Search

Alan M. Siegel

Examiner (ID: 16980)

Most Active Art Unit
1206
Art Unit(s)
1204, 3506, 1103, 1203, 1206, 1621
Total Applications
1919
Issued Applications
1371
Pending Applications
37
Abandoned Applications
511

Applications

Application numberTitle of the applicationFiling DateStatus
Array ( [id] => 10929605 [patent_doc_number] => 20140332626 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-11-13 [patent_title] => 'AIRCRAFT REACTION LINK AND MOVING SURFACE DRIVE UNIT' [patent_app_type] => utility [patent_app_number] => 14/267194 [patent_app_country] => US [patent_app_date] => 2014-05-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 20 [patent_figures_cnt] => 20 [patent_no_of_words] => 11696 [patent_no_of_claims] => 15 [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] =>[firstpage_image] =>[orig_patent_app_number] => 14267194 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/267194
Aircraft reaction link and moving surface drive unit Apr 30, 2014 Issued
Array ( [id] => 11463570 [patent_doc_number] => 09580187 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2017-02-28 [patent_title] => 'Rotor index sensor system' [patent_app_type] => utility [patent_app_number] => 14/258582 [patent_app_country] => US [patent_app_date] => 2014-04-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 8 [patent_no_of_words] => 2875 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 175 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14258582 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/258582
Rotor index sensor system Apr 21, 2014 Issued
Array ( [id] => 10406278 [patent_doc_number] => 20150291288 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-10-15 [patent_title] => 'ENGINE INLET CONFIGURATION' [patent_app_type] => utility [patent_app_number] => 14/252236 [patent_app_country] => US [patent_app_date] => 2014-04-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 1840 [patent_no_of_claims] => 15 [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] =>[firstpage_image] =>[orig_patent_app_number] => 14252236 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/252236
Engine inlet configuration Apr 13, 2014 Issued
Array ( [id] => 9558130 [patent_doc_number] => 20140175842 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-06-26 [patent_title] => 'Aircraft Side-Ledge Console' [patent_app_type] => utility [patent_app_number] => 14/195459 [patent_app_country] => US [patent_app_date] => 2014-03-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 11 [patent_no_of_words] => 2575 [patent_no_of_claims] => 16 [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] =>[firstpage_image] =>[orig_patent_app_number] => 14195459 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/195459
Aircraft side-ledge console Mar 2, 2014 Issued
Array ( [id] => 9682353 [patent_doc_number] => 20140239116 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-08-28 [patent_title] => 'TWIN-FUSELAGE ROTORCRAFT' [patent_app_type] => utility [patent_app_number] => 14/180735 [patent_app_country] => US [patent_app_date] => 2014-02-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 4061 [patent_no_of_claims] => 16 [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] =>[firstpage_image] =>[orig_patent_app_number] => 14180735 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/180735
Twin-fuselage rotorcraft Feb 13, 2014 Issued
Array ( [id] => 9667727 [patent_doc_number] => 20140231589 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-08-21 [patent_title] => 'Gyroless Three-Axis Sun Acquisition Using Sun Sensor and Unscented Kalman Filter' [patent_app_type] => utility [patent_app_number] => 14/181492 [patent_app_country] => US [patent_app_date] => 2014-02-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 6696 [patent_no_of_claims] => 20 [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] =>[firstpage_image] =>[orig_patent_app_number] => 14181492 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/181492
Gyroless three-axis sun acquisition using sun sensor and unscented kalman filter Feb 13, 2014 Issued
Array ( [id] => 11428767 [patent_doc_number] => 09567075 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2017-02-14 [patent_title] => 'Tilt wing aerial vehicle' [patent_app_type] => utility [patent_app_number] => 14/176960 [patent_app_country] => US [patent_app_date] => 2014-02-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 10 [patent_no_of_words] => 2708 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 213 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14176960 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/176960
Tilt wing aerial vehicle Feb 9, 2014 Issued
Array ( [id] => 10175720 [patent_doc_number] => 09205909 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2015-12-08 [patent_title] => 'Aircraft door arrangement' [patent_app_type] => utility [patent_app_number] => 14/165048 [patent_app_country] => US [patent_app_date] => 2014-01-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 3929 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 407 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14165048 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/165048
Aircraft door arrangement Jan 26, 2014 Issued
Array ( [id] => 11230677 [patent_doc_number] => 09457896 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2016-10-04 [patent_title] => 'Electric taxi system with speed control (ETSSC)' [patent_app_type] => utility [patent_app_number] => 14/163332 [patent_app_country] => US [patent_app_date] => 2014-01-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 3170 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 87 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14163332 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/163332
Electric taxi system with speed control (ETSSC) Jan 23, 2014 Issued
Array ( [id] => 10482933 [patent_doc_number] => 20150367952 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-12-24 [patent_title] => 'STRUCTURE FOR FEEDING AIR TO AN AUXILIARY POWER UNIT IN AN AIRCRAFT' [patent_app_type] => utility [patent_app_number] => 14/763796 [patent_app_country] => US [patent_app_date] => 2014-01-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 2196 [patent_no_of_claims] => 10 [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] =>[firstpage_image] =>[orig_patent_app_number] => 14763796 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/763796
Structure for feeding air to an auxiliary power unit in an aircraft Jan 22, 2014 Issued
Array ( [id] => 10614122 [patent_doc_number] => 09333550 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2016-05-10 [patent_title] => 'Wing panel and aircraft main wing' [patent_app_type] => utility [patent_app_number] => 14/160852 [patent_app_country] => US [patent_app_date] => 2014-01-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 8 [patent_no_of_words] => 2322 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 134 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14160852 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/160852
Wing panel and aircraft main wing Jan 21, 2014 Issued
Array ( [id] => 14325851 [patent_doc_number] => 10293925 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2019-05-21 [patent_title] => Systems and methods for implementing directional force weighting with circular force generators [patent_app_type] => utility [patent_app_number] => 14/759126 [patent_app_country] => US [patent_app_date] => 2014-01-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 9 [patent_no_of_words] => 2650 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 10 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14759126 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/759126
Systems and methods for implementing directional force weighting with circular force generators Jan 16, 2014 Issued
Array ( [id] => 11218508 [patent_doc_number] => 09446835 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2016-09-20 [patent_title] => 'Aircraft wing' [patent_app_type] => utility [patent_app_number] => 14/154321 [patent_app_country] => US [patent_app_date] => 2014-01-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 14 [patent_figures_cnt] => 28 [patent_no_of_words] => 8991 [patent_no_of_claims] => 3 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 96 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14154321 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/154321
Aircraft wing Jan 13, 2014 Issued
Array ( [id] => 10469228 [patent_doc_number] => 20150354244 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-12-10 [patent_title] => 'FLEXIBLE SHADOW-GENERATING WIND-ENERGY DEVICE INTENDED TO PROVIDE SOLAR PROTECTION' [patent_app_type] => utility [patent_app_number] => 14/760899 [patent_app_country] => US [patent_app_date] => 2014-01-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 11 [patent_no_of_words] => 2639 [patent_no_of_claims] => 26 [patent_no_of_ind_claims] => 7 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14760899 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/760899
FLEXIBLE SHADOW-GENERATING WIND-ENERGY DEVICE INTENDED TO PROVIDE SOLAR PROTECTION Jan 13, 2014 Abandoned
Array ( [id] => 14611051 [patent_doc_number] => 10358211 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2019-07-23 [patent_title] => Rotor apparatus [patent_app_type] => utility [patent_app_number] => 15/108867 [patent_app_country] => US [patent_app_date] => 2014-01-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 6 [patent_no_of_words] => 3105 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 112 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15108867 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/108867
Rotor apparatus Jan 1, 2014 Issued
Array ( [id] => 9557508 [patent_doc_number] => 20140175221 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-06-26 [patent_title] => 'Aircraft comprising a cockpit delocalized outside an upper part of the nose' [patent_app_type] => utility [patent_app_number] => 14/138406 [patent_app_country] => US [patent_app_date] => 2013-12-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 2554 [patent_no_of_claims] => 7 [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] =>[firstpage_image] =>[orig_patent_app_number] => 14138406 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/138406
Aircraft comprising a cockpit delocalized outside an upper part of the nose Dec 22, 2013 Issued
Array ( [id] => 9557513 [patent_doc_number] => 20140175225 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-06-26 [patent_title] => 'AIRCRAFT COCKPIT HAVING A LOWERED FLOOR FOR WALKING ON' [patent_app_type] => utility [patent_app_number] => 14/138572 [patent_app_country] => US [patent_app_date] => 2013-12-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 7651 [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] =>[firstpage_image] =>[orig_patent_app_number] => 14138572 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/138572
AIRCRAFT COCKPIT HAVING A LOWERED FLOOR FOR WALKING ON Dec 22, 2013 Abandoned
Array ( [id] => 12285382 [patent_doc_number] => 09932116 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2018-04-03 [patent_title] => Universal water activated release system [patent_app_type] => utility [patent_app_number] => 14/135744 [patent_app_country] => US [patent_app_date] => 2013-12-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 1553 [patent_no_of_claims] => 5 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 124 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14135744 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/135744
Universal water activated release system Dec 19, 2013 Issued
Array ( [id] => 11230675 [patent_doc_number] => 09457894 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2016-10-04 [patent_title] => 'Variable-width aerodynamic device' [patent_app_type] => utility [patent_app_number] => 14/136350 [patent_app_country] => US [patent_app_date] => 2013-12-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 4 [patent_no_of_words] => 2034 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 194 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14136350 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/136350
Variable-width aerodynamic device Dec 19, 2013 Issued
Array ( [id] => 9542172 [patent_doc_number] => 20140166819 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-06-19 [patent_title] => 'Flap System For An Aircraft, Method For Adjusting The Lift Of An Aircraft And Aircraft Comprising A Main Wing And At Least One Flap System' [patent_app_type] => utility [patent_app_number] => 14/134102 [patent_app_country] => US [patent_app_date] => 2013-12-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 3423 [patent_no_of_claims] => 14 [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] =>[firstpage_image] =>[orig_patent_app_number] => 14134102 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/134102
Flap system for an aircraft, method for adjusting the lift of an aircraft and aircraft comprising a main wing and at least one flap system Dec 18, 2013 Issued
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