Search

Stephen A. Holzen

Examiner (ID: 19331)

Most Active Art Unit
3644
Art Unit(s)
3644
Total Applications
432
Issued Applications
318
Pending Applications
37
Abandoned Applications
77

Applications

Application numberTitle of the applicationFiling DateStatus
Array ( [id] => 1367538 [patent_doc_number] => 06547188 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2003-04-15 [patent_title] => 'Process and device for inerting an aircraft fuel tank' [patent_app_type] => B2 [patent_app_number] => 10/128297 [patent_app_country] => US [patent_app_date] => 2002-04-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 2475 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 153 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/547/06547188.pdf [firstpage_image] =>[orig_patent_app_number] => 10128297 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/128297
Process and device for inerting an aircraft fuel tank Apr 23, 2002 Issued
Array ( [id] => 1210108 [patent_doc_number] => 06708921 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2004-03-23 [patent_title] => 'Composite flapping flexure' [patent_app_type] => B2 [patent_app_number] => 10/120279 [patent_app_country] => US [patent_app_date] => 2002-04-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 7 [patent_no_of_words] => 3848 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 127 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/708/06708921.pdf [firstpage_image] =>[orig_patent_app_number] => 10120279 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/120279
Composite flapping flexure Apr 9, 2002 Issued
Array ( [id] => 6505199 [patent_doc_number] => 20020134892 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2002-09-26 [patent_title] => 'Aft fuselage control system for forward lifting elevator aircraft' [patent_app_type] => new [patent_app_number] => 10/120055 [patent_app_country] => US [patent_app_date] => 2002-04-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2684 [patent_no_of_claims] => 2 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 188 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0134/20020134892.pdf [firstpage_image] =>[orig_patent_app_number] => 10120055 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/120055
Aft fuselage control system for forward lifting elevator aircraft Apr 8, 2002 Issued
Array ( [id] => 492253 [patent_doc_number] => 07207518 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2007-04-24 [patent_title] => 'Cartridge with fin deployment mechanism' [patent_app_type] => utility [patent_app_number] => 10/477155 [patent_app_country] => US [patent_app_date] => 2002-04-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 13 [patent_no_of_words] => 3907 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 131 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/207/07207518.pdf [firstpage_image] =>[orig_patent_app_number] => 10477155 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/477155
Cartridge with fin deployment mechanism Apr 7, 2002 Issued
10/117618 JAM RESISTANT AND INTRUDER-PROOF FLIGHT DECK DOOR Apr 4, 2002 Abandoned
Array ( [id] => 1331178 [patent_doc_number] => 06585188 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2003-07-01 [patent_title] => 'Rescue vehicle' [patent_app_type] => B2 [patent_app_number] => 10/116789 [patent_app_country] => US [patent_app_date] => 2002-04-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 4 [patent_no_of_words] => 1863 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 240 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/585/06585188.pdf [firstpage_image] =>[orig_patent_app_number] => 10116789 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/116789
Rescue vehicle Apr 3, 2002 Issued
Array ( [id] => 6153605 [patent_doc_number] => 20020145080 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2002-10-10 [patent_title] => 'Suction conveying system, such as a vacuum wastewater system for an aircraft' [patent_app_type] => new [patent_app_number] => 10/116842 [patent_app_country] => US [patent_app_date] => 2002-04-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 4749 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 177 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0145/20020145080.pdf [firstpage_image] =>[orig_patent_app_number] => 10116842 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/116842
Suction conveying system, such as a vacuum wastewater system for an aircraft Apr 3, 2002 Abandoned
Array ( [id] => 1238582 [patent_doc_number] => 06682019 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2004-01-27 [patent_title] => 'Minimum energy wheel configurations for energy storage and attitude control' [patent_app_type] => B2 [patent_app_number] => 10/116605 [patent_app_country] => US [patent_app_date] => 2002-04-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 4 [patent_no_of_words] => 2206 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 150 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/682/06682019.pdf [firstpage_image] =>[orig_patent_app_number] => 10116605 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/116605
Minimum energy wheel configurations for energy storage and attitude control Apr 3, 2002 Issued
Array ( [id] => 1251535 [patent_doc_number] => 06669147 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2003-12-30 [patent_title] => 'Deployable radiator for a space vehicle' [patent_app_type] => B2 [patent_app_number] => 10/114277 [patent_app_country] => US [patent_app_date] => 2002-04-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 13 [patent_no_of_words] => 4234 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 107 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/669/06669147.pdf [firstpage_image] =>[orig_patent_app_number] => 10114277 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/114277
Deployable radiator for a space vehicle Apr 2, 2002 Issued
Array ( [id] => 1217319 [patent_doc_number] => 06702234 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2004-03-09 [patent_title] => 'Fault tolerant attitude control system for zero momentum spacecraft' [patent_app_type] => B1 [patent_app_number] => 10/108571 [patent_app_country] => US [patent_app_date] => 2002-03-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 2689 [patent_no_of_claims] => 52 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 94 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/702/06702234.pdf [firstpage_image] =>[orig_patent_app_number] => 10108571 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/108571
Fault tolerant attitude control system for zero momentum spacecraft Mar 28, 2002 Issued
Array ( [id] => 6962620 [patent_doc_number] => 20050229806 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-10-20 [patent_title] => 'Method of synchronizing fin fold-out on a fin-stabilized artillery shell, and an artillery shell designed in accordance therewith' [patent_app_type] => utility [patent_app_number] => 10/471458 [patent_app_country] => US [patent_app_date] => 2002-03-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 3228 [patent_no_of_claims] => 12 [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/A1/0229/20050229806.pdf [firstpage_image] =>[orig_patent_app_number] => 10471458 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/471458
Method of synchronizing fin fold-out on a fin-stabilized artillery shell, and an artillery shell designed in accordance therewith Mar 19, 2002 Issued
Array ( [id] => 1231527 [patent_doc_number] => 06688554 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2004-02-10 [patent_title] => 'Threat-resistant cushion' [patent_app_type] => B2 [patent_app_number] => 10/098640 [patent_app_country] => US [patent_app_date] => 2002-03-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 7 [patent_no_of_words] => 2006 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 6 [patent_words_short_claim] => 64 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/688/06688554.pdf [firstpage_image] =>[orig_patent_app_number] => 10098640 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/098640
Threat-resistant cushion Mar 14, 2002 Issued
Array ( [id] => 1296826 [patent_doc_number] => 06619584 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2003-09-16 [patent_title] => 'Road/air vehicle' [patent_app_type] => B1 [patent_app_number] => 10/096755 [patent_app_country] => US [patent_app_date] => 2002-03-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 23 [patent_figures_cnt] => 30 [patent_no_of_words] => 5521 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 102 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/619/06619584.pdf [firstpage_image] =>[orig_patent_app_number] => 10096755 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/096755
Road/air vehicle Mar 10, 2002 Issued
Array ( [id] => 1213393 [patent_doc_number] => 06705572 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2004-03-16 [patent_title] => 'Emergency low altitude parachute wherein canopy is deployed and inflated prior to use' [patent_app_type] => B1 [patent_app_number] => 10/091252 [patent_app_country] => US [patent_app_date] => 2002-03-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 2869 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 147 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/705/06705572.pdf [firstpage_image] =>[orig_patent_app_number] => 10091252 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/091252
Emergency low altitude parachute wherein canopy is deployed and inflated prior to use Mar 4, 2002 Issued
Array ( [id] => 1299732 [patent_doc_number] => 06616102 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2003-09-09 [patent_title] => 'Apparatus for deicing aircraft' [patent_app_type] => B1 [patent_app_number] => 10/090352 [patent_app_country] => US [patent_app_date] => 2002-03-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 13 [patent_figures_cnt] => 18 [patent_no_of_words] => 2814 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 155 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/616/06616102.pdf [firstpage_image] =>[orig_patent_app_number] => 10090352 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/090352
Apparatus for deicing aircraft Mar 3, 2002 Issued
Array ( [id] => 6845259 [patent_doc_number] => 20030164426 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2003-09-04 [patent_title] => 'GUIDED AIRBORNE VEHICLE, CARGO AND PERSONNEL DELIVERY SYSTEM' [patent_app_type] => new [patent_app_number] => 10/086476 [patent_app_country] => US [patent_app_date] => 2002-03-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 4872 [patent_no_of_claims] => 35 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 67 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0164/20030164426.pdf [firstpage_image] =>[orig_patent_app_number] => 10086476 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/086476
Guided airborne vehicle, cargo and personnel delivery system Feb 28, 2002 Issued
Array ( [id] => 6012106 [patent_doc_number] => 20020100835 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2002-08-01 [patent_title] => 'Tandem powered power tilting aircraft' [patent_app_type] => new [patent_app_number] => 10/086220 [patent_app_country] => US [patent_app_date] => 2002-02-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 12 [patent_no_of_words] => 6001 [patent_no_of_claims] => 87 [patent_no_of_ind_claims] => 29 [patent_words_short_claim] => 57 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0100/20020100835.pdf [firstpage_image] =>[orig_patent_app_number] => 10086220 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/086220
Tandem powered power tilting aircraft Feb 27, 2002 Abandoned
Array ( [id] => 6361069 [patent_doc_number] => 20020117120 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2002-08-29 [patent_title] => 'Automatic pet blanket' [patent_app_type] => new [patent_app_number] => 10/085947 [patent_app_country] => US [patent_app_date] => 2002-02-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 4098 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 5 [patent_words_short_claim] => 41 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0117/20020117120.pdf [firstpage_image] =>[orig_patent_app_number] => 10085947 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/085947
Automatic pet blanket Feb 27, 2002 Issued
Array ( [id] => 1326613 [patent_doc_number] => 06592073 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2003-07-15 [patent_title] => 'Amphibious aircraft' [patent_app_type] => B1 [patent_app_number] => 10/083081 [patent_app_country] => US [patent_app_date] => 2002-02-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 8 [patent_no_of_words] => 1622 [patent_no_of_claims] => 18 [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] => patents/06/592/06592073.pdf [firstpage_image] =>[orig_patent_app_number] => 10083081 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/083081
Amphibious aircraft Feb 25, 2002 Issued
Array ( [id] => 6832584 [patent_doc_number] => 20030160129 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2003-08-28 [patent_title] => 'ROTATIONAL CANTED-JOINT MISSILE CONTROL SYSTEM' [patent_app_type] => new [patent_app_number] => 10/083518 [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] => 1399 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 211 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0160/20030160129.pdf [firstpage_image] =>[orig_patent_app_number] => 10083518 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/083518
Rotational canted-joint missile control system Feb 24, 2002 Issued
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