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] => 7301004
[patent_doc_number] => 20040113018
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-06-17
[patent_title] => 'Aircraft'
[patent_app_type] => new
[patent_app_number] => 10/731330
[patent_app_country] => US
[patent_app_date] => 2003-12-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 1542
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 150
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0113/20040113018.pdf
[firstpage_image] =>[orig_patent_app_number] => 10731330
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/731330 | Aircraft | Dec 9, 2003 | Issued |
Array
(
[id] => 7439747
[patent_doc_number] => 20040195435
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-10-07
[patent_title] => 'Wing with inflatable struts'
[patent_app_type] => new
[patent_app_number] => 10/732046
[patent_app_country] => US
[patent_app_date] => 2003-12-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 4932
[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] => publication
[pdf_file] => publications/A1/0195/20040195435.pdf
[firstpage_image] =>[orig_patent_app_number] => 10732046
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/732046 | Wing with inflatable struts | Dec 8, 2003 | Issued |
Array
(
[id] => 88159
[patent_doc_number] => 07735311
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-06-15
[patent_title] => 'Pulsed detonation engines manufactured from materials having low thermal stability'
[patent_app_type] => utility
[patent_app_number] => 10/730020
[patent_app_country] => US
[patent_app_date] => 2003-12-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 7
[patent_no_of_words] => 3667
[patent_no_of_claims] => 24
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 23
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/735/07735311.pdf
[firstpage_image] =>[orig_patent_app_number] => 10730020
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/730020 | Pulsed detonation engines manufactured from materials having low thermal stability | Dec 8, 2003 | Issued |
Array
(
[id] => 1070699
[patent_doc_number] => 06840479
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2005-01-11
[patent_title] => 'Airframe mounted accessory drive (AMAD) power take-off shaft auxiliary power generation'
[patent_app_type] => utility
[patent_app_number] => 10/728634
[patent_app_country] => US
[patent_app_date] => 2003-12-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 10
[patent_no_of_words] => 3906
[patent_no_of_claims] => 34
[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/06/840/06840479.pdf
[firstpage_image] =>[orig_patent_app_number] => 10728634
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/728634 | Airframe mounted accessory drive (AMAD) power take-off shaft auxiliary power generation | Dec 4, 2003 | Issued |
Array
(
[id] => 632890
[patent_doc_number] => 07128293
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2006-10-31
[patent_title] => 'Helicopter'
[patent_app_type] => utility
[patent_app_number] => 10/726573
[patent_app_country] => US
[patent_app_date] => 2003-12-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 7
[patent_no_of_words] => 5151
[patent_no_of_claims] => 29
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 79
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/128/07128293.pdf
[firstpage_image] =>[orig_patent_app_number] => 10726573
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/726573 | Helicopter | Dec 3, 2003 | Issued |
Array
(
[id] => 7419961
[patent_doc_number] => 20040182966
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-09-23
[patent_title] => 'Method for managing in-flight refuelling of a fleet of aircraft'
[patent_app_type] => new
[patent_app_number] => 10/479409
[patent_app_country] => US
[patent_app_date] => 2003-12-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 12801
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 633
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0182/20040182966.pdf
[firstpage_image] =>[orig_patent_app_number] => 10479409
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/479409 | Method for managing in-flight refuelling of a fleet of aircraft | Dec 2, 2003 | Issued |
Array
(
[id] => 7058731
[patent_doc_number] => 20050001090
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-01-06
[patent_title] => 'Wing driving apparatus'
[patent_app_type] => utility
[patent_app_number] => 10/720927
[patent_app_country] => US
[patent_app_date] => 2003-11-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 7209
[patent_no_of_claims] => 2
[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/A1/0001/20050001090.pdf
[firstpage_image] =>[orig_patent_app_number] => 10720927
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/720927 | Wing driving apparatus | Nov 23, 2003 | Issued |
Array
(
[id] => 7233680
[patent_doc_number] => 20040256521
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-12-23
[patent_title] => 'Method for accelerating destruction of a vortex formed by a wing of an aircraft'
[patent_app_type] => new
[patent_app_number] => 10/717465
[patent_app_country] => US
[patent_app_date] => 2003-11-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 4968
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 63
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0256/20040256521.pdf
[firstpage_image] =>[orig_patent_app_number] => 10717465
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/717465 | Method for accelerating destruction of a vortex formed by a wing of an aircraft | Nov 20, 2003 | Abandoned |
Array
(
[id] => 7318566
[patent_doc_number] => 20040135030
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-07-15
[patent_title] => 'Method of opening and closing a bin relative to a support structure of a baggage compartment'
[patent_app_type] => new
[patent_app_number] => 10/712035
[patent_app_country] => US
[patent_app_date] => 2003-11-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 4390
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 38
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0135/20040135030.pdf
[firstpage_image] =>[orig_patent_app_number] => 10712035
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/712035 | Method of opening and closing a bin relative to a support structure of a baggage compartment | Nov 13, 2003 | Abandoned |
Array
(
[id] => 7168722
[patent_doc_number] => 20050121555
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-06-09
[patent_title] => 'Mach weighted area ruling for supersonic vehicles'
[patent_app_type] => utility
[patent_app_number] => 10/706673
[patent_app_country] => US
[patent_app_date] => 2003-11-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 4622
[patent_no_of_claims] => 12
[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/A1/0121/20050121555.pdf
[firstpage_image] =>[orig_patent_app_number] => 10706673
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/706673 | Mach weighted area ruling for supersonic vehicles | Nov 10, 2003 | Issued |
Array
(
[id] => 1033104
[patent_doc_number] => 06874731
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2005-04-05
[patent_title] => 'Modular overhead stowage bin systems and associated methods'
[patent_app_type] => utility
[patent_app_number] => 10/703797
[patent_app_country] => US
[patent_app_date] => 2003-11-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 4199
[patent_no_of_claims] => 51
[patent_no_of_ind_claims] => 8
[patent_words_short_claim] => 180
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/874/06874731.pdf
[firstpage_image] =>[orig_patent_app_number] => 10703797
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/703797 | Modular overhead stowage bin systems and associated methods | Nov 6, 2003 | Issued |
Array
(
[id] => 5571847
[patent_doc_number] => 20090139206
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-06-04
[patent_title] => 'Dual-mode chemical-electric thrusters for spacecraft'
[patent_app_type] => utility
[patent_app_number] => 10/701030
[patent_app_country] => US
[patent_app_date] => 2003-11-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2234
[patent_no_of_claims] => 36
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0139/20090139206.pdf
[firstpage_image] =>[orig_patent_app_number] => 10701030
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/701030 | Dual-mode chemical-electric thrusters for spacecraft | Nov 2, 2003 | Issued |
Array
(
[id] => 670536
[patent_doc_number] => 07090165
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2006-08-15
[patent_title] => 'Aeroengine nacelle'
[patent_app_type] => utility
[patent_app_number] => 10/697945
[patent_app_country] => US
[patent_app_date] => 2003-10-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_no_of_words] => 3144
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 105
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/090/07090165.pdf
[firstpage_image] =>[orig_patent_app_number] => 10697945
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/697945 | Aeroengine nacelle | Oct 30, 2003 | Issued |
Array
(
[id] => 787235
[patent_doc_number] => 06986481
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2006-01-17
[patent_title] => 'Extendable joined wing system for a fluid-born body'
[patent_app_type] => utility
[patent_app_number] => 10/698580
[patent_app_country] => US
[patent_app_date] => 2003-10-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 21
[patent_no_of_words] => 5396
[patent_no_of_claims] => 41
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 168
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/986/06986481.pdf
[firstpage_image] =>[orig_patent_app_number] => 10698580
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/698580 | Extendable joined wing system for a fluid-born body | Oct 30, 2003 | Issued |
Array
(
[id] => 7132587
[patent_doc_number] => 20050178919
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-08-18
[patent_title] => 'System and method for an ambient atmosphere ion thruster'
[patent_app_type] => utility
[patent_app_number] => 10/698847
[patent_app_country] => US
[patent_app_date] => 2003-10-30
[patent_effective_date] => 0000-00-00
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[patent_no_of_claims] => 40
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0178/20050178919.pdf
[firstpage_image] =>[orig_patent_app_number] => 10698847
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/698847 | System and method for an ambient atmosphere ion thruster | Oct 29, 2003 | Issued |
Array
(
[id] => 5773644
[patent_doc_number] => 20060102775
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-05-18
[patent_title] => 'Landing gear'
[patent_app_type] => utility
[patent_app_number] => 10/533376
[patent_app_country] => US
[patent_app_date] => 2003-10-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_no_of_claims] => 23
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0102/20060102775.pdf
[firstpage_image] =>[orig_patent_app_number] => 10533376
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/533376 | Landing gear noise reduction | Oct 22, 2003 | Issued |
Array
(
[id] => 7328514
[patent_doc_number] => 20040129837
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-07-08
[patent_title] => 'Laminar flow wing for transonic cruise'
[patent_app_type] => new
[patent_app_number] => 10/693411
[patent_app_country] => US
[patent_app_date] => 2003-10-23
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0129/20040129837.pdf
[firstpage_image] =>[orig_patent_app_number] => 10693411
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/693411 | Laminar flow wing for transonic cruise | Oct 22, 2003 | Issued |
Array
(
[id] => 7370691
[patent_doc_number] => 20040079837
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-04-29
[patent_title] => 'Anti-hijacking system operable in emergencies to deactivate on-board flight controls and remotely pilot aircraft utilizing autopilot'
[patent_app_type] => new
[patent_app_number] => 10/684316
[patent_app_country] => US
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[pdf_file] => publications/A1/0079/20040079837.pdf
[firstpage_image] =>[orig_patent_app_number] => 10684316
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/684316 | Anti-hijacking system operable in emergencies to deactivate on-board flight controls and remotely pilot aircraft utilizing autopilot | Oct 10, 2003 | Abandoned |
Array
(
[id] => 6990624
[patent_doc_number] => 20050089661
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-04-28
[patent_title] => 'CRYOGENIC FUEL TANK INSULATION ASSEMBLY'
[patent_app_type] => utility
[patent_app_number] => 10/605599
[patent_app_country] => US
[patent_app_date] => 2003-10-11
[patent_effective_date] => 0000-00-00
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[pdf_file] => publications/A1/0089/20050089661.pdf
[firstpage_image] =>[orig_patent_app_number] => 10605599
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/605599 | Cryogenic fuel tank insulation assembly | Oct 10, 2003 | Issued |
Array
(
[id] => 653564
[patent_doc_number] => 07108226
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[patent_kind] => B2
[patent_issue_date] => 2006-09-19
[patent_title] => 'Interior seating architecture for aircraft'
[patent_app_type] => utility
[patent_app_number] => 10/605586
[patent_app_country] => US
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/108/07108226.pdf
[firstpage_image] =>[orig_patent_app_number] => 10605586
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/605586 | Interior seating architecture for aircraft | Oct 9, 2003 | Issued |