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] => 873885 [patent_doc_number] => 07357357 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2008-04-15 [patent_title] => 'Aircraft mode suppression' [patent_app_type] => utility [patent_app_number] => 11/078646 [patent_app_country] => US [patent_app_date] => 2005-03-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 6197 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 106 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/357/07357357.pdf [firstpage_image] =>[orig_patent_app_number] => 11078646 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/078646
Aircraft mode suppression Mar 10, 2005 Issued
Array ( [id] => 7227245 [patent_doc_number] => 20050269445 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-12-08 [patent_title] => 'Mounting of engine onto an aircraft structure' [patent_app_type] => utility [patent_app_number] => 11/073646 [patent_app_country] => US [patent_app_date] => 2005-03-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 3410 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 6 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0269/20050269445.pdf [firstpage_image] =>[orig_patent_app_number] => 11073646 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/073646
Mounting of engine onto an aircraft structure Mar 7, 2005 Issued
Array ( [id] => 5735889 [patent_doc_number] => 20060006279 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-01-12 [patent_title] => 'CONTROL SYSTEM FOR ROTORCRAFT FOR PREVENTING THE VORTEX RING STATE' [patent_app_type] => utility [patent_app_number] => 11/069396 [patent_app_country] => US [patent_app_date] => 2005-03-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 3881 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 6 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0006/20060006279.pdf [firstpage_image] =>[orig_patent_app_number] => 11069396 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/069396
Control system for rotorcraft for preventing the vortex ring state Feb 28, 2005 Issued
Array ( [id] => 579961 [patent_doc_number] => 07434767 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2008-10-14 [patent_title] => 'Spacecraft adapter having embedded resources, and methods of forming same' [patent_app_type] => utility [patent_app_number] => 11/068343 [patent_app_country] => US [patent_app_date] => 2005-02-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 4 [patent_no_of_words] => 2262 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 112 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/434/07434767.pdf [firstpage_image] =>[orig_patent_app_number] => 11068343 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/068343
Spacecraft adapter having embedded resources, and methods of forming same Feb 27, 2005 Issued
Array ( [id] => 855165 [patent_doc_number] => 07374133 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2008-05-20 [patent_title] => 'Wing having a negative dihedron for towing a load' [patent_app_type] => utility [patent_app_number] => 11/067842 [patent_app_country] => US [patent_app_date] => 2005-02-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 12 [patent_no_of_words] => 4526 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 142 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/374/07374133.pdf [firstpage_image] =>[orig_patent_app_number] => 11067842 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/067842
Wing having a negative dihedron for towing a load Feb 27, 2005 Issued
Array ( [id] => 379478 [patent_doc_number] => 07309047 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2007-12-18 [patent_title] => 'Systems and methods for controlling flexible communication links used for aircraft refueling' [patent_app_type] => utility [patent_app_number] => 11/067331 [patent_app_country] => US [patent_app_date] => 2005-02-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 3399 [patent_no_of_claims] => 25 [patent_no_of_ind_claims] => 7 [patent_words_short_claim] => 99 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/309/07309047.pdf [firstpage_image] =>[orig_patent_app_number] => 11067331 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/067331
Systems and methods for controlling flexible communication links used for aircraft refueling Feb 24, 2005 Issued
Array ( [id] => 6955467 [patent_doc_number] => 20050211837 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-09-29 [patent_title] => 'Interior layout of an aircraft cabin' [patent_app_type] => utility [patent_app_number] => 11/065559 [patent_app_country] => US [patent_app_date] => 2005-02-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 4233 [patent_no_of_claims] => 25 [patent_no_of_ind_claims] => 13 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0211/20050211837.pdf [firstpage_image] =>[orig_patent_app_number] => 11065559 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/065559
Interior layout of an aircraft cabin Feb 24, 2005 Issued
Array ( [id] => 4685461 [patent_doc_number] => 20080029642 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-02-07 [patent_title] => 'FAST-PIVOT MISSILE FLIGHT CONTROL SURFACE' [patent_app_type] => utility [patent_app_number] => 11/067038 [patent_app_country] => US [patent_app_date] => 2005-02-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 4260 [patent_no_of_claims] => 14 [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/A1/0029/20080029642.pdf [firstpage_image] =>[orig_patent_app_number] => 11067038 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/067038
Fast-pivot missile flight control surface Feb 24, 2005 Issued
Array ( [id] => 5222770 [patent_doc_number] => 20070252036 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-11-01 [patent_title] => 'SYSTEMS AND METHODS FOR BRAKING AIRCRAFT, INCLUDING BRAKING INTERMEDIATE MAIN GEARS AND DIFFERENTIAL BRAKING' [patent_app_type] => utility [patent_app_number] => 11/067053 [patent_app_country] => US [patent_app_date] => 2005-02-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 12 [patent_no_of_words] => 5475 [patent_no_of_claims] => 22 [patent_no_of_ind_claims] => 10 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0252/20070252036.pdf [firstpage_image] =>[orig_patent_app_number] => 11067053 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/067053
Systems and methods for braking aircraft, including braking intermediate main gears and differential braking Feb 23, 2005 Issued
Array ( [id] => 5616735 [patent_doc_number] => 20060186267 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-08-24 [patent_title] => 'Systems and methods for braking aircraft, including braking intermediate main gears and differential braking' [patent_app_type] => utility [patent_app_number] => 11/064615 [patent_app_country] => US [patent_app_date] => 2005-02-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 12 [patent_no_of_words] => 5475 [patent_no_of_claims] => 29 [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/A1/0186/20060186267.pdf [firstpage_image] =>[orig_patent_app_number] => 11064615 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/064615
Systems and methods for braking aircraft, including braking intermediate main gears and differential braking Feb 22, 2005 Issued
Array ( [id] => 7202325 [patent_doc_number] => 20050257749 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-11-24 [patent_title] => 'Solar powered bird feeder' [patent_app_type] => utility [patent_app_number] => 11/063059 [patent_app_country] => US [patent_app_date] => 2005-02-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 2229 [patent_no_of_claims] => 7 [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/A1/0257/20050257749.pdf [firstpage_image] =>[orig_patent_app_number] => 11063059 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/063059
Solar powered bird feeder Feb 21, 2005 Issued
Array ( [id] => 611790 [patent_doc_number] => 07147182 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2006-12-12 [patent_title] => 'Gas-powered tip-jet-driven tilt-rotor compound VTOL aircraft' [patent_app_type] => utility [patent_app_number] => 11/062536 [patent_app_country] => US [patent_app_date] => 2005-02-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 13 [patent_no_of_words] => 5163 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 242 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/147/07147182.pdf [firstpage_image] =>[orig_patent_app_number] => 11062536 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/062536
Gas-powered tip-jet-driven tilt-rotor compound VTOL aircraft Feb 21, 2005 Issued
Array ( [id] => 417654 [patent_doc_number] => 07275711 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2007-10-02 [patent_title] => 'Gas-powered tip-jet-driven compound VTOL aircraft' [patent_app_type] => utility [patent_app_number] => 11/062537 [patent_app_country] => US [patent_app_date] => 2005-02-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 12 [patent_no_of_words] => 5969 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 43 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/275/07275711.pdf [firstpage_image] =>[orig_patent_app_number] => 11062537 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/062537
Gas-powered tip-jet-driven compound VTOL aircraft Feb 21, 2005 Issued
Array ( [id] => 450463 [patent_doc_number] => 07246769 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2007-07-24 [patent_title] => 'Vehicles particularly useful as VTOL vehicles' [patent_app_type] => utility [patent_app_number] => 11/061652 [patent_app_country] => US [patent_app_date] => 2005-02-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 23 [patent_no_of_words] => 4958 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 106 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/246/07246769.pdf [firstpage_image] =>[orig_patent_app_number] => 11061652 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/061652
Vehicles particularly useful as VTOL vehicles Feb 21, 2005 Issued
Array ( [id] => 466340 [patent_doc_number] => 07232091 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2007-06-19 [patent_title] => 'Mounting system inserted between an aircraft engine and a rigid structure of an attachment strut fixed under a wing of this aircraft' [patent_app_type] => utility [patent_app_number] => 11/059444 [patent_app_country] => US [patent_app_date] => 2005-02-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 11 [patent_no_of_words] => 10720 [patent_no_of_claims] => 22 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 123 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/232/07232091.pdf [firstpage_image] =>[orig_patent_app_number] => 11059444 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/059444
Mounting system inserted between an aircraft engine and a rigid structure of an attachment strut fixed under a wing of this aircraft Feb 16, 2005 Issued
Array ( [id] => 544067 [patent_doc_number] => 07156343 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2007-01-02 [patent_title] => 'Mounting system inserted between an aircraft engine and a rigid structure of an attachment strut fixed under a wing of this aircraft' [patent_app_type] => utility [patent_app_number] => 11/059440 [patent_app_country] => US [patent_app_date] => 2005-02-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 1 [patent_no_of_words] => 3637 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 41 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/156/07156343.pdf [firstpage_image] =>[orig_patent_app_number] => 11059440 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/059440
Mounting system inserted between an aircraft engine and a rigid structure of an attachment strut fixed under a wing of this aircraft Feb 16, 2005 Issued
Array ( [id] => 5735896 [patent_doc_number] => 20060006286 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-01-12 [patent_title] => 'Hinge cover integration into door seal edges' [patent_app_type] => utility [patent_app_number] => 11/051595 [patent_app_country] => US [patent_app_date] => 2005-02-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 2173 [patent_no_of_claims] => 23 [patent_no_of_ind_claims] => 10 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0006/20060006286.pdf [firstpage_image] =>[orig_patent_app_number] => 11051595 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/051595
Hinge cover integration into door seal edges Feb 3, 2005 Issued
Array ( [id] => 615090 [patent_doc_number] => 07143976 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2006-12-05 [patent_title] => 'UAV arresting hook for use with UAV recovery system' [patent_app_type] => utility [patent_app_number] => 11/051842 [patent_app_country] => US [patent_app_date] => 2005-02-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 12 [patent_no_of_words] => 3040 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 47 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/143/07143976.pdf [firstpage_image] =>[orig_patent_app_number] => 11051842 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/051842
UAV arresting hook for use with UAV recovery system Feb 3, 2005 Issued
Array ( [id] => 6928206 [patent_doc_number] => 20050279238 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-12-22 [patent_title] => 'CURRENT MODULATION-BASED COMMUNICATION FROM SLAVE DEVICE' [patent_app_type] => utility [patent_app_number] => 11/049574 [patent_app_country] => US [patent_app_date] => 2005-02-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 14 [patent_figures_cnt] => 14 [patent_no_of_words] => 9511 [patent_no_of_claims] => 11 [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/A1/0279/20050279238.pdf [firstpage_image] =>[orig_patent_app_number] => 11049574 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/049574
Current modulation-based communication for slave device Jan 31, 2005 Issued
Array ( [id] => 5664497 [patent_doc_number] => 20060169847 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-08-03 [patent_title] => 'Aerospace vehicle leading edge slat devices and corresponding methods' [patent_app_type] => utility [patent_app_number] => 11/048320 [patent_app_country] => US [patent_app_date] => 2005-01-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 5979 [patent_no_of_claims] => 26 [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/A1/0169/20060169847.pdf [firstpage_image] =>[orig_patent_app_number] => 11048320 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/048320
Aerospace vehicle leading edge slat devices and corresponding methods Jan 30, 2005 Issued
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