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 |
---|---|---|---|
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
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[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
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[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
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[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
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[patent_no_of_words] => 4955
[patent_no_of_claims] => 38
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[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
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[patent_no_of_words] => 3203
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[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
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[patent_maintenance] => 1
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[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
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[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
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[patent_no_of_words] => 3800
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[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
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[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
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[patent_drawing_sheets_cnt] => 37
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[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
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[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
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[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
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[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
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[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
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[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 |