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] => 10340062 [patent_doc_number] => 20150225067 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-08-13 [patent_title] => 'RAIL SYSTEM FOR SEAT ASSEMBLY IN AN AIRCRAFT' [patent_app_type] => utility [patent_app_number] => 14/613806 [patent_app_country] => US [patent_app_date] => 2015-02-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 4196 [patent_no_of_claims] => 17 [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] => 14613806 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/613806
Rail system for seat assembly in an aircraft Feb 3, 2015 Issued
Array ( [id] => 11880473 [patent_doc_number] => 09751633 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2017-09-05 [patent_title] => 'Aircraft safety device' [patent_app_type] => utility [patent_app_number] => 14/613575 [patent_app_country] => US [patent_app_date] => 2015-02-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 13 [patent_no_of_words] => 5956 [patent_no_of_claims] => 5 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 126 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14613575 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/613575
Aircraft safety device Feb 3, 2015 Issued
Array ( [id] => 12468687 [patent_doc_number] => 09988143 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2018-06-05 [patent_title] => Landing gear deployment systems and methods [patent_app_type] => utility [patent_app_number] => 14/614330 [patent_app_country] => US [patent_app_date] => 2015-02-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 14 [patent_figures_cnt] => 23 [patent_no_of_words] => 13228 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 345 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14614330 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/614330
Landing gear deployment systems and methods Feb 3, 2015 Issued
Array ( [id] => 10318191 [patent_doc_number] => 20150203195 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-07-23 [patent_title] => 'SHOCK ABSORBER ASSEMBLY' [patent_app_type] => utility [patent_app_number] => 14/597818 [patent_app_country] => US [patent_app_date] => 2015-01-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 4345 [patent_no_of_claims] => 22 [patent_no_of_ind_claims] => 5 [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] => 14597818 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/597818
Shock absorber assembly Jan 14, 2015 Issued
Array ( [id] => 10325404 [patent_doc_number] => 20150210408 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-07-30 [patent_title] => 'Spacecraft Having Electronic Components As Structural Members And Related Methods' [patent_app_type] => utility [patent_app_number] => 14/596999 [patent_app_country] => US [patent_app_date] => 2015-01-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 12 [patent_no_of_words] => 5913 [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] => 14596999 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/596999
Spacecraft having electronic components as structural members and related methods Jan 13, 2015 Issued
Array ( [id] => 10262117 [patent_doc_number] => 20150147114 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-05-28 [patent_title] => 'MULTI-DIRECTIONAL LOAD JOINT SYSTEM' [patent_app_type] => utility [patent_app_number] => 14/594292 [patent_app_country] => US [patent_app_date] => 2015-01-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 4196 [patent_no_of_claims] => 19 [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] => 14594292 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/594292
Multi-directional load joint system Jan 11, 2015 Issued
Array ( [id] => 13236511 [patent_doc_number] => 10131445 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2018-11-20 [patent_title] => Containment system and increased strength radome assembly [patent_app_type] => utility [patent_app_number] => 14/590670 [patent_app_country] => US [patent_app_date] => 2015-01-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 17 [patent_figures_cnt] => 20 [patent_no_of_words] => 7827 [patent_no_of_claims] => 23 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 172 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14590670 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/590670
Containment system and increased strength radome assembly Jan 5, 2015 Issued
Array ( [id] => 11894898 [patent_doc_number] => 09764820 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2017-09-19 [patent_title] => 'Horizontal tail surface' [patent_app_type] => utility [patent_app_number] => 14/587683 [patent_app_country] => US [patent_app_date] => 2014-12-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 15 [patent_no_of_words] => 7927 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 193 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14587683 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/587683
Horizontal tail surface Dec 30, 2014 Issued
Array ( [id] => 12171817 [patent_doc_number] => 09889943 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2018-02-13 [patent_title] => 'Assembly for an aircraft, comprising an engine attachment body equipped with at least one shackle support fitting that passes into the box section of the attachment pylon' [patent_app_type] => utility [patent_app_number] => 14/571786 [patent_app_country] => US [patent_app_date] => 2014-12-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 10 [patent_no_of_words] => 4256 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 143 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14571786 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/571786
Assembly for an aircraft, comprising an engine attachment body equipped with at least one shackle support fitting that passes into the box section of the attachment pylon Dec 15, 2014 Issued
Array ( [id] => 13118919 [patent_doc_number] => 10077808 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2018-09-18 [patent_title] => Roller profile for hourglass roller bearings in aircraft [patent_app_type] => utility [patent_app_number] => 14/572260 [patent_app_country] => US [patent_app_date] => 2014-12-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 17 [patent_figures_cnt] => 18 [patent_no_of_words] => 4112 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 257 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14572260 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/572260
Roller profile for hourglass roller bearings in aircraft Dec 15, 2014 Issued
Array ( [id] => 10422198 [patent_doc_number] => 20150307209 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-10-29 [patent_title] => 'LINE CAPTURE DEVICES FOR UNMANNED AIRCRAFT, AND ASSOCIATED SYSTEMS AND METHODS' [patent_app_type] => utility [patent_app_number] => 14/569443 [patent_app_country] => US [patent_app_date] => 2014-12-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 5181 [patent_no_of_claims] => 21 [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] => 14569443 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/569443
Line capture devices for unmanned aircraft, and associated systems and methods Dec 11, 2014 Issued
Array ( [id] => 10298519 [patent_doc_number] => 20150183518 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-07-02 [patent_title] => 'AIRCRAFT CONFIGURATION' [patent_app_type] => utility [patent_app_number] => 14/565775 [patent_app_country] => US [patent_app_date] => 2014-12-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 2978 [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] => 14565775 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/565775
Aircraft configuration Dec 9, 2014 Issued
Array ( [id] => 10281186 [patent_doc_number] => 20150166183 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-06-18 [patent_title] => 'Seating Arrangement' [patent_app_type] => utility [patent_app_number] => 14/566644 [patent_app_country] => US [patent_app_date] => 2014-12-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 31 [patent_figures_cnt] => 31 [patent_no_of_words] => 13126 [patent_no_of_claims] => 29 [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] => 14566644 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/566644
Seating arrangement Dec 9, 2014 Issued
Array ( [id] => 10406271 [patent_doc_number] => 20150291280 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-10-15 [patent_title] => 'AIRCRAFT ELECTRIC BRAKING SYSTEM' [patent_app_type] => utility [patent_app_number] => 14/554609 [patent_app_country] => US [patent_app_date] => 2014-11-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 12 [patent_no_of_words] => 6131 [patent_no_of_claims] => 24 [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] => 14554609 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/554609
Aircraft electric braking system Nov 25, 2014 Issued
Array ( [id] => 11773170 [patent_doc_number] => 09381995 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2016-07-05 [patent_title] => 'Advanced pitch stabilizer' [patent_app_type] => utility [patent_app_number] => 14/554142 [patent_app_country] => US [patent_app_date] => 2014-11-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 20 [patent_no_of_words] => 7641 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 533 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14554142 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/554142
Advanced pitch stabilizer Nov 25, 2014 Issued
Array ( [id] => 11690604 [patent_doc_number] => 20170166320 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2017-06-15 [patent_title] => 'METHOD AND SYSTEM FOR OPTIMIZED PRODUCTION OF NON-PROPULSIVE ENERGY' [patent_app_type] => utility [patent_app_number] => 15/039026 [patent_app_country] => US [patent_app_date] => 2014-11-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 2727 [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] => 15039026 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/039026
Method and system for optimized production of non-propulsive energy Nov 24, 2014 Issued
Array ( [id] => 10281192 [patent_doc_number] => 20150166189 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-06-18 [patent_title] => 'ASSEMBLY COMPRISING AN ARTICULATION SPINDLE SUPPORTED BY A CLEVIS AND IMMOBILIZED IN TRANSLATION BY A BLOCKING DEVICE INTEGRATING A DOUBLE ANTI-ROTATION SYSTEM' [patent_app_type] => utility [patent_app_number] => 14/553342 [patent_app_country] => US [patent_app_date] => 2014-11-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 3644 [patent_no_of_claims] => 9 [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] => 14553342 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/553342
Assembly comprising an articulation spindle supported by a clevis and immobilized in translation by a blocking device integrating a double anti-rotation system Nov 24, 2014 Issued
Array ( [id] => 9913978 [patent_doc_number] => 20150069182 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-03-12 [patent_title] => 'MODULAR OVERHEAD BIN' [patent_app_type] => utility [patent_app_number] => 14/540582 [patent_app_country] => US [patent_app_date] => 2014-11-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 4599 [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] => 14540582 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/540582
Modular overhead bin Nov 12, 2014 Issued
Array ( [id] => 15784275 [patent_doc_number] => 10625844 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2020-04-21 [patent_title] => Fuselage with structural and non-structural stanchions [patent_app_type] => utility [patent_app_number] => 14/537791 [patent_app_country] => US [patent_app_date] => 2014-11-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 13 [patent_figures_cnt] => 14 [patent_no_of_words] => 6913 [patent_no_of_claims] => 23 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 103 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14537791 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/537791
Fuselage with structural and non-structural stanchions Nov 9, 2014 Issued
Array ( [id] => 10244719 [patent_doc_number] => 20150129714 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-05-14 [patent_title] => 'CONNECTION DEVICE FOR MEANS OF AIRPLANE' [patent_app_type] => utility [patent_app_number] => 14/535813 [patent_app_country] => US [patent_app_date] => 2014-11-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 2639 [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] => 14535813 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/535813
Connection device for means of airplane Nov 6, 2014 Issued
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