
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] => 235648
[patent_doc_number] => 07594626
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2009-09-29
[patent_title] => 'Magnetically induced aircraft landing wheel rotation'
[patent_app_type] => utility
[patent_app_number] => 11/448875
[patent_app_country] => US
[patent_app_date] => 2006-06-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 6210
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 120
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/594/07594626.pdf
[firstpage_image] =>[orig_patent_app_number] => 11448875
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/448875 | Magnetically induced aircraft landing wheel rotation | Jun 7, 2006 | Issued |
| 11/449440 | Cell operated unmanned aerial vehicle | Jun 6, 2006 | Abandoned |
Array
(
[id] => 81530
[patent_doc_number] => 07740205
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2010-06-22
[patent_title] => 'Auxiliary wing and flap assembly for an aircraft'
[patent_app_type] => utility
[patent_app_number] => 11/448271
[patent_app_country] => US
[patent_app_date] => 2006-06-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 4
[patent_no_of_words] => 3375
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 403
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/740/07740205.pdf
[firstpage_image] =>[orig_patent_app_number] => 11448271
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/448271 | Auxiliary wing and flap assembly for an aircraft | Jun 5, 2006 | Issued |
Array
(
[id] => 5007875
[patent_doc_number] => 20070278352
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-12-06
[patent_title] => 'Low-energy locking hinge mechanism for deployable devices'
[patent_app_type] => utility
[patent_app_number] => 11/446443
[patent_app_country] => US
[patent_app_date] => 2006-06-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 8405
[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] => publications/A1/0278/20070278352.pdf
[firstpage_image] =>[orig_patent_app_number] => 11446443
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/446443 | Low-energy locking hinge mechanism for deployable devices | May 31, 2006 | Issued |
Array
(
[id] => 5167628
[patent_doc_number] => 20070068059
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-03-29
[patent_title] => 'Accessory devices for firearms'
[patent_app_type] => utility
[patent_app_number] => 11/443612
[patent_app_country] => US
[patent_app_date] => 2006-05-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 8703
[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/A1/0068/20070068059.pdf
[firstpage_image] =>[orig_patent_app_number] => 11443612
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/443612 | Accessory devices for firearms | May 29, 2006 | Issued |
Array
(
[id] => 5082745
[patent_doc_number] => 20070272796
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-11-29
[patent_title] => 'Ducted open rotor apparatus and method'
[patent_app_type] => utility
[patent_app_number] => 11/442547
[patent_app_country] => US
[patent_app_date] => 2006-05-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 3480
[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/A1/0272/20070272796.pdf
[firstpage_image] =>[orig_patent_app_number] => 11442547
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/442547 | Ducted open rotor apparatus and method | May 25, 2006 | Issued |
Array
(
[id] => 5388885
[patent_doc_number] => 20090206197
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-08-20
[patent_title] => 'Actuator and flap arrangement with actuator interconnection'
[patent_app_type] => utility
[patent_app_number] => 11/440558
[patent_app_country] => US
[patent_app_date] => 2006-05-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 5431
[patent_no_of_claims] => 38
[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/A1/0206/20090206197.pdf
[firstpage_image] =>[orig_patent_app_number] => 11440558
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/440558 | Actuator and flap arrangement with actuator interconnection | May 24, 2006 | Abandoned |
Array
(
[id] => 5082750
[patent_doc_number] => 20070272801
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-11-29
[patent_title] => 'Autonomously controlled GPS-guided parafoil recovery apparatus'
[patent_app_type] => utility
[patent_app_number] => 11/440566
[patent_app_country] => US
[patent_app_date] => 2006-05-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 3354
[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/A1/0272/20070272801.pdf
[firstpage_image] =>[orig_patent_app_number] => 11440566
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/440566 | Autonomously controlled GPS-guided parafoil recovery apparatus | May 23, 2006 | Abandoned |
Array
(
[id] => 5026101
[patent_doc_number] => 20070267547
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-11-22
[patent_title] => 'Flexible reefing loops for parachutes'
[patent_app_type] => utility
[patent_app_number] => 11/443846
[patent_app_country] => US
[patent_app_date] => 2006-05-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 1830
[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/A1/0267/20070267547.pdf
[firstpage_image] =>[orig_patent_app_number] => 11443846
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/443846 | Flexible reefing loops for parachutes | May 21, 2006 | Abandoned |
Array
(
[id] => 5388216
[patent_doc_number] => 20090205528
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-08-20
[patent_title] => 'Multiple part munition'
[patent_app_type] => utility
[patent_app_number] => 11/921517
[patent_app_country] => US
[patent_app_date] => 2006-05-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 1402
[patent_no_of_claims] => 10
[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/A1/0205/20090205528.pdf
[firstpage_image] =>[orig_patent_app_number] => 11921517
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/921517 | Multiple part munition | May 16, 2006 | Issued |
Array
(
[id] => 869065
[patent_doc_number] => 07360333
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2008-04-22
[patent_title] => 'Accessory devices for firearms'
[patent_app_type] => utility
[patent_app_number] => 11/436293
[patent_app_country] => US
[patent_app_date] => 2006-05-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 23
[patent_no_of_words] => 8709
[patent_no_of_claims] => 36
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 83
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/360/07360333.pdf
[firstpage_image] =>[orig_patent_app_number] => 11436293
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/436293 | Accessory devices for firearms | May 16, 2006 | Issued |
Array
(
[id] => 5461356
[patent_doc_number] => 20090321556
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-12-31
[patent_title] => 'Helicopter with an improved vibration control device'
[patent_app_type] => utility
[patent_app_number] => 11/436928
[patent_app_country] => US
[patent_app_date] => 2006-05-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2086
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 1
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0321/20090321556.pdf
[firstpage_image] =>[orig_patent_app_number] => 11436928
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/436928 | Helicopter with an improved vibration control device | May 14, 2006 | Issued |
Array
(
[id] => 210573
[patent_doc_number] => 07621480
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2009-11-24
[patent_title] => 'De-rotation system for a counter-rotating, coaxial rotor hub shaft fairing'
[patent_app_type] => utility
[patent_app_number] => 11/432875
[patent_app_country] => US
[patent_app_date] => 2006-05-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 17
[patent_no_of_words] => 4784
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 71
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/621/07621480.pdf
[firstpage_image] =>[orig_patent_app_number] => 11432875
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/432875 | De-rotation system for a counter-rotating, coaxial rotor hub shaft fairing | May 11, 2006 | Issued |
Array
(
[id] => 4996821
[patent_doc_number] => 20070039455
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-02-22
[patent_title] => 'Synchronously timed fuse procedure or process'
[patent_app_type] => utility
[patent_app_number] => 11/414194
[patent_app_country] => US
[patent_app_date] => 2006-05-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 864
[patent_no_of_claims] => 12
[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/A1/0039/20070039455.pdf
[firstpage_image] =>[orig_patent_app_number] => 11414194
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/414194 | Synchronously timed fuse procedure or process | Apr 30, 2006 | Issued |
Array
(
[id] => 4469653
[patent_doc_number] => 07866600
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-01-11
[patent_title] => 'Integrated engine air particle filter assembly'
[patent_app_type] => utility
[patent_app_number] => 11/911365
[patent_app_country] => US
[patent_app_date] => 2006-04-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 10
[patent_no_of_words] => 3361
[patent_no_of_claims] => 26
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 74
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/866/07866600.pdf
[firstpage_image] =>[orig_patent_app_number] => 11911365
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/911365 | Integrated engine air particle filter assembly | Apr 12, 2006 | Issued |
Array
(
[id] => 5123312
[patent_doc_number] => 20070235582
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-10-11
[patent_title] => 'High speed vertical take-off and land aircraft with active fan balancing system'
[patent_app_type] => utility
[patent_app_number] => 11/401666
[patent_app_country] => US
[patent_app_date] => 2006-04-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_no_of_words] => 3569
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0235/20070235582.pdf
[firstpage_image] =>[orig_patent_app_number] => 11401666
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/401666 | High speed vertical take-off and land aircraft with active fan balancing system | Apr 10, 2006 | Issued |
Array
(
[id] => 4820370
[patent_doc_number] => 20080121759
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-05-29
[patent_title] => 'REMOTELY LOCATED CRYOCOOLER'
[patent_app_type] => utility
[patent_app_number] => 11/398268
[patent_app_country] => US
[patent_app_date] => 2006-04-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 14
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[patent_no_of_words] => 7850
[patent_no_of_claims] => 22
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0121/20080121759.pdf
[firstpage_image] =>[orig_patent_app_number] => 11398268
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/398268 | Remotely located cryocooler | Apr 4, 2006 | Issued |
Array
(
[id] => 4559504
[patent_doc_number] => 07828244
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-11-09
[patent_title] => 'Supply system for an aircraft'
[patent_app_type] => utility
[patent_app_number] => 11/909381
[patent_app_country] => US
[patent_app_date] => 2006-03-24
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/828/07828244.pdf
[firstpage_image] =>[orig_patent_app_number] => 11909381
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/909381 | Supply system for an aircraft | Mar 23, 2006 | Issued |
Array
(
[id] => 5868813
[patent_doc_number] => 20060163430
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-07-27
[patent_title] => 'Attendant cabin display system'
[patent_app_type] => utility
[patent_app_number] => 11/387657
[patent_app_country] => US
[patent_app_date] => 2006-03-23
[patent_effective_date] => 0000-00-00
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[pdf_file] => publications/A1/0163/20060163430.pdf
[firstpage_image] =>[orig_patent_app_number] => 11387657
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/387657 | Attendant cabin display system | Mar 22, 2006 | Abandoned |
Array
(
[id] => 5048905
[patent_doc_number] => 20070029449
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-02-08
[patent_title] => 'Modular construction of an aircraft control system'
[patent_app_type] => utility
[patent_app_number] => 11/385270
[patent_app_country] => US
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[pdf_file] => publications/A1/0029/20070029449.pdf
[firstpage_image] =>[orig_patent_app_number] => 11385270
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/385270 | Modular construction of an aircraft control system | Mar 20, 2006 | Issued |