
Hubert G. Cheung
Examiner (ID: 17731, Phone: (571)270-1396 , Office: P/2157 )
| Most Active Art Unit | 2157 |
| Art Unit(s) | 2152, 2157, 2168, 2169, 2159 |
| Total Applications | 437 |
| Issued Applications | 248 |
| Pending Applications | 50 |
| Abandoned Applications | 150 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 6169264
[patent_doc_number] => 20110174924
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-07-21
[patent_title] => 'LANDING GEAR MECHANISM FOR AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 13/001976
[patent_app_country] => US
[patent_app_date] => 2009-06-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 22
[patent_figures_cnt] => 22
[patent_no_of_words] => 7048
[patent_no_of_claims] => 29
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0174/20110174924.pdf
[firstpage_image] =>[orig_patent_app_number] => 13001976
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/001976 | Landing gear mechanism for aircraft | Jun 29, 2009 | Issued |
Array
(
[id] => 6323621
[patent_doc_number] => 20100326365
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-12-30
[patent_title] => 'REUSABLE WATER LINE GROMMET AND DISPOSABLE CAGE BOX'
[patent_app_type] => utility
[patent_app_number] => 12/494714
[patent_app_country] => US
[patent_app_date] => 2009-06-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 4495
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[pdf_file] => publications/A1/0326/20100326365.pdf
[firstpage_image] =>[orig_patent_app_number] => 12494714
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/494714 | Reusable water line grommet and disposable cage box | Jun 29, 2009 | Issued |
Array
(
[id] => 9880786
[patent_doc_number] => 08967539
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-03-03
[patent_title] => 'Method for assembling a floor in a cockpit structure previously constructed from a section of aircraft fuselage'
[patent_app_type] => utility
[patent_app_number] => 13/001699
[patent_app_country] => US
[patent_app_date] => 2009-06-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 13
[patent_no_of_words] => 5773
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13001699
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/001699 | Method for assembling a floor in a cockpit structure previously constructed from a section of aircraft fuselage | Jun 24, 2009 | Issued |
Array
(
[id] => 9830598
[patent_doc_number] => 08939405
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-01-27
[patent_title] => 'Aircraft fuselage element'
[patent_app_type] => utility
[patent_app_number] => 13/000952
[patent_app_country] => US
[patent_app_date] => 2009-06-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[patent_no_of_words] => 2199
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13000952
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/000952 | Aircraft fuselage element | Jun 18, 2009 | Issued |
Array
(
[id] => 6183746
[patent_doc_number] => 20110168837
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-07-14
[patent_title] => 'AIRCRAFT PROPULSION SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 13/001172
[patent_app_country] => US
[patent_app_date] => 2009-06-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[pdf_file] => publications/A1/0168/20110168837.pdf
[firstpage_image] =>[orig_patent_app_number] => 13001172
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/001172 | Aircraft propulsion system | Jun 17, 2009 | Issued |
Array
(
[id] => 9237573
[patent_doc_number] => 08602358
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-12-10
[patent_title] => 'Interface element, aircraft interior equipment component and method for installing an aircraft interior equipment component'
[patent_app_type] => utility
[patent_app_number] => 12/999710
[patent_app_country] => US
[patent_app_date] => 2009-06-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_no_of_words] => 4419
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12999710
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/999710 | Interface element, aircraft interior equipment component and method for installing an aircraft interior equipment component | Jun 14, 2009 | Issued |
Array
(
[id] => 5962641
[patent_doc_number] => 20110147530
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-06-23
[patent_title] => 'AUXILIARY FUEL TANK SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 12/993039
[patent_app_country] => US
[patent_app_date] => 2009-05-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
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[patent_no_of_words] => 3187
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0147/20110147530.pdf
[firstpage_image] =>[orig_patent_app_number] => 12993039
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/993039 | AUXILIARY FUEL TANK SYSTEM | May 18, 2009 | Abandoned |
Array
(
[id] => 6113834
[patent_doc_number] => 20110073717
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-03-31
[patent_title] => 'AIRCRAFT WITH A HYBRID ENERGY SUPPLY'
[patent_app_type] => utility
[patent_app_number] => 12/994808
[patent_app_country] => US
[patent_app_date] => 2009-05-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
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[patent_no_of_words] => 1729
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[pdf_file] => publications/A1/0073/20110073717.pdf
[firstpage_image] =>[orig_patent_app_number] => 12994808
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/994808 | AIRCRAFT WITH A HYBRID ENERGY SUPPLY | May 13, 2009 | Abandoned |
Array
(
[id] => 7659933
[patent_doc_number] => 20110309202
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-12-22
[patent_title] => 'Wingtec Holding Limited'
[patent_app_type] => utility
[patent_app_number] => 12/865892
[patent_app_country] => US
[patent_app_date] => 2009-02-03
[patent_effective_date] => 0000-00-00
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[pdf_file] => publications/A1/0309/20110309202.pdf
[firstpage_image] =>[orig_patent_app_number] => 12865892
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/865892 | Wingtec Holding Limited | Feb 2, 2009 | Abandoned |
Array
(
[id] => 8795861
[patent_doc_number] => 08434721
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-05-07
[patent_title] => 'Aircraft tank system and method for refueling an aircraft using an eration/deaeration device with a shut-off valve'
[patent_app_type] => utility
[patent_app_number] => 12/865522
[patent_app_country] => US
[patent_app_date] => 2009-02-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12865522
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/865522 | Aircraft tank system and method for refueling an aircraft using an eration/deaeration device with a shut-off valve | Feb 1, 2009 | Issued |
Array
(
[id] => 9237563
[patent_doc_number] => 08602348
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-12-10
[patent_title] => 'Flying-wing aircraft'
[patent_app_type] => utility
[patent_app_number] => 12/865429
[patent_app_country] => US
[patent_app_date] => 2009-02-02
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12865429
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/865429 | Flying-wing aircraft | Feb 1, 2009 | Issued |
Array
(
[id] => 6072114
[patent_doc_number] => 20110138678
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-06-16
[patent_title] => 'INSECT TRAP'
[patent_app_type] => utility
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[patent_app_country] => US
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[patent_effective_date] => 0000-00-00
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[pdf_file] => publications/A1/0138/20110138678.pdf
[firstpage_image] =>[orig_patent_app_number] => 12865513
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/865513 | Insect trap | Jan 28, 2009 | Issued |
Array
(
[id] => 5955360
[patent_doc_number] => 20110180662
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-07-28
[patent_title] => 'LANDING GEAR'
[patent_app_type] => utility
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[pdf_file] => publications/A1/0180/20110180662.pdf
[firstpage_image] =>[orig_patent_app_number] => 12864371
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/864371 | LANDING GEAR | Jan 25, 2009 | Abandoned |
Array
(
[id] => 6568129
[patent_doc_number] => 20100320316
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-12-23
[patent_title] => 'AIR INTAKE FOR AIRCRAFT NACELLE, AND PROPULSION ASSEMBLY INCLUDING SUCH AIR INTAKE'
[patent_app_type] => utility
[patent_app_number] => 12/864901
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[pdf_file] => publications/A1/0320/20100320316.pdf
[firstpage_image] =>[orig_patent_app_number] => 12864901
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/864901 | Air intake for aircraft nacelle, and propulsion assembly including such air intake | Jan 20, 2009 | Issued |
Array
(
[id] => 6367369
[patent_doc_number] => 20100314501
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-12-16
[patent_title] => 'LOCKING SYSTEM FOR AIR INTAKE STRUCTURE FOR TURBOJET ENGINE NACELLE'
[patent_app_type] => utility
[patent_app_number] => 12/811347
[patent_app_country] => US
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[pdf_file] => publications/A1/0314/20100314501.pdf
[firstpage_image] =>[orig_patent_app_number] => 12811347
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/811347 | Locking system for air intake structure for turbojet engine nacelle | Nov 27, 2008 | Issued |
Array
(
[id] => 6230891
[patent_doc_number] => 20100264273
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-10-21
[patent_title] => 'FUSELAGE STRUCTURE FOR AN AIRCRAFT FUSELAGE IN COMPOSITE MATERIAL AND AIRCRAFT EQUIPPED WITH SUCH A FUSELAGE STRUCTURE'
[patent_app_type] => utility
[patent_app_number] => 12/681836
[patent_app_country] => US
[patent_app_date] => 2008-09-29
[patent_effective_date] => 0000-00-00
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[pdf_file] => publications/A1/0264/20100264273.pdf
[firstpage_image] =>[orig_patent_app_number] => 12681836
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/681836 | Fuselage structure for an aircraft fuselage in composite material and aircraft equipped with such a fuselage structure | Sep 28, 2008 | Issued |
Array
(
[id] => 7659209
[patent_doc_number] => 20110308478
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-12-22
[patent_title] => 'LABORATORY ANIMAL RETAINING APPLIANCE'
[patent_app_type] => utility
[patent_app_number] => 13/062303
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[firstpage_image] =>[orig_patent_app_number] => 13062303
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/062303 | Laboratory animal retaining appliance | Sep 3, 2008 | Issued |
Array
(
[id] => 6582354
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[patent_issue_date] => 2010-12-09
[patent_title] => 'STRUCTURAL FRAME MADE OF A COMPOSITE MATERIAL AND AIRCRAFT FUSELAGE COMPRISING SUCH A FRAME'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/676725 | Structural frame made of a composite material and aircraft fuselage comprising such a frame | Sep 3, 2008 | Issued |
Array
(
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[patent_title] => 'GALLEY UNIT'
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[firstpage_image] =>[orig_patent_app_number] => 13060228
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/060228 | GALLEY UNIT | Aug 21, 2008 | Abandoned |
Array
(
[id] => 6072675
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[patent_issue_date] => 2011-06-16
[patent_title] => 'AERODYNAMIC WING WITH IMPROVED LINE ATTACHMENT'
[patent_app_type] => utility
[patent_app_number] => 12/995161
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[patent_app_date] => 2008-05-30
[patent_effective_date] => 0000-00-00
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[pdf_file] => publications/A1/0139/20110139053.pdf
[firstpage_image] =>[orig_patent_app_number] => 12995161
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/995161 | Aerodynamic wing with improved line attachment | May 29, 2008 | Issued |