
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] => 9955618
[patent_doc_number] => 09003800
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-04-14
[patent_title] => 'Gas turbine combustor'
[patent_app_type] => utility
[patent_app_number] => 13/539559
[patent_app_country] => US
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Array
(
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Array
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Array
(
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[patent_title] => 'Gas turbine combustor'
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Array
(
[id] => 9948684
[patent_doc_number] => 08997453
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-04-07
[patent_title] => 'Igniter for a turbomachine and mounting assembly therefor'
[patent_app_type] => utility
[patent_app_number] => 13/537461
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/537461 | Igniter for a turbomachine and mounting assembly therefor | Jun 28, 2012 | Issued |
Array
(
[id] => 9258508
[patent_doc_number] => 20130340437
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[patent_kind] => A1
[patent_issue_date] => 2013-12-26
[patent_title] => 'TURBINE ENGINE COMBUSTOR WALL WITH NON-UNIFORM DISTRIBUTION OF EFFUSION APERTURES'
[patent_app_type] => utility
[patent_app_number] => 13/531132
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/531132 | Turbine engine combustor wall with non-uniform distribution of effusion apertures | Jun 21, 2012 | Issued |
Array
(
[id] => 8728933
[patent_doc_number] => 20130074502
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-03-28
[patent_title] => 'TRANSITION PIECE OF COMBUSTOR, GAS TURBINE HAVING THE SAME, AND PRODUCING METHOD FOR TRANSITION PIECE'
[patent_app_type] => utility
[patent_app_number] => 13/526010
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13526010
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/526010 | Transition piece of combustor, gas turbine having the same, and producing method for transition piece | Jun 17, 2012 | Issued |
Array
(
[id] => 9613291
[patent_doc_number] => 20140203148
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-07-24
[patent_title] => 'CRYOGENIC THRUSTER ASSEMBLY'
[patent_app_type] => utility
[patent_app_number] => 14/127055
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/127055 | Cryogenic thruster assembly using regenerative heating from main and settling thrusters | Jun 6, 2012 | Issued |
Array
(
[id] => 8849840
[patent_doc_number] => 20130139515
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-06-06
[patent_title] => 'Integral gas turbine, flywheel, generator, and method for hybrid operation thereof'
[patent_app_type] => utility
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/506962 | Integral gas turbine, flywheel, generator, and method for hybrid operation thereof | May 28, 2012 | Issued |
Array
(
[id] => 9298065
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[patent_issue_date] => 2014-02-11
[patent_title] => 'Segment component in high-temperature casting material for an annular combustion chamber, annular combustion chamber for an aircraft engine, aircraft engine and method for the manufacture of an annular combustion chamber'
[patent_app_type] => utility
[patent_app_number] => 13/480696
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/480696 | Segment component in high-temperature casting material for an annular combustion chamber, annular combustion chamber for an aircraft engine, aircraft engine and method for the manufacture of an annular combustion chamber | May 24, 2012 | Issued |
Array
(
[id] => 9392951
[patent_doc_number] => 20140090357
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[patent_issue_date] => 2014-04-03
[patent_title] => 'HALL-EFFECT THRUSTER'
[patent_app_type] => utility
[patent_app_number] => 14/123175
[patent_app_country] => US
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/123175 | Hall-effect thruster | May 22, 2012 | Issued |
Array
(
[id] => 8498379
[patent_doc_number] => 20120297787
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[patent_issue_date] => 2012-11-29
[patent_title] => 'FLOW STRAIGHTENER AND MIXER'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/469819 | Flow straightener and mixer | May 10, 2012 | Issued |
Array
(
[id] => 9373508
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Array
(
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[patent_title] => 'Reheat burner injection system with fuel lances'
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Array
(
[id] => 8562292
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[patent_title] => 'COOLING SCHEME FOR AN INCREASED GAS TURBINE EFFICIENCY'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/465830 | Cooling scheme for an increased gas turbine efficiency | May 6, 2012 | Issued |
Array
(
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/459783 | GEARED TURBOFAN WITH DISTRIBUTED ACCESSORY GEARBOXES | Apr 29, 2012 | Abandoned |
Array
(
[id] => 10057838
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/459811 | Method for operating a gas turbine power plant with exhaust gas recirculation | Apr 29, 2012 | Issued |
Array
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Array
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Array
(
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[patent_title] => 'VAFN SYSTEMS WITH NOZZLE LOCKING ASSEMBLIES'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/426275 | VAFN SYSTEMS WITH NOZZLE LOCKING ASSEMBLIES | Mar 20, 2012 | Abandoned |