Search

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 numberTitle of the applicationFiling DateStatus
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 [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/06/431/06431494.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 [patent_no_of_ind_claims] => 21 [patent_words_short_claim] => 24 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 393 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_figures_cnt] => 3 [patent_no_of_words] => 2277 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 3 [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 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 1978 [patent_no_of_claims] => 22 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 55 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 7 [patent_no_of_words] => 2265 [patent_no_of_claims] => 2 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 182 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 3200 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 68 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [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' [patent_app_type] => new [patent_app_number] => 09/862940 [patent_app_country] => US [patent_app_date] => 2001-05-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 3154 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 5 [patent_words_short_claim] => 62 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0011/20020011539.pdf [firstpage_image] =>[orig_patent_app_number] => 09862940 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/862940
Hovering gyro aircraft May 21, 2001 Issued
Array ( [id] => 5948297 [patent_doc_number] => 20020005462 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2002-01-17 [patent_title] => 'Deployment system for a moveable wing surface' [patent_app_type] => new [patent_app_number] => 09/860000 [patent_app_country] => US [patent_app_date] => 2001-05-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 4113 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 95 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0005/20020005462.pdf [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 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2002-12-05 [patent_title] => 'Spacecraft dependent on non-intrusive servicing' [patent_app_type] => new [patent_app_number] => 09/845370 [patent_app_country] => US [patent_app_date] => 2001-04-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 5201 [patent_no_of_claims] => 28 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 71 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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
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