Frederick Lyndon Lagman

Array ( [id] => 8214782 [patent_doc_number] => 08193476 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-06-05 [patent_title] => 'Solid-fuel pellet thrust and control actuation system to maneuver a flight vehicle' [patent_app_type] => utility [patent_app_number] => 12/203302 [patent_app_country] => US [patent_app_date] => 2008-09-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 13 [patent_figures_cnt] => 20 [patent_no_of_words] => 5843 [patent_no_of_claims] => 27 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 185 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/08/193/08193476.pdf [firstpage_image] =>[orig_patent_app_number] => 12203302 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 8541844 [patent_doc_number] => 08317130 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2012-11-27 [patent_title] => 'Landing gear mount' [patent_app_type] => utility [patent_app_number] => 12/200318 [patent_app_country] => US [patent_app_date] => 2008-08-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 2249 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 128 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12200318 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 8338681 [patent_doc_number] => 08240600 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-08-14 [patent_title] => 'Pylon for suspending an engine beneath an aircraft wing' [patent_app_type] => utility [patent_app_number] => 12/199218 [patent_app_country] => US [patent_app_date] => 2008-08-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 2 [patent_no_of_words] => 1756 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 121 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12199218 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6215429 [patent_doc_number] => 20100051754 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-03-04 [patent_title] => 'Aircraft' [patent_app_type] => utility [patent_app_number] => 12/198940 [patent_app_country] => US [patent_app_date] => 2008-08-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 6013 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0051/20100051754.pdf [firstpage_image] =>[orig_patent_app_number] => 12198940 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 8355738 [patent_doc_number] => 20120210901 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-08-23 [patent_title] => 'SELF-SPRUNG STABILIZATION FIN SYSTEM FOR GUN-LAUNCHED ARTILLERY PROJECTILES' [patent_app_type] => utility [patent_app_number] => 12/193330 [patent_app_country] => US [patent_app_date] => 2008-08-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 2531 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12193330 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 8161099 [patent_doc_number] => 08172178 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-05-08 [patent_title] => 'Device for generating aerodynamic disturbances so as to protect the outer surface of an aircraft against elevated temperatures' [patent_app_type] => utility [patent_app_number] => 12/192148 [patent_app_country] => US [patent_app_date] => 2008-08-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 15 [patent_no_of_words] => 3403 [patent_no_of_claims] => 14 [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/08/172/08172178.pdf [firstpage_image] =>[orig_patent_app_number] => 12192148 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 8245178 [patent_doc_number] => 08203108 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-06-19 [patent_title] => 'Fuze guidance system with multiple caliber capability' [patent_app_type] => utility [patent_app_number] => 12/188568 [patent_app_country] => US [patent_app_date] => 2008-08-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 15 [patent_no_of_words] => 3334 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 64 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/08/203/08203108.pdf [firstpage_image] =>[orig_patent_app_number] => 12188568 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 8316305 [patent_doc_number] => 08231077 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-07-31 [patent_title] => 'Torque counter-action device' [patent_app_type] => utility [patent_app_number] => 12/187494 [patent_app_country] => US [patent_app_date] => 2008-08-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 2315 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 106 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12187494 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6335147 [patent_doc_number] => 20100019099 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-01-28 [patent_title] => 'Integrally Ribbed Rogallo Wing Array' [patent_app_type] => utility [patent_app_number] => 12/181095 [patent_app_country] => US [patent_app_date] => 2008-07-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 2573 [patent_no_of_claims] => 26 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0019/20100019099.pdf [firstpage_image] =>[orig_patent_app_number] => 12181095 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6335144 [patent_doc_number] => 20100019098 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-01-28 [patent_title] => 'Ducted Fan Core for Use with an Unmanned Aerial Vehicle' [patent_app_type] => utility [patent_app_number] => 12/179690 [patent_app_country] => US [patent_app_date] => 2008-07-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 2823 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0019/20100019098.pdf [firstpage_image] =>[orig_patent_app_number] => 12179690 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 8268975 [patent_doc_number] => 08210473 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-07-03 [patent_title] => 'Folding wing root mechanism' [patent_app_type] => utility [patent_app_number] => 12/177862 [patent_app_country] => US [patent_app_date] => 2008-07-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 2480 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 236 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12177862 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6499808 [patent_doc_number] => 20100012773 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-01-21 [patent_title] => 'Aircrft Structure' [patent_app_type] => utility [patent_app_number] => 12/174516 [patent_app_country] => US [patent_app_date] => 2008-07-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 14 [patent_figures_cnt] => 14 [patent_no_of_words] => 2630 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0012/20100012773.pdf [firstpage_image] =>[orig_patent_app_number] => 12174516 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 8541845 [patent_doc_number] => 08317131 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-11-27 [patent_title] => 'Braking-energy equalization system' [patent_app_type] => utility [patent_app_number] => 12/168958 [patent_app_country] => US [patent_app_date] => 2008-07-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 4 [patent_no_of_words] => 2477 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 120 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12168958 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5449599 [patent_doc_number] => 20090065635 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-03-12 [patent_title] => 'Pitch-oscillation limitation system applied to an aircraft' [patent_app_type] => utility [patent_app_number] => 12/168988 [patent_app_country] => US [patent_app_date] => 2008-07-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 2740 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0065/20090065635.pdf [firstpage_image] =>[orig_patent_app_number] => 12168988 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 8243856 [patent_doc_number] => 08201773 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2012-06-19 [patent_title] => 'Flexible self-erecting substructures for sensor networks' [patent_app_type] => utility [patent_app_number] => 12/167075 [patent_app_country] => US [patent_app_date] => 2008-07-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 15 [patent_no_of_words] => 3829 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 90 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/08/201/08201773.pdf [firstpage_image] =>[orig_patent_app_number] => 12167075 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 8444871 [patent_doc_number] => 08286916 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-10-16 [patent_title] => 'Retractable aerodynamic device permitting the control of the wake trajectory of an aircraft trap' [patent_app_type] => utility [patent_app_number] => 12/165965 [patent_app_country] => US [patent_app_date] => 2008-07-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 14 [patent_no_of_words] => 3322 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 158 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12165965 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5461362 [patent_doc_number] => 20090321562 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-12-31 [patent_title] => 'METHODS AND APPARATUS FOR AN ASYMMETRICAL FAIRING' [patent_app_type] => utility [patent_app_number] => 12/165357 [patent_app_country] => US [patent_app_date] => 2008-06-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 2466 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0321/20090321562.pdf [firstpage_image] =>[orig_patent_app_number] => 12165357 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5461359 [patent_doc_number] => 20090321559 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-12-31 [patent_title] => 'Aircraft noise reduction apparatus' [patent_app_type] => utility [patent_app_number] => 12/153493 [patent_app_country] => US [patent_app_date] => 2008-05-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 2369 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0321/20090321559.pdf [firstpage_image] =>[orig_patent_app_number] => 12153493 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5549644 [patent_doc_number] => 20090283630 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-11-19 [patent_title] => 'Lighter-than-air vehicle for shading' [patent_app_type] => utility [patent_app_number] => 12/153259 [patent_app_country] => US [patent_app_date] => 2008-05-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 1732 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0283/20090283630.pdf [firstpage_image] =>[orig_patent_app_number] => 12153259 [rel_patent_id] =>[rel_patent_doc_number] =>)