
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] => 4253178
[patent_doc_number] => 06244534
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2001-06-12
[patent_title] => 'Airborne electromagnetic system'
[patent_app_type] => 1
[patent_app_number] => 9/212377
[patent_app_country] => US
[patent_app_date] => 1998-12-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 4
[patent_no_of_words] => 4395
[patent_no_of_claims] => 21
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 39
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/244/06244534.pdf
[firstpage_image] =>[orig_patent_app_number] => 212377
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/212377 | Airborne electromagnetic system | Dec 15, 1998 | Issued |
Array
(
[id] => 4077145
[patent_doc_number] => 06095457
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-08-01
[patent_title] => 'Airfoil and wing configuration'
[patent_app_type] => 1
[patent_app_number] => 9/210978
[patent_app_country] => US
[patent_app_date] => 1998-12-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 4
[patent_no_of_words] => 2538
[patent_no_of_claims] => 15
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[patent_words_short_claim] => 74
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/095/06095457.pdf
[firstpage_image] =>[orig_patent_app_number] => 210978
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/210978 | Airfoil and wing configuration | Dec 13, 1998 | Issued |
Array
(
[id] => 4383761
[patent_doc_number] => 06170378
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2001-01-09
[patent_title] => 'Method and apparatus for defeating high-velocity projectiles'
[patent_app_type] => 1
[patent_app_number] => 9/189105
[patent_app_country] => US
[patent_app_date] => 1998-11-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 8
[patent_no_of_words] => 3142
[patent_no_of_claims] => 19
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[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/170/06170378.pdf
[firstpage_image] =>[orig_patent_app_number] => 189105
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/189105 | Method and apparatus for defeating high-velocity projectiles | Nov 8, 1998 | Issued |
Array
(
[id] => 3890976
[patent_doc_number] => 06000386
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-12-14
[patent_title] => 'Toy gun with fluid pulsator'
[patent_app_type] => 1
[patent_app_number] => 9/175107
[patent_app_country] => US
[patent_app_date] => 1998-10-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 17
[patent_figures_cnt] => 33
[patent_no_of_words] => 11314
[patent_no_of_claims] => 39
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 259
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/000/06000386.pdf
[firstpage_image] =>[orig_patent_app_number] => 175107
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/175107 | Toy gun with fluid pulsator | Oct 18, 1998 | Issued |
Array
(
[id] => 4276406
[patent_doc_number] => 06196501
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2001-03-06
[patent_title] => 'Satellite architecture with deployable electrical equipment'
[patent_app_type] => 1
[patent_app_number] => 9/168029
[patent_app_country] => US
[patent_app_date] => 1998-10-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 10
[patent_no_of_words] => 4019
[patent_no_of_claims] => 27
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 84
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/196/06196501.pdf
[firstpage_image] =>[orig_patent_app_number] => 168029
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/168029 | Satellite architecture with deployable electrical equipment | Oct 6, 1998 | Issued |
| 09/166869 | AIRCRAFT WINDOW | Oct 5, 1998 | Abandoned |
Array
(
[id] => 4226930
[patent_doc_number] => 06135392
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-10-24
[patent_title] => 'Spacecraft attitude control actuator and method'
[patent_app_type] => 1
[patent_app_number] => 9/162729
[patent_app_country] => US
[patent_app_date] => 1998-09-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 7
[patent_no_of_words] => 2889
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/135/06135392.pdf
[firstpage_image] =>[orig_patent_app_number] => 162729
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/162729 | Spacecraft attitude control actuator and method | Sep 28, 1998 | Issued |
Array
(
[id] => 4340247
[patent_doc_number] => 06189833
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2001-02-20
[patent_title] => 'Aircraft sliding door system'
[patent_app_type] => 1
[patent_app_number] => 9/162818
[patent_app_country] => US
[patent_app_date] => 1998-09-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 14
[patent_no_of_words] => 5821
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[patent_words_short_claim] => 80
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/189/06189833.pdf
[firstpage_image] =>[orig_patent_app_number] => 162818
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/162818 | Aircraft sliding door system | Sep 28, 1998 | Issued |
Array
(
[id] => 4068101
[patent_doc_number] => 06131848
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-10-17
[patent_title] => 'Roadable airplane drive through an automotive transaxle'
[patent_app_type] => 1
[patent_app_number] => 9/160808
[patent_app_country] => US
[patent_app_date] => 1998-09-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 17
[patent_figures_cnt] => 20
[patent_no_of_words] => 5977
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 116
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/131/06131848.pdf
[firstpage_image] =>[orig_patent_app_number] => 160808
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/160808 | Roadable airplane drive through an automotive transaxle | Sep 24, 1998 | Issued |
Array
(
[id] => 4174973
[patent_doc_number] => 06042052
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-03-28
[patent_title] => 'Retractable step fairing for amphibian airplane'
[patent_app_type] => 1
[patent_app_number] => 9/160140
[patent_app_country] => US
[patent_app_date] => 1998-09-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
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[patent_no_of_words] => 3071
[patent_no_of_claims] => 12
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[pdf_file] => patents/06/042/06042052.pdf
[firstpage_image] =>[orig_patent_app_number] => 160140
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/160140 | Retractable step fairing for amphibian airplane | Sep 24, 1998 | Issued |
Array
(
[id] => 4340290
[patent_doc_number] => 06189836
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2001-02-20
[patent_title] => 'Model-following control system using acceleration feedback'
[patent_app_type] => 1
[patent_app_number] => 9/160598
[patent_app_country] => US
[patent_app_date] => 1998-09-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
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[patent_no_of_words] => 9594
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[pdf_file] => patents/06/189/06189836.pdf
[firstpage_image] =>[orig_patent_app_number] => 160598
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/160598 | Model-following control system using acceleration feedback | Sep 24, 1998 | Issued |
Array
(
[id] => 4178826
[patent_doc_number] => 06129312
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-10-10
[patent_title] => 'Aircraft decompression vent assembly'
[patent_app_type] => 1
[patent_app_number] => 9/160629
[patent_app_country] => US
[patent_app_date] => 1998-09-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
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[pdf_file] => patents/06/129/06129312.pdf
[firstpage_image] =>[orig_patent_app_number] => 160629
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/160629 | Aircraft decompression vent assembly | Sep 23, 1998 | Issued |
Array
(
[id] => 4092976
[patent_doc_number] => 06056242
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-05-02
[patent_title] => 'Parachute release apparatus and method'
[patent_app_type] => 1
[patent_app_number] => 9/159665
[patent_app_country] => US
[patent_app_date] => 1998-09-24
[patent_effective_date] => 0000-00-00
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[pdf_file] => patents/06/056/06056242.pdf
[firstpage_image] =>[orig_patent_app_number] => 159665
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/159665 | Parachute release apparatus and method | Sep 23, 1998 | Issued |
Array
(
[id] => 4276643
[patent_doc_number] => 06182927
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2001-02-06
[patent_title] => 'Medium earth orbit augmentation of a global positioning system for global navigation'
[patent_app_type] => 1
[patent_app_number] => 9/159740
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[patent_app_date] => 1998-09-24
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[pdf_file] => patents/06/182/06182927.pdf
[firstpage_image] =>[orig_patent_app_number] => 159740
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/159740 | Medium earth orbit augmentation of a global positioning system for global navigation | Sep 23, 1998 | Issued |
Array
(
[id] => 4304196
[patent_doc_number] => 06247671
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2001-06-19
[patent_title] => 'Ion doping apparatus and method for aerodynamic flow control'
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[patent_app_number] => 9/158502
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[pdf_file] => patents/06/247/06247671.pdf
[firstpage_image] =>[orig_patent_app_number] => 158502
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/158502 | Ion doping apparatus and method for aerodynamic flow control | Sep 22, 1998 | Issued |
Array
(
[id] => 4099064
[patent_doc_number] => 06045095
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[patent_kind] => NA
[patent_issue_date] => 2000-04-04
[patent_title] => 'Vane-airfoil combination'
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[patent_app_number] => 9/159153
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[pdf_file] => patents/06/045/06045095.pdf
[firstpage_image] =>[orig_patent_app_number] => 159153
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/159153 | Vane-airfoil combination | Sep 22, 1998 | Issued |
Array
(
[id] => 4113568
[patent_doc_number] => 06145790
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[patent_issue_date] => 2000-11-14
[patent_title] => 'Attitude determination system and method'
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[pdf_file] => patents/06/145/06145790.pdf
[firstpage_image] =>[orig_patent_app_number] => 158675
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/158675 | Attitude determination system and method | Sep 21, 1998 | Issued |
Array
(
[id] => 3921437
[patent_doc_number] => 05975464
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[patent_issue_date] => 1999-11-02
[patent_title] => 'Aircraft with removable structural payload module'
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[patent_app_number] => 9/158186
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[pdf_file] => patents/05/975/05975464.pdf
[firstpage_image] =>[orig_patent_app_number] => 158186
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/158186 | Aircraft with removable structural payload module | Sep 21, 1998 | Issued |
Array
(
[id] => 4083507
[patent_doc_number] => 06098922
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[patent_issue_date] => 2000-08-08
[patent_title] => 'Lifting-fuselage/wing aircraft having low induced drag'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 09/157377 | Lifting-fuselage/wing aircraft having low induced drag | Sep 20, 1998 | Issued |
Array
(
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[patent_issue_date] => 2000-04-18
[patent_title] => 'Vertical take off and landing aircraft'
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[firstpage_image] =>[orig_patent_app_number] => 157730
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/157730 | Vertical take off and landing aircraft | Sep 20, 1998 | Issued |