
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] => 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
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[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
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[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
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[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
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[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
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[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
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[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
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[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
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[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
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[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
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[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 |