
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 number | Title of the application | Filing Date | Status |
|---|---|---|---|
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
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[patent_no_of_words] => 1622
[patent_no_of_claims] => 18
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[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 |