
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] => 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] => 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
[patent_app_country] => US
[patent_app_date] => 1998-09-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 11
[patent_no_of_words] => 5051
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 168
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[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] => 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
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 8
[patent_no_of_words] => 2922
[patent_no_of_claims] => 48
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 111
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[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] => 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
[patent_figures_cnt] => 13
[patent_no_of_words] => 1571
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 121
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[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] => 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'
[patent_app_type] => 1
[patent_app_number] => 9/158502
[patent_app_country] => US
[patent_app_date] => 1998-09-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 8
[patent_no_of_words] => 4865
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 8
[patent_words_short_claim] => 20
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[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
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-04-04
[patent_title] => 'Vane-airfoil combination'
[patent_app_type] => 1
[patent_app_number] => 9/159153
[patent_app_country] => US
[patent_app_date] => 1998-09-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 13
[patent_no_of_words] => 5774
[patent_no_of_claims] => 21
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 63
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[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
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-11-14
[patent_title] => 'Attitude determination system and method'
[patent_app_type] => 1
[patent_app_number] => 9/158675
[patent_app_country] => US
[patent_app_date] => 1998-09-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2347
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 135
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[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
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-11-02
[patent_title] => 'Aircraft with removable structural payload module'
[patent_app_type] => 1
[patent_app_number] => 9/158186
[patent_app_country] => US
[patent_app_date] => 1998-09-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 13
[patent_no_of_words] => 5723
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 128
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[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] => 4216191
[patent_doc_number] => 06164599
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-12-26
[patent_title] => 'Aerofoil profile with variable profile adaptation'
[patent_app_type] => 1
[patent_app_number] => 9/157711
[patent_app_country] => US
[patent_app_date] => 1998-09-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 3317
[patent_no_of_claims] => 18
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/164/06164599.pdf
[firstpage_image] =>[orig_patent_app_number] => 157711
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/157711 | Aerofoil profile with variable profile adaptation | Sep 20, 1998 | Issued |
Array
(
[id] => 4108131
[patent_doc_number] => 06126113
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-10-03
[patent_title] => 'Helicopter removable drive train platform'
[patent_app_type] => 1
[patent_app_number] => 9/158358
[patent_app_country] => US
[patent_app_date] => 1998-09-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 7
[patent_no_of_words] => 3344
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 71
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/126/06126113.pdf
[firstpage_image] =>[orig_patent_app_number] => 158358
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/158358 | Helicopter removable drive train platform | Sep 20, 1998 | Issued |
Array
(
[id] => 4083507
[patent_doc_number] => 06098922
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-08-08
[patent_title] => 'Lifting-fuselage/wing aircraft having low induced drag'
[patent_app_type] => 1
[patent_app_number] => 9/157377
[patent_app_country] => US
[patent_app_date] => 1998-09-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[patent_no_of_words] => 6623
[patent_no_of_claims] => 28
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/098/06098922.pdf
[firstpage_image] =>[orig_patent_app_number] => 157377
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/157377 | Lifting-fuselage/wing aircraft having low induced drag | Sep 20, 1998 | Issued |
Array
(
[id] => 4218224
[patent_doc_number] => 06073882
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-06-13
[patent_title] => 'Flying vehicle with retractable wing assembly'
[patent_app_type] => 1
[patent_app_number] => 9/158354
[patent_app_country] => US
[patent_app_date] => 1998-09-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
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[pdf_file] => patents/06/073/06073882.pdf
[firstpage_image] =>[orig_patent_app_number] => 158354
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/158354 | Flying vehicle with retractable wing assembly | Sep 20, 1998 | Issued |
Array
(
[id] => 4087928
[patent_doc_number] => 06050520
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-04-18
[patent_title] => 'Vertical take off and landing aircraft'
[patent_app_type] => 1
[patent_app_number] => 9/157730
[patent_app_country] => US
[patent_app_date] => 1998-09-21
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[pdf_file] => patents/06/050/06050520.pdf
[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 |
Array
(
[id] => 4150310
[patent_doc_number] => 06138956
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[patent_kind] => NA
[patent_issue_date] => 2000-10-31
[patent_title] => 'Aerofoil profile with variable profile adaptation'
[patent_app_type] => 1
[patent_app_number] => 9/157738
[patent_app_country] => US
[patent_app_date] => 1998-09-21
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[pdf_file] => patents/06/138/06138956.pdf
[firstpage_image] =>[orig_patent_app_number] => 157738
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/157738 | Aerofoil profile with variable profile adaptation | Sep 20, 1998 | Issued |
Array
(
[id] => 4178770
[patent_doc_number] => 06129308
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-10-10
[patent_title] => 'Delta-shaped aircraft with variable camber fuselage and wing'
[patent_app_type] => 1
[patent_app_number] => 9/157745
[patent_app_country] => US
[patent_app_date] => 1998-09-21
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[pdf_file] => patents/06/129/06129308.pdf
[firstpage_image] =>[orig_patent_app_number] => 157745
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/157745 | Delta-shaped aircraft with variable camber fuselage and wing | Sep 20, 1998 | Issued |
Array
(
[id] => 4008350
[patent_doc_number] => 05992797
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-11-30
[patent_title] => 'Dual upper deck airplane'
[patent_app_type] => 1
[patent_app_number] => 9/157086
[patent_app_country] => US
[patent_app_date] => 1998-09-18
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[pdf_file] => patents/05/992/05992797.pdf
[firstpage_image] =>[orig_patent_app_number] => 157086
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/157086 | Dual upper deck airplane | Sep 17, 1998 | Issued |
Array
(
[id] => 4155506
[patent_doc_number] => 06082674
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-07-04
[patent_title] => 'Aircraft window escuthcheon assembly'
[patent_app_type] => 1
[patent_app_number] => 9/154306
[patent_app_country] => US
[patent_app_date] => 1998-09-16
[patent_effective_date] => 0000-00-00
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[pdf_file] => patents/06/082/06082674.pdf
[firstpage_image] =>[orig_patent_app_number] => 154306
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/154306 | Aircraft window escuthcheon assembly | Sep 15, 1998 | Issued |
Array
(
[id] => 7637842
[patent_doc_number] => 06378809
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-04-30
[patent_title] => 'AFT deployable thermal radiators for spacecraft'
[patent_app_type] => B1
[patent_app_number] => 09/154396
[patent_app_country] => US
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[pdf_file] => patents/06/378/06378809.pdf
[firstpage_image] =>[orig_patent_app_number] => 09154396
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/154396 | AFT deployable thermal radiators for spacecraft | Sep 15, 1998 | Issued |
Array
(
[id] => 4167634
[patent_doc_number] => 06019320
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[patent_kind] => NA
[patent_issue_date] => 2000-02-01
[patent_title] => 'Spacecraft acquisition of sun pointing'
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[patent_app_number] => 9/153123
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[pdf_file] => patents/06/019/06019320.pdf
[firstpage_image] =>[orig_patent_app_number] => 153123
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/153123 | Spacecraft acquisition of sun pointing | Sep 14, 1998 | Issued |
Array
(
[id] => 4128489
[patent_doc_number] => 06062513
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[patent_issue_date] => 2000-05-16
[patent_title] => 'Total energy based flight control system'
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[pdf_file] => patents/06/062/06062513.pdf
[firstpage_image] =>[orig_patent_app_number] => 152732
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/152732 | Total energy based flight control system | Sep 13, 1998 | Issued |