William Alexander Grant

Array ( [id] => 3792856 [patent_doc_number] => 05810296 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-09-22 [patent_title] => 'Integrated restraint/release/deployment initiation device' [patent_app_type] => 1 [patent_app_number] => 8/711714 [patent_app_country] => US [patent_app_date] => 1996-08-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 9 [patent_no_of_words] => 4244 [patent_no_of_claims] => 30 [patent_no_of_ind_claims] => 6 [patent_words_short_claim] => 167 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/810/05810296.pdf [firstpage_image] =>[orig_patent_app_number] => 711714 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 3746561 [patent_doc_number] => 05850988 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-12-22 [patent_title] => 'Radiosonde balloon launching system' [patent_app_type] => 1 [patent_app_number] => 8/700238 [patent_app_country] => US [patent_app_date] => 1996-08-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 14 [patent_figures_cnt] => 20 [patent_no_of_words] => 4092 [patent_no_of_claims] => 32 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 74 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/850/05850988.pdf [firstpage_image] =>[orig_patent_app_number] => 700238 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4008043 [patent_doc_number] => 05924649 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1999-07-20 [patent_title] => 'Aircraft with supporting wings having members for taking up tensile and compressive forces' [patent_app_type] => 1 [patent_app_number] => 8/694817 [patent_app_country] => US [patent_app_date] => 1996-08-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 3528 [patent_no_of_claims] => 26 [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/05/924/05924649.pdf [firstpage_image] =>[orig_patent_app_number] => 694817 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 3757382 [patent_doc_number] => 05806805 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-09-15 [patent_title] => 'Fault tolerant actuation system for flight control actuators' [patent_app_type] => 1 [patent_app_number] => 8/693956 [patent_app_country] => US [patent_app_date] => 1996-08-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 11 [patent_no_of_words] => 7853 [patent_no_of_claims] => 22 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 214 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/806/05806805.pdf [firstpage_image] =>[orig_patent_app_number] => 693956 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 3726289 [patent_doc_number] => 05752676 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-05-19 [patent_title] => 'Spacecraft with integrated array of solar cells and electronically scannable antenna' [patent_app_type] => 1 [patent_app_number] => 8/692996 [patent_app_country] => US [patent_app_date] => 1996-08-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 1747 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 38 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/752/05752676.pdf [firstpage_image] =>[orig_patent_app_number] => 692996 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 3892499 [patent_doc_number] => 05897077 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1999-04-27 [patent_title] => 'Quick-change skid landing gear' [patent_app_type] => 1 [patent_app_number] => 8/693514 [patent_app_country] => US [patent_app_date] => 1996-08-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 13 [patent_no_of_words] => 4122 [patent_no_of_claims] => 25 [patent_no_of_ind_claims] => 7 [patent_words_short_claim] => 82 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/897/05897077.pdf [firstpage_image] =>[orig_patent_app_number] => 693514 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 3851521 [patent_doc_number] => 05836543 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-11-17 [patent_title] => 'Discus-shaped aerodyne vehicle for extremely high velocities' [patent_app_type] => 1 [patent_app_number] => 8/666581 [patent_app_country] => US [patent_app_date] => 1996-08-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 3 [patent_no_of_words] => 3653 [patent_no_of_claims] => 14 [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/05/836/05836543.pdf [firstpage_image] =>[orig_patent_app_number] => 666581 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 3797242 [patent_doc_number] => 05788183 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-08-04 [patent_title] => 'Device for adapting the position of the seat proper for a seat having a back that folds down to a sleeping position' [patent_app_type] => 1 [patent_app_number] => 8/687994 [patent_app_country] => US [patent_app_date] => 1996-07-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 7 [patent_no_of_words] => 4489 [patent_no_of_claims] => 41 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 210 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/788/05788183.pdf [firstpage_image] =>[orig_patent_app_number] => 687994 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 3755392 [patent_doc_number] => 05732904 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-03-31 [patent_title] => 'Device for signature reduction' [patent_app_type] => 1 [patent_app_number] => 8/680606 [patent_app_country] => US [patent_app_date] => 1996-07-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 7 [patent_no_of_words] => 1983 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 79 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/732/05732904.pdf [firstpage_image] =>[orig_patent_app_number] => 680606 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 3856949 [patent_doc_number] => 05823470 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-10-20 [patent_title] => 'Split torque proprotor transmission' [patent_app_type] => 1 [patent_app_number] => 8/682026 [patent_app_country] => US [patent_app_date] => 1996-07-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 4 [patent_no_of_words] => 4090 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 125 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/823/05823470.pdf [firstpage_image] =>[orig_patent_app_number] => 682026 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 3783467 [patent_doc_number] => 05826829 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-10-27 [patent_title] => 'Spacecraft control system with a trihedral momentum bias wheel configuration' [patent_app_type] => 1 [patent_app_number] => 8/679575 [patent_app_country] => US [patent_app_date] => 1996-07-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 4 [patent_no_of_words] => 6431 [patent_no_of_claims] => 21 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 126 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/826/05826829.pdf [firstpage_image] =>[orig_patent_app_number] => 679575 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 3882156 [patent_doc_number] => 05838567 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-11-17 [patent_title] => 'System and method for incremental fabrication of circuit boards' [patent_app_type] => 1 [patent_app_number] => 8/677989 [patent_app_country] => US [patent_app_date] => 1996-07-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 15 [patent_figures_cnt] => 16 [patent_no_of_words] => 8247 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 5 [patent_words_short_claim] => 127 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/838/05838567.pdf [firstpage_image] =>[orig_patent_app_number] => 677989 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 3755385 [patent_doc_number] => 05755407 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-05-26 [patent_title] => 'Slotted nut type releasing device for microsatellite ejector' [patent_app_type] => 1 [patent_app_number] => 8/677316 [patent_app_country] => US [patent_app_date] => 1996-07-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 3 [patent_no_of_words] => 1730 [patent_no_of_claims] => 7 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 171 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/755/05755407.pdf [firstpage_image] =>[orig_patent_app_number] => 677316 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 3817016 [patent_doc_number] => 05738300 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-04-14 [patent_title] => 'Helicopter autopilot providing airspeed control' [patent_app_type] => 1 [patent_app_number] => 8/682505 [patent_app_country] => US [patent_app_date] => 1996-07-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 2968 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 40 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/738/05738300.pdf [firstpage_image] =>[orig_patent_app_number] => 682505 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 3912963 [patent_doc_number] => 05927656 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1999-07-27 [patent_title] => 'Wing leading edge flap and method therefor' [patent_app_type] => 1 [patent_app_number] => 8/673675 [patent_app_country] => US [patent_app_date] => 1996-06-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 7 [patent_no_of_words] => 3810 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 263 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/927/05927656.pdf [firstpage_image] =>[orig_patent_app_number] => 673675 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 3817139 [patent_doc_number] => 05738308 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-04-14 [patent_title] => 'Ion thruster support and positioning system' [patent_app_type] => 1 [patent_app_number] => 8/695685 [patent_app_country] => US [patent_app_date] => 1996-06-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 3859 [patent_no_of_claims] => 23 [patent_no_of_ind_claims] => 5 [patent_words_short_claim] => 124 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/738/05738308.pdf [firstpage_image] =>[orig_patent_app_number] => 695685 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 3860516 [patent_doc_number] => 05746393 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-05-05 [patent_title] => 'Aircraft wheel rotating apparatus' [patent_app_type] => 1 [patent_app_number] => 8/670266 [patent_app_country] => US [patent_app_date] => 1996-06-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 3 [patent_no_of_words] => 2248 [patent_no_of_claims] => 2 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 279 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/746/05746393.pdf [firstpage_image] =>[orig_patent_app_number] => 670266 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 3871655 [patent_doc_number] => 05833174 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-11-10 [patent_title] => 'Billowing rotary kite' [patent_app_type] => 1 [patent_app_number] => 8/667432 [patent_app_country] => US [patent_app_date] => 1996-06-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 7 [patent_no_of_words] => 3810 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 185 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/833/05833174.pdf [firstpage_image] =>[orig_patent_app_number] => 667432 [rel_patent_id] =>[rel_patent_doc_number] =>)