Search

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 numberTitle of the applicationFiling DateStatus
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 [patent_figures_cnt] => 34 [patent_no_of_words] => 9319 [patent_no_of_claims] => 51 [patent_no_of_ind_claims] => 7 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_figures_cnt] => 3 [patent_no_of_words] => 3668 [patent_no_of_claims] => 19 [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/A1/0269/20050269443.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 [patent_figures_cnt] => 13 [patent_no_of_words] => 26741 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 8 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 1209 [patent_no_of_claims] => 1 [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/A1/0207/20060207147.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 [patent_app_date] => 2005-03-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 937 [patent_no_of_claims] => 1 [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/A1/0207/20060207148.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 [patent_figures_cnt] => 11 [patent_no_of_words] => 4613 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 102 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 3715 [patent_no_of_claims] => 25 [patent_no_of_ind_claims] => 11 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [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 [patent_app_date] => 2005-03-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 13 [patent_figures_cnt] => 18 [patent_no_of_words] => 2632 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 232 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [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 [patent_country] => US [patent_kind] => B2 [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 [patent_app_date] => 2005-03-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 12 [patent_no_of_words] => 5461 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 93 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_app_country] => US [patent_app_date] => 2005-03-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 3774 [patent_no_of_claims] => 14 [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/A1/0230/20050230538.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
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