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] => 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 [patent_figures_cnt] => 14 [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 [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] => 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 [patent_no_of_ind_claims] => 1 [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 [patent_figures_cnt] => 5 [patent_no_of_words] => 4286 [patent_no_of_claims] => 43 [patent_no_of_ind_claims] => 9 [patent_words_short_claim] => 21 [patent_maintenance] => 1 [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 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 215 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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
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