
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] => 4309937
[patent_doc_number] => 06328262
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2001-12-11
[patent_title] => 'Method for forming a parachute and a parachute formed thereby'
[patent_app_type] => 1
[patent_app_number] => 9/710735
[patent_app_country] => US
[patent_app_date] => 2000-11-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 7
[patent_no_of_words] => 1979
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 154
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/328/06328262.pdf
[firstpage_image] =>[orig_patent_app_number] => 710735
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/710735 | Method for forming a parachute and a parachute formed thereby | Nov 7, 2000 | Issued |
Array
(
[id] => 1347457
[patent_doc_number] => 06568638
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2003-05-27
[patent_title] => 'Modular spacecraft structure'
[patent_app_type] => B1
[patent_app_number] => 09/706833
[patent_app_country] => US
[patent_app_date] => 2000-11-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 13
[patent_no_of_words] => 2926
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 44
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/568/06568638.pdf
[firstpage_image] =>[orig_patent_app_number] => 09706833
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/706833 | Modular spacecraft structure | Nov 6, 2000 | Issued |
Array
(
[id] => 1381724
[patent_doc_number] => 06530540
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2003-03-11
[patent_title] => 'Flapping-wing flying device'
[patent_app_type] => B1
[patent_app_number] => 09/705431
[patent_app_country] => US
[patent_app_date] => 2000-11-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 18
[patent_no_of_words] => 5875
[patent_no_of_claims] => 21
[patent_no_of_ind_claims] => 8
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/530/06530540.pdf
[firstpage_image] =>[orig_patent_app_number] => 09705431
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/705431 | Flapping-wing flying device | Nov 2, 2000 | Issued |
Array
(
[id] => 1511875
[patent_doc_number] => 06419189
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-07-16
[patent_title] => 'Hot ruddervator apparatus and method for an aerospacecraft'
[patent_app_type] => B1
[patent_app_number] => 09/703568
[patent_app_country] => US
[patent_app_date] => 2000-11-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 8
[patent_no_of_words] => 2436
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 111
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/419/06419189.pdf
[firstpage_image] =>[orig_patent_app_number] => 09703568
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/703568 | Hot ruddervator apparatus and method for an aerospacecraft | Oct 31, 2000 | Issued |
Array
(
[id] => 4309907
[patent_doc_number] => 06328260
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2001-12-11
[patent_title] => 'Wing spar modification kit'
[patent_app_type] => 1
[patent_app_number] => 9/696127
[patent_app_country] => US
[patent_app_date] => 2000-10-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 7
[patent_no_of_words] => 3920
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 298
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/328/06328260.pdf
[firstpage_image] =>[orig_patent_app_number] => 696127
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/696127 | Wing spar modification kit | Oct 24, 2000 | Issued |
Array
(
[id] => 1584316
[patent_doc_number] => 06481670
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-11-19
[patent_title] => 'Apparatus for spacecraft thermal management'
[patent_app_type] => B1
[patent_app_number] => 09/693534
[patent_app_country] => US
[patent_app_date] => 2000-10-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 4538
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 5
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/481/06481670.pdf
[firstpage_image] =>[orig_patent_app_number] => 09693534
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/693534 | Apparatus for spacecraft thermal management | Oct 19, 2000 | Issued |
Array
(
[id] => 1577107
[patent_doc_number] => 06422518
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-07-23
[patent_title] => 'Aircraft with means for a premature breakdown of the wing vortex pair'
[patent_app_type] => B1
[patent_app_number] => 09/692434
[patent_app_country] => US
[patent_app_date] => 2000-10-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 12
[patent_no_of_words] => 5125
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 213
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/422/06422518.pdf
[firstpage_image] =>[orig_patent_app_number] => 09692434
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/692434 | Aircraft with means for a premature breakdown of the wing vortex pair | Oct 18, 2000 | Issued |
Array
(
[id] => 7641515
[patent_doc_number] => 06394392
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-05-28
[patent_title] => 'Aircraft having multiple fuselages'
[patent_app_type] => B1
[patent_app_number] => 09/691930
[patent_app_country] => US
[patent_app_date] => 2000-10-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 24
[patent_figures_cnt] => 24
[patent_no_of_words] => 4676
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 2
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/394/06394392.pdf
[firstpage_image] =>[orig_patent_app_number] => 09691930
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/691930 | Aircraft having multiple fuselages | Oct 17, 2000 | Issued |
Array
(
[id] => 1405920
[patent_doc_number] => 06502497
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2003-01-07
[patent_title] => 'Suspension device for connecting an item of on-board equipment to the structure of a vehicle, particularly a rotary-wing aircraft'
[patent_app_type] => B1
[patent_app_number] => 09/689724
[patent_app_country] => US
[patent_app_date] => 2000-10-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 10
[patent_no_of_words] => 5623
[patent_no_of_claims] => 17
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/502/06502497.pdf
[firstpage_image] =>[orig_patent_app_number] => 09689724
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/689724 | Suspension device for connecting an item of on-board equipment to the structure of a vehicle, particularly a rotary-wing aircraft | Oct 12, 2000 | Issued |
Array
(
[id] => 1045230
[patent_doc_number] => 06863240
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2005-03-08
[patent_title] => 'Hovering body'
[patent_app_type] => utility
[patent_app_number] => 10/110607
[patent_app_country] => US
[patent_app_date] => 2000-10-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 12
[patent_no_of_words] => 5361
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[pdf_file] => patents/06/863/06863240.pdf
[firstpage_image] =>[orig_patent_app_number] => 10110607
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/110607 | Hovering body | Oct 10, 2000 | Issued |
Array
(
[id] => 1511879
[patent_doc_number] => 06419190
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-07-16
[patent_title] => 'Airborne cleaning and painting robot'
[patent_app_type] => B1
[patent_app_number] => 09/684382
[patent_app_country] => US
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[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/419/06419190.pdf
[firstpage_image] =>[orig_patent_app_number] => 09684382
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/684382 | Airborne cleaning and painting robot | Oct 9, 2000 | Issued |
Array
(
[id] => 1434393
[patent_doc_number] => 06354032
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-03-12
[patent_title] => 'Trigger stop'
[patent_app_type] => B1
[patent_app_number] => 09/680917
[patent_app_country] => US
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[patent_drawing_sheets_cnt] => 2
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[pdf_file] => patents/06/354/06354032.pdf
[firstpage_image] =>[orig_patent_app_number] => 09680917
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/680917 | Trigger stop | Oct 5, 2000 | Issued |
Array
(
[id] => 1473750
[patent_doc_number] => 06450453
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-09-17
[patent_title] => 'Active steering of an appendage on a spacecraft using piezoelectric actuators'
[patent_app_type] => B1
[patent_app_number] => 09/684225
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[pdf_file] => patents/06/450/06450453.pdf
[firstpage_image] =>[orig_patent_app_number] => 09684225
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/684225 | Active steering of an appendage on a spacecraft using piezoelectric actuators | Oct 5, 2000 | Issued |
Array
(
[id] => 1577083
[patent_doc_number] => 06422510
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-07-23
[patent_title] => 'Shimmy-free aircraft tail wheel conversion'
[patent_app_type] => B1
[patent_app_number] => 09/679965
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[pdf_file] => patents/06/422/06422510.pdf
[firstpage_image] =>[orig_patent_app_number] => 09679965
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/679965 | Shimmy-free aircraft tail wheel conversion | Oct 4, 2000 | Issued |
Array
(
[id] => 1148402
[patent_doc_number] => 06764049
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2004-07-20
[patent_title] => 'Artificial satellite with an orbit having a long staying time in a zenith direction, an orbit control method and a communication system therewith'
[patent_app_type] => B1
[patent_app_number] => 09/672951
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[firstpage_image] =>[orig_patent_app_number] => 09672951
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/672951 | Artificial satellite with an orbit having a long staying time in a zenith direction, an orbit control method and a communication system therewith | Sep 28, 2000 | Issued |
Array
(
[id] => 1577101
[patent_doc_number] => 06422516
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[patent_kind] => B1
[patent_issue_date] => 2002-07-23
[patent_title] => 'Artificial satellite with an orbit having a long staying time in a zenith direction, an orbit control method and a communication system therewith'
[patent_app_type] => B1
[patent_app_number] => 09/672061
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[firstpage_image] =>[orig_patent_app_number] => 09672061
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/672061 | Artificial satellite with an orbit having a long staying time in a zenith direction, an orbit control method and a communication system therewith | Sep 28, 2000 | Issued |
Array
(
[id] => 4309962
[patent_doc_number] => 06328264
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[patent_kind] => NA
[patent_issue_date] => 2001-12-11
[patent_title] => 'Artificial satellite with an orbit having a long staying time in a zenith direction, an orbit control method and a communication system therewith'
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Array
(
[id] => 1567923
[patent_doc_number] => 06497390
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[patent_issue_date] => 2002-12-24
[patent_title] => 'Thermal protection system especially for space vehicles'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 09/669128 | Thermal protection system especially for space vehicles | Sep 24, 2000 | Issued |
| 09/666387 | Articulated set of sequentially opened solar generator panels | Sep 19, 2000 | Abandoned |
Array
(
[id] => 1396636
[patent_doc_number] => 06517029
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[patent_title] => 'Friction and stiction compensation for spacecraft attitude control'
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[patent_app_number] => 09/660749
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[rel_patent_id] =>[rel_patent_doc_number] =>) 09/660749 | Friction and stiction compensation for spacecraft attitude control | Sep 12, 2000 | Issued |