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] => 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 |