Stephen A. Holzen

Array ( [id] => 5856109 [patent_doc_number] => 20020121576 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2002-09-05 [patent_title] => 'Process and device for accelerating the destruction of at least two vortices in the wake of a moving body, particularly an aircraft' [patent_app_type] => new [patent_app_number] => 10/080407 [patent_app_country] => US [patent_app_date] => 2002-02-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 4882 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 266 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0121/20020121576.pdf [firstpage_image] =>[orig_patent_app_number] => 10080407 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6738098 [patent_doc_number] => 20030155466 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2003-08-21 [patent_title] => 'DOT (DEPARTMENT OF TRANSPORTATION) LAVATORY AND SHOWER COMBINATION' [patent_app_type] => new [patent_app_number] => 10/078859 [patent_app_country] => US [patent_app_date] => 2002-02-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 2582 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 7 [patent_words_short_claim] => 46 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0155/20030155466.pdf [firstpage_image] =>[orig_patent_app_number] => 10078859 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 1220615 [patent_doc_number] => 06698691 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2004-03-02 [patent_title] => 'Process for de-icing by forced circulation of a fluid, an air intake cowling of a reaction motor and device for practicing the same' [patent_app_type] => B2 [patent_app_number] => 10/074053 [patent_app_country] => US [patent_app_date] => 2002-02-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 9 [patent_no_of_words] => 4513 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 108 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/698/06698691.pdf [firstpage_image] =>[orig_patent_app_number] => 10074053 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 1220594 [patent_doc_number] => 06698687 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2004-03-02 [patent_title] => 'Aircraft wing heat exchanger apparatus and method' [patent_app_type] => B2 [patent_app_number] => 10/075063 [patent_app_country] => US [patent_app_date] => 2002-02-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 2 [patent_no_of_words] => 2191 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 5 [patent_words_short_claim] => 185 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/698/06698687.pdf [firstpage_image] =>[orig_patent_app_number] => 10075063 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 1224654 [patent_doc_number] => 06695263 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2004-02-24 [patent_title] => 'System for geosynchronous spacecraft rapid earth reacquisition' [patent_app_type] => B1 [patent_app_number] => 10/073013 [patent_app_country] => US [patent_app_date] => 2002-02-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 3568 [patent_no_of_claims] => 56 [patent_no_of_ind_claims] => 6 [patent_words_short_claim] => 61 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/695/06695263.pdf [firstpage_image] =>[orig_patent_app_number] => 10073013 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6205238 [patent_doc_number] => 20020070313 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2002-06-13 [patent_title] => 'Liquid hydrogen stratospheric aircraft' [patent_app_type] => new [patent_app_number] => 10/073828 [patent_app_country] => US [patent_app_date] => 2002-02-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 8305 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 37 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0070/20020070313.pdf [firstpage_image] =>[orig_patent_app_number] => 10073828 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 1257165 [patent_doc_number] => 06663045 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2003-12-16 [patent_title] => 'Method and apparatus for actuating an aircraft nose portion' [patent_app_type] => B2 [patent_app_number] => 10/073496 [patent_app_country] => US [patent_app_date] => 2002-02-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 8 [patent_no_of_words] => 4053 [patent_no_of_claims] => 82 [patent_no_of_ind_claims] => 15 [patent_words_short_claim] => 80 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/663/06663045.pdf [firstpage_image] =>[orig_patent_app_number] => 10073496 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6520549 [patent_doc_number] => 20020109041 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2002-08-15 [patent_title] => 'Spiralling missile - A' [patent_app_type] => new [patent_app_number] => 10/067963 [patent_app_country] => US [patent_app_date] => 2002-02-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 1424 [patent_no_of_claims] => 27 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 218 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0109/20020109041.pdf [firstpage_image] =>[orig_patent_app_number] => 10067963 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 1514365 [patent_doc_number] => 06499693 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-12-31 [patent_title] => 'Aircraft to respond to threats' [patent_app_type] => B1 [patent_app_number] => 09/683740 [patent_app_country] => US [patent_app_date] => 2002-02-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 4225 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 80 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/499/06499693.pdf [firstpage_image] =>[orig_patent_app_number] => 09683740 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 1377785 [patent_doc_number] => 06536710 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2003-03-25 [patent_title] => 'Overhead lattice support structure' [patent_app_type] => B1 [patent_app_number] => 10/071997 [patent_app_country] => US [patent_app_date] => 2002-02-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2693 [patent_no_of_claims] => 39 [patent_no_of_ind_claims] => 7 [patent_words_short_claim] => 62 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/536/06536710.pdf [firstpage_image] =>[orig_patent_app_number] => 10071997 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 1274840 [patent_doc_number] => 06641083 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2003-11-04 [patent_title] => 'Balloon' [patent_app_type] => B2 [patent_app_number] => 10/061274 [patent_app_country] => US [patent_app_date] => 2002-02-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 3680 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 69 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/641/06641083.pdf [firstpage_image] =>[orig_patent_app_number] => 10061274 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 1286593 [patent_doc_number] => 06629668 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2003-10-07 [patent_title] => 'Jump correcting projectile system' [patent_app_type] => B1 [patent_app_number] => 10/062092 [patent_app_country] => US [patent_app_date] => 2002-02-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 2 [patent_no_of_words] => 2732 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 250 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/629/06629668.pdf [firstpage_image] =>[orig_patent_app_number] => 10062092 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 1245987 [patent_doc_number] => 06672541 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2004-01-06 [patent_title] => 'Flight crew rest and attendant rest environmental control system' [patent_app_type] => B2 [patent_app_number] => 10/058819 [patent_app_country] => US [patent_app_date] => 2002-01-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2478 [patent_no_of_claims] => 22 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 116 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/672/06672541.pdf [firstpage_image] =>[orig_patent_app_number] => 10058819 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 1400778 [patent_doc_number] => 06513756 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2003-02-04 [patent_title] => 'Installation of single passenger interface unit and method thereof' [patent_app_type] => B1 [patent_app_number] => 10/057289 [patent_app_country] => US [patent_app_date] => 2002-01-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2355 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 99 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/513/06513756.pdf [firstpage_image] =>[orig_patent_app_number] => 10057289 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5900754 [patent_doc_number] => 20020139894 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2002-10-03 [patent_title] => 'Roadable aircraft boat that flies in a wind of its own making' [patent_app_type] => new [patent_app_number] => 10/057194 [patent_app_country] => US [patent_app_date] => 2002-01-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 22 [patent_figures_cnt] => 22 [patent_no_of_words] => 9730 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 40 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0139/20020139894.pdf [firstpage_image] =>[orig_patent_app_number] => 10057194 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5981666 [patent_doc_number] => 20020096603 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2002-07-25 [patent_title] => 'Supporting structure for a solar sail of a satellite' [patent_app_type] => new [patent_app_number] => 10/053615 [patent_app_country] => US [patent_app_date] => 2002-01-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 3420 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 109 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0096/20020096603.pdf [firstpage_image] =>[orig_patent_app_number] => 10053615 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5981657 [patent_doc_number] => 20020096599 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2002-07-25 [patent_title] => 'Hybrid winged airship (dynastat)' [patent_app_type] => new [patent_app_number] => 10/050934 [patent_app_country] => US [patent_app_date] => 2002-01-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 14 [patent_figures_cnt] => 14 [patent_no_of_words] => 6268 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 354 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0096/20020096599.pdf [firstpage_image] =>[orig_patent_app_number] => 10050934 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 1301112 [patent_doc_number] => 06612298 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2003-09-02 [patent_title] => 'Safety for sporting pellet or air guns' [patent_app_type] => B2 [patent_app_number] => 10/041991 [patent_app_country] => US [patent_app_date] => 2002-01-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 15 [patent_no_of_words] => 2599 [patent_no_of_claims] => 1 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 342 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/612/06612298.pdf [firstpage_image] =>[orig_patent_app_number] => 10041991 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6269083 [patent_doc_number] => 20020104921 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2002-08-08 [patent_title] => 'Electrical remote-control and remote-power flying saucer' [patent_app_type] => new [patent_app_number] => 10/048091 [patent_app_country] => US [patent_app_date] => 2001-12-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 4605 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 8 [patent_words_short_claim] => 28 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0104/20020104921.pdf [firstpage_image] =>[orig_patent_app_number] => 10048091 [rel_patent_id] =>[rel_patent_doc_number] =>)