
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 number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 6461538
[patent_doc_number] => 20100006703
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-01-14
[patent_title] => 'SYSTEM FOR RELEASING OPPOSING TENSIONED LINES'
[patent_app_type] => utility
[patent_app_number] => 12/375214
[patent_app_country] => US
[patent_app_date] => 2007-07-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 20
[patent_figures_cnt] => 20
[patent_no_of_words] => 9545
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 6
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0006/20100006703.pdf
[firstpage_image] =>[orig_patent_app_number] => 12375214
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/375214 | SYSTEM FOR RELEASING OPPOSING TENSIONED LINES | Jul 29, 2007 | Abandoned |
Array
(
[id] => 5518339
[patent_doc_number] => 20090026320
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-01-29
[patent_title] => 'Fighting Kite'
[patent_app_type] => utility
[patent_app_number] => 11/829290
[patent_app_country] => US
[patent_app_date] => 2007-07-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 3459
[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/A1/0026/20090026320.pdf
[firstpage_image] =>[orig_patent_app_number] => 11829290
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/829290 | Fighting Kite | Jul 26, 2007 | Abandoned |
Array
(
[id] => 6466605
[patent_doc_number] => 20100212201
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-08-26
[patent_title] => 'Adaptive configuration for a firearm'
[patent_app_type] => utility
[patent_app_number] => 11/879650
[patent_app_country] => US
[patent_app_date] => 2007-07-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2663
[patent_no_of_claims] => 18
[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/A1/0212/20100212201.pdf
[firstpage_image] =>[orig_patent_app_number] => 11879650
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/879650 | Adaptive configuration for a firearm | Jul 17, 2007 | Issued |
Array
(
[id] => 6246788
[patent_doc_number] => 20100025537
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-02-04
[patent_title] => 'Leading Edge Flap Apparatuses and Associated Methods'
[patent_app_type] => utility
[patent_app_number] => 11/778995
[patent_app_country] => US
[patent_app_date] => 2007-07-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 4944
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 6
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0025/20100025537.pdf
[firstpage_image] =>[orig_patent_app_number] => 11778995
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/778995 | Leading edge flap apparatuses and associated methods | Jul 16, 2007 | Issued |
Array
(
[id] => 4603698
[patent_doc_number] => 07984676
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2011-07-26
[patent_title] => 'Systems and methods for a rear anchored projectile'
[patent_app_type] => utility
[patent_app_number] => 11/771956
[patent_app_country] => US
[patent_app_date] => 2007-06-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 18
[patent_no_of_words] => 5690
[patent_no_of_claims] => 24
[patent_no_of_ind_claims] => 11
[patent_words_short_claim] => 47
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/984/07984676.pdf
[firstpage_image] =>[orig_patent_app_number] => 11771956
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/771956 | Systems and methods for a rear anchored projectile | Jun 28, 2007 | Issued |
Array
(
[id] => 6409842
[patent_doc_number] => 20100275806
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-11-04
[patent_title] => 'SYSTEMS AND METHODS FOR DEPLOYING AN ELECTRODE USING TORSION'
[patent_app_type] => utility
[patent_app_number] => 11/771240
[patent_app_country] => US
[patent_app_date] => 2007-06-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 6300
[patent_no_of_claims] => 20
[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/A1/0275/20100275806.pdf
[firstpage_image] =>[orig_patent_app_number] => 11771240
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/771240 | Systems and methods for deploying an electrode using torsion | Jun 28, 2007 | Issued |
Array
(
[id] => 277155
[patent_doc_number] => 07556221
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2009-07-07
[patent_title] => 'Aircraft ice protection method'
[patent_app_type] => utility
[patent_app_number] => 11/769774
[patent_app_country] => US
[patent_app_date] => 2007-06-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 8
[patent_no_of_words] => 3062
[patent_no_of_claims] => 19
[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/07/556/07556221.pdf
[firstpage_image] =>[orig_patent_app_number] => 11769774
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/769774 | Aircraft ice protection method | Jun 27, 2007 | Issued |
Array
(
[id] => 4805799
[patent_doc_number] => 20080169377
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-07-17
[patent_title] => 'MOUNTING DEVICE FOR AN AIRCRAFT ENGINE COMPRISING TWO THRUST RECOVERY RODS WITH A DOUBLE REAR MECHANICAL CONNECTION'
[patent_app_type] => utility
[patent_app_number] => 11/769179
[patent_app_country] => US
[patent_app_date] => 2007-06-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 12
[patent_no_of_words] => 5071
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 6
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0169/20080169377.pdf
[firstpage_image] =>[orig_patent_app_number] => 11769179
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/769179 | Mounting device for an aircraft engine comprising two thrust recovery rods with a double rear mechanical connection | Jun 26, 2007 | Issued |
Array
(
[id] => 4569687
[patent_doc_number] => 07849800
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-12-14
[patent_title] => 'Hybrid spin/fin stabilized projectile'
[patent_app_type] => utility
[patent_app_number] => 11/821759
[patent_app_country] => US
[patent_app_date] => 2007-06-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 10
[patent_no_of_words] => 3223
[patent_no_of_claims] => 30
[patent_no_of_ind_claims] => 6
[patent_words_short_claim] => 87
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/849/07849800.pdf
[firstpage_image] =>[orig_patent_app_number] => 11821759
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/821759 | Hybrid spin/fin stabilized projectile | Jun 23, 2007 | Issued |
Array
(
[id] => 194991
[patent_doc_number] => 07637456
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2009-12-29
[patent_title] => 'Power starter for micro air vehicles'
[patent_app_type] => utility
[patent_app_number] => 11/765169
[patent_app_country] => US
[patent_app_date] => 2007-06-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 7
[patent_no_of_words] => 3945
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 153
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/637/07637456.pdf
[firstpage_image] =>[orig_patent_app_number] => 11765169
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/765169 | Power starter for micro air vehicles | Jun 18, 2007 | Issued |
Array
(
[id] => 8959795
[patent_doc_number] => 20130199397
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-08-08
[patent_title] => 'MULTI COMPONENT REACTIVE METAL PENETRATORS, AND THEIR METHOD OF MANUFACTURE'
[patent_app_type] => utility
[patent_app_number] => 11/764106
[patent_app_country] => US
[patent_app_date] => 2007-06-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2742
[patent_no_of_claims] => 22
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 11764106
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/764106 | MULTI COMPONENT REACTIVE METAL PENETRATORS, AND THEIR METHOD OF MANUFACTURE | Jun 14, 2007 | Abandoned |
Array
(
[id] => 4820362
[patent_doc_number] => 20080121753
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-05-29
[patent_title] => 'Positive lift vehicle'
[patent_app_type] => utility
[patent_app_number] => 11/818270
[patent_app_country] => US
[patent_app_date] => 2007-06-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 1686
[patent_no_of_claims] => 11
[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/A1/0121/20080121753.pdf
[firstpage_image] =>[orig_patent_app_number] => 11818270
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/818270 | Positive lift vehicle | Jun 12, 2007 | Abandoned |
Array
(
[id] => 5222771
[patent_doc_number] => 20070252037
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-11-01
[patent_title] => 'Air-taxi stands, boarding bridges for air taxis, and methods of using same'
[patent_app_type] => utility
[patent_app_number] => 11/811238
[patent_app_country] => US
[patent_app_date] => 2007-06-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 23
[patent_figures_cnt] => 23
[patent_no_of_words] => 14015
[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/A1/0252/20070252037.pdf
[firstpage_image] =>[orig_patent_app_number] => 11811238
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/811238 | Air-taxi stands, boarding bridges for air taxis, and methods of using same | Jun 7, 2007 | Abandoned |
Array
(
[id] => 4768467
[patent_doc_number] => 20080054121
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-03-06
[patent_title] => 'Ducted fan VTOL vehicles'
[patent_app_type] => utility
[patent_app_number] => 11/798187
[patent_app_country] => US
[patent_app_date] => 2007-05-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 66
[patent_figures_cnt] => 66
[patent_no_of_words] => 20084
[patent_no_of_claims] => 16
[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/A1/0054/20080054121.pdf
[firstpage_image] =>[orig_patent_app_number] => 11798187
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/798187 | Ducted fan VTOL vehicles | May 9, 2007 | Abandoned |
Array
(
[id] => 89759
[patent_doc_number] => 07731126
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-06-08
[patent_title] => 'Autonomous passenger seat'
[patent_app_type] => utility
[patent_app_number] => 11/743190
[patent_app_country] => US
[patent_app_date] => 2007-05-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 1
[patent_no_of_words] => 1405
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 21
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/731/07731126.pdf
[firstpage_image] =>[orig_patent_app_number] => 11743190
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/743190 | Autonomous passenger seat | May 1, 2007 | Issued |
Array
(
[id] => 249942
[patent_doc_number] => 07581697
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2009-09-01
[patent_title] => 'Design methods and configurations for supersonic aircraft'
[patent_app_type] => utility
[patent_app_number] => 11/743631
[patent_app_country] => US
[patent_app_date] => 2007-05-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 17
[patent_figures_cnt] => 17
[patent_no_of_words] => 14330
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 134
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/581/07581697.pdf
[firstpage_image] =>[orig_patent_app_number] => 11743631
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/743631 | Design methods and configurations for supersonic aircraft | May 1, 2007 | Issued |
Array
(
[id] => 6089197
[patent_doc_number] => 20110000389
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-01-06
[patent_title] => 'SYSTEM AND METHOD FOR GENERATING AND DIRECTING VERY LOUD SOUNDS'
[patent_app_type] => utility
[patent_app_number] => 11/785320
[patent_app_country] => US
[patent_app_date] => 2007-04-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 16
[patent_figures_cnt] => 16
[patent_no_of_words] => 9940
[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/A1/0000/20110000389.pdf
[firstpage_image] =>[orig_patent_app_number] => 11785320
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/785320 | System and method for generating and directing very loud sounds | Apr 16, 2007 | Issued |
Array
(
[id] => 6128105
[patent_doc_number] => 20110005420
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-01-13
[patent_title] => 'SYSTEM AND METHOD FOR IGNITION OF A GASEOUS OR DISPERSED FUEL-OXIDANT MIXTURE'
[patent_app_type] => utility
[patent_app_number] => 11/785321
[patent_app_country] => US
[patent_app_date] => 2007-04-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 14
[patent_figures_cnt] => 14
[patent_no_of_words] => 8072
[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/A1/0005/20110005420.pdf
[firstpage_image] =>[orig_patent_app_number] => 11785321
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/785321 | System and method for ignition of a gaseous or dispersed fuel-oxidant mixture | Apr 16, 2007 | Issued |
Array
(
[id] => 9258673
[patent_doc_number] => 20130340602
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-12-26
[patent_title] => 'LIGHTWEIGHT PROJECTILE RESISTANT ARMOR SYSTEM WITH SURFACE ENHANCEMENT'
[patent_app_type] => utility
[patent_app_number] => 11/735626
[patent_app_country] => US
[patent_app_date] => 2007-04-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2840
[patent_no_of_claims] => 18
[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] =>[firstpage_image] =>[orig_patent_app_number] => 11735626
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/735626 | Lightweight projectile resistant armor system with surface enhancement | Apr 15, 2007 | Issued |
Array
(
[id] => 10842510
[patent_doc_number] => 08869673
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-10-28
[patent_title] => 'Structural panel with ballistic protection'
[patent_app_type] => utility
[patent_app_number] => 11/735594
[patent_app_country] => US
[patent_app_date] => 2007-04-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 15
[patent_figures_cnt] => 21
[patent_no_of_words] => 3827
[patent_no_of_claims] => 23
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 75
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 11735594
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/735594 | Structural panel with ballistic protection | Apr 15, 2007 | Issued |