Search

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 numberTitle of the applicationFiling DateStatus
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 [patent_words_short_claim] => 54 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_maintenance] => 1 [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 [patent_words_short_claim] => 120 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_words_short_claim] => 4 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 205 [patent_maintenance] => 1 [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 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 384 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [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 [patent_app_date] => 2000-10-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 15 [patent_no_of_words] => 2042 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 194 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_app_date] => 2000-10-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 6 [patent_no_of_words] => 1830 [patent_no_of_claims] => 2 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 198 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [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 [patent_app_country] => US [patent_app_date] => 2000-10-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 5 [patent_no_of_words] => 2285 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 100 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [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 [patent_app_country] => US [patent_app_date] => 2000-10-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2350 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 150 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [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 [patent_app_country] => US [patent_app_date] => 2000-09-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 14 [patent_figures_cnt] => 19 [patent_no_of_words] => 16681 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 7 [patent_words_short_claim] => 111 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/764/06764049.pdf [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 [patent_country] => US [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 [patent_app_country] => US [patent_app_date] => 2000-09-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 14 [patent_figures_cnt] => 19 [patent_no_of_words] => 16679 [patent_no_of_claims] => 25 [patent_no_of_ind_claims] => 25 [patent_words_short_claim] => 129 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/422/06422516.pdf [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 [patent_country] => US [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' [patent_app_type] => 1 [patent_app_number] => 9/672062 [patent_app_country] => US [patent_app_date] => 2000-09-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 14 [patent_figures_cnt] => 19 [patent_no_of_words] => 17137 [patent_no_of_claims] => 24 [patent_no_of_ind_claims] => 6 [patent_words_short_claim] => 151 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/328/06328264.pdf [firstpage_image] =>[orig_patent_app_number] => 672062 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/672062
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] => 1567923 [patent_doc_number] => 06497390 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-12-24 [patent_title] => 'Thermal protection system especially for space vehicles' [patent_app_type] => B1 [patent_app_number] => 09/669128 [patent_app_country] => US [patent_app_date] => 2000-09-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 9 [patent_no_of_words] => 2899 [patent_no_of_claims] => 22 [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/06/497/06497390.pdf [firstpage_image] =>[orig_patent_app_number] => 09669128 [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 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2003-02-11 [patent_title] => 'Friction and stiction compensation for spacecraft attitude control' [patent_app_type] => B1 [patent_app_number] => 09/660749 [patent_app_country] => US [patent_app_date] => 2000-09-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 5327 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 112 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/517/06517029.pdf [firstpage_image] =>[orig_patent_app_number] => 09660749 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/660749
Friction and stiction compensation for spacecraft attitude control Sep 12, 2000 Issued
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