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] => 30893 [patent_doc_number] => 07784737 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2010-08-31 [patent_title] => 'Drag reduction fairing' [patent_app_type] => utility [patent_app_number] => 11/230177 [patent_app_country] => US [patent_app_date] => 2005-09-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 3694 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 194 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/784/07784737.pdf [firstpage_image] =>[orig_patent_app_number] => 11230177 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/230177
Drag reduction fairing Sep 18, 2005 Issued
Array ( [id] => 5726092 [patent_doc_number] => 20060056852 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-03-16 [patent_title] => 'Method of optical transmission between a terminal onboard a spacecraft and a remote terminal, and spacecraft suitable for such a method' [patent_app_type] => utility [patent_app_number] => 11/223582 [patent_app_country] => US [patent_app_date] => 2005-09-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 3067 [patent_no_of_claims] => 8 [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/A1/0056/20060056852.pdf [firstpage_image] =>[orig_patent_app_number] => 11223582 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/223582
Method of optical transmission between a terminal onboard a spacecraft and a remote terminal, and spacecraft suitable for such a method Sep 8, 2005 Abandoned
Array ( [id] => 5727347 [patent_doc_number] => 20060058107 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-03-16 [patent_title] => 'Children\'s play container for transportation vehicles, in particular for passenger aircraft' [patent_app_type] => utility [patent_app_number] => 11/220251 [patent_app_country] => US [patent_app_date] => 2005-09-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 2421 [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/A1/0058/20060058107.pdf [firstpage_image] =>[orig_patent_app_number] => 11220251 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/220251
Children's play container for transportation vehicles, in particular for passenger aircraft Sep 5, 2005 Issued
Array ( [id] => 861976 [patent_doc_number] => 07367151 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2008-05-06 [patent_title] => 'Gun bore cleaning system' [patent_app_type] => utility [patent_app_number] => 11/219093 [patent_app_country] => US [patent_app_date] => 2005-09-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 16 [patent_figures_cnt] => 22 [patent_no_of_words] => 3268 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 64 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/367/07367151.pdf [firstpage_image] =>[orig_patent_app_number] => 11219093 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/219093
Gun bore cleaning system Aug 31, 2005 Issued
Array ( [id] => 372566 [patent_doc_number] => 07472868 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2009-01-06 [patent_title] => 'Systems and methods for controlling an aerial refueling device' [patent_app_type] => utility [patent_app_number] => 11/217696 [patent_app_country] => US [patent_app_date] => 2005-09-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 8 [patent_no_of_words] => 3945 [patent_no_of_claims] => 21 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 111 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/472/07472868.pdf [firstpage_image] =>[orig_patent_app_number] => 11217696 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/217696
Systems and methods for controlling an aerial refueling device Aug 31, 2005 Issued
Array ( [id] => 5684924 [patent_doc_number] => 20060283239 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-12-21 [patent_title] => 'On-board device for measuring the mass and the position of the center of gravity of an aircraft' [patent_app_type] => utility [patent_app_number] => 11/212777 [patent_app_country] => US [patent_app_date] => 2005-08-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2253 [patent_no_of_claims] => 10 [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/A1/0283/20060283239.pdf [firstpage_image] =>[orig_patent_app_number] => 11212777 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/212777
On-board device for measuring the mass and the position of the center of gravity of an aircraft Aug 28, 2005 Issued
Array ( [id] => 5707959 [patent_doc_number] => 20060049303 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-03-09 [patent_title] => 'Mechanical density altitude compensation device for helicopter tail rotors' [patent_app_type] => utility [patent_app_number] => 11/209540 [patent_app_country] => US [patent_app_date] => 2005-08-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 6734 [patent_no_of_claims] => 22 [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/A1/0049/20060049303.pdf [firstpage_image] =>[orig_patent_app_number] => 11209540 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/209540
Mechanical density altitude compensation device for helicopter tail rotors Aug 22, 2005 Abandoned
Array ( [id] => 525940 [patent_doc_number] => 07172159 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2007-02-06 [patent_title] => 'Parachute steering system' [patent_app_type] => utility [patent_app_number] => 11/209075 [patent_app_country] => US [patent_app_date] => 2005-08-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 10 [patent_no_of_words] => 1961 [patent_no_of_claims] => 4 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 119 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/172/07172159.pdf [firstpage_image] =>[orig_patent_app_number] => 11209075 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/209075
Parachute steering system Aug 21, 2005 Issued
Array ( [id] => 9138783 [patent_doc_number] => 08579237 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-11-12 [patent_title] => 'System for setting the span load distribution of a wing' [patent_app_type] => utility [patent_app_number] => 11/206313 [patent_app_country] => US [patent_app_date] => 2005-08-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 2 [patent_no_of_words] => 1596 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 120 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 11206313 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/206313
System for setting the span load distribution of a wing Aug 16, 2005 Issued
Array ( [id] => 573490 [patent_doc_number] => 07445181 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2008-11-04 [patent_title] => 'Variable energy attenuating apparatus' [patent_app_type] => utility [patent_app_number] => 11/202177 [patent_app_country] => US [patent_app_date] => 2005-08-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 14 [patent_no_of_words] => 4676 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 110 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/445/07445181.pdf [firstpage_image] =>[orig_patent_app_number] => 11202177 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/202177
Variable energy attenuating apparatus Aug 11, 2005 Issued
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] => 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
Menu