
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 number | Title of the application | Filing Date | Status |
|---|---|---|---|
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
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[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
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[patent_no_of_words] => 5956
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[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
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[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
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[patent_no_of_words] => 4345
[patent_no_of_claims] => 22
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[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
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[patent_no_of_words] => 5913
[patent_no_of_claims] => 20
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[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
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[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
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[patent_no_of_words] => 7827
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[patent_maintenance] => 1
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[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
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[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
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[patent_no_of_words] => 4256
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[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
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[patent_no_of_words] => 4112
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[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
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[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
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[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
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[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
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[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
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[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
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[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
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[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
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/540582 | Modular overhead bin | Nov 12, 2014 | Issued |
Array
(
[id] => 15784275
[patent_doc_number] => 10625844
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[patent_kind] => B2
[patent_issue_date] => 2020-04-21
[patent_title] => Fuselage with structural and non-structural stanchions
[patent_app_type] => utility
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/537791 | Fuselage with structural and non-structural stanchions | Nov 9, 2014 | Issued |
Array
(
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[patent_title] => 'CONNECTION DEVICE FOR MEANS OF AIRPLANE'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/535813 | Connection device for means of airplane | Nov 6, 2014 | Issued |