Search

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 numberTitle of the applicationFiling DateStatus
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 [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] => 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 [patent_no_of_ind_claims] => 5 [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 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 0 [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 [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/A1/0165/20090165436.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 [patent_figures_cnt] => 4 [patent_no_of_words] => 4542 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 146 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [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] => 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 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 171 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_figures_cnt] => 4 [patent_no_of_words] => 3267 [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] => 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 [patent_figures_cnt] => 6 [patent_no_of_words] => 3809 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_figures_cnt] => 10 [patent_no_of_words] => 5488 [patent_no_of_claims] => 27 [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/A1/0110/20080110175.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 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 16 [patent_figures_cnt] => 16 [patent_no_of_words] => 8573 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 6 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0058/20100058730.pdf [firstpage_image] =>[orig_patent_app_number] => 12306832 [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 [patent_figures_cnt] => 3 [patent_no_of_words] => 1283 [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] => 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 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2685 [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] => publications/A1/0293/20090293486.pdf [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 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 4 [patent_no_of_words] => 2672 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 132 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [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 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 18 [patent_no_of_words] => 5067 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 303 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12446402 [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 [patent_app_number] => 11/907332 [patent_app_country] => US [patent_app_date] => 2007-10-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 2268 [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] => publications/A1/0120/20090120095.pdf [firstpage_image] =>[orig_patent_app_number] => 11907332 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/907332
Combustion liner thimble insert and related method Oct 10, 2007 Issued
Array ( [id] => 4731473 [patent_doc_number] => 20080048451 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-02-28 [patent_title] => 'TURBINE INSTALLATION HAVING A CONNECTABLE AUXILIARY GROUP' [patent_app_type] => utility [patent_app_number] => 11/863617 [patent_app_country] => US [patent_app_date] => 2007-09-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 11 [patent_no_of_words] => 10784 [patent_no_of_claims] => 25 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0048/20080048451.pdf [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 [patent_doc_number] => 08312727 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-11-20 [patent_title] => 'Vibration damper' [patent_app_type] => utility [patent_app_number] => 11/862163 [patent_app_country] => US [patent_app_date] => 2007-09-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 8 [patent_no_of_words] => 4695 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 138 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [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 [patent_doc_number] => 20090077972 [patent_country] => US [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 [patent_app_country] => US [patent_app_date] => 2007-09-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 11 [patent_no_of_words] => 5646 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [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
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