
Valerie Lynn Woodward
Examiner (ID: 8835, Phone: (571)270-1479 , Office: P/3771 )
| Most Active Art Unit | 3771 |
| Art Unit(s) | 3785, 3771 |
| Total Applications | 995 |
| Issued Applications | 694 |
| Pending Applications | 59 |
| Abandoned Applications | 258 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 7564597
[patent_doc_number] => 20110284660
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-11-24
[patent_title] => 'THRUST REVERSER FOR A TURBOFAN ENGINE NACELLE'
[patent_app_type] => utility
[patent_app_number] => 13/131292
[patent_app_country] => US
[patent_app_date] => 2009-11-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0284/20110284660.pdf
[firstpage_image] =>[orig_patent_app_number] => 13131292
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/131292 | Thrust reverser for a turbofan engine nacelle | Nov 22, 2009 | Issued |
Array
(
[id] => 9181914
[patent_doc_number] => 08621840
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-01-07
[patent_title] => 'Control device and method of a gas turbine electric energy production plant'
[patent_app_type] => utility
[patent_app_number] => 12/601258
[patent_app_country] => US
[patent_app_date] => 2009-11-21
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12601258
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/601258 | Control device and method of a gas turbine electric energy production plant | Nov 20, 2009 | Issued |
Array
(
[id] => 6511462
[patent_doc_number] => 20100122519
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-05-20
[patent_title] => 'ULTRA-LOW SULFUR FUEL AND METHOD FOR REDUCED CONTRAIL FORMATION'
[patent_app_type] => utility
[patent_app_number] => 12/614640
[patent_app_country] => US
[patent_app_date] => 2009-11-09
[patent_effective_date] => 0000-00-00
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[pdf_file] => publications/A1/0122/20100122519.pdf
[firstpage_image] =>[orig_patent_app_number] => 12614640
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/614640 | ULTRA-LOW SULFUR FUEL AND METHOD FOR REDUCED CONTRAIL FORMATION | Nov 8, 2009 | Abandoned |
Array
(
[id] => 6384502
[patent_doc_number] => 20100162712
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-07-01
[patent_title] => 'QUENCH JET ARRANGEMENT FOR ANNULAR RICH-QUENCH-LEAN GAS TURBINE COMBUSTORS'
[patent_app_type] => utility
[patent_app_number] => 12/607815
[patent_app_country] => US
[patent_app_date] => 2009-10-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
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[pdf_file] => publications/A1/0162/20100162712.pdf
[firstpage_image] =>[orig_patent_app_number] => 12607815
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/607815 | Quench jet arrangement for annular rich-quench-lean gas turbine combustors | Oct 27, 2009 | Issued |
Array
(
[id] => 9399492
[patent_doc_number] => 08689537
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2014-04-08
[patent_title] => 'Micro-cavity discharge thruster (MCDT)'
[patent_app_type] => utility
[patent_app_number] => 12/589182
[patent_app_country] => US
[patent_app_date] => 2009-10-19
[patent_effective_date] => 0000-00-00
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/589182 | Micro-cavity discharge thruster (MCDT) | Oct 18, 2009 | Issued |
Array
(
[id] => 9501202
[patent_doc_number] => 08739508
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2014-06-03
[patent_title] => 'Shock cancellation mechanism for the control of unsteady interaction in contra-rotating high- and low-pressure turbines'
[patent_app_type] => utility
[patent_app_number] => 12/569015
[patent_app_country] => US
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12569015
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/569015 | Shock cancellation mechanism for the control of unsteady interaction in contra-rotating high- and low-pressure turbines | Sep 28, 2009 | Issued |
Array
(
[id] => 5970183
[patent_doc_number] => 20110067377
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-03-24
[patent_title] => 'GAS TURBINE COMBUSTION DYNAMICS CONTROL SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 12/562158
[patent_app_country] => US
[patent_app_date] => 2009-09-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[firstpage_image] =>[orig_patent_app_number] => 12562158
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/562158 | GAS TURBINE COMBUSTION DYNAMICS CONTROL SYSTEM | Sep 17, 2009 | Abandoned |
Array
(
[id] => 9438607
[patent_doc_number] => 08707705
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-04-29
[patent_title] => 'Impingement cooled transition piece aft frame'
[patent_app_type] => utility
[patent_app_number] => 12/553153
[patent_app_country] => US
[patent_app_date] => 2009-09-03
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/553153 | Impingement cooled transition piece aft frame | Sep 2, 2009 | Issued |
Array
(
[id] => 6096619
[patent_doc_number] => 20110162387
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-07-07
[patent_title] => 'TURBINE COOLING SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 13/119291
[patent_app_country] => US
[patent_app_date] => 2009-08-19
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/119291 | Turbine cooling system | Aug 18, 2009 | Issued |
Array
(
[id] => 6445002
[patent_doc_number] => 20100038455
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-02-18
[patent_title] => 'LIQUID EJECTOR'
[patent_app_type] => utility
[patent_app_number] => 12/508160
[patent_app_country] => US
[patent_app_date] => 2009-07-23
[patent_effective_date] => 0000-00-00
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[pdf_file] => publications/A1/0038/20100038455.pdf
[firstpage_image] =>[orig_patent_app_number] => 12508160
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/508160 | LIQUID EJECTOR | Jul 22, 2009 | Abandoned |
Array
(
[id] => 9373506
[patent_doc_number] => 08677754
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[patent_kind] => B2
[patent_issue_date] => 2014-03-25
[patent_title] => 'Fuel supply system for a gas-turbine engine'
[patent_app_type] => utility
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/501602 | Fuel supply system for a gas-turbine engine | Jul 12, 2009 | Issued |
Array
(
[id] => 9243294
[patent_doc_number] => 08607569
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[patent_kind] => B2
[patent_issue_date] => 2013-12-17
[patent_title] => 'Methods and systems to thermally protect fuel nozzles in combustion systems'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/495918 | Methods and systems to thermally protect fuel nozzles in combustion systems | Jun 30, 2009 | Issued |
Array
(
[id] => 6322200
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[patent_title] => 'SYSTEM AND METHOD FOR ASSEMBLING A THRUST REVERSER FOR A GAS TURBINE PROPULSION SYSTEM'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/495248 | System and method for assembling a thrust reverser for a gas turbine propulsion system | Jun 29, 2009 | Issued |
Array
(
[id] => 5460293
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[patent_title] => 'METHOD FOR PRIMARY CONTROL OF A COMBINED GAS AND STEAM TURBINE ARRANGEMENT'
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Array
(
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/993398 | Lean fuel intake gas turbine system | Jun 9, 2009 | Issued |
Array
(
[id] => 6345843
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[patent_title] => 'Combustor Apparatus for Use in a Gas Turbine Engine'
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Array
(
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Array
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Array
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Array
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/428582 | Passive boundary layer bleed system for nacelle inlet airflow control | Apr 22, 2009 | Issued |