
Khatol S. Shahnan Shah
Examiner (ID: 17264, Phone: (571)272-0863 , Office: P/1645 )
| Most Active Art Unit | 1645 |
| Art Unit(s) | 1645 |
| Total Applications | 686 |
| Issued Applications | 338 |
| Pending Applications | 112 |
| Abandoned Applications | 261 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 6557076
[patent_doc_number] => 20100319357
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-12-23
[patent_title] => 'DEVICE AND A METHOD FOR STARTING A TURBINE ENGINE FITTED TO A HELICOPTER, MAKING USE OF AN ELECTRICAL ENERGY SOURCE THAT INCLUDES DISCHARGE BOOSTER MEMBERS'
[patent_app_type] => utility
[patent_app_number] => 12/816608
[patent_app_country] => US
[patent_app_date] => 2010-06-16
[patent_effective_date] => 0000-00-00
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[patent_figures_cnt] => 3
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0319/20100319357.pdf
[firstpage_image] =>[orig_patent_app_number] => 12816608
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/816608 | Device and a method for starting a turbine engine fitted to a helicopter, making use of an electrical energy source that includes discharge booster members | Jun 15, 2010 | Issued |
Array
(
[id] => 7576044
[patent_doc_number] => 20110289926
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-12-01
[patent_title] => 'EXTRUDED FLUID MANIFOLD FOR GAS TURBOMACHINE COMBUSTOR CASING'
[patent_app_type] => utility
[patent_app_number] => 12/791341
[patent_app_country] => US
[patent_app_date] => 2010-06-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[pdf_file] => publications/A1/0289/20110289926.pdf
[firstpage_image] =>[orig_patent_app_number] => 12791341
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/791341 | Extruded fluid manifold for gas turbomachine combustor casing | May 31, 2010 | Issued |
Array
(
[id] => 7576051
[patent_doc_number] => 20110289933
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-12-01
[patent_title] => 'Hybrid Prefilming Airblast, Prevaporizing, Lean-Premixing Dual-Fuel Nozzle for a Gas Turbine Combustor'
[patent_app_type] => utility
[patent_app_number] => 12/787990
[patent_app_country] => US
[patent_app_date] => 2010-05-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[pdf_file] => publications/A1/0289/20110289933.pdf
[firstpage_image] =>[orig_patent_app_number] => 12787990
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/787990 | Hybrid prefilming airblast, prevaporizing, lean-premixing dual-fuel nozzle for gas turbine combustor | May 25, 2010 | Issued |
Array
(
[id] => 6571336
[patent_doc_number] => 20100307159
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-12-09
[patent_title] => 'FUEL INJECTOR FOR A GAS TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 12/785707
[patent_app_country] => US
[patent_app_date] => 2010-05-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
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[firstpage_image] =>[orig_patent_app_number] => 12785707
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/785707 | Fuel injector for a gas turbine engine | May 23, 2010 | Issued |
Array
(
[id] => 7563645
[patent_doc_number] => 20110283708
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-11-24
[patent_title] => 'LANDFILL GAS UTILIZATION'
[patent_app_type] => utility
[patent_app_number] => 12/786361
[patent_app_country] => US
[patent_app_date] => 2010-05-24
[patent_effective_date] => 0000-00-00
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[firstpage_image] =>[orig_patent_app_number] => 12786361
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/786361 | LANDFILL GAS UTILIZATION | May 23, 2010 | Abandoned |
Array
(
[id] => 9935060
[patent_doc_number] => 08984853
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-03-24
[patent_title] => 'Accessing a valve assembly of a turbomachine'
[patent_app_type] => utility
[patent_app_number] => 12/784731
[patent_app_country] => US
[patent_app_date] => 2010-05-21
[patent_effective_date] => 0000-00-00
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/784731 | Accessing a valve assembly of a turbomachine | May 20, 2010 | Issued |
Array
(
[id] => 7582932
[patent_doc_number] => 20110277442
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-11-17
[patent_title] => 'Seal for Gas Turbine Filter'
[patent_app_type] => utility
[patent_app_number] => 12/778982
[patent_app_country] => US
[patent_app_date] => 2010-05-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[pdf_file] => publications/A1/0277/20110277442.pdf
[firstpage_image] =>[orig_patent_app_number] => 12778982
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/778982 | Seal for Gas Turbine Filter | May 11, 2010 | Abandoned |
Array
(
[id] => 6252610
[patent_doc_number] => 20100293920
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-11-25
[patent_title] => 'PROPFAN ENGINE'
[patent_app_type] => utility
[patent_app_number] => 12/777582
[patent_app_country] => US
[patent_app_date] => 2010-05-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[pdf_file] => publications/A1/0293/20100293920.pdf
[firstpage_image] =>[orig_patent_app_number] => 12777582
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/777582 | Propfan engine | May 10, 2010 | Issued |
Array
(
[id] => 7557848
[patent_doc_number] => 20110271679
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-11-10
[patent_title] => 'Liquid Fuel System and Method'
[patent_app_type] => utility
[patent_app_number] => 12/773053
[patent_app_country] => US
[patent_app_date] => 2010-05-04
[patent_effective_date] => 0000-00-00
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[pdf_file] => publications/A1/0271/20110271679.pdf
[firstpage_image] =>[orig_patent_app_number] => 12773053
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/773053 | Liquid fuel system and method | May 3, 2010 | Issued |
Array
(
[id] => 9501203
[patent_doc_number] => 08739509
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-06-03
[patent_title] => 'Single shaft combined cycle power plant start-up method and single shaft combined cycle power plant'
[patent_app_type] => utility
[patent_app_number] => 12/772556
[patent_app_country] => US
[patent_app_date] => 2010-05-03
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/772556 | Single shaft combined cycle power plant start-up method and single shaft combined cycle power plant | May 2, 2010 | Issued |
Array
(
[id] => 9501205
[patent_doc_number] => 08739511
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2014-06-03
[patent_title] => 'Can-annular combustor with staged and tangential fuel-air nozzles for use on gas turbine engines'
[patent_app_type] => utility
[patent_app_number] => 12/772353
[patent_app_country] => US
[patent_app_date] => 2010-05-03
[patent_effective_date] => 0000-00-00
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/772353 | Can-annular combustor with staged and tangential fuel-air nozzles for use on gas turbine engines | May 2, 2010 | Issued |
Array
(
[id] => 6181450
[patent_doc_number] => 20110167795
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-07-14
[patent_title] => 'NANOTHERMITE THRUSTERS WITH A NANOTHERMITE PROPELLANT'
[patent_app_type] => utility
[patent_app_number] => 12/763809
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/763809 | NANOTHERMITE THRUSTERS WITH A NANOTHERMITE PROPELLANT | Apr 19, 2010 | Abandoned |
Array
(
[id] => 7700643
[patent_doc_number] => 20110225947
[patent_country] => US
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[patent_issue_date] => 2011-09-22
[patent_title] => 'SYSTEM AND METHODS FOR ALTERING AIR FLOW IN A COMBUSTOR'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/725602 | SYSTEM AND METHODS FOR ALTERING AIR FLOW IN A COMBUSTOR | Mar 16, 2010 | Abandoned |
Array
(
[id] => 6009344
[patent_doc_number] => 20110219741
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-09-15
[patent_title] => 'DETERMINING FAN PARAMETERS THROUGH PRESSURE MONITORING'
[patent_app_type] => utility
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/723835 | Determining fan parameters through pressure monitoring | Mar 14, 2010 | Issued |
Array
(
[id] => 6009377
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[patent_title] => 'CIRCUMFERENTIALLY VARIED QUENCH JET ARRANGEMENT FOR GAS TURBINE COMBUSTORS'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/720431 | Circumferentially varied quench jet arrangement for gas turbine combustors | Mar 8, 2010 | Issued |
Array
(
[id] => 6087598
[patent_doc_number] => 20110217157
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-09-08
[patent_title] => 'CONTROL VALVE WITH RADIAL SEALS'
[patent_app_type] => utility
[patent_app_number] => 12/718665
[patent_app_country] => US
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/718665 | Control valve with radial seals | Mar 4, 2010 | Issued |
Array
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Array
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Array
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/652021 | System for providing air flow to a sulfur recovery unit | Jan 3, 2010 | Issued |
Array
(
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/645998 | GAS TURBINE ENGINE | Dec 22, 2009 | Abandoned |