
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] => 4979784
[patent_doc_number] => 20070084337
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-04-19
[patent_title] => 'MINE-DETONATION-RESISTANT UNDERSTRUCTURE FOR A VEHICLE'
[patent_app_type] => utility
[patent_app_number] => 10/809294
[patent_app_country] => US
[patent_app_date] => 2004-03-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2276
[patent_no_of_claims] => 18
[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/A1/0084/20070084337.pdf
[firstpage_image] =>[orig_patent_app_number] => 10809294
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/809294 | Mine-detonation-resistant understructure for a vehicle | Mar 24, 2004 | Issued |
Array
(
[id] => 438289
[patent_doc_number] => 07258304
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2007-08-21
[patent_title] => 'Cushioned grounding clamp'
[patent_app_type] => utility
[patent_app_number] => 10/808850
[patent_app_country] => US
[patent_app_date] => 2004-03-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 8
[patent_no_of_words] => 2773
[patent_no_of_claims] => 21
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 165
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/258/07258304.pdf
[firstpage_image] =>[orig_patent_app_number] => 10808850
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/808850 | Cushioned grounding clamp | Mar 24, 2004 | Issued |
Array
(
[id] => 1029578
[patent_doc_number] => 06877694
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2005-04-12
[patent_title] => 'Aircraft security system'
[patent_app_type] => utility
[patent_app_number] => 10/809037
[patent_app_country] => US
[patent_app_date] => 2004-03-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 4
[patent_no_of_words] => 2704
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 18
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/877/06877694.pdf
[firstpage_image] =>[orig_patent_app_number] => 10809037
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/809037 | Aircraft security system | Mar 24, 2004 | Issued |
Array
(
[id] => 7057779
[patent_doc_number] => 20050000138
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-01-06
[patent_title] => 'Apparatus and method for preventing the bolt carrier of a firearm from moving forward after firing the last round of ammunition, and signaling when the firearm has run out of ammunition.'
[patent_app_type] => utility
[patent_app_number] => 10/708731
[patent_app_country] => US
[patent_app_date] => 2004-03-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 2210
[patent_no_of_claims] => 4
[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/A1/0000/20050000138.pdf
[firstpage_image] =>[orig_patent_app_number] => 10708731
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/708731 | Apparatus and method for preventing the bolt carrier of a firearm from moving forward after firing the last round of ammunition, and signaling when the firearm has run out of ammunition. | Mar 20, 2004 | Abandoned |
Array
(
[id] => 7431035
[patent_doc_number] => 20040194364
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-10-07
[patent_title] => 'Range finder'
[patent_app_type] => new
[patent_app_number] => 10/804372
[patent_app_country] => US
[patent_app_date] => 2004-03-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 3326
[patent_no_of_claims] => 31
[patent_no_of_ind_claims] => 7
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0194/20040194364.pdf
[firstpage_image] =>[orig_patent_app_number] => 10804372
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/804372 | Range finder | Mar 18, 2004 | Abandoned |
Array
(
[id] => 1011757
[patent_doc_number] => 06896224
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2005-05-24
[patent_title] => 'Apparatus and method for mitigating toe strike in aircraft'
[patent_app_type] => utility
[patent_app_number] => 10/807577
[patent_app_country] => US
[patent_app_date] => 2004-03-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 7
[patent_no_of_words] => 1549
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 67
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/896/06896224.pdf
[firstpage_image] =>[orig_patent_app_number] => 10807577
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/807577 | Apparatus and method for mitigating toe strike in aircraft | Mar 17, 2004 | Issued |
Array
(
[id] => 984461
[patent_doc_number] => 06923403
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2005-08-02
[patent_title] => 'Tailed flying wing aircraft'
[patent_app_type] => utility
[patent_app_number] => 10/803307
[patent_app_country] => US
[patent_app_date] => 2004-03-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 9
[patent_no_of_words] => 5416
[patent_no_of_claims] => 3
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 582
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/923/06923403.pdf
[firstpage_image] =>[orig_patent_app_number] => 10803307
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/803307 | Tailed flying wing aircraft | Mar 17, 2004 | Issued |
Array
(
[id] => 7362293
[patent_doc_number] => 20040217231
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-11-04
[patent_title] => 'Spacecraft and launch system'
[patent_app_type] => new
[patent_app_number] => 10/803124
[patent_app_country] => US
[patent_app_date] => 2004-03-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 4025
[patent_no_of_claims] => 33
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 87
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0217/20040217231.pdf
[firstpage_image] =>[orig_patent_app_number] => 10803124
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/803124 | Spacecraft and launch system | Mar 15, 2004 | Issued |
Array
(
[id] => 525918
[patent_doc_number] => 07172156
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2007-02-06
[patent_title] => 'Increasing the performance of aircraft on-board inert gas generating systems by turbocharging'
[patent_app_type] => utility
[patent_app_number] => 10/802968
[patent_app_country] => US
[patent_app_date] => 2004-03-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 9
[patent_no_of_words] => 4604
[patent_no_of_claims] => 37
[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/07/172/07172156.pdf
[firstpage_image] =>[orig_patent_app_number] => 10802968
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/802968 | Increasing the performance of aircraft on-board inert gas generating systems by turbocharging | Mar 15, 2004 | Issued |
Array
(
[id] => 7107798
[patent_doc_number] => 20050205315
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-09-22
[patent_title] => 'Light armored vehicle'
[patent_app_type] => utility
[patent_app_number] => 10/801298
[patent_app_country] => US
[patent_app_date] => 2004-03-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 3278
[patent_no_of_claims] => 20
[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/A1/0205/20050205315.pdf
[firstpage_image] =>[orig_patent_app_number] => 10801298
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/801298 | Light armored vehicle | Mar 15, 2004 | Abandoned |
Array
(
[id] => 1079679
[patent_doc_number] => 06834835
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2004-12-28
[patent_title] => 'Telescopic wing system'
[patent_app_type] => B1
[patent_app_number] => 10/799400
[patent_app_country] => US
[patent_app_date] => 2004-03-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[patent_no_of_words] => 4958
[patent_no_of_claims] => 16
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/834/06834835.pdf
[firstpage_image] =>[orig_patent_app_number] => 10799400
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/799400 | Telescopic wing system | Mar 11, 2004 | Issued |
Array
(
[id] => 799849
[patent_doc_number] => 07424989
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2008-09-16
[patent_title] => 'Intelligent multifunctional actuation system for vibration and buffet suppression'
[patent_app_type] => utility
[patent_app_number] => 10/798687
[patent_app_country] => US
[patent_app_date] => 2004-03-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/424/07424989.pdf
[firstpage_image] =>[orig_patent_app_number] => 10798687
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/798687 | Intelligent multifunctional actuation system for vibration and buffet suppression | Mar 10, 2004 | Issued |
Array
(
[id] => 1029576
[patent_doc_number] => 06877692
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2005-04-12
[patent_title] => 'Oscillating foil propulsion system'
[patent_app_type] => utility
[patent_app_number] => 10/792692
[patent_app_country] => US
[patent_app_date] => 2004-03-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/877/06877692.pdf
[firstpage_image] =>[orig_patent_app_number] => 10792692
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/792692 | Oscillating foil propulsion system | Mar 4, 2004 | Issued |
Array
(
[id] => 873886
[patent_doc_number] => 07357358
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2008-04-15
[patent_title] => 'Aircraft leading edge device systems and corresponding sizing methods'
[patent_app_type] => utility
[patent_app_number] => 10/789100
[patent_app_country] => US
[patent_app_date] => 2004-02-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
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[patent_no_of_words] => 6120
[patent_no_of_claims] => 20
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[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/357/07357358.pdf
[firstpage_image] =>[orig_patent_app_number] => 10789100
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/789100 | Aircraft leading edge device systems and corresponding sizing methods | Feb 26, 2004 | Issued |
Array
(
[id] => 7337981
[patent_doc_number] => 20040245378
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-12-09
[patent_title] => 'Autonomous control method for a small, unmanned helicopter'
[patent_app_type] => new
[patent_app_number] => 10/786051
[patent_app_country] => US
[patent_app_date] => 2004-02-26
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0245/20040245378.pdf
[firstpage_image] =>[orig_patent_app_number] => 10786051
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/786051 | Autonomous control method for a small, unmanned helicopter | Feb 25, 2004 | Abandoned |
Array
(
[id] => 5628523
[patent_doc_number] => 20060144991
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-07-06
[patent_title] => 'Swept-wing box-type aircraft with high fligh static stability'
[patent_app_type] => utility
[patent_app_number] => 10/546505
[patent_app_country] => US
[patent_app_date] => 2004-02-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0144/20060144991.pdf
[firstpage_image] =>[orig_patent_app_number] => 10546505
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/546505 | Swept-wing box-type aircraft with high fligh static stability | Feb 18, 2004 | Abandoned |
Array
(
[id] => 973324
[patent_doc_number] => 06931978
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2005-08-23
[patent_title] => 'Rebound attenuation device for automatic firearms'
[patent_app_type] => utility
[patent_app_number] => 10/780890
[patent_app_country] => US
[patent_app_date] => 2004-02-19
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/931/06931978.pdf
[firstpage_image] =>[orig_patent_app_number] => 10780890
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/780890 | Rebound attenuation device for automatic firearms | Feb 18, 2004 | Issued |
Array
(
[id] => 7172566
[patent_doc_number] => 20050188579
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-09-01
[patent_title] => 'Firearm cartridge clip'
[patent_app_type] => utility
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[patent_app_country] => US
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[pdf_file] => publications/A1/0188/20050188579.pdf
[firstpage_image] =>[orig_patent_app_number] => 10778425
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/778425 | Firearm cartridge clip | Feb 11, 2004 | Issued |
Array
(
[id] => 703257
[patent_doc_number] => 07059075
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2006-06-13
[patent_title] => 'Cylinder retaining mechanism'
[patent_app_type] => utility
[patent_app_number] => 10/776388
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[pdf_file] => patents/07/059/07059075.pdf
[firstpage_image] =>[orig_patent_app_number] => 10776388
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/776388 | Cylinder retaining mechanism | Feb 10, 2004 | Issued |
Array
(
[id] => 501514
[patent_doc_number] => 07194833
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2007-03-27
[patent_title] => 'Firing mechanism for semi-automatic pistols'
[patent_app_type] => utility
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[patent_app_country] => US
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/194/07194833.pdf
[firstpage_image] =>[orig_patent_app_number] => 10775611
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/775611 | Firing mechanism for semi-automatic pistols | Feb 9, 2004 | Issued |