
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 number | Title of the application | Filing Date | Status |
|---|---|---|---|
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
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[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
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[patent_no_of_words] => 2421
[patent_no_of_claims] => 14
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[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
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[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
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[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
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[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
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[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
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[patent_words_short_claim] => 119
[patent_maintenance] => 1
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[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
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[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
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[patent_no_of_words] => 4676
[patent_no_of_claims] => 9
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[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
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[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
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[patent_no_of_words] => 9414
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[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
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[patent_app_country] => US
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[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
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[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
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[patent_app_country] => US
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[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
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[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
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[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
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[patent_issue_date] => 2008-09-23
[patent_title] => 'Linear acoustic pulsejet'
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[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
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[patent_title] => 'Layout of the top part of an aircraft cabin'
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[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
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[patent_kind] => A1
[patent_issue_date] => 2007-04-26
[patent_title] => 'Lightweight composite armor'
[patent_app_type] => utility
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[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 |