Search

William L. Oen

Examiner (ID: 8179)

Most Active Art Unit
2855
Art Unit(s)
3621, 2855, 2616, 2214, 5855
Total Applications
1098
Issued Applications
945
Pending Applications
84
Abandoned Applications
69

Applications

Application numberTitle of the applicationFiling DateStatus
Array ( [id] => 1142963 [patent_doc_number] => 06769649 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2004-08-03 [patent_title] => 'Ram air parachute canopy with improved nose structure' [patent_app_type] => B2 [patent_app_number] => 10/315459 [patent_app_country] => US [patent_app_date] => 2002-12-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 11 [patent_no_of_words] => 4117 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 102 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/769/06769649.pdf [firstpage_image] =>[orig_patent_app_number] => 10315459 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/315459
Ram air parachute canopy with improved nose structure Dec 8, 2002 Issued
Array ( [id] => 1061417 [patent_doc_number] => 06848649 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2005-02-01 [patent_title] => 'V/STOL biplane aircraft' [patent_app_type] => utility [patent_app_number] => 10/313580 [patent_app_country] => US [patent_app_date] => 2002-12-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 18 [patent_figures_cnt] => 41 [patent_no_of_words] => 18523 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 420 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/848/06848649.pdf [firstpage_image] =>[orig_patent_app_number] => 10313580 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/313580
V/STOL biplane aircraft Dec 8, 2002 Issued
Array ( [id] => 1193965 [patent_doc_number] => 06726150 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2004-04-27 [patent_title] => 'Method and apparatus for stiffener reinforcement of a ram air parachute canopy' [patent_app_type] => B2 [patent_app_number] => 10/315488 [patent_app_country] => US [patent_app_date] => 2002-12-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 5 [patent_no_of_words] => 1835 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 40 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/726/06726150.pdf [firstpage_image] =>[orig_patent_app_number] => 10315488 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/315488
Method and apparatus for stiffener reinforcement of a ram air parachute canopy Dec 8, 2002 Issued
Array ( [id] => 6666594 [patent_doc_number] => 20030111577 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2003-06-19 [patent_title] => 'Membrane structure' [patent_app_type] => new [patent_app_number] => 10/310840 [patent_app_country] => US [patent_app_date] => 2002-12-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 5115 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 156 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0111/20030111577.pdf [firstpage_image] =>[orig_patent_app_number] => 10310840 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/310840
Membrane structure Dec 5, 2002 Issued
Array ( [id] => 6694767 [patent_doc_number] => 20030106961 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2003-06-12 [patent_title] => 'Method and device for steepening a landing approach of an aircraft' [patent_app_type] => new [patent_app_number] => 10/313052 [patent_app_country] => US [patent_app_date] => 2002-12-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 3234 [patent_no_of_claims] => 22 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 74 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0106/20030106961.pdf [firstpage_image] =>[orig_patent_app_number] => 10313052 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/313052
Method and device for steepening a landing approach of an aircraft Dec 5, 2002 Issued
Array ( [id] => 453905 [patent_doc_number] => 07243879 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2007-07-17 [patent_title] => 'Lattice fin for missiles or other fluid-born bodies and method for producing same' [patent_app_type] => utility [patent_app_number] => 10/313222 [patent_app_country] => US [patent_app_date] => 2002-12-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 17 [patent_no_of_words] => 5324 [patent_no_of_claims] => 21 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 117 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/243/07243879.pdf [firstpage_image] =>[orig_patent_app_number] => 10313222 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/313222
Lattice fin for missiles or other fluid-born bodies and method for producing same Dec 5, 2002 Issued
Array ( [id] => 502850 [patent_doc_number] => 07198225 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2007-04-03 [patent_title] => 'Aircraft control system' [patent_app_type] => utility [patent_app_number] => 10/310415 [patent_app_country] => US [patent_app_date] => 2002-12-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 28 [patent_figures_cnt] => 38 [patent_no_of_words] => 14299 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 142 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/198/07198225.pdf [firstpage_image] =>[orig_patent_app_number] => 10310415 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/310415
Aircraft control system Dec 4, 2002 Issued
Array ( [id] => 7080386 [patent_doc_number] => 20050045766 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-03-03 [patent_title] => 'FORM FACTORED COMPLIANT METALLIC TRANSITION ELEMENT FOR ATTACHING A CERAMIC ELEMENT TO A METALLIC ELEMENT' [patent_app_type] => utility [patent_app_number] => 10/313713 [patent_app_country] => US [patent_app_date] => 2002-12-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 4913 [patent_no_of_claims] => 30 [patent_no_of_ind_claims] => 9 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0045/20050045766.pdf [firstpage_image] =>[orig_patent_app_number] => 10313713 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/313713
Form factored compliant metallic transition element for attaching a ceramic element to a metallic element Dec 3, 2002 Issued
Array ( [id] => 8100903 [patent_doc_number] => 08152099 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-04-10 [patent_title] => 'Method of landing an aircraft and apparatus therefor' [patent_app_type] => utility [patent_app_number] => 10/497317 [patent_app_country] => US [patent_app_date] => 2002-12-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 7 [patent_no_of_words] => 5867 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 68 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/08/152/08152099.pdf [firstpage_image] =>[orig_patent_app_number] => 10497317 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/497317
Method of landing an aircraft and apparatus therefor Dec 2, 2002 Issued
Array ( [id] => 1253779 [patent_doc_number] => 06666407 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2003-12-23 [patent_title] => 'Helicopter undercarriage' [patent_app_type] => B2 [patent_app_number] => 10/304910 [patent_app_country] => US [patent_app_date] => 2002-11-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 2517 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 120 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/666/06666407.pdf [firstpage_image] =>[orig_patent_app_number] => 10304910 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/304910
Helicopter undercarriage Nov 25, 2002 Issued
Array ( [id] => 615099 [patent_doc_number] => 07143981 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2006-12-05 [patent_title] => 'Parachute rescue system for multistory buildings' [patent_app_type] => utility [patent_app_number] => 10/494519 [patent_app_country] => US [patent_app_date] => 2002-11-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 4 [patent_no_of_words] => 2876 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 5 [patent_words_short_claim] => 53 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/143/07143981.pdf [firstpage_image] =>[orig_patent_app_number] => 10494519 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/494519
Parachute rescue system for multistory buildings Nov 12, 2002 Issued
Array ( [id] => 1243660 [patent_doc_number] => 06676072 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2004-01-13 [patent_title] => 'Short duration, high-torque rocket nozzle' [patent_app_type] => B1 [patent_app_number] => 10/292948 [patent_app_country] => US [patent_app_date] => 2002-11-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 2 [patent_no_of_words] => 4061 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 131 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/676/06676072.pdf [firstpage_image] =>[orig_patent_app_number] => 10292948 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/292948
Short duration, high-torque rocket nozzle Nov 12, 2002 Issued
Array ( [id] => 7352915 [patent_doc_number] => 20040089763 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-05-13 [patent_title] => 'Personal flight vehicle and system' [patent_app_type] => new [patent_app_number] => 10/293826 [patent_app_country] => US [patent_app_date] => 2002-11-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 37 [patent_figures_cnt] => 37 [patent_no_of_words] => 13285 [patent_no_of_claims] => 27 [patent_no_of_ind_claims] => 5 [patent_words_short_claim] => 26 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0089/20040089763.pdf [firstpage_image] =>[orig_patent_app_number] => 10293826 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/293826
Personal flight vehicle and system Nov 11, 2002 Issued
Array ( [id] => 7188824 [patent_doc_number] => 20040084566 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-05-06 [patent_title] => 'Multi-nozzle grid missile propulsion system' [patent_app_type] => new [patent_app_number] => 10/288943 [patent_app_country] => US [patent_app_date] => 2002-11-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 9158 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 39 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0084/20040084566.pdf [firstpage_image] =>[orig_patent_app_number] => 10288943 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/288943
Multi-nozzle grid missile propulsion system Nov 5, 2002 Abandoned
Array ( [id] => 7147227 [patent_doc_number] => 20050023410 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-02-03 [patent_title] => 'Multipurpose airfoil assembly' [patent_app_type] => utility [patent_app_number] => 10/286290 [patent_app_country] => US [patent_app_date] => 2002-11-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 4176 [patent_no_of_claims] => 21 [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/A1/0023/20050023410.pdf [firstpage_image] =>[orig_patent_app_number] => 10286290 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/286290
Multipurpose airfoil assembly Oct 31, 2002 Abandoned
Array ( [id] => 7188826 [patent_doc_number] => 20040084567 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-05-06 [patent_title] => 'Guided parafoil system for delivering lightweight payloads' [patent_app_type] => new [patent_app_number] => 10/284699 [patent_app_country] => US [patent_app_date] => 2002-10-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 2953 [patent_no_of_claims] => 21 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 105 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0084/20040084567.pdf [firstpage_image] =>[orig_patent_app_number] => 10284699 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/284699
Guided parafoil system for delivering lightweight payloads Oct 29, 2002 Issued
Array ( [id] => 7370667 [patent_doc_number] => 20040079834 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-04-29 [patent_title] => 'ACTIVE SYSTEM FOR WIDE AREA SUPPRESSION OF ENGINE VORTEX' [patent_app_type] => new [patent_app_number] => 10/280411 [patent_app_country] => US [patent_app_date] => 2002-10-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 3346 [patent_no_of_claims] => 23 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 80 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0079/20040079834.pdf [firstpage_image] =>[orig_patent_app_number] => 10280411 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/280411
Active system for wide area suppression of engine vortex Oct 24, 2002 Issued
Array ( [id] => 6854062 [patent_doc_number] => 20030127563 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2003-07-10 [patent_title] => 'Differential pressure sensing release system' [patent_app_type] => new [patent_app_number] => 10/280271 [patent_app_country] => US [patent_app_date] => 2002-10-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 1727 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 145 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0127/20030127563.pdf [firstpage_image] =>[orig_patent_app_number] => 10280271 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/280271
Differential pressure sensing release system Oct 24, 2002 Abandoned
Array ( [id] => 1224635 [patent_doc_number] => 06695258 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2004-02-24 [patent_title] => 'Kite device' [patent_app_type] => B1 [patent_app_number] => 10/286922 [patent_app_country] => US [patent_app_date] => 2002-10-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 11 [patent_no_of_words] => 883 [patent_no_of_claims] => 3 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 156 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/695/06695258.pdf [firstpage_image] =>[orig_patent_app_number] => 10286922 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/286922
Kite device Oct 24, 2002 Issued
Array ( [id] => 351699 [patent_doc_number] => 07490793 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2009-02-17 [patent_title] => 'Wireless landing gear monitoring system' [patent_app_type] => utility [patent_app_number] => 10/273659 [patent_app_country] => US [patent_app_date] => 2002-10-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 8 [patent_no_of_words] => 3713 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 158 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/490/07490793.pdf [firstpage_image] =>[orig_patent_app_number] => 10273659 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/273659
Wireless landing gear monitoring system Oct 17, 2002 Issued
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