-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 8
[patent_no_of_words] => 2225
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 72
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/513/06513753.pdf
[firstpage_image] =>[orig_patent_app_number] => 09930340
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/930340 | Transmission support structure for a rotary wing aircraft | Aug 13, 2001 | Issued |
Array
(
[id] => 1446607
[patent_doc_number] => 06454216
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-09-24
[patent_title] => 'Reusable booster for the first stage of a launcher'
[patent_app_type] => B1
[patent_app_number] => 09/869273
[patent_app_country] => US
[patent_app_date] => 2001-08-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 11
[patent_no_of_words] => 5115
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 325
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/454/06454216.pdf
[firstpage_image] =>[orig_patent_app_number] => 09869273
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/869273 | Reusable booster for the first stage of a launcher | Aug 7, 2001 | Issued |
Array
(
[id] => 6713694
[patent_doc_number] => 20030025042
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-02-06
[patent_title] => 'Solar wing and tether mechanisms for asteroid uncooperative docking and asteroid orbit adjustments'
[patent_app_type] => new
[patent_app_number] => 09/923260
[patent_app_country] => US
[patent_app_date] => 2001-08-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 1822
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 43
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0025/20030025042.pdf
[firstpage_image] =>[orig_patent_app_number] => 09923260
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/923260 | Solar wing and tether mechanisms for asteroid uncooperative docking and asteroid orbit adjustments | Aug 5, 2001 | Abandoned |
Array
(
[id] => 5798351
[patent_doc_number] => 20020008176
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-01-24
[patent_title] => 'Suspension for air generation units in aircraft'
[patent_app_type] => new
[patent_app_number] => 09/908481
[patent_app_country] => US
[patent_app_date] => 2001-07-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 4628
[patent_no_of_claims] => 25
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 151
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0008/20020008176.pdf
[firstpage_image] =>[orig_patent_app_number] => 09908481
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/908481 | Suspension for air generation units in aircraft | Jul 17, 2001 | Issued |
Array
(
[id] => 1525594
[patent_doc_number] => 06478262
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-11-12
[patent_title] => 'Flight control system for a hybrid aircraft in the yaw axis'
[patent_app_type] => B1
[patent_app_number] => 09/907068
[patent_app_country] => US
[patent_app_date] => 2001-07-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 8
[patent_no_of_words] => 3345
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 136
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/478/06478262.pdf
[firstpage_image] =>[orig_patent_app_number] => 09907068
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/907068 | Flight control system for a hybrid aircraft in the yaw axis | Jul 16, 2001 | Issued |
Array
(
[id] => 1598698
[patent_doc_number] => 06431494
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-08-13
[patent_title] => 'Flight control system for a hybrid aircraft in the roll axis'
[patent_app_type] => B1
[patent_app_number] => 09/907006
[patent_app_country] => US
[patent_app_date] => 2001-07-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 8
[patent_no_of_words] => 3612
[patent_no_of_claims] => 19
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/431/06431494.pdf
[firstpage_image] =>[orig_patent_app_number] => 09907006
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/907006 | Flight control system for a hybrid aircraft in the roll axis | Jul 16, 2001 | Issued |
Array
(
[id] => 6221656
[patent_doc_number] => 20020003189
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-01-10
[patent_title] => 'Articulated drive'
[patent_app_type] => new
[patent_app_number] => 09/903782
[patent_app_country] => US
[patent_app_date] => 2001-07-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 10289
[patent_no_of_claims] => 44
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0003/20020003189.pdf
[firstpage_image] =>[orig_patent_app_number] => 09903782
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/903782 | Articulated drive | Jul 10, 2001 | Issued |
Array
(
[id] => 1463382
[patent_doc_number] => 06457675
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-10-01
[patent_title] => 'Hydraulic actuation system for cargo doors with cam-type latches'
[patent_app_type] => B1
[patent_app_number] => 09/891582
[patent_app_country] => US
[patent_app_date] => 2001-06-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 21
[patent_no_of_words] => 6004
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/457/06457675.pdf
[firstpage_image] =>[orig_patent_app_number] => 09891582
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/891582 | Hydraulic actuation system for cargo doors with cam-type latches | Jun 24, 2001 | Issued |
Array
(
[id] => 5948292
[patent_doc_number] => 20020005458
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-01-17
[patent_title] => 'Airfoil suitable for forward and reverse flow'
[patent_app_type] => new
[patent_app_number] => 09/877268
[patent_app_country] => US
[patent_app_date] => 2001-06-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[patent_no_of_words] => 2277
[patent_no_of_claims] => 12
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[patent_words_short_claim] => 102
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0005/20020005458.pdf
[firstpage_image] =>[orig_patent_app_number] => 09877268
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/877268 | Airfoil suitable for forward and reverse flow | Jun 7, 2001 | Abandoned |
Array
(
[id] => 6028497
[patent_doc_number] => 20020017592
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-02-14
[patent_title] => 'Method and device for improving the thermal comfort in passenger airplanes'
[patent_app_type] => new
[patent_app_number] => 09/874371
[patent_app_country] => US
[patent_app_date] => 2001-06-06
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0017/20020017592.pdf
[firstpage_image] =>[orig_patent_app_number] => 09874371
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/874371 | Method and device for improving the thermal comfort in passenger airplanes | Jun 5, 2001 | Issued |
Array
(
[id] => 1345054
[patent_doc_number] => 06572052
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2003-06-03
[patent_title] => 'Process and device for determining roll angle'
[patent_app_type] => B1
[patent_app_number] => 09/830254
[patent_app_country] => US
[patent_app_date] => 2001-06-06
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/572/06572052.pdf
[firstpage_image] =>[orig_patent_app_number] => 09830254
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/830254 | Process and device for determining roll angle | Jun 5, 2001 | Issued |
Array
(
[id] => 6881577
[patent_doc_number] => 20010048049
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2001-12-06
[patent_title] => 'Landing gear shock absorber with variable viscosity fluid'
[patent_app_type] => new
[patent_app_number] => 09/863658
[patent_app_country] => US
[patent_app_date] => 2001-05-23
[patent_effective_date] => 0000-00-00
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[pdf_file] => publications/A1/0048/20010048049.pdf
[firstpage_image] =>[orig_patent_app_number] => 09863658
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/863658 | Landing gear shock absorber with variable viscosity fluid | May 22, 2001 | Issued |
Array
(
[id] => 5885610
[patent_doc_number] => 20020011539
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-01-31
[patent_title] => 'Hovering gyro aircraft'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 09/862940 | Hovering gyro aircraft | May 21, 2001 | Issued |
Array
(
[id] => 5948297
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[patent_kind] => A1
[patent_issue_date] => 2002-01-17
[patent_title] => 'Deployment system for a moveable wing surface'
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[firstpage_image] =>[orig_patent_app_number] => 09860000
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/860000 | Deployment system for a moveable wing surface | May 16, 2001 | Abandoned |
Array
(
[id] => 6382547
[patent_doc_number] => 20020179775
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[patent_title] => 'Spacecraft dependent on non-intrusive servicing'
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0179/20020179775.pdf
[firstpage_image] =>[orig_patent_app_number] => 09845370
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/845370 | Spacecraft dependent on non-intrusive servicing | Apr 29, 2001 | Abandoned |