John W. Eldred

Array ( [id] => 4150310 [patent_doc_number] => 06138956 [patent_country] => US [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 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 19 [patent_no_of_words] => 6824 [patent_no_of_claims] => 21 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 123 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/138/06138956.pdf [firstpage_image] =>[orig_patent_app_number] => 157738 [rel_patent_id] =>[rel_patent_doc_number] =>)

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 [patent_figures_cnt] => 25 [patent_no_of_words] => 5640 [patent_no_of_claims] => 21 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 77 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/073/06073882.pdf [firstpage_image] =>[orig_patent_app_number] => 158354 [rel_patent_id] =>[rel_patent_doc_number] =>)

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 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 184 [patent_maintenance] => 1 [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] =>)

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 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 6 [patent_no_of_words] => 3612 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 100 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/129/06129308.pdf [firstpage_image] =>[orig_patent_app_number] => 157745 [rel_patent_id] =>[rel_patent_doc_number] =>)

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] =>)

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 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 6 [patent_no_of_words] => 3410 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 168 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/992/05992797.pdf [firstpage_image] =>[orig_patent_app_number] => 157086 [rel_patent_id] =>[rel_patent_doc_number] =>)

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 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 5 [patent_no_of_words] => 2826 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 125 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/082/06082674.pdf [firstpage_image] =>[orig_patent_app_number] => 154306 [rel_patent_id] =>[rel_patent_doc_number] =>)

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 [patent_app_date] => 1998-09-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 1731 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 9 [patent_words_short_claim] => 57 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/378/06378809.pdf [firstpage_image] =>[orig_patent_app_number] => 09154396 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4167634 [patent_doc_number] => 06019320 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 2000-02-01 [patent_title] => 'Spacecraft acquisition of sun pointing' [patent_app_type] => 1 [patent_app_number] => 9/153123 [patent_app_country] => US [patent_app_date] => 1998-09-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 8 [patent_no_of_words] => 4018 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 239 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/019/06019320.pdf [firstpage_image] =>[orig_patent_app_number] => 153123 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4128489 [patent_doc_number] => 06062513 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 2000-05-16 [patent_title] => 'Total energy based flight control system' [patent_app_type] => 1 [patent_app_number] => 9/152732 [patent_app_country] => US [patent_app_date] => 1998-09-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 8300 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 167 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/062/06062513.pdf [firstpage_image] =>[orig_patent_app_number] => 152732 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4067244 [patent_doc_number] => 06053454 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 2000-04-25 [patent_title] => 'Modular spacecraft payload support structure' [patent_app_type] => 1 [patent_app_number] => 9/148581 [patent_app_country] => US [patent_app_date] => 1998-09-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 8 [patent_no_of_words] => 2496 [patent_no_of_claims] => 31 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 100 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/053/06053454.pdf [firstpage_image] =>[orig_patent_app_number] => 148581 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4345534 [patent_doc_number] => 06168114 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 2001-01-02 [patent_title] => 'Aircraft door assembly' [patent_app_type] => 1 [patent_app_number] => 9/148151 [patent_app_country] => US [patent_app_date] => 1998-09-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 6 [patent_no_of_words] => 3053 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 167 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/168/06168114.pdf [firstpage_image] =>[orig_patent_app_number] => 148151 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4087379 [patent_doc_number] => 06065720 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 2000-05-23 [patent_title] => 'Manufacture of aircraft' [patent_app_type] => 1 [patent_app_number] => 9/144263 [patent_app_country] => US [patent_app_date] => 1998-08-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 1538 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 90 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/065/06065720.pdf [firstpage_image] =>[orig_patent_app_number] => 144263 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 3924174 [patent_doc_number] => 05996939 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1999-12-07 [patent_title] => 'Aerial refueling boom with translating pivot' [patent_app_type] => 1 [patent_app_number] => 9/141699 [patent_app_country] => US [patent_app_date] => 1998-08-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 7 [patent_no_of_words] => 3181 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 74 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/996/05996939.pdf [firstpage_image] =>[orig_patent_app_number] => 141699 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4128413 [patent_doc_number] => 06062508 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 2000-05-16 [patent_title] => 'Compound aircraft' [patent_app_type] => 1 [patent_app_number] => 9/139898 [patent_app_country] => US [patent_app_date] => 1998-08-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 12 [patent_no_of_words] => 4191 [patent_no_of_claims] => 29 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 161 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/062/06062508.pdf [firstpage_image] =>[orig_patent_app_number] => 139898 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 3982744 [patent_doc_number] => 06003504 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1999-12-21 [patent_title] => 'Paint ball gun' [patent_app_type] => 1 [patent_app_number] => 9/137641 [patent_app_country] => US [patent_app_date] => 1998-08-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 2927 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 112 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/003/06003504.pdf [firstpage_image] =>[orig_patent_app_number] => 137641 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4289717 [patent_doc_number] => 06325330 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 2001-12-04 [patent_title] => 'Power generation, transmission, and distribution system for an aerostat using a lightweight tether' [patent_app_type] => 1 [patent_app_number] => 9/136115 [patent_app_country] => US [patent_app_date] => 1998-08-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 4 [patent_no_of_words] => 4330 [patent_no_of_claims] => 21 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 94 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/325/06325330.pdf [firstpage_image] =>[orig_patent_app_number] => 136115 [rel_patent_id] =>[rel_patent_doc_number] =>)