
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] => 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
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[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
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[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
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[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
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[patent_no_of_words] => 5089
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[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
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[patent_no_of_words] => 8268
[patent_no_of_claims] => 86
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[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
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[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
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[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
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[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
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[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 |