
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] => 6244683
[patent_doc_number] => 20100024431
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-02-04
[patent_title] => 'METHOD OF DETECTING A PARTIAL FLAME FAILURE IN A GAS TURBINE ENGINE AND A GAS TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 12/524788
[patent_app_country] => US
[patent_app_date] => 2008-01-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 5030
[patent_no_of_claims] => 21
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[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0024/20100024431.pdf
[firstpage_image] =>[orig_patent_app_number] => 12524788
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/524788 | Method of detecting a partial flame failure in a gas turbine engine and a gas turbine engine | Jan 27, 2008 | Issued |
Array
(
[id] => 7794016
[patent_doc_number] => 08122720
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-02-28
[patent_title] => 'Fuel nozzle apparatus, gas turbine, and method of controlling fuel nozzle apparatus'
[patent_app_type] => utility
[patent_app_number] => 12/010393
[patent_app_country] => US
[patent_app_date] => 2008-01-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 12
[patent_no_of_words] => 12846
[patent_no_of_claims] => 10
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[patent_words_short_claim] => 258
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/122/08122720.pdf
[firstpage_image] =>[orig_patent_app_number] => 12010393
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/010393 | Fuel nozzle apparatus, gas turbine, and method of controlling fuel nozzle apparatus | Jan 23, 2008 | Issued |
Array
(
[id] => 5352148
[patent_doc_number] => 20090183492
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-07-23
[patent_title] => 'COMBUSTION LEAN-BLOWOUT PROTECTION VIA NOZZLE EQUIVALENCE RATIO CONTROL'
[patent_app_type] => utility
[patent_app_number] => 12/017507
[patent_app_country] => US
[patent_app_date] => 2008-01-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 1624
[patent_no_of_claims] => 20
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0183/20090183492.pdf
[firstpage_image] =>[orig_patent_app_number] => 12017507
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/017507 | COMBUSTION LEAN-BLOWOUT PROTECTION VIA NOZZLE EQUIVALENCE RATIO CONTROL | Jan 21, 2008 | Abandoned |
Array
(
[id] => 8824503
[patent_doc_number] => 20130125548
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-05-23
[patent_title] => 'FLOW CONDITIONER FOR FUEL INJECTOR FOR COMBUSTOR AND METHOD FOR LOW-NOx COMBUSTOR'
[patent_app_type] => utility
[patent_app_number] => 12/015366
[patent_app_country] => US
[patent_app_date] => 2008-01-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 3308
[patent_no_of_claims] => 20
[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] =>[firstpage_image] =>[orig_patent_app_number] => 12015366
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/015366 | Flow conditioner for fuel injector for combustor and method for low-NOx combustor | Jan 15, 2008 | Issued |
Array
(
[id] => 5430851
[patent_doc_number] => 20090165436
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-07-02
[patent_title] => 'Premixed, preswirled plasma-assisted pilot'
[patent_app_type] => utility
[patent_app_number] => 12/005807
[patent_app_country] => US
[patent_app_date] => 2007-12-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 4473
[patent_no_of_claims] => 61
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0165/20090165436.pdf
[firstpage_image] =>[orig_patent_app_number] => 12005807
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/005807 | Premixed, preswirled plasma-assisted pilot | Dec 27, 2007 | Abandoned |
Array
(
[id] => 7499740
[patent_doc_number] => 08033095
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-10-11
[patent_title] => 'Drive device on the basis of a gel-type propellant and method for conveying propellant'
[patent_app_type] => utility
[patent_app_number] => 12/005651
[patent_app_country] => US
[patent_app_date] => 2007-12-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_no_of_words] => 4542
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/033/08033095.pdf
[firstpage_image] =>[orig_patent_app_number] => 12005651
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/005651 | Drive device on the basis of a gel-type propellant and method for conveying propellant | Dec 26, 2007 | Issued |
Array
(
[id] => 6528779
[patent_doc_number] => 20100043448
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-02-25
[patent_title] => 'GAS TURBINE ENGINE COMBUSTOR AND METHOD FOR DELIVERING PURGE GAS INTO A COMBUSTION CHAMBER OF THE COMBUSTOR'
[patent_app_type] => utility
[patent_app_number] => 11/965397
[patent_app_country] => US
[patent_app_date] => 2007-12-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 4808
[patent_no_of_claims] => 20
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0043/20100043448.pdf
[firstpage_image] =>[orig_patent_app_number] => 11965397
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/965397 | Gas turbine engine combustor and method for delivering purge gas into a combustion chamber of the combustor | Dec 26, 2007 | Issued |
Array
(
[id] => 9284121
[patent_doc_number] => 08640439
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-02-04
[patent_title] => 'Hybrid drive for an aircraft'
[patent_app_type] => utility
[patent_app_number] => 11/998437
[patent_app_country] => US
[patent_app_date] => 2007-11-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 3601
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 11998437
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/998437 | Hybrid drive for an aircraft | Nov 28, 2007 | Issued |
Array
(
[id] => 5571880
[patent_doc_number] => 20090139239
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-06-04
[patent_title] => 'QUENCH JET ARRANGEMENT FOR ANNULAR RICH-QUENCH-LEAN GAS TURBINE COMBUSTORS'
[patent_app_type] => utility
[patent_app_number] => 11/947337
[patent_app_country] => US
[patent_app_date] => 2007-11-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0139/20090139239.pdf
[firstpage_image] =>[orig_patent_app_number] => 11947337
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/947337 | Quench jet arrangement for annular rich-quench-lean gas turbine combustors | Nov 28, 2007 | Issued |
Array
(
[id] => 6315056
[patent_doc_number] => 20100242488
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-09-30
[patent_title] => ' GAS TURBINE ENGINE AND METHOD OF OPERATION'
[patent_app_type] => utility
[patent_app_number] => 12/742031
[patent_app_country] => US
[patent_app_date] => 2007-11-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0242/20100242488.pdf
[firstpage_image] =>[orig_patent_app_number] => 12742031
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/742031 | GAS TURBINE ENGINE AND METHOD OF OPERATION | Nov 28, 2007 | Abandoned |
Array
(
[id] => 4900764
[patent_doc_number] => 20080110175
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-05-15
[patent_title] => 'Cowling for connecting a hot gas source to a stirling engine or a turbine'
[patent_app_type] => utility
[patent_app_number] => 11/983517
[patent_app_country] => US
[patent_app_date] => 2007-11-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
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[patent_no_of_words] => 5488
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[pdf_file] => publications/A1/0110/20080110175.pdf
[firstpage_image] =>[orig_patent_app_number] => 11983517
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/983517 | Cowling for connecting a hot gas source to a stirling engine or a turbine | Nov 9, 2007 | Abandoned |
Array
(
[id] => 6548843
[patent_doc_number] => 20100058730
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-03-11
[patent_title] => 'GAS TURBINE POWER GENERATION SYSTEM AND METHOD OF DETECTING CALORIFIC ABNORMALITY OF THE SAME'
[patent_app_type] => utility
[patent_app_number] => 12/306832
[patent_app_country] => US
[patent_app_date] => 2007-11-09
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/306832 | GAS TURBINE POWER GENERATION SYSTEM AND METHOD OF DETECTING CALORIFIC ABNORMALITY OF THE SAME | Nov 8, 2007 | Abandoned |
Array
(
[id] => 5262055
[patent_doc_number] => 20090114740
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-05-07
[patent_title] => 'NOZZLE ASSEMBLY WITH FLOW CONDUITS'
[patent_app_type] => utility
[patent_app_number] => 11/933537
[patent_app_country] => US
[patent_app_date] => 2007-11-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[pdf_file] => publications/A1/0114/20090114740.pdf
[firstpage_image] =>[orig_patent_app_number] => 11933537
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/933537 | Nozzle assembly with flow conduits | Oct 31, 2007 | Issued |
Array
(
[id] => 5298834
[patent_doc_number] => 20090293486
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-12-03
[patent_title] => 'COMBUSTORS WITH IGNITERS HAVING PROTRUSIONS'
[patent_app_type] => utility
[patent_app_number] => 11/925347
[patent_app_country] => US
[patent_app_date] => 2007-10-26
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[firstpage_image] =>[orig_patent_app_number] => 11925347
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/925347 | COMBUSTORS WITH IGNITERS HAVING PROTRUSIONS | Oct 25, 2007 | Abandoned |
Array
(
[id] => 8338203
[patent_doc_number] => 08240120
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-08-14
[patent_title] => 'Vibration management for gas turbine engines'
[patent_app_type] => utility
[patent_app_number] => 11/923897
[patent_app_country] => US
[patent_app_date] => 2007-10-25
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 11923897
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/923897 | Vibration management for gas turbine engines | Oct 24, 2007 | Issued |
Array
(
[id] => 9993811
[patent_doc_number] => 09038392
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-05-26
[patent_title] => 'Gas turbine combustor'
[patent_app_type] => utility
[patent_app_number] => 12/446402
[patent_app_country] => US
[patent_app_date] => 2007-10-17
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/446402 | Gas turbine combustor | Oct 16, 2007 | Issued |
Array
(
[id] => 5406197
[patent_doc_number] => 20090120095
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-05-14
[patent_title] => 'Combustion liner thimble insert and related method'
[patent_app_type] => utility
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[rel_patent_id] =>[rel_patent_doc_number] =>) 11/907332 | Combustion liner thimble insert and related method | Oct 10, 2007 | Issued |
Array
(
[id] => 4731473
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[patent_title] => 'TURBINE INSTALLATION HAVING A CONNECTABLE AUXILIARY GROUP'
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[firstpage_image] =>[orig_patent_app_number] => 11863617
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/863617 | Turbine installation having a connectable auxiliary group | Sep 27, 2007 | Issued |
Array
(
[id] => 8537011
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[patent_title] => 'Vibration damper'
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 11862163
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/862163 | Vibration damper | Sep 25, 2007 | Issued |
Array
(
[id] => 5504766
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[patent_kind] => A1
[patent_issue_date] => 2009-03-26
[patent_title] => 'TOROIDAL RING MANIFOLD FOR SECONDARY FUEL NOZZLE OF A DLN GAS TURBINE'
[patent_app_type] => utility
[patent_app_number] => 11/859087
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[pdf_file] => publications/A1/0077/20090077972.pdf
[firstpage_image] =>[orig_patent_app_number] => 11859087
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/859087 | TOROIDAL RING MANIFOLD FOR SECONDARY FUEL NOZZLE OF A DLN GAS TURBINE | Sep 20, 2007 | Abandoned |