Search

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 numberTitle of the applicationFiling DateStatus
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 [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] => 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 [patent_no_of_claims] => 15 [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] => 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 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 333 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_figures_cnt] => 6 [patent_no_of_words] => 2199 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 239 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_figures_cnt] => 5 [patent_no_of_words] => 4467 [patent_no_of_claims] => 15 [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] => 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 [patent_figures_cnt] => 6 [patent_no_of_words] => 4419 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 212 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_figures_cnt] => 10 [patent_no_of_words] => 3187 [patent_no_of_claims] => 17 [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] => 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 [patent_figures_cnt] => 2 [patent_no_of_words] => 1729 [patent_no_of_claims] => 6 [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] => 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 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 6320 [patent_no_of_claims] => 33 [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] => 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 [patent_figures_cnt] => 2 [patent_no_of_words] => 4328 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 188 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 39 [patent_no_of_words] => 5933 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 175 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_app_number] => 12/865513 [patent_app_country] => US [patent_app_date] => 2009-01-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 16 [patent_figures_cnt] => 16 [patent_no_of_words] => 8248 [patent_no_of_claims] => 17 [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] => 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 [patent_app_number] => 12/864371 [patent_app_country] => US [patent_app_date] => 2009-01-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 1349 [patent_no_of_claims] => 11 [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] => 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 [patent_app_country] => US [patent_app_date] => 2009-01-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2531 [patent_no_of_claims] => 19 [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] => 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 [patent_app_date] => 2008-11-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 3532 [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] => 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 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 3513 [patent_no_of_claims] => 11 [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] => 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 [patent_app_country] => US [patent_app_date] => 2008-09-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 11 [patent_no_of_words] => 7923 [patent_no_of_claims] => 10 [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] => publications/A1/0308/20110308478.pdf [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 [patent_doc_number] => 20100308165 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-12-09 [patent_title] => 'STRUCTURAL FRAME MADE OF A COMPOSITE MATERIAL AND AIRCRAFT FUSELAGE COMPRISING SUCH A FRAME' [patent_app_type] => utility [patent_app_number] => 12/676725 [patent_app_country] => US [patent_app_date] => 2008-09-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 3142 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 7 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0308/20100308165.pdf [firstpage_image] =>[orig_patent_app_number] => 12676725 [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 ( [id] => 5931803 [patent_doc_number] => 20110210203 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-09-01 [patent_title] => 'GALLEY UNIT' [patent_app_type] => utility [patent_app_number] => 13/060228 [patent_app_country] => US [patent_app_date] => 2008-08-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 2723 [patent_no_of_claims] => 17 [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] => publications/A1/0210/20110210203.pdf [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 [patent_doc_number] => 20110139053 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-06-16 [patent_title] => 'AERODYNAMIC WING WITH IMPROVED LINE ATTACHMENT' [patent_app_type] => utility [patent_app_number] => 12/995161 [patent_app_country] => US [patent_app_date] => 2008-05-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 5747 [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] => 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
Menu