Stephen A. Holzen

Array ( [id] => 6955454 [patent_doc_number] => 20050211824 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-09-29 [patent_title] => 'Turbine engine arrangements' [patent_app_type] => utility [patent_app_number] => 11/036360 [patent_app_country] => US [patent_app_date] => 2005-01-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 2504 [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/A1/0211/20050211824.pdf [firstpage_image] =>[orig_patent_app_number] => 11036360 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5691521 [patent_doc_number] => 20060151666 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-07-13 [patent_title] => 'Vertical take-off and landing (VTOL) aircraft with distributed thrust and control' [patent_app_type] => utility [patent_app_number] => 11/035263 [patent_app_country] => US [patent_app_date] => 2005-01-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 11 [patent_no_of_words] => 8220 [patent_no_of_claims] => 52 [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/A1/0151/20060151666.pdf [firstpage_image] =>[orig_patent_app_number] => 11035263 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5892410 [patent_doc_number] => 20060000947 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-01-05 [patent_title] => 'Passenger sitting/sleeping arrangement' [patent_app_type] => utility [patent_app_number] => 11/026251 [patent_app_country] => US [patent_app_date] => 2004-12-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 3074 [patent_no_of_claims] => 18 [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/A1/0000/20060000947.pdf [firstpage_image] =>[orig_patent_app_number] => 11026251 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6980960 [patent_doc_number] => 20050151028 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-07-14 [patent_title] => 'Apparatus for driving and adjusting flaps hinged to an aircraft' [patent_app_type] => utility [patent_app_number] => 11/021723 [patent_app_country] => US [patent_app_date] => 2004-12-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 2224 [patent_no_of_claims] => 6 [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/A1/0151/20050151028.pdf [firstpage_image] =>[orig_patent_app_number] => 11021723 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5817771 [patent_doc_number] => 20060022084 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-02-02 [patent_title] => 'Convertible aircraft provided with two tilt fans on either side of the fuselage, and with a non-tilting fan inserted in the fuselage' [patent_app_type] => utility [patent_app_number] => 11/016902 [patent_app_country] => US [patent_app_date] => 2004-12-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2854 [patent_no_of_claims] => 22 [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/A1/0022/20060022084.pdf [firstpage_image] =>[orig_patent_app_number] => 11016902 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6993886 [patent_doc_number] => 20050133662 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-06-23 [patent_title] => 'Convertible aircraft provided with two tilt fans on either side of the fuselage and with a third tilt fan arranged on the tail of the aircraft' [patent_app_type] => utility [patent_app_number] => 11/016763 [patent_app_country] => US [patent_app_date] => 2004-12-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2680 [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] => publications/A1/0133/20050133662.pdf [firstpage_image] =>[orig_patent_app_number] => 11016763 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 443851 [patent_doc_number] => 07252269 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2007-08-07 [patent_title] => 'Asymmetrical low-profile bulkhead' [patent_app_type] => utility [patent_app_number] => 11/017421 [patent_app_country] => US [patent_app_date] => 2004-12-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 21 [patent_no_of_words] => 4201 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 95 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/252/07252269.pdf [firstpage_image] =>[orig_patent_app_number] => 11017421 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6955459 [patent_doc_number] => 20050211829 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-09-29 [patent_title] => 'Magnetic Motive System' [patent_app_type] => utility [patent_app_number] => 10/905125 [patent_app_country] => US [patent_app_date] => 2004-12-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 4818 [patent_no_of_claims] => 39 [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/A1/0211/20050211829.pdf [firstpage_image] =>[orig_patent_app_number] => 10905125 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 472577 [patent_doc_number] => 07226018 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2007-06-05 [patent_title] => 'Landing gear method and apparatus for braking and maneuvering' [patent_app_type] => utility [patent_app_number] => 11/011756 [patent_app_country] => US [patent_app_date] => 2004-12-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 7283 [patent_no_of_claims] => 52 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 197 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/226/07226018.pdf [firstpage_image] =>[orig_patent_app_number] => 11011756 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 463703 [patent_doc_number] => 07234667 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2007-06-26 [patent_title] => 'Modular aerospace plane' [patent_app_type] => utility [patent_app_number] => 11/007855 [patent_app_country] => US [patent_app_date] => 2004-12-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 12 [patent_no_of_words] => 4811 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 189 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/234/07234667.pdf [firstpage_image] =>[orig_patent_app_number] => 11007855 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5703004 [patent_doc_number] => 20060192051 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-08-31 [patent_title] => 'Reconfigurable interior sidewall' [patent_app_type] => utility [patent_app_number] => 11/004292 [patent_app_country] => US [patent_app_date] => 2004-12-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 4740 [patent_no_of_claims] => 30 [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/A1/0192/20060192051.pdf [firstpage_image] =>[orig_patent_app_number] => 11004292 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 653568 [patent_doc_number] => 07108229 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2006-09-19 [patent_title] => 'Arrangement and method for the generation of water on board an aircraft' [patent_app_type] => utility [patent_app_number] => 10/999052 [patent_app_country] => US [patent_app_date] => 2004-11-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 4 [patent_no_of_words] => 3120 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 135 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/108/07108229.pdf [firstpage_image] =>[orig_patent_app_number] => 10999052 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 427640 [patent_doc_number] => 07267303 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2007-09-11 [patent_title] => 'Method and system for providing cruciform steered, bent biconic and plasma suppression for maximum accuracy' [patent_app_type] => utility [patent_app_number] => 10/990393 [patent_app_country] => US [patent_app_date] => 2004-11-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 18 [patent_figures_cnt] => 20 [patent_no_of_words] => 8782 [patent_no_of_claims] => 5 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 80 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/267/07267303.pdf [firstpage_image] =>[orig_patent_app_number] => 10990393 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5773678 [patent_doc_number] => 20060102791 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-05-18 [patent_title] => 'Interoperable aerial refueling apparatus and methods' [patent_app_type] => utility [patent_app_number] => 10/992153 [patent_app_country] => US [patent_app_date] => 2004-11-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 2994 [patent_no_of_claims] => 44 [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/A1/0102/20060102791.pdf [firstpage_image] =>[orig_patent_app_number] => 10992153 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7139769 [patent_doc_number] => 20050116093 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-06-02 [patent_title] => 'Mounting structure for mounting a turboprop under an aircraft wing' [patent_app_type] => utility [patent_app_number] => 10/987151 [patent_app_country] => US [patent_app_date] => 2004-11-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 6248 [patent_no_of_claims] => 11 [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/A1/0116/20050116093.pdf [firstpage_image] =>[orig_patent_app_number] => 10987151 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5908584 [patent_doc_number] => 20060124801 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-06-15 [patent_title] => 'Shape changing structure' [patent_app_type] => utility [patent_app_number] => 10/988292 [patent_app_country] => US [patent_app_date] => 2004-11-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 5245 [patent_no_of_claims] => 29 [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/A1/0124/20060124801.pdf [firstpage_image] =>[orig_patent_app_number] => 10988292 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 417674 [patent_doc_number] => 07275722 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2007-10-02 [patent_title] => 'Wing tip device' [patent_app_type] => utility [patent_app_number] => 10/986451 [patent_app_country] => US [patent_app_date] => 2004-11-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 6 [patent_no_of_words] => 6590 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 219 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/275/07275722.pdf [firstpage_image] =>[orig_patent_app_number] => 10986451 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 440937 [patent_doc_number] => 07255305 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2007-08-14 [patent_title] => 'Flying device utilizing natural principles' [patent_app_type] => utility [patent_app_number] => 10/979046 [patent_app_country] => US [patent_app_date] => 2004-11-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 18 [patent_figures_cnt] => 27 [patent_no_of_words] => 10857 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 235 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/255/07255305.pdf [firstpage_image] =>[orig_patent_app_number] => 10979046 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5804906 [patent_doc_number] => 20060091258 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-05-04 [patent_title] => 'Autonomous, back-packable computer-controlled breakaway unmanned aerial vehicle (UAV)' [patent_app_type] => utility [patent_app_number] => 10/976153 [patent_app_country] => US [patent_app_date] => 2004-10-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 17 [patent_figures_cnt] => 17 [patent_no_of_words] => 7561 [patent_no_of_claims] => 29 [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/A1/0091/20060091258.pdf [firstpage_image] =>[orig_patent_app_number] => 10976153 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 466358 [patent_doc_number] => 07232096 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2007-06-19 [patent_title] => 'Positive lock seat device' [patent_app_type] => utility [patent_app_number] => 10/973829 [patent_app_country] => US [patent_app_date] => 2004-10-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 1814 [patent_no_of_claims] => 44 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 91 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/232/07232096.pdf [firstpage_image] =>[orig_patent_app_number] => 10973829 [rel_patent_id] =>[rel_patent_doc_number] =>)