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] => 224017
[patent_doc_number] => 07604198
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2009-10-20
[patent_title] => 'Rotorcraft having coaxial counter-rotating rotors which produce both vertical and horizontal thrust and method of controlled flight in all six degrees of freedom'
[patent_app_type] => utility
[patent_app_number] => 10/672003
[patent_app_country] => US
[patent_app_date] => 2003-09-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 23
[patent_figures_cnt] => 34
[patent_no_of_words] => 11485
[patent_no_of_claims] => 26
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 233
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/604/07604198.pdf
[firstpage_image] =>[orig_patent_app_number] => 10672003
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/672003 | Rotorcraft having coaxial counter-rotating rotors which produce both vertical and horizontal thrust and method of controlled flight in all six degrees of freedom | Sep 24, 2003 | Issued |
Array
(
[id] => 7008200
[patent_doc_number] => 20050061916
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-03-24
[patent_title] => 'Cross section for a supersonic airplane'
[patent_app_type] => utility
[patent_app_number] => 10/668823
[patent_app_country] => US
[patent_app_date] => 2003-09-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 4914
[patent_no_of_claims] => 48
[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/A1/0061/20050061916.pdf
[firstpage_image] =>[orig_patent_app_number] => 10668823
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/668823 | Cross section for a supersonic airplane | Sep 21, 2003 | Issued |
Array
(
[id] => 7078649
[patent_doc_number] => 20050044770
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-03-03
[patent_title] => 'Two barreled ferrule fishing lure'
[patent_app_type] => utility
[patent_app_number] => 10/654854
[patent_app_country] => US
[patent_app_date] => 2003-09-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 1769
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0044/20050044770.pdf
[firstpage_image] =>[orig_patent_app_number] => 10654854
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/654854 | Two barreled ferrule fishing lure | Sep 2, 2003 | Abandoned |
Array
(
[id] => 7080384
[patent_doc_number] => 20050045764
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-03-03
[patent_title] => 'Canard position and dihedral for boom reduction and pitch/directional control'
[patent_app_type] => utility
[patent_app_number] => 10/652128
[patent_app_country] => US
[patent_app_date] => 2003-08-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 18
[patent_figures_cnt] => 18
[patent_no_of_words] => 5757
[patent_no_of_claims] => 20
[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/A1/0045/20050045764.pdf
[firstpage_image] =>[orig_patent_app_number] => 10652128
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/652128 | Canard position and dihedral for boom reduction and pitch/directional control | Aug 28, 2003 | Abandoned |
Array
(
[id] => 692557
[patent_doc_number] => 07070146
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2006-07-04
[patent_title] => 'Aircraft thickness/camber control device for low sonic boom'
[patent_app_type] => utility
[patent_app_number] => 10/651782
[patent_app_country] => US
[patent_app_date] => 2003-08-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 14
[patent_figures_cnt] => 18
[patent_no_of_words] => 5881
[patent_no_of_claims] => 21
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 96
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/070/07070146.pdf
[firstpage_image] =>[orig_patent_app_number] => 10651782
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/651782 | Aircraft thickness/camber control device for low sonic boom | Aug 28, 2003 | Issued |
Array
(
[id] => 7219670
[patent_doc_number] => 20050077429
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-04-14
[patent_title] => 'Method for producing lateral ejection apparattii for helicopter or plane'
[patent_app_type] => utility
[patent_app_number] => 10/645044
[patent_app_country] => US
[patent_app_date] => 2003-08-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 2821
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0077/20050077429.pdf
[firstpage_image] =>[orig_patent_app_number] => 10645044
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/645044 | Method for producing lateral ejection apparattii for helicopter or plane | Aug 17, 2003 | Abandoned |
Array
(
[id] => 7267636
[patent_doc_number] => 20040056154
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-03-25
[patent_title] => 'VTOL personal aircraft'
[patent_app_type] => new
[patent_app_number] => 10/640123
[patent_app_country] => US
[patent_app_date] => 2003-08-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2036
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 141
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0056/20040056154.pdf
[firstpage_image] =>[orig_patent_app_number] => 10640123
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/640123 | VTOL personal aircraft | Aug 12, 2003 | Issued |
Array
(
[id] => 7205198
[patent_doc_number] => 20050258305
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-11-24
[patent_title] => 'Dual hull airship controlled by thrust vectoring'
[patent_app_type] => utility
[patent_app_number] => 10/523238
[patent_app_country] => US
[patent_app_date] => 2003-08-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2978
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0258/20050258305.pdf
[firstpage_image] =>[orig_patent_app_number] => 10523238
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/523238 | Dual hull airship controlled by thrust vectoring | Aug 10, 2003 | Issued |
Array
(
[id] => 7620997
[patent_doc_number] => 06942180
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2005-09-13
[patent_title] => 'Steerable dual wheel power tug for aircraft'
[patent_app_type] => utility
[patent_app_number] => 10/636175
[patent_app_country] => US
[patent_app_date] => 2003-08-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 18
[patent_figures_cnt] => 27
[patent_no_of_words] => 3652
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 227
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/942/06942180.pdf
[firstpage_image] =>[orig_patent_app_number] => 10636175
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/636175 | Steerable dual wheel power tug for aircraft | Aug 6, 2003 | Issued |
Array
(
[id] => 7147229
[patent_doc_number] => 20050023412
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-02-03
[patent_title] => 'Nacelle inlet lip anti-icing with engine oil'
[patent_app_type] => utility
[patent_app_number] => 10/628368
[patent_app_country] => US
[patent_app_date] => 2003-07-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 3260
[patent_no_of_claims] => 25
[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/A1/0023/20050023412.pdf
[firstpage_image] =>[orig_patent_app_number] => 10628368
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/628368 | Nacelle inlet lip anti-icing with engine oil | Jul 28, 2003 | Issued |
Array
(
[id] => 983605
[patent_doc_number] => 06922939
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2005-08-02
[patent_title] => 'Fishing lure'
[patent_app_type] => utility
[patent_app_number] => 10/627077
[patent_app_country] => US
[patent_app_date] => 2003-07-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 13
[patent_no_of_words] => 5220
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 102
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/922/06922939.pdf
[firstpage_image] =>[orig_patent_app_number] => 10627077
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/627077 | Fishing lure | Jul 24, 2003 | Issued |
Array
(
[id] => 5773681
[patent_doc_number] => 20060102794
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-05-18
[patent_title] => 'Control apparatus for kite powered conveyance device'
[patent_app_type] => utility
[patent_app_number] => 10/522684
[patent_app_country] => US
[patent_app_date] => 2003-07-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 11
[patent_no_of_words] => 3382
[patent_no_of_claims] => 41
[patent_no_of_ind_claims] => 16
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0102/20060102794.pdf
[firstpage_image] =>[orig_patent_app_number] => 10522684
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/522684 | Control apparatus for kite powered conveyance device | Jul 20, 2003 | Issued |
Array
(
[id] => 942652
[patent_doc_number] => 06966262
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2005-11-22
[patent_title] => 'Current modulation-based communication from slave device'
[patent_app_type] => utility
[patent_app_number] => 10/619687
[patent_app_country] => US
[patent_app_date] => 2003-07-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
[patent_figures_cnt] => 17
[patent_no_of_words] => 9486
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 72
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/966/06966262.pdf
[firstpage_image] =>[orig_patent_app_number] => 10619687
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/619687 | Current modulation-based communication from slave device | Jul 14, 2003 | Issued |
Array
(
[id] => 7147231
[patent_doc_number] => 20050023413
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-02-03
[patent_title] => 'Aircraft cabin module'
[patent_app_type] => utility
[patent_app_number] => 10/477614
[patent_app_country] => US
[patent_app_date] => 2003-07-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 3964
[patent_no_of_claims] => 29
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0023/20050023413.pdf
[firstpage_image] =>[orig_patent_app_number] => 10477614
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/477614 | Aircraft cabin module | Jul 14, 2003 | Issued |
Array
(
[id] => 7337984
[patent_doc_number] => 20040245380
[patent_country] => US
[patent_kind] => A9
[patent_issue_date] => 2004-12-09
[patent_title] => 'Passive aerodynamic sonic boom suppression for supersonic aircraft'
[patent_app_type] => corrected
[patent_app_number] => 10/614393
[patent_app_country] => US
[patent_app_date] => 2003-07-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 14
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[patent_no_of_words] => 4861
[patent_no_of_claims] => 28
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 81
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A9/0245/20040245380.pdf
[firstpage_image] =>[orig_patent_app_number] => 10614393
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/614393 | Passive aerodynamic sonic boom suppression for supersonic aircraft | Jul 2, 2003 | Issued |
Array
(
[id] => 7337984
[patent_doc_number] => 20040245380
[patent_country] => US
[patent_kind] => A9
[patent_issue_date] => 2004-12-09
[patent_title] => 'Passive aerodynamic sonic boom suppression for supersonic aircraft'
[patent_app_type] => corrected
[patent_app_number] => 10/614393
[patent_app_country] => US
[patent_app_date] => 2003-07-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 14
[patent_figures_cnt] => 14
[patent_no_of_words] => 4861
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[patent_no_of_ind_claims] => 4
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A9/0245/20040245380.pdf
[firstpage_image] =>[orig_patent_app_number] => 10614393
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/614393 | Passive aerodynamic sonic boom suppression for supersonic aircraft | Jul 2, 2003 | Issued |
Array
(
[id] => 249937
[patent_doc_number] => 07581692
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2009-09-01
[patent_title] => 'Fluidic chevrons and configurable thermal shield for jet noise reduction'
[patent_app_type] => utility
[patent_app_number] => 10/610718
[patent_app_country] => US
[patent_app_date] => 2003-06-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 13
[patent_no_of_words] => 2426
[patent_no_of_claims] => 8
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[patent_words_short_claim] => 66
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/581/07581692.pdf
[firstpage_image] =>[orig_patent_app_number] => 10610718
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/610718 | Fluidic chevrons and configurable thermal shield for jet noise reduction | Jun 29, 2003 | Issued |
Array
(
[id] => 7403130
[patent_doc_number] => 20040262451
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-12-30
[patent_title] => 'EFFICIENT WING TIP DEVICES AND METHODS FOR INCORPORATING SUCH DEVICES INTO EXISTING WING DESIGNS'
[patent_app_type] => new
[patent_app_number] => 10/611212
[patent_app_country] => US
[patent_app_date] => 2003-06-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_no_of_words] => 4286
[patent_no_of_claims] => 43
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0262/20040262451.pdf
[firstpage_image] =>[orig_patent_app_number] => 10611212
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/611212 | Efficient wing tip devices and methods for incorporating such devices into existing wing designs | Jun 29, 2003 | Issued |
Array
(
[id] => 7356586
[patent_doc_number] => 20040004157
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-01-08
[patent_title] => 'Lighweight remotely controlled aircraft'
[patent_app_type] => new
[patent_app_number] => 10/296137
[patent_app_country] => US
[patent_app_date] => 2003-06-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 11
[patent_no_of_words] => 5232
[patent_no_of_claims] => 22
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[patent_words_short_claim] => 215
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0004/20040004157.pdf
[firstpage_image] =>[orig_patent_app_number] => 10296137
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/296137 | Lightweight remotely controlled aircraft | Jun 29, 2003 | Issued |
Array
(
[id] => 7362912
[patent_doc_number] => 20040025478
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-02-12
[patent_title] => 'Artificial manes'
[patent_app_type] => new
[patent_app_number] => 10/399094
[patent_app_country] => US
[patent_app_date] => 2003-06-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 4214
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 26
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0025/20040025478.pdf
[firstpage_image] =>[orig_patent_app_number] => 10399094
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/399094 | Artificial manes | Jun 23, 2003 | Abandoned |