Search

John W. Eldred

Examiner (ID: 10195)

Most Active Art Unit
3641
Art Unit(s)
3644, 3641, 2201, 2899
Total Applications
3389
Issued Applications
2819
Pending Applications
192
Abandoned Applications
398

Applications

Application numberTitle of the applicationFiling DateStatus
Array ( [id] => 5817773 [patent_doc_number] => 20060022086 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-02-02 [patent_title] => 'Forward pivoted full flying control tail boom' [patent_app_type] => utility [patent_app_number] => 11/201820 [patent_app_country] => US [patent_app_date] => 2005-08-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 4496 [patent_no_of_claims] => 48 [patent_no_of_ind_claims] => 18 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0022/20060022086.pdf [firstpage_image] =>[orig_patent_app_number] => 11201820 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/201820
Forward pivoted full flying control tail boom Aug 10, 2005 Issued
Array ( [id] => 5151855 [patent_doc_number] => 20070034737 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-02-15 [patent_title] => 'Dual axis control for cycloidal propeller' [patent_app_type] => utility [patent_app_number] => 11/200319 [patent_app_country] => US [patent_app_date] => 2005-08-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 12 [patent_no_of_words] => 9414 [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/A1/0034/20070034737.pdf [firstpage_image] =>[orig_patent_app_number] => 11200319 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/200319
Dual axis control for cycloidal propeller Aug 8, 2005 Abandoned
Array ( [id] => 5151864 [patent_doc_number] => 20070034746 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-02-15 [patent_title] => 'System for aerodynamic flows and associated method' [patent_app_type] => utility [patent_app_number] => 11/200515 [patent_app_country] => US [patent_app_date] => 2005-08-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 11 [patent_no_of_words] => 5737 [patent_no_of_claims] => 20 [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/A1/0034/20070034746.pdf [firstpage_image] =>[orig_patent_app_number] => 11200515 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/200515
System for aerodynamic flows and associated method Aug 8, 2005 Issued
Array ( [id] => 287988 [patent_doc_number] => 07546983 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2009-06-16 [patent_title] => 'Spacecraft power acquisition method for wing-stowed configuration' [patent_app_type] => utility [patent_app_number] => 11/200215 [patent_app_country] => US [patent_app_date] => 2005-08-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 14 [patent_figures_cnt] => 18 [patent_no_of_words] => 7588 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 178 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/546/07546983.pdf [firstpage_image] =>[orig_patent_app_number] => 11200215 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/200215
Spacecraft power acquisition method for wing-stowed configuration Aug 8, 2005 Issued
Array ( [id] => 165772 [patent_doc_number] => 07665695 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2010-02-23 [patent_title] => 'Unified attitude control for spacecraft transfer orbit operations' [patent_app_type] => utility [patent_app_number] => 11/199932 [patent_app_country] => US [patent_app_date] => 2005-08-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 14 [patent_figures_cnt] => 18 [patent_no_of_words] => 7403 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 104 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/665/07665695.pdf [firstpage_image] =>[orig_patent_app_number] => 11199932 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/199932
Unified attitude control for spacecraft transfer orbit operations Aug 8, 2005 Issued
Array ( [id] => 202348 [patent_doc_number] => 07628149 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2009-12-08 [patent_title] => 'Variable bore paintball barrel connector system' [patent_app_type] => utility [patent_app_number] => 11/197189 [patent_app_country] => US [patent_app_date] => 2005-08-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 7 [patent_no_of_words] => 3884 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 197 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/628/07628149.pdf [firstpage_image] =>[orig_patent_app_number] => 11197189 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/197189
Variable bore paintball barrel connector system Aug 3, 2005 Issued
Array ( [id] => 5823512 [patent_doc_number] => 20060060694 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-03-23 [patent_title] => 'Autonomous control method for small unmanned helicopter' [patent_app_type] => utility [patent_app_number] => 11/194466 [patent_app_country] => US [patent_app_date] => 2005-08-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 19 [patent_figures_cnt] => 19 [patent_no_of_words] => 10406 [patent_no_of_claims] => 20 [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/A1/0060/20060060694.pdf [firstpage_image] =>[orig_patent_app_number] => 11194466 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/194466
Autonomous control method for small unmanned helicopter Aug 1, 2005 Issued
Array ( [id] => 797466 [patent_doc_number] => 07427048 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2008-09-23 [patent_title] => 'Linear acoustic pulsejet' [patent_app_type] => utility [patent_app_number] => 11/190264 [patent_app_country] => US [patent_app_date] => 2005-07-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 13 [patent_figures_cnt] => 19 [patent_no_of_words] => 5634 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 105 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/427/07427048.pdf [firstpage_image] =>[orig_patent_app_number] => 11190264 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/190264
Linear acoustic pulsejet Jul 26, 2005 Issued
Array ( [id] => 399913 [patent_doc_number] => 07290735 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2007-11-06 [patent_title] => 'Layout of the top part of an aircraft cabin' [patent_app_type] => utility [patent_app_number] => 11/188703 [patent_app_country] => US [patent_app_date] => 2005-07-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 5 [patent_no_of_words] => 2661 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 113 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/290/07290735.pdf [firstpage_image] =>[orig_patent_app_number] => 11188703 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/188703
Layout of the top part of an aircraft cabin Jul 25, 2005 Issued
Array ( [id] => 5598511 [patent_doc_number] => 20060288855 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-12-28 [patent_title] => 'Ceramic bodies for armor panel' [patent_app_type] => utility [patent_app_number] => 11/188031 [patent_app_country] => US [patent_app_date] => 2005-07-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 6757 [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/A1/0288/20060288855.pdf [firstpage_image] =>[orig_patent_app_number] => 11188031 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/188031
Ceramic bodies for armor panel Jul 21, 2005 Issued
Array ( [id] => 5037315 [patent_doc_number] => 20070089597 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-04-26 [patent_title] => 'Lightweight composite armor' [patent_app_type] => utility [patent_app_number] => 11/187378 [patent_app_country] => US [patent_app_date] => 2005-07-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 12 [patent_no_of_words] => 3465 [patent_no_of_claims] => 15 [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/A1/0089/20070089597.pdf [firstpage_image] =>[orig_patent_app_number] => 11187378 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/187378
Lightweight composite armor Jul 21, 2005 Issued
Array ( [id] => 5238650 [patent_doc_number] => 20070017140 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-01-25 [patent_title] => 'Magazine loader' [patent_app_type] => utility [patent_app_number] => 11/182818 [patent_app_country] => US [patent_app_date] => 2005-07-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 2151 [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/A1/0017/20070017140.pdf [firstpage_image] =>[orig_patent_app_number] => 11182818 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/182818
Magazine loader Jul 17, 2005 Issued
Array ( [id] => 5202102 [patent_doc_number] => 20070023581 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-02-01 [patent_title] => 'Omnidirectional aircraft' [patent_app_type] => utility [patent_app_number] => 11/182877 [patent_app_country] => US [patent_app_date] => 2005-07-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 2797 [patent_no_of_claims] => 8 [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/A1/0023/20070023581.pdf [firstpage_image] =>[orig_patent_app_number] => 11182877 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/182877
Omnidirectional aircraft Jul 15, 2005 Abandoned
Array ( [id] => 5239543 [patent_doc_number] => 20070018034 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-01-25 [patent_title] => 'Thrust vectoring' [patent_app_type] => utility [patent_app_number] => 11/178521 [patent_app_country] => US [patent_app_date] => 2005-07-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 25 [patent_figures_cnt] => 25 [patent_no_of_words] => 15290 [patent_no_of_claims] => 19 [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/A1/0018/20070018034.pdf [firstpage_image] =>[orig_patent_app_number] => 11178521 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/178521
Thrust vectoring Jul 11, 2005 Abandoned
Array ( [id] => 5756520 [patent_doc_number] => 20060207465 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-09-21 [patent_title] => 'Methods and apparatus for increasing aerodynamic performance of projectiles' [patent_app_type] => utility [patent_app_number] => 11/178750 [patent_app_country] => US [patent_app_date] => 2005-07-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 5089 [patent_no_of_claims] => 11 [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/A1/0207/20060207465.pdf [firstpage_image] =>[orig_patent_app_number] => 11178750 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/178750
Projectile having circumferential members for varying a base cone angle of the projectile as a function of speed Jul 10, 2005 Issued
Array ( [id] => 5822894 [patent_doc_number] => 20060060076 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-03-23 [patent_title] => 'Systems for attaching a noise suppressor to a firearm' [patent_app_type] => utility [patent_app_number] => 11/171178 [patent_app_country] => US [patent_app_date] => 2005-06-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 8268 [patent_no_of_claims] => 86 [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/A1/0060/20060060076.pdf [firstpage_image] =>[orig_patent_app_number] => 11171178 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/171178
Systems for attaching a noise suppressor to a firearm Jun 28, 2005 Issued
Array ( [id] => 4952452 [patent_doc_number] => 20080185476 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-08-07 [patent_title] => 'Dual Motor Dual Concentric Valve' [patent_app_type] => utility [patent_app_number] => 11/814923 [patent_app_country] => US [patent_app_date] => 2005-06-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 3171 [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/A1/0185/20080185476.pdf [firstpage_image] =>[orig_patent_app_number] => 11814923 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/814923
Dual motor dual concentric valve Jun 26, 2005 Issued
Array ( [id] => 365058 [patent_doc_number] => 07478578 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2009-01-20 [patent_title] => 'Commercial airliner missile protection using formation drone aircraft' [patent_app_type] => utility [patent_app_number] => 11/165975 [patent_app_country] => US [patent_app_date] => 2005-06-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 11 [patent_no_of_words] => 4769 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 117 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/478/07478578.pdf [firstpage_image] =>[orig_patent_app_number] => 11165975 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/165975
Commercial airliner missile protection using formation drone aircraft Jun 23, 2005 Issued
Array ( [id] => 4991378 [patent_doc_number] => 20070006722 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-01-11 [patent_title] => 'Modular launch-cell system' [patent_app_type] => utility [patent_app_number] => 11/159171 [patent_app_country] => US [patent_app_date] => 2005-06-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2060 [patent_no_of_claims] => 6 [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/A1/0006/20070006722.pdf [firstpage_image] =>[orig_patent_app_number] => 11159171 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/159171
Modular launch-cell system Jun 22, 2005 Issued
Array ( [id] => 4723691 [patent_doc_number] => 20080203232 [patent_country] => US [patent_kind] => A9 [patent_issue_date] => 2008-08-28 [patent_title] => 'System and method for reducing the loads acting on the fuselage structure in means of transport' [patent_app_type] => utility [patent_app_number] => 11/154916 [patent_app_country] => US [patent_app_date] => 2005-06-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 5698 [patent_no_of_claims] => 18 [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/A9/0203/20080203232.pdf [firstpage_image] =>[orig_patent_app_number] => 11154916 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/154916
System and method for reducing the loads acting on the fuselage structure in means of transport Jun 15, 2005 Abandoned
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