Stephen A. Holzen

Array ( [id] => 7439829 [patent_doc_number] => 20040195443 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-10-07 [patent_title] => 'Self stowing thrust reverser' [patent_app_type] => new [patent_app_number] => 10/781410 [patent_app_country] => US [patent_app_date] => 2004-02-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 4648 [patent_no_of_claims] => 25 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 126 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0195/20040195443.pdf [firstpage_image] =>[orig_patent_app_number] => 10781410 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 1102301 [patent_doc_number] => 06811123 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2004-11-02 [patent_title] => 'Store ejection system with integral isolation valve and associated ejection method' [patent_app_type] => B1 [patent_app_number] => 10/780202 [patent_app_country] => US [patent_app_date] => 2004-02-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 5372 [patent_no_of_claims] => 25 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 149 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/811/06811123.pdf [firstpage_image] =>[orig_patent_app_number] => 10780202 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 1029585 [patent_doc_number] => 06877698 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2005-04-12 [patent_title] => 'Aircraft evacuation slide inflation system using a stored liquified gas capable of thermal decomposition' [patent_app_type] => utility [patent_app_number] => 10/778287 [patent_app_country] => US [patent_app_date] => 2004-02-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 3 [patent_no_of_words] => 2823 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 144 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/877/06877698.pdf [firstpage_image] =>[orig_patent_app_number] => 10778287 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 1055066 [patent_doc_number] => 06854689 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2005-02-15 [patent_title] => 'Methods and systems for operating aircraft landing gears' [patent_app_type] => utility [patent_app_number] => 10/774981 [patent_app_country] => US [patent_app_date] => 2004-02-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 4870 [patent_no_of_claims] => 37 [patent_no_of_ind_claims] => 6 [patent_words_short_claim] => 110 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/854/06854689.pdf [firstpage_image] =>[orig_patent_app_number] => 10774981 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6949539 [patent_doc_number] => 20050224633 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-10-13 [patent_title] => 'LOW-DRAG ROTOR/WING FLAP' [patent_app_type] => utility [patent_app_number] => 10/770764 [patent_app_country] => US [patent_app_date] => 2004-02-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 3109 [patent_no_of_claims] => 36 [patent_no_of_ind_claims] => 5 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0224/20050224633.pdf [firstpage_image] =>[orig_patent_app_number] => 10770764 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7048307 [patent_doc_number] => 20050184194 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-08-25 [patent_title] => 'Hoist for aircraft cabin construction' [patent_app_type] => utility [patent_app_number] => 10/768935 [patent_app_country] => US [patent_app_date] => 2004-01-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 3226 [patent_no_of_claims] => 27 [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/A1/0184/20050184194.pdf [firstpage_image] =>[orig_patent_app_number] => 10768935 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 667563 [patent_doc_number] => 07093798 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2006-08-22 [patent_title] => 'Transformable airplane' [patent_app_type] => utility [patent_app_number] => 10/769125 [patent_app_country] => US [patent_app_date] => 2004-01-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 25 [patent_no_of_words] => 4986 [patent_no_of_claims] => 75 [patent_no_of_ind_claims] => 9 [patent_words_short_claim] => 77 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/093/07093798.pdf [firstpage_image] =>[orig_patent_app_number] => 10769125 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 771109 [patent_doc_number] => 07000872 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2006-02-21 [patent_title] => 'Circular parachute' [patent_app_type] => utility [patent_app_number] => 10/769151 [patent_app_country] => US [patent_app_date] => 2004-01-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 2898 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 157 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/000/07000872.pdf [firstpage_image] =>[orig_patent_app_number] => 10769151 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 1016663 [patent_doc_number] => 06889940 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2005-05-10 [patent_title] => 'Auxiliary fuel tank systems for aircraft and methods for their manufacture and use' [patent_app_type] => utility [patent_app_number] => 10/768269 [patent_app_country] => US [patent_app_date] => 2004-01-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 16 [patent_no_of_words] => 8895 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 132 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/889/06889940.pdf [firstpage_image] =>[orig_patent_app_number] => 10768269 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7132513 [patent_doc_number] => 20050178880 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-08-18 [patent_title] => 'Auxiliary fuel tank systems for aircraft and methods for their manufacture and use' [patent_app_type] => utility [patent_app_number] => 10/768267 [patent_app_country] => US [patent_app_date] => 2004-01-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 12 [patent_no_of_words] => 8954 [patent_no_of_claims] => 51 [patent_no_of_ind_claims] => 7 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0178/20050178880.pdf [firstpage_image] =>[orig_patent_app_number] => 10768267 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7132511 [patent_doc_number] => 20050178879 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-08-18 [patent_title] => 'VTOL tailsitter flying wing' [patent_app_type] => utility [patent_app_number] => 10/757483 [patent_app_country] => US [patent_app_date] => 2004-01-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 2046 [patent_no_of_claims] => 4 [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/A1/0178/20050178879.pdf [firstpage_image] =>[orig_patent_app_number] => 10757483 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 608303 [patent_doc_number] => 07150431 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2006-12-19 [patent_title] => 'Electrical generator fluid-flow-coolant filtration' [patent_app_type] => utility [patent_app_number] => 10/757880 [patent_app_country] => US [patent_app_date] => 2004-01-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 2 [patent_no_of_words] => 2012 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 168 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/150/07150431.pdf [firstpage_image] =>[orig_patent_app_number] => 10757880 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 664494 [patent_doc_number] => 07097137 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2006-08-29 [patent_title] => 'Launch and recovery system for unmanned aerial vehicles' [patent_app_type] => utility [patent_app_number] => 10/754251 [patent_app_country] => US [patent_app_date] => 2004-01-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 20 [patent_figures_cnt] => 32 [patent_no_of_words] => 13643 [patent_no_of_claims] => 39 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 143 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/097/07097137.pdf [firstpage_image] =>[orig_patent_app_number] => 10754251 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 1013644 [patent_doc_number] => 06892983 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2005-05-17 [patent_title] => 'Anti-hijacking system' [patent_app_type] => utility [patent_app_number] => 10/753550 [patent_app_country] => US [patent_app_date] => 2004-01-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 18 [patent_no_of_words] => 3105 [patent_no_of_claims] => 12 [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/06/892/06892983.pdf [firstpage_image] =>[orig_patent_app_number] => 10753550 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7337989 [patent_doc_number] => 20040245383 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-12-09 [patent_title] => 'Mounting arrangement for a gas turbine engine' [patent_app_type] => new [patent_app_number] => 10/751931 [patent_app_country] => US [patent_app_date] => 2004-01-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 4638 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 3 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0245/20040245383.pdf [firstpage_image] =>[orig_patent_app_number] => 10751931 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7132565 [patent_doc_number] => 20050178913 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-08-18 [patent_title] => 'Modification design for the improvement of slow flying aircraft\'s wing' [patent_app_type] => utility [patent_app_number] => 10/747513 [patent_app_country] => US [patent_app_date] => 2003-12-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 944 [patent_no_of_claims] => 2 [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/A1/0178/20050178913.pdf [firstpage_image] =>[orig_patent_app_number] => 10747513 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 1051840 [patent_doc_number] => 06857599 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2005-02-22 [patent_title] => 'Highly swept canard with low sweep wing supersonic aircraft configuration' [patent_app_type] => utility [patent_app_number] => 10/746744 [patent_app_country] => US [patent_app_date] => 2003-12-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 3 [patent_no_of_words] => 754 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 109 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/857/06857599.pdf [firstpage_image] =>[orig_patent_app_number] => 10746744 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7058740 [patent_doc_number] => 20050001099 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-01-06 [patent_title] => 'Safety device for parachute canopy' [patent_app_type] => utility [patent_app_number] => 10/740924 [patent_app_country] => US [patent_app_date] => 2003-12-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2762 [patent_no_of_claims] => 12 [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/A1/0001/20050001099.pdf [firstpage_image] =>[orig_patent_app_number] => 10740924 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 1084607 [patent_doc_number] => 06830221 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2004-12-14 [patent_title] => 'Integrated glass ceramic spacecraft' [patent_app_type] => B1 [patent_app_number] => 10/742058 [patent_app_country] => US [patent_app_date] => 2003-12-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 10821 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 111 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/830/06830221.pdf [firstpage_image] =>[orig_patent_app_number] => 10742058 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 937745 [patent_doc_number] => 06971609 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2005-12-06 [patent_title] => 'Asymmetric passenger arrangement' [patent_app_type] => utility [patent_app_number] => 10/740952 [patent_app_country] => US [patent_app_date] => 2003-12-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 1531 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 129 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/971/06971609.pdf [firstpage_image] =>[orig_patent_app_number] => 10740952 [rel_patent_id] =>[rel_patent_doc_number] =>)