
Sumesh Kaushal
Examiner (ID: 405)
| Most Active Art Unit | 1633 |
| Art Unit(s) | 1633, OPIM, 1636, OPA |
| Total Applications | 513 |
| Issued Applications | 223 |
| Pending Applications | 79 |
| Abandoned Applications | 211 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 5377182
[patent_doc_number] => 20090189021
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-07-30
[patent_title] => 'AUXILIARY AIRCRAFT FUEL TANKS, SYSTEMS AND METHODS PROVIDING VISUAL LEAK DETECTION'
[patent_app_type] => utility
[patent_app_number] => 12/019726
[patent_app_country] => US
[patent_app_date] => 2008-01-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 2699
[patent_no_of_claims] => 11
[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/A1/0189/20090189021.pdf
[firstpage_image] =>[orig_patent_app_number] => 12019726
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/019726 | Auxiliary aircraft fuel tanks, systems and methods providing visual leak detection | Jan 24, 2008 | Issued |
Array
(
[id] => 4843048
[patent_doc_number] => 20080179456
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-07-31
[patent_title] => 'Flexible cable connection to monuments inside of an aircraft cabin'
[patent_app_type] => utility
[patent_app_number] => 12/009820
[patent_app_country] => US
[patent_app_date] => 2008-01-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2419
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 3
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[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0179/20080179456.pdf
[firstpage_image] =>[orig_patent_app_number] => 12009820
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/009820 | Flexible cable connection to monuments inside of an aircraft cabin | Jan 21, 2008 | Issued |
Array
(
[id] => 4513756
[patent_doc_number] => 07938369
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-05-10
[patent_title] => 'Method and apparatus for aerial fuel transfer'
[patent_app_type] => utility
[patent_app_number] => 12/017661
[patent_app_country] => US
[patent_app_date] => 2008-01-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 8
[patent_no_of_words] => 5127
[patent_no_of_claims] => 15
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/938/07938369.pdf
[firstpage_image] =>[orig_patent_app_number] => 12017661
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/017661 | Method and apparatus for aerial fuel transfer | Jan 21, 2008 | Issued |
Array
(
[id] => 7539013
[patent_doc_number] => 08056850
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-11-15
[patent_title] => 'Particle-filled wing-to-body fairing and method for reducing fairing vibrations'
[patent_app_type] => utility
[patent_app_number] => 12/016741
[patent_app_country] => US
[patent_app_date] => 2008-01-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 6
[patent_no_of_words] => 2390
[patent_no_of_claims] => 25
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 88
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/056/08056850.pdf
[firstpage_image] =>[orig_patent_app_number] => 12016741
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/016741 | Particle-filled wing-to-body fairing and method for reducing fairing vibrations | Jan 17, 2008 | Issued |
Array
(
[id] => 4610309
[patent_doc_number] => 07988103
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-08-02
[patent_title] => 'Solid state supersonic flow actuator and method of use'
[patent_app_type] => utility
[patent_app_number] => 12/015142
[patent_app_country] => US
[patent_app_date] => 2008-01-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 17
[patent_no_of_words] => 7784
[patent_no_of_claims] => 6
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[patent_words_short_claim] => 185
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/988/07988103.pdf
[firstpage_image] =>[orig_patent_app_number] => 12015142
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/015142 | Solid state supersonic flow actuator and method of use | Jan 15, 2008 | Issued |
Array
(
[id] => 4638212
[patent_doc_number] => 08016237
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-09-13
[patent_title] => 'Methods and apparatus for an integrated aerodynamic panel'
[patent_app_type] => utility
[patent_app_number] => 11/954974
[patent_app_country] => US
[patent_app_date] => 2007-12-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2078
[patent_no_of_claims] => 20
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/016/08016237.pdf
[firstpage_image] =>[orig_patent_app_number] => 11954974
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/954974 | Methods and apparatus for an integrated aerodynamic panel | Dec 11, 2007 | Issued |
Array
(
[id] => 5275249
[patent_doc_number] => 20090127381
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-05-21
[patent_title] => 'System, method and apparatus for aircraft having counter-rotating, ring-winged rotors'
[patent_app_type] => utility
[patent_app_number] => 11/985722
[patent_app_country] => US
[patent_app_date] => 2007-11-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 1323
[patent_no_of_claims] => 29
[patent_no_of_ind_claims] => 2
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0127/20090127381.pdf
[firstpage_image] =>[orig_patent_app_number] => 11985722
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/985722 | System, method and apparatus for aircraft having counter-rotating, ring-winged rotors | Nov 15, 2007 | Issued |
Array
(
[id] => 6246791
[patent_doc_number] => 20100025540
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-02-04
[patent_title] => 'Compact ultralight aircraft reduced dimensions, with vertical take-off and landing'
[patent_app_type] => utility
[patent_app_number] => 12/311984
[patent_app_country] => US
[patent_app_date] => 2007-11-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 2252
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 1
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[patent_maintenance] => 1
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[pdf_file] => publications/A1/0025/20100025540.pdf
[firstpage_image] =>[orig_patent_app_number] => 12311984
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/311984 | Compact ultralight aircraft reduced dimensions, with vertical take-off and landing | Nov 11, 2007 | Abandoned |
Array
(
[id] => 4527260
[patent_doc_number] => 07871037
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-01-18
[patent_title] => 'Emergency landing apparatus'
[patent_app_type] => utility
[patent_app_number] => 11/936883
[patent_app_country] => US
[patent_app_date] => 2007-11-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
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[patent_no_of_words] => 2880
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/871/07871037.pdf
[firstpage_image] =>[orig_patent_app_number] => 11936883
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/936883 | Emergency landing apparatus | Nov 7, 2007 | Issued |
Array
(
[id] => 6445220
[patent_doc_number] => 20100038477
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-02-18
[patent_title] => 'SYSTEM AND METHODS FOR AIRBORNE LAUNCH AND RECOVERY OF AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 11/874804
[patent_app_country] => US
[patent_app_date] => 2007-10-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 5436
[patent_no_of_claims] => 49
[patent_no_of_ind_claims] => 6
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0038/20100038477.pdf
[firstpage_image] =>[orig_patent_app_number] => 11874804
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/874804 | System and methods for airborne launch and recovery of aircraft | Oct 17, 2007 | Issued |
Array
(
[id] => 7770773
[patent_doc_number] => 08118262
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-02-21
[patent_title] => 'Hybrid parachute'
[patent_app_type] => utility
[patent_app_number] => 11/914930
[patent_app_country] => US
[patent_app_date] => 2007-09-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
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[patent_no_of_words] => 5014
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/118/08118262.pdf
[firstpage_image] =>[orig_patent_app_number] => 11914930
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/914930 | Hybrid parachute | Sep 20, 2007 | Issued |
Array
(
[id] => 8211222
[patent_doc_number] => 08191821
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-06-05
[patent_title] => 'Actuator'
[patent_app_type] => utility
[patent_app_number] => 12/310687
[patent_app_country] => US
[patent_app_date] => 2007-09-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[pdf_file] => patents/08/191/08191821.pdf
[firstpage_image] =>[orig_patent_app_number] => 12310687
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/310687 | Actuator | Sep 10, 2007 | Issued |
Array
(
[id] => 5388891
[patent_doc_number] => 20090206203
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-08-20
[patent_title] => 'AIRCRAFT WING BOX AND MANUFACTURE THEREOF'
[patent_app_type] => utility
[patent_app_number] => 12/309040
[patent_app_country] => US
[patent_app_date] => 2007-07-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
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[pdf_file] => publications/A1/0206/20090206203.pdf
[firstpage_image] =>[orig_patent_app_number] => 12309040
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/309040 | Aircraft wing box and manufacture thereof | Jul 18, 2007 | Issued |
Array
(
[id] => 5549645
[patent_doc_number] => 20090283631
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-11-19
[patent_title] => 'ENGINE ASSEMBLY FOR AIRCRAFT COMPRISING AN AERODYNAMIC COUPLING FAIRING MOUNTED ON TWO SEPARATE ELEMENTS'
[patent_app_type] => utility
[patent_app_number] => 12/307142
[patent_app_country] => US
[patent_app_date] => 2007-07-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0283/20090283631.pdf
[firstpage_image] =>[orig_patent_app_number] => 12307142
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/307142 | Aircraft engine assembly comprising a junction aerodynamic fairing mounted on two separate elements | Jul 9, 2007 | Issued |
Array
(
[id] => 5299925
[patent_doc_number] => 20090294577
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-12-03
[patent_title] => 'DEVICE FOR AUTONOMOUS MOVEMENT OF AN AIRCRAFT ON THE GROUND'
[patent_app_type] => utility
[patent_app_number] => 12/306669
[patent_app_country] => US
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[pdf_file] => publications/A1/0294/20090294577.pdf
[firstpage_image] =>[orig_patent_app_number] => 12306669
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/306669 | DEVICE FOR AUTONOMOUS MOVEMENT OF AN AIRCRAFT ON THE GROUND | Jun 27, 2007 | Abandoned |
Array
(
[id] => 8014537
[patent_doc_number] => 08136765
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-03-20
[patent_title] => 'Method of launching into operational orbit an artificial satellite and associated propulsion device'
[patent_app_type] => utility
[patent_app_number] => 12/306592
[patent_app_country] => US
[patent_app_date] => 2007-06-26
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[pdf_file] => patents/08/136/08136765.pdf
[firstpage_image] =>[orig_patent_app_number] => 12306592
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/306592 | Method of launching into operational orbit an artificial satellite and associated propulsion device | Jun 25, 2007 | Issued |
Array
(
[id] => 4469680
[patent_doc_number] => 07866609
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-01-11
[patent_title] => 'Passive removal of suction air for laminar flow control, and associated systems and methods'
[patent_app_type] => utility
[patent_app_number] => 11/763569
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[firstpage_image] =>[orig_patent_app_number] => 11763569
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/763569 | Passive removal of suction air for laminar flow control, and associated systems and methods | Jun 14, 2007 | Issued |
Array
(
[id] => 4610306
[patent_doc_number] => 07988101
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[patent_issue_date] => 2011-08-02
[patent_title] => 'Airfoil trailing edge plasma flow control apparatus and method'
[patent_app_type] => utility
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[rel_patent_id] =>[rel_patent_doc_number] =>) 11/753857 | Airfoil trailing edge plasma flow control apparatus and method | May 24, 2007 | Issued |
Array
(
[id] => 5299899
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[patent_issue_date] => 2009-12-03
[patent_title] => 'APPARATUS AND METHOD FOR BLENDING FLUIDS'
[patent_app_type] => utility
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[firstpage_image] =>[orig_patent_app_number] => 11751307
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/751307 | Apparatus and method for blending fluids | May 20, 2007 | Issued |
Array
(
[id] => 8003561
[patent_doc_number] => 08083178
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[patent_issue_date] => 2011-12-27
[patent_title] => 'Method and device for piloting an aircraft optimizing the control of the ailerons in an enhanced-lift configuration'
[patent_app_type] => utility
[patent_app_number] => 12/294588
[patent_app_country] => US
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[patent_effective_date] => 0000-00-00
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[pdf_file] => patents/08/083/08083178.pdf
[firstpage_image] =>[orig_patent_app_number] => 12294588
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/294588 | Method and device for piloting an aircraft optimizing the control of the ailerons in an enhanced-lift configuration | May 20, 2007 | Issued |