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
09/647168 Method for deploying an emergency parachute and parachute system comprising a parachute deployed according to said method Oct 10, 2000 Abandoned
Array ( [id] => 1490369 [patent_doc_number] => 06402092 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-06-11 [patent_title] => 'Turbojet-engine thrust reverser with doors mounted on centered pivots' [patent_app_type] => B1 [patent_app_number] => 09/684677 [patent_app_country] => US [patent_app_date] => 2000-10-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 9 [patent_no_of_words] => 1864 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 247 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/402/06402092.pdf [firstpage_image] =>[orig_patent_app_number] => 09684677 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/684677
Turbojet-engine thrust reverser with doors mounted on centered pivots Oct 10, 2000 Issued
Array ( [id] => 1580820 [patent_doc_number] => 06357697 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-03-19 [patent_title] => 'Kite structure' [patent_app_type] => B1 [patent_app_number] => 09/686568 [patent_app_country] => US [patent_app_date] => 2000-10-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 1423 [patent_no_of_claims] => 5 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 210 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/357/06357697.pdf [firstpage_image] =>[orig_patent_app_number] => 09686568 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/686568
Kite structure Oct 10, 2000 Issued
09/676968 Composite skin panel opening edge and method for manufacture Oct 1, 2000 Abandoned
Array ( [id] => 1562704 [patent_doc_number] => 06338456 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-01-15 [patent_title] => 'Landing impact absorbing deployment system for aircraft with damaged landing gear' [patent_app_type] => B1 [patent_app_number] => 09/671861 [patent_app_country] => US [patent_app_date] => 2000-09-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 4 [patent_no_of_words] => 1033 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 83 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/338/06338456.pdf [firstpage_image] =>[orig_patent_app_number] => 09671861 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/671861
Landing impact absorbing deployment system for aircraft with damaged landing gear Sep 27, 2000 Issued
Array ( [id] => 1499466 [patent_doc_number] => 06464173 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-10-15 [patent_title] => 'Paradrogue assembly' [patent_app_type] => B1 [patent_app_number] => 09/672671 [patent_app_country] => US [patent_app_date] => 2000-09-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 8 [patent_no_of_words] => 1241 [patent_no_of_claims] => 7 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 76 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/464/06464173.pdf [firstpage_image] =>[orig_patent_app_number] => 09672671 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/672671
Paradrogue assembly Sep 27, 2000 Issued
Array ( [id] => 1449506 [patent_doc_number] => 06460802 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-10-08 [patent_title] => 'Helicopter propulsion and control system' [patent_app_type] => B1 [patent_app_number] => 09/660784 [patent_app_country] => US [patent_app_date] => 2000-09-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 9 [patent_no_of_words] => 4955 [patent_no_of_claims] => 38 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 157 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/460/06460802.pdf [firstpage_image] =>[orig_patent_app_number] => 09660784 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/660784
Helicopter propulsion and control system Sep 12, 2000 Issued
Array ( [id] => 1483895 [patent_doc_number] => 06427947 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-08-06 [patent_title] => 'Interface pallet system' [patent_app_type] => B1 [patent_app_number] => 09/656486 [patent_app_country] => US [patent_app_date] => 2000-09-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 7 [patent_no_of_words] => 3203 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 153 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/427/06427947.pdf [firstpage_image] =>[orig_patent_app_number] => 09656486 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/656486
Interface pallet system Sep 6, 2000 Issued
Array ( [id] => 1558067 [patent_doc_number] => 06360989 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-03-26 [patent_title] => 'Nacelle assembly for a gas turbine engine' [patent_app_type] => B1 [patent_app_number] => 09/657266 [patent_app_country] => US [patent_app_date] => 2000-09-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 12 [patent_no_of_words] => 3368 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 97 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/360/06360989.pdf [firstpage_image] =>[orig_patent_app_number] => 09657266 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/657266
Nacelle assembly for a gas turbine engine Sep 6, 2000 Issued
Array ( [id] => 1588766 [patent_doc_number] => 06382560 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-05-07 [patent_title] => 'High speed vertical take-off and land aircraft' [patent_app_type] => B1 [patent_app_number] => 09/655966 [patent_app_country] => US [patent_app_date] => 2000-09-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 20 [patent_no_of_words] => 7071 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 116 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/382/06382560.pdf [firstpage_image] =>[orig_patent_app_number] => 09655966 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/655966
High speed vertical take-off and land aircraft Sep 5, 2000 Issued
Array ( [id] => 1459585 [patent_doc_number] => 06349901 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-02-26 [patent_title] => 'Landing gear' [patent_app_type] => B1 [patent_app_number] => 09/651487 [patent_app_country] => US [patent_app_date] => 2000-08-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 4 [patent_no_of_words] => 4392 [patent_no_of_claims] => 30 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 94 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/349/06349901.pdf [firstpage_image] =>[orig_patent_app_number] => 09651487 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/651487
Landing gear Aug 29, 2000 Issued
Array ( [id] => 1528497 [patent_doc_number] => 06409121 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-06-25 [patent_title] => 'In flight autolubrication system for the mechanical members of aircraft landing gear' [patent_app_type] => B1 [patent_app_number] => 09/652589 [patent_app_country] => US [patent_app_date] => 2000-08-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 14 [patent_no_of_words] => 3800 [patent_no_of_claims] => 4 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 52 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/409/06409121.pdf [firstpage_image] =>[orig_patent_app_number] => 09652589 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/652589
In flight autolubrication system for the mechanical members of aircraft landing gear Aug 29, 2000 Issued
Array ( [id] => 4326641 [patent_doc_number] => 06332592 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 2001-12-25 [patent_title] => 'Method for velocity precision pointing in spin-stabilized spacecraft or rockets' [patent_app_type] => 1 [patent_app_number] => 9/635225 [patent_app_country] => US [patent_app_date] => 2000-08-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 10 [patent_no_of_words] => 4578 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 166 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/332/06332592.pdf [firstpage_image] =>[orig_patent_app_number] => 635225 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/635225
Method for velocity precision pointing in spin-stabilized spacecraft or rockets Aug 8, 2000 Issued
Array ( [id] => 1544935 [patent_doc_number] => 06398160 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-06-04 [patent_title] => 'Inflatable airfoils, and elevated and propulsion driven vehicles' [patent_app_type] => B1 [patent_app_number] => 09/617765 [patent_app_country] => US [patent_app_date] => 2000-07-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 37 [patent_figures_cnt] => 38 [patent_no_of_words] => 10938 [patent_no_of_claims] => 31 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 127 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/398/06398160.pdf [firstpage_image] =>[orig_patent_app_number] => 09617765 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/617765
Inflatable airfoils, and elevated and propulsion driven vehicles Jul 16, 2000 Issued
Array ( [id] => 1355046 [patent_doc_number] => 06561463 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2003-05-13 [patent_title] => 'Flight control module with integrated spoiler actuator control electronics' [patent_app_type] => B1 [patent_app_number] => 09/616195 [patent_app_country] => US [patent_app_date] => 2000-07-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 5 [patent_no_of_words] => 2968 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 82 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/561/06561463.pdf [firstpage_image] =>[orig_patent_app_number] => 09616195 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/616195
Flight control module with integrated spoiler actuator control electronics Jul 13, 2000 Issued
Array ( [id] => 1574288 [patent_doc_number] => 06446911 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-09-10 [patent_title] => 'Method for controlling actuators on a vehicle' [patent_app_type] => B1 [patent_app_number] => 09/616295 [patent_app_country] => US [patent_app_date] => 2000-07-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 4 [patent_no_of_words] => 3108 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 81 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/446/06446911.pdf [firstpage_image] =>[orig_patent_app_number] => 09616295 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/616295
Method for controlling actuators on a vehicle Jul 13, 2000 Issued
09/615992 CONVERTIBLE DUAL TAXILANE Jul 13, 2000 Abandoned
Array ( [id] => 1517368 [patent_doc_number] => 06412732 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-07-02 [patent_title] => 'Apparatus and method for enhancement of aerodynamic performance by using pulse excitation control' [patent_app_type] => B1 [patent_app_number] => 09/610896 [patent_app_country] => US [patent_app_date] => 2000-07-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 12 [patent_no_of_words] => 7998 [patent_no_of_claims] => 25 [patent_no_of_ind_claims] => 5 [patent_words_short_claim] => 77 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/412/06412732.pdf [firstpage_image] =>[orig_patent_app_number] => 09610896 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/610896
Apparatus and method for enhancement of aerodynamic performance by using pulse excitation control Jul 5, 2000 Issued
Array ( [id] => 7641512 [patent_doc_number] => 06394395 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-05-28 [patent_title] => 'Combination solar array assembly and antenna for a satellite' [patent_app_type] => B1 [patent_app_number] => 09/609987 [patent_app_country] => US [patent_app_date] => 2000-07-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 17 [patent_no_of_words] => 2848 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 4 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/394/06394395.pdf [firstpage_image] =>[orig_patent_app_number] => 09609987 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/609987
Combination solar array assembly and antenna for a satellite Jul 4, 2000 Issued
Array ( [id] => 1454370 [patent_doc_number] => 06390414 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-05-21 [patent_title] => 'Self-adjusting air intake' [patent_app_type] => B1 [patent_app_number] => 09/582572 [patent_app_country] => US [patent_app_date] => 2000-06-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 7 [patent_no_of_words] => 3485 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 95 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/390/06390414.pdf [firstpage_image] =>[orig_patent_app_number] => 09582572 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/582572
Self-adjusting air intake Jun 26, 2000 Issued
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