
John W. Eldred
Examiner (ID: 597, Phone: (571)272-6901 , Office: P/3641 )
| Most Active Art Unit | 3641 |
| Art Unit(s) | 2899, 3644, 2201, 3641 |
| Total Applications | 3399 |
| Issued Applications | 2824 |
| Pending Applications | 195 |
| Abandoned Applications | 399 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 5723976
[patent_doc_number] => 20060054736
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-03-16
[patent_title] => 'VTOL personal aircraft'
[patent_app_type] => utility
[patent_app_number] => 11/114836
[patent_app_country] => US
[patent_app_date] => 2005-04-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 2468
[patent_no_of_claims] => 21
[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/A1/0054/20060054736.pdf
[firstpage_image] =>[orig_patent_app_number] => 11114836
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/114836 | VTOL personal aircraft | Apr 25, 2005 | Issued |
Array
(
[id] => 262899
[patent_doc_number] => 07568656
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2009-08-04
[patent_title] => 'System for controlling the lift of aircraft'
[patent_app_type] => utility
[patent_app_number] => 11/115554
[patent_app_country] => US
[patent_app_date] => 2005-04-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 4
[patent_no_of_words] => 2829
[patent_no_of_claims] => 21
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 78
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/568/07568656.pdf
[firstpage_image] =>[orig_patent_app_number] => 11115554
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/115554 | System for controlling the lift of aircraft | Apr 25, 2005 | Issued |
Array
(
[id] => 5685691
[patent_doc_number] => 20060284006
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-12-21
[patent_title] => 'MISSILE CONTROL SYSTEM AND METHOD'
[patent_app_type] => utility
[patent_app_number] => 11/113511
[patent_app_country] => US
[patent_app_date] => 2005-04-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 2413
[patent_no_of_claims] => 20
[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/A1/0284/20060284006.pdf
[firstpage_image] =>[orig_patent_app_number] => 11113511
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/113511 | Missile control system and method | Apr 24, 2005 | Issued |
Array
(
[id] => 737349
[patent_doc_number] => 07028951
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2006-04-18
[patent_title] => 'Parachute reefing system'
[patent_app_type] => utility
[patent_app_number] => 11/110277
[patent_app_country] => US
[patent_app_date] => 2005-04-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 6
[patent_no_of_words] => 3223
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 158
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/028/07028951.pdf
[firstpage_image] =>[orig_patent_app_number] => 11110277
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/110277 | Parachute reefing system | Apr 19, 2005 | Issued |
Array
(
[id] => 557325
[patent_doc_number] => 07461816
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2008-12-09
[patent_title] => 'Internal arrangement of the walls of the fuselage of an aircraft'
[patent_app_type] => utility
[patent_app_number] => 11/109677
[patent_app_country] => US
[patent_app_date] => 2005-04-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 3291
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 186
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/461/07461816.pdf
[firstpage_image] =>[orig_patent_app_number] => 11109677
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/109677 | Internal arrangement of the walls of the fuselage of an aircraft | Apr 19, 2005 | Issued |
Array
(
[id] => 5728994
[patent_doc_number] => 20060254108
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-11-16
[patent_title] => 'Electrical discharge immobilization weapon projectile having multiple deployed contacts'
[patent_app_type] => utility
[patent_app_number] => 11/110201
[patent_app_country] => US
[patent_app_date] => 2005-04-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 2033
[patent_no_of_claims] => 24
[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/A1/0254/20060254108.pdf
[firstpage_image] =>[orig_patent_app_number] => 11110201
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/110201 | Electrical discharge immobilization weapon projectile having multiple deployed contacts | Apr 19, 2005 | Abandoned |
Array
(
[id] => 7227252
[patent_doc_number] => 20050269448
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-12-08
[patent_title] => 'Method for ensuring the safety of an aircraft flying horizontally at low speed'
[patent_app_type] => utility
[patent_app_number] => 11/099675
[patent_app_country] => US
[patent_app_date] => 2005-04-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 1913
[patent_no_of_claims] => 6
[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/A1/0269/20050269448.pdf
[firstpage_image] =>[orig_patent_app_number] => 11099675
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/099675 | Method for ensuring the safety of an aircraft flying horizontally at low speed | Apr 5, 2005 | Issued |
Array
(
[id] => 724026
[patent_doc_number] => 07040211
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2006-05-09
[patent_title] => 'Mortar bomb retention apparatus'
[patent_app_type] => utility
[patent_app_number] => 10/907574
[patent_app_country] => US
[patent_app_date] => 2005-04-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 11
[patent_no_of_words] => 1678
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 130
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/040/07040211.pdf
[firstpage_image] =>[orig_patent_app_number] => 10907574
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/907574 | Mortar bomb retention apparatus | Apr 5, 2005 | Issued |
Array
(
[id] => 5796308
[patent_doc_number] => 20060032985
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-02-16
[patent_title] => 'Clutch driven reaction wheel steering unit'
[patent_app_type] => utility
[patent_app_number] => 11/099379
[patent_app_country] => US
[patent_app_date] => 2005-04-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2062
[patent_no_of_claims] => 20
[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/A1/0032/20060032985.pdf
[firstpage_image] =>[orig_patent_app_number] => 11099379
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/099379 | Clutch driven reaction wheel steering unit | Apr 4, 2005 | Abandoned |
Array
(
[id] => 858695
[patent_doc_number] => 07370831
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2008-05-13
[patent_title] => 'Power strip for seats'
[patent_app_type] => utility
[patent_app_number] => 11/090875
[patent_app_country] => US
[patent_app_date] => 2005-03-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 5322
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 132
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/370/07370831.pdf
[firstpage_image] =>[orig_patent_app_number] => 11090875
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/090875 | Power strip for seats | Mar 24, 2005 | Issued |
Array
(
[id] => 4863575
[patent_doc_number] => 20080142634
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-06-19
[patent_title] => 'Landing Gear Noise Attenuation'
[patent_app_type] => utility
[patent_app_number] => 10/599495
[patent_app_country] => US
[patent_app_date] => 2005-03-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 34
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[patent_no_of_words] => 9319
[patent_no_of_claims] => 51
[patent_no_of_ind_claims] => 7
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[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0142/20080142634.pdf
[firstpage_image] =>[orig_patent_app_number] => 10599495
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/599495 | Landing gear noise attenuation | Mar 24, 2005 | Issued |
Array
(
[id] => 7227234
[patent_doc_number] => 20050269443
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-12-08
[patent_title] => 'Air intake structure for aircraft engine'
[patent_app_type] => utility
[patent_app_number] => 11/086380
[patent_app_country] => US
[patent_app_date] => 2005-03-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[patent_no_of_words] => 3668
[patent_no_of_claims] => 19
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0269/20050269443.pdf
[firstpage_image] =>[orig_patent_app_number] => 11086380
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/086380 | Air intake structure for aircraft engine | Mar 22, 2005 | Issued |
Array
(
[id] => 5757191
[patent_doc_number] => 20060208136
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-09-21
[patent_title] => 'Centripetal reflex method of space launch'
[patent_app_type] => utility
[patent_app_number] => 11/084780
[patent_app_country] => US
[patent_app_date] => 2005-03-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0208/20060208136.pdf
[firstpage_image] =>[orig_patent_app_number] => 11084780
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/084780 | Centripetal reflex method of space launch | Mar 20, 2005 | Issued |
Array
(
[id] => 5756202
[patent_doc_number] => 20060207147
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-09-21
[patent_title] => 'SELF-CONTAINED TRIGGERPLATE ACTION FOR LOW PROFILE FIREARMS'
[patent_app_type] => utility
[patent_app_number] => 10/907098
[patent_app_country] => US
[patent_app_date] => 2005-03-19
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0207/20060207147.pdf
[firstpage_image] =>[orig_patent_app_number] => 10907098
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/907098 | SELF-CONTAINED TRIGGERPLATE ACTION FOR LOW PROFILE FIREARMS | Mar 18, 2005 | Abandoned |
Array
(
[id] => 5756203
[patent_doc_number] => 20060207148
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-09-21
[patent_title] => 'IMPROVED SELF-OPENING ACTION'
[patent_app_type] => utility
[patent_app_number] => 10/907097
[patent_app_country] => US
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[patent_effective_date] => 0000-00-00
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[pdf_file] => publications/A1/0207/20060207148.pdf
[firstpage_image] =>[orig_patent_app_number] => 10907097
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/907097 | IMPROVED SELF-OPENING ACTION | Mar 18, 2005 | Abandoned |
Array
(
[id] => 847848
[patent_doc_number] => 07380361
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2008-06-03
[patent_title] => 'System and method for increased magazine capacity for a firearm'
[patent_app_type] => utility
[patent_app_number] => 10/907038
[patent_app_country] => US
[patent_app_date] => 2005-03-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_no_of_words] => 4613
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/380/07380361.pdf
[firstpage_image] =>[orig_patent_app_number] => 10907038
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/907038 | System and method for increased magazine capacity for a firearm | Mar 16, 2005 | Issued |
Array
(
[id] => 4835240
[patent_doc_number] => 20080276821
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-11-13
[patent_title] => 'Projectile and System for Providing Air-to-Surface Reconnaissance'
[patent_app_type] => utility
[patent_app_number] => 10/592881
[patent_app_country] => US
[patent_app_date] => 2005-03-15
[patent_effective_date] => 0000-00-00
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[pdf_file] => publications/A1/0276/20080276821.pdf
[firstpage_image] =>[orig_patent_app_number] => 10592881
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/592881 | Projectile and System for Providing Air-to-Surface Reconnaissance | Mar 14, 2005 | Abandoned |
Array
(
[id] => 873880
[patent_doc_number] => 07357354
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2008-04-15
[patent_title] => 'Aircraft door hinge assembly'
[patent_app_type] => utility
[patent_app_number] => 11/078465
[patent_app_country] => US
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[pdf_file] => patents/07/357/07357354.pdf
[firstpage_image] =>[orig_patent_app_number] => 11078465
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/078465 | Aircraft door hinge assembly | Mar 10, 2005 | Issued |
Array
(
[id] => 376189
[patent_doc_number] => 07311287
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[patent_issue_date] => 2007-12-25
[patent_title] => 'Methods for incorporating area ruled surfaces in a supersonic aircraft'
[patent_app_type] => utility
[patent_app_number] => 11/078632
[patent_app_country] => US
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/311/07311287.pdf
[firstpage_image] =>[orig_patent_app_number] => 11078632
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/078632 | Methods for incorporating area ruled surfaces in a supersonic aircraft | Mar 10, 2005 | Issued |
Array
(
[id] => 6963641
[patent_doc_number] => 20050230538
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-10-20
[patent_title] => 'Fuselage spar for aircraft and central sparbox provided with such a spar'
[patent_app_type] => utility
[patent_app_number] => 11/070648
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0230/20050230538.pdf
[firstpage_image] =>[orig_patent_app_number] => 11070648
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/070648 | Fuselage spar for aircraft and central sparbox provided with such a spar | Mar 1, 2005 | Issued |