
John W. Eldred
Examiner (ID: 13524)
| Most Active Art Unit | 3641 |
| Art Unit(s) | 2201, 3644, 3641, 2899 |
| Total Applications | 3345 |
| Issued Applications | 2791 |
| Pending Applications | 194 |
| Abandoned Applications | 390 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 7549324
[patent_doc_number] => 08061653
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-11-22
[patent_title] => 'Landing gear'
[patent_app_type] => utility
[patent_app_number] => 12/068599
[patent_app_country] => US
[patent_app_date] => 2008-02-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 15
[patent_no_of_words] => 6023
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 9
[patent_words_short_claim] => 100
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/061/08061653.pdf
[firstpage_image] =>[orig_patent_app_number] => 12068599
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/068599 | Landing gear | Feb 7, 2008 | Issued |
Array
(
[id] => 246179
[patent_doc_number] => 07584928
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2009-09-08
[patent_title] => 'Drogue parachute drag force actuated programmable controller to generate an event trigger signal'
[patent_app_type] => utility
[patent_app_number] => 12/011075
[patent_app_country] => US
[patent_app_date] => 2008-01-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2695
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 54
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/584/07584928.pdf
[firstpage_image] =>[orig_patent_app_number] => 12011075
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/011075 | Drogue parachute drag force actuated programmable controller to generate an event trigger signal | Jan 23, 2008 | Issued |
Array
(
[id] => 183417
[patent_doc_number] => 07648101
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-01-19
[patent_title] => 'Method and apparatus for fast deploying and retrieving of towed bodies'
[patent_app_type] => utility
[patent_app_number] => 12/009916
[patent_app_country] => US
[patent_app_date] => 2008-01-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
[patent_figures_cnt] => 15
[patent_no_of_words] => 5394
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 93
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/648/07648101.pdf
[firstpage_image] =>[orig_patent_app_number] => 12009916
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/009916 | Method and apparatus for fast deploying and retrieving of towed bodies | Jan 22, 2008 | Issued |
Array
(
[id] => 8907578
[patent_doc_number] => 08479631
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-07-09
[patent_title] => 'Propellant holder for an explosion-driven setting tool and an explosion-driven setting tool'
[patent_app_type] => utility
[patent_app_number] => 11/967062
[patent_app_country] => US
[patent_app_date] => 2007-12-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 9
[patent_no_of_words] => 2962
[patent_no_of_claims] => 4
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 140
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 11967062
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/967062 | Propellant holder for an explosion-driven setting tool and an explosion-driven setting tool | Dec 28, 2007 | Issued |
Array
(
[id] => 4762558
[patent_doc_number] => 20080173767
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-07-24
[patent_title] => 'AIRCRAFT WITH A MODIFIED GEAR, AND METHOD OF PRODUCING THE GEAR'
[patent_app_type] => utility
[patent_app_number] => 11/964877
[patent_app_country] => US
[patent_app_date] => 2007-12-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 3095
[patent_no_of_claims] => 9
[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/A1/0173/20080173767.pdf
[firstpage_image] =>[orig_patent_app_number] => 11964877
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/964877 | Aircraft with a modified gear, and method of producing the gear | Dec 26, 2007 | Issued |
Array
(
[id] => 6229807
[patent_doc_number] => 20100263566
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-10-21
[patent_title] => 'Reduced Collateral Damage Bomb (RCDB) Including Fuse System with Shaped Charges and a System and Method of Making Same'
[patent_app_type] => utility
[patent_app_number] => 11/961844
[patent_app_country] => US
[patent_app_date] => 2007-12-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 16
[patent_figures_cnt] => 16
[patent_no_of_words] => 8158
[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/A1/0263/20100263566.pdf
[firstpage_image] =>[orig_patent_app_number] => 11961844
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/961844 | Reduced collateral damage bomb (RCDB) including fuse system with shaped charges and a system and method of making same | Dec 19, 2007 | Issued |
Array
(
[id] => 30885
[patent_doc_number] => 07784732
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-08-31
[patent_title] => 'Boundary-layer-ingesting inlet flow control system'
[patent_app_type] => utility
[patent_app_number] => 11/958673
[patent_app_country] => US
[patent_app_date] => 2007-12-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 5
[patent_no_of_words] => 3230
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 43
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/784/07784732.pdf
[firstpage_image] =>[orig_patent_app_number] => 11958673
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/958673 | Boundary-layer-ingesting inlet flow control system | Dec 17, 2007 | Issued |
Array
(
[id] => 6579988
[patent_doc_number] => 20100000399
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-01-07
[patent_title] => 'BARRIER'
[patent_app_type] => utility
[patent_app_number] => 12/518640
[patent_app_country] => US
[patent_app_date] => 2007-12-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 3745
[patent_no_of_claims] => 17
[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/A1/0000/20100000399.pdf
[firstpage_image] =>[orig_patent_app_number] => 12518640
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/518640 | BARRIER | Dec 16, 2007 | Abandoned |
Array
(
[id] => 4511865
[patent_doc_number] => 07938065
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-05-10
[patent_title] => 'Efficient exploding foil initiator and process for making same'
[patent_app_type] => utility
[patent_app_number] => 12/002195
[patent_app_country] => US
[patent_app_date] => 2007-12-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 7
[patent_no_of_words] => 9875
[patent_no_of_claims] => 23
[patent_no_of_ind_claims] => 7
[patent_words_short_claim] => 39
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/938/07938065.pdf
[firstpage_image] =>[orig_patent_app_number] => 12002195
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/002195 | Efficient exploding foil initiator and process for making same | Dec 13, 2007 | Issued |
Array
(
[id] => 9880781
[patent_doc_number] => 08967534
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-03-03
[patent_title] => 'Aircraft landing gear assembly shimmy damper'
[patent_app_type] => utility
[patent_app_number] => 11/956118
[patent_app_country] => US
[patent_app_date] => 2007-12-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 29
[patent_figures_cnt] => 40
[patent_no_of_words] => 9880
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 9
[patent_words_short_claim] => 134
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 11956118
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/956118 | Aircraft landing gear assembly shimmy damper | Dec 12, 2007 | Issued |
Array
(
[id] => 8273873
[patent_doc_number] => 20120167752
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-07-05
[patent_title] => 'BALLISTIC TICKET BOARD'
[patent_app_type] => utility
[patent_app_number] => 11/955485
[patent_app_country] => US
[patent_app_date] => 2007-12-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2417
[patent_no_of_claims] => 19
[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] =>[firstpage_image] =>[orig_patent_app_number] => 11955485
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/955485 | BALLISTIC TICKET BOARD | Dec 12, 2007 | Abandoned |
Array
(
[id] => 6244287
[patent_doc_number] => 20100024276
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-02-04
[patent_title] => 'Kellis \"T\" scope mounting system'
[patent_app_type] => utility
[patent_app_number] => 12/001049
[patent_app_country] => US
[patent_app_date] => 2007-12-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 1801
[patent_no_of_claims] => 3
[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/A1/0024/20100024276.pdf
[firstpage_image] =>[orig_patent_app_number] => 12001049
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/001049 | Kellis "T" scope mounting system | Dec 9, 2007 | Abandoned |
Array
(
[id] => 149174
[patent_doc_number] => 07681832
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-03-23
[patent_title] => 'Ducted fan air vehicle with deployable wings'
[patent_app_type] => utility
[patent_app_number] => 11/947585
[patent_app_country] => US
[patent_app_date] => 2007-11-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 10
[patent_no_of_words] => 3024
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 111
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/681/07681832.pdf
[firstpage_image] =>[orig_patent_app_number] => 11947585
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/947585 | Ducted fan air vehicle with deployable wings | Nov 28, 2007 | Issued |
Array
(
[id] => 4782353
[patent_doc_number] => 20080135682
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-06-12
[patent_title] => 'Arrangement And Method For Installing A Component In An Aircraft'
[patent_app_type] => utility
[patent_app_number] => 11/946080
[patent_app_country] => US
[patent_app_date] => 2007-11-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 3147
[patent_no_of_claims] => 15
[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/A1/0135/20080135682.pdf
[firstpage_image] =>[orig_patent_app_number] => 11946080
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/946080 | Arrangement and method for installing a component in an aircraft | Nov 27, 2007 | Issued |
Array
(
[id] => 4870504
[patent_doc_number] => 20080197238
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-08-21
[patent_title] => 'PHOTONIC LASER-BASED PROPULSION HAVING AN ACTIVE INTRACAVITY THRUST AMPLIFICATION SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 11/943480
[patent_app_country] => US
[patent_app_date] => 2007-11-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 9257
[patent_no_of_claims] => 25
[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] => publications/A1/0197/20080197238.pdf
[firstpage_image] =>[orig_patent_app_number] => 11943480
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/943480 | PHOTONIC LASER-BASED PROPULSION HAVING AN ACTIVE INTRACAVITY THRUST AMPLIFICATION SYSTEM | Nov 19, 2007 | Abandoned |
Array
(
[id] => 6150803
[patent_doc_number] => 20110155015
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-06-30
[patent_title] => 'SABOT'
[patent_app_type] => utility
[patent_app_number] => 11/934292
[patent_app_country] => US
[patent_app_date] => 2007-11-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 3348
[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/A1/0155/20110155015.pdf
[firstpage_image] =>[orig_patent_app_number] => 11934292
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/934292 | Sabot | Nov 1, 2007 | Issued |
Array
(
[id] => 313728
[patent_doc_number] => 07523692
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2009-04-28
[patent_title] => 'Aircraft defense system against manpads with IR/UV seekers'
[patent_app_type] => utility
[patent_app_number] => 11/982579
[patent_app_country] => US
[patent_app_date] => 2007-11-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 7359
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 96
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/523/07523692.pdf
[firstpage_image] =>[orig_patent_app_number] => 11982579
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/982579 | Aircraft defense system against manpads with IR/UV seekers | Nov 1, 2007 | Issued |
| 11/934113 | Reflective Sighting Apparatus for Firearms | Nov 1, 2007 | Abandoned |
Array
(
[id] => 255534
[patent_doc_number] => 07575198
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2009-08-18
[patent_title] => 'Control handle for use with a towable airfoil'
[patent_app_type] => utility
[patent_app_number] => 11/927344
[patent_app_country] => US
[patent_app_date] => 2007-10-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 21
[patent_figures_cnt] => 32
[patent_no_of_words] => 7820
[patent_no_of_claims] => 25
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 62
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/575/07575198.pdf
[firstpage_image] =>[orig_patent_app_number] => 11927344
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/927344 | Control handle for use with a towable airfoil | Oct 28, 2007 | Issued |
Array
(
[id] => 6566142
[patent_doc_number] => 20100095863
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-04-22
[patent_title] => 'SABOT FOR ELASTOMERIC PROJECTILE'
[patent_app_type] => utility
[patent_app_number] => 11/927216
[patent_app_country] => US
[patent_app_date] => 2007-10-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 16
[patent_figures_cnt] => 16
[patent_no_of_words] => 8327
[patent_no_of_claims] => 21
[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/A1/0095/20100095863.pdf
[firstpage_image] =>[orig_patent_app_number] => 11927216
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/927216 | Sabot for elastomeric projectile | Oct 28, 2007 | Issued |