Search

On S. Mung

Examiner (ID: 10080, Phone: (571)270-7557 , Office: P/2486 )

Most Active Art Unit
2486
Art Unit(s)
2486, 2483
Total Applications
753
Issued Applications
517
Pending Applications
70
Abandoned Applications
183

Applications

Application numberTitle of the applicationFiling DateStatus
Array ( [id] => 12325242 [patent_doc_number] => 09944395 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2018-04-17 [patent_title] => Method for automated and individualized processing of luggage in an aircraft and aircraft hold for implementing same [patent_app_type] => utility [patent_app_number] => 14/108861 [patent_app_country] => US [patent_app_date] => 2013-12-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 5 [patent_no_of_words] => 6828 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 135 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14108861 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/108861
Method for automated and individualized processing of luggage in an aircraft and aircraft hold for implementing same Dec 16, 2013 Issued
Array ( [id] => 10169031 [patent_doc_number] => 09199732 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2015-12-01 [patent_title] => 'Tilt rotor aircraft with fixed engine arrangement' [patent_app_type] => utility [patent_app_number] => 14/101953 [patent_app_country] => US [patent_app_date] => 2013-12-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 2879 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 120 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14101953 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/101953
Tilt rotor aircraft with fixed engine arrangement Dec 9, 2013 Issued
Array ( [id] => 10429853 [patent_doc_number] => 20150314865 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-11-05 [patent_title] => 'CONVERTIBLE AIRCRAFT PROVIDED WITH TWO DUCTED ROTORS AT THE WING TIPS AND WITH A HORIZONTAL FAN IN THE FUSELAGE' [patent_app_type] => utility [patent_app_number] => 14/650231 [patent_app_country] => US [patent_app_date] => 2013-12-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 5268 [patent_no_of_claims] => 8 [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] => 14650231 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/650231
CONVERTIBLE AIRCRAFT PROVIDED WITH TWO DUCTED ROTORS AT THE WING TIPS AND WITH A HORIZONTAL FAN IN THE FUSELAGE Dec 8, 2013 Abandoned
Array ( [id] => 10273576 [patent_doc_number] => 20150158573 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-06-11 [patent_title] => 'IN-WING DEVICE RETENTION' [patent_app_type] => utility [patent_app_number] => 14/097478 [patent_app_country] => US [patent_app_date] => 2013-12-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 3142 [patent_no_of_claims] => 16 [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] => 14097478 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/097478
In-wing device retention Dec 4, 2013 Issued
Array ( [id] => 10429870 [patent_doc_number] => 20150314883 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-11-05 [patent_title] => 'Intake for an Engine of an Aircraft' [patent_app_type] => utility [patent_app_number] => 14/649754 [patent_app_country] => US [patent_app_date] => 2013-12-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 3283 [patent_no_of_claims] => 16 [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] => 14649754 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/649754
Intake for an engine of an aircraft Dec 1, 2013 Issued
Array ( [id] => 10429850 [patent_doc_number] => 20150314862 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-11-05 [patent_title] => 'WHEEL MOTORIZING SYSTEM, NOTABLY FOR AN AIRCRAFT WHEEL' [patent_app_type] => utility [patent_app_number] => 14/648114 [patent_app_country] => US [patent_app_date] => 2013-11-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 4538 [patent_no_of_claims] => 17 [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] => 14648114 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/648114
Wheel motorizing system, notably for an aircraft wheel Nov 28, 2013 Issued
Array ( [id] => 10436733 [patent_doc_number] => 20150321745 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-11-12 [patent_title] => 'Wing and Application Thereof' [patent_app_type] => utility [patent_app_number] => 14/647500 [patent_app_country] => US [patent_app_date] => 2013-11-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 24 [patent_figures_cnt] => 24 [patent_no_of_words] => 14998 [patent_no_of_claims] => 94 [patent_no_of_ind_claims] => 10 [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] => 14647500 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/647500
Wing and application thereof Nov 24, 2013 Issued
Array ( [id] => 10429869 [patent_doc_number] => 20150314881 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-11-05 [patent_title] => 'SAFETY APPARATUS FOR A MULTI-BLADE AIRCRAFT' [patent_app_type] => utility [patent_app_number] => 14/646912 [patent_app_country] => US [patent_app_date] => 2013-11-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 2929 [patent_no_of_claims] => 14 [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] => 14646912 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/646912
SAFETY APPARATUS FOR A MULTI-BLADE AIRCRAFT Nov 24, 2013 Abandoned
Array ( [id] => 9515002 [patent_doc_number] => 20140151494 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-06-05 [patent_title] => 'VERTICAL TAKE-OFF AND LANDING (VTOL) AERIAL VEHICLE AND METHOD OF OPERATING SUCH A VTOL AERIAL VEHICLE' [patent_app_type] => utility [patent_app_number] => 14/088662 [patent_app_country] => US [patent_app_date] => 2013-11-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 5792 [patent_no_of_claims] => 29 [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] => 14088662 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/088662
VERTICAL TAKE-OFF AND LANDING (VTOL) AERIAL VEHICLE AND METHOD OF OPERATING SUCH A VTOL AERIAL VEHICLE Nov 24, 2013 Abandoned
Array ( [id] => 12106008 [patent_doc_number] => 09862478 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2018-01-09 [patent_title] => 'Modular structural assembly' [patent_app_type] => utility [patent_app_number] => 14/085354 [patent_app_country] => US [patent_app_date] => 2013-11-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 4 [patent_no_of_words] => 1688 [patent_no_of_claims] => 21 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 181 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14085354 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/085354
Modular structural assembly Nov 19, 2013 Issued
Array ( [id] => 10451645 [patent_doc_number] => 20150336659 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-11-26 [patent_title] => 'HYPERSONIC LAMINAR FLOW CONTROL' [patent_app_type] => utility [patent_app_number] => 14/443992 [patent_app_country] => US [patent_app_date] => 2013-11-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 21 [patent_figures_cnt] => 21 [patent_no_of_words] => 8836 [patent_no_of_claims] => 20 [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] => 14443992 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/443992
Hypersonic laminar flow control Nov 18, 2013 Issued
Array ( [id] => 11894903 [patent_doc_number] => 09764826 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2017-09-19 [patent_title] => 'Landing gear assembly and methods' [patent_app_type] => utility [patent_app_number] => 14/647586 [patent_app_country] => US [patent_app_date] => 2013-11-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 4036 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 237 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14647586 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/647586
Landing gear assembly and methods Nov 18, 2013 Issued
Array ( [id] => 9474060 [patent_doc_number] => 20140131523 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-05-15 [patent_title] => 'ABOVE-THE-FLOOR RUDDER AND BRAKE CONTROL SYSTEM' [patent_app_type] => utility [patent_app_number] => 14/077110 [patent_app_country] => US [patent_app_date] => 2013-11-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 21 [patent_figures_cnt] => 21 [patent_no_of_words] => 7796 [patent_no_of_claims] => 20 [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] => 14077110 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/077110
ABOVE-THE-FLOOR RUDDER AND BRAKE CONTROL SYSTEM Nov 10, 2013 Abandoned
Array ( [id] => 12112532 [patent_doc_number] => 09868512 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2018-01-16 [patent_title] => 'Airplane wing, an airplane and a flap system' [patent_app_type] => utility [patent_app_number] => 14/440272 [patent_app_country] => US [patent_app_date] => 2013-10-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 5717 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 317 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14440272 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/440272
Airplane wing, an airplane and a flap system Oct 28, 2013 Issued
Array ( [id] => 10223869 [patent_doc_number] => 20150108862 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-04-23 [patent_title] => 'Aircraft Vehicle and a Fixing Sleeve' [patent_app_type] => utility [patent_app_number] => 14/127186 [patent_app_country] => US [patent_app_date] => 2013-10-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 14 [patent_figures_cnt] => 14 [patent_no_of_words] => 6000 [patent_no_of_claims] => 30 [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] => 14127186 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/127186
Aircraft vehicle and a fixing sleeve Oct 21, 2013 Issued
Array ( [id] => 11800342 [patent_doc_number] => 09541177 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2017-01-10 [patent_title] => 'Ratcheting shape memory alloy actuators and systems and methods including the same' [patent_app_type] => utility [patent_app_number] => 14/051957 [patent_app_country] => US [patent_app_date] => 2013-10-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 25 [patent_no_of_words] => 12167 [patent_no_of_claims] => 22 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 105 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14051957 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/051957
Ratcheting shape memory alloy actuators and systems and methods including the same Oct 10, 2013 Issued
Array ( [id] => 11225123 [patent_doc_number] => 09452837 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2016-09-27 [patent_title] => 'Aircraft lavatory unit' [patent_app_type] => utility [patent_app_number] => 14/435149 [patent_app_country] => US [patent_app_date] => 2013-10-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 13 [patent_figures_cnt] => 16 [patent_no_of_words] => 5828 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 88 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14435149 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/435149
Aircraft lavatory unit Oct 8, 2013 Issued
Array ( [id] => 11225115 [patent_doc_number] => 09452829 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2016-09-27 [patent_title] => 'Yaw control of co-axial rotor' [patent_app_type] => utility [patent_app_number] => 14/049091 [patent_app_country] => US [patent_app_date] => 2013-10-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 5 [patent_no_of_words] => 6395 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 114 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14049091 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/049091
Yaw control of co-axial rotor Oct 7, 2013 Issued
Array ( [id] => 10175722 [patent_doc_number] => 09205911 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2015-12-08 [patent_title] => 'Pitch stabilizer and rotary-wing aircraft equipped with such stabilizer' [patent_app_type] => utility [patent_app_number] => 14/028690 [patent_app_country] => US [patent_app_date] => 2013-09-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 6 [patent_no_of_words] => 5973 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 197 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14028690 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/028690
Pitch stabilizer and rotary-wing aircraft equipped with such stabilizer Sep 16, 2013 Issued
Array ( [id] => 9508547 [patent_doc_number] => 20140145038 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-05-29 [patent_title] => 'ORBIT ATTITUDE CONTROL DEVICE, AND METHOD OF CONTROLLING ORBIT ATTITUDE' [patent_app_type] => utility [patent_app_number] => 14/018698 [patent_app_country] => US [patent_app_date] => 2013-09-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 4269 [patent_no_of_claims] => 8 [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] => 14018698 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/018698
Orbit attitude control device, and method of controlling orbit attitude Sep 4, 2013 Issued
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