Frederick Lyndon Lagman

Array ( [id] => 8770862 [patent_doc_number] => 08424803 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-04-23 [patent_title] => 'Attachment arrangement for a cargo compartment floor of an aircraft and aircraft with an attachment arrangement of this type' [patent_app_type] => utility [patent_app_number] => 12/777745 [patent_app_country] => US [patent_app_date] => 2010-05-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 10 [patent_no_of_words] => 3449 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 309 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12777745 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 8122639 [patent_doc_number] => 20120085867 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-04-12 [patent_title] => 'HEATING SYSTEM' [patent_app_type] => utility [patent_app_number] => 13/318889 [patent_app_country] => US [patent_app_date] => 2010-05-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 15 [patent_figures_cnt] => 15 [patent_no_of_words] => 7448 [patent_no_of_claims] => 21 [patent_no_of_ind_claims] => 6 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0085/20120085867.pdf [firstpage_image] =>[orig_patent_app_number] => 13318889 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6582244 [patent_doc_number] => 20100308154 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-12-09 [patent_title] => 'METHOD OF CONTROLLING A HYBRID HELICOPTER IN YAW, AND A HYBRID HELICOPTER PROVIDED WITH A YAW CONTROL DEVICE SUITABLE FOR IMPLEMENTING SAID METHOD' [patent_app_type] => utility [patent_app_number] => 12/774283 [patent_app_country] => US [patent_app_date] => 2010-05-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 10420 [patent_no_of_claims] => 16 [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/A1/0308/20100308154.pdf [firstpage_image] =>[orig_patent_app_number] => 12774283 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6192819 [patent_doc_number] => 20110024573 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-02-03 [patent_title] => 'EXTENDED WINGLET WITH LOAD BALANCING CHARACTERISTICS' [patent_app_type] => utility [patent_app_number] => 12/774697 [patent_app_country] => US [patent_app_date] => 2010-05-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 2324 [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/A1/0024/20110024573.pdf [firstpage_image] =>[orig_patent_app_number] => 12774697 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6415548 [patent_doc_number] => 20100276547 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-11-04 [patent_title] => 'SYSTEMS FOR SOLAR POWER BEAMING FROM SPACE' [patent_app_type] => utility [patent_app_number] => 12/773036 [patent_app_country] => US [patent_app_date] => 2010-05-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 4855 [patent_no_of_claims] => 42 [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/A1/0276/20100276547.pdf [firstpage_image] =>[orig_patent_app_number] => 12773036 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 8224536 [patent_doc_number] => 20120138748 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-06-07 [patent_title] => 'TERMINATOR TAPE SATELLITE DEORBIT MODULE' [patent_app_type] => utility [patent_app_number] => 13/318330 [patent_app_country] => US [patent_app_date] => 2010-04-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 1469 [patent_no_of_claims] => 19 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13318330 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7570741 [patent_doc_number] => 20110266397 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-11-03 [patent_title] => 'SOLAR THERMAL ROTORCRAFT' [patent_app_type] => utility [patent_app_number] => 12/771160 [patent_app_country] => US [patent_app_date] => 2010-04-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 16 [patent_figures_cnt] => 16 [patent_no_of_words] => 7638 [patent_no_of_claims] => 45 [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/A1/0266/20110266397.pdf [firstpage_image] =>[orig_patent_app_number] => 12771160 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 8541852 [patent_doc_number] => 08317137 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-11-27 [patent_title] => 'Switchable article and device to generate a lateral or transverse Casimir force for propulsion, guidance and maneuvering of a space vehicle' [patent_app_type] => utility [patent_app_number] => 12/768719 [patent_app_country] => US [patent_app_date] => 2010-04-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 8 [patent_no_of_words] => 7283 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 110 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12768719 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6036041 [patent_doc_number] => 20110089288 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-04-21 [patent_title] => 'POWER ASSISTED TOY FLYING DEVICE' [patent_app_type] => utility [patent_app_number] => 12/761457 [patent_app_country] => US [patent_app_date] => 2010-04-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 20 [patent_figures_cnt] => 20 [patent_no_of_words] => 16470 [patent_no_of_claims] => 46 [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/A1/0089/20110089288.pdf [firstpage_image] =>[orig_patent_app_number] => 12761457 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7507048 [patent_doc_number] => 20110254301 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-10-20 [patent_title] => 'AERODYNAMICALLY CONTROLLED GRAPPLE ASSEMBLY' [patent_app_type] => utility [patent_app_number] => 12/761015 [patent_app_country] => US [patent_app_date] => 2010-04-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 3269 [patent_no_of_claims] => 19 [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/A1/0254/20110254301.pdf [firstpage_image] =>[orig_patent_app_number] => 12761015 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6374272 [patent_doc_number] => 20100301158 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-12-02 [patent_title] => 'AIRCRAFT HAVING A LIFT/PROPULSION UNIT' [patent_app_type] => utility [patent_app_number] => 12/761155 [patent_app_country] => US [patent_app_date] => 2010-04-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 2628 [patent_no_of_claims] => 16 [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/A1/0301/20100301158.pdf [firstpage_image] =>[orig_patent_app_number] => 12761155 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7479540 [patent_doc_number] => 20110248119 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-10-13 [patent_title] => 'STRUCTURAL CONNECTORS AND METHODS OF USING SAME' [patent_app_type] => utility [patent_app_number] => 12/756263 [patent_app_country] => US [patent_app_date] => 2010-04-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 33 [patent_figures_cnt] => 33 [patent_no_of_words] => 9894 [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/A1/0248/20110248119.pdf [firstpage_image] =>[orig_patent_app_number] => 12756263 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 8409205 [patent_doc_number] => 08272596 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-09-25 [patent_title] => 'Amphibious aircraft' [patent_app_type] => utility [patent_app_number] => 12/756282 [patent_app_country] => US [patent_app_date] => 2010-04-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 3938 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 290 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12756282 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 8261017 [patent_doc_number] => 20120160445 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-06-28 [patent_title] => 'COOLER FOR AN AIRCRAFT COOLING SYSTEM, AIRCRAFT COOLING SYSTEM AND METHOD FOR OPERATING AN AIRCRAFT COOLING SYSTEM' [patent_app_type] => utility [patent_app_number] => 13/256828 [patent_app_country] => US [patent_app_date] => 2010-03-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 11033 [patent_no_of_claims] => 31 [patent_no_of_ind_claims] => 13 [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] => 13256828 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6183755 [patent_doc_number] => 20110168846 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-07-14 [patent_title] => 'STATIC LINE PIGGYBACK PARACHUTE SYSTEM' [patent_app_type] => utility [patent_app_number] => 12/684179 [patent_app_country] => US [patent_app_date] => 2010-01-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 8065 [patent_no_of_claims] => 26 [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/A1/0168/20110168846.pdf [firstpage_image] =>[orig_patent_app_number] => 12684179 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6183752 [patent_doc_number] => 20110168843 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-07-14 [patent_title] => 'TURBOMACHINE NACELLE AND ANTI-ICING SYSTEM AND METHOD THEREFOR' [patent_app_type] => utility [patent_app_number] => 12/649568 [patent_app_country] => US [patent_app_date] => 2009-12-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 3843 [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/A1/0168/20110168843.pdf [firstpage_image] =>[orig_patent_app_number] => 12649568 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6051750 [patent_doc_number] => 20110108664 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-05-12 [patent_title] => 'FLAP ACTUATOR' [patent_app_type] => utility [patent_app_number] => 12/648767 [patent_app_country] => US [patent_app_date] => 2009-12-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 4007 [patent_no_of_claims] => 23 [patent_no_of_ind_claims] => 19 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0108/20110108664.pdf [firstpage_image] =>[orig_patent_app_number] => 12648767 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 8590330 [patent_doc_number] => 08348200 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-01-08 [patent_title] => 'Synthetic jet actuator system and related methods' [patent_app_type] => utility [patent_app_number] => 12/646338 [patent_app_country] => US [patent_app_date] => 2009-12-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 16 [patent_no_of_words] => 9837 [patent_no_of_claims] => 26 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 92 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12646338 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5962642 [patent_doc_number] => 20110147531 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-06-23 [patent_title] => 'PORTABLE ONBOARD VEHICULAR HOIST SYSTEMS' [patent_app_type] => utility [patent_app_number] => 12/645445 [patent_app_country] => US [patent_app_date] => 2009-12-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 3747 [patent_no_of_claims] => 32 [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/A1/0147/20110147531.pdf [firstpage_image] =>[orig_patent_app_number] => 12645445 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5962644 [patent_doc_number] => 20110147533 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-06-23 [patent_title] => 'MORPHING DUCTED FAN FOR VERTICAL TAKE-OFF AND LANDING VEHICLE' [patent_app_type] => utility [patent_app_number] => 12/643839 [patent_app_country] => US [patent_app_date] => 2009-12-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 8874 [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/A1/0147/20110147533.pdf [firstpage_image] =>[orig_patent_app_number] => 12643839 [rel_patent_id] =>[rel_patent_doc_number] =>)