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] => 7799260 [patent_doc_number] => 08127525 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-03-06 [patent_title] => 'System for dissipating energy in the event of a turbine shaft breaking in a gas turbine engine' [patent_app_type] => utility [patent_app_number] => 12/126407 [patent_app_country] => US [patent_app_date] => 2008-05-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 2 [patent_no_of_words] => 1966 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 227 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/08/127/08127525.pdf [firstpage_image] =>[orig_patent_app_number] => 12126407 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/126407
System for dissipating energy in the event of a turbine shaft breaking in a gas turbine engine May 22, 2008 Issued
Array ( [id] => 6482682 [patent_doc_number] => 20100199627 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-08-12 [patent_title] => 'Gas Turbo Set and Method for Controlling a Gas Turbo Set' [patent_app_type] => utility [patent_app_number] => 12/601055 [patent_app_country] => US [patent_app_date] => 2008-05-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 3174 [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/A1/0199/20100199627.pdf [firstpage_image] =>[orig_patent_app_number] => 12601055 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/601055
Gas turbo set and method for controlling a gas turbo set May 15, 2008 Issued
Array ( [id] => 6497009 [patent_doc_number] => 20100218481 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-09-02 [patent_title] => 'TWO-PULSE ROCKET MOTOR' [patent_app_type] => utility [patent_app_number] => 12/599874 [patent_app_country] => US [patent_app_date] => 2008-05-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 6077 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0218/20100218481.pdf [firstpage_image] =>[orig_patent_app_number] => 12599874 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/599874
Two-pulse rocket motor May 8, 2008 Issued
Array ( [id] => 6236873 [patent_doc_number] => 20100132330 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-06-03 [patent_title] => 'METHOD AND APPARATUS FOR SUPPRESSING AEROENGINE CONTRAILS' [patent_app_type] => utility [patent_app_number] => 12/451503 [patent_app_country] => US [patent_app_date] => 2008-04-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 3002 [patent_no_of_claims] => 18 [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/A1/0132/20100132330.pdf [firstpage_image] =>[orig_patent_app_number] => 12451503 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/451503
Method and apparatus for suppressing aeroengine contrails Apr 27, 2008 Issued
Array ( [id] => 5455116 [patent_doc_number] => 20090255268 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-10-15 [patent_title] => 'Divergent cooling thimbles for combustor liners and related method' [patent_app_type] => utility [patent_app_number] => 12/081167 [patent_app_country] => US [patent_app_date] => 2008-04-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 1867 [patent_no_of_claims] => 17 [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/A1/0255/20090255268.pdf [firstpage_image] =>[orig_patent_app_number] => 12081167 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/081167
Divergent cooling thimbles for combustor liners and related method Apr 10, 2008 Abandoned
Array ( [id] => 9164646 [patent_doc_number] => 08590316 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-11-26 [patent_title] => 'CMC mixer with structural outer cowling' [patent_app_type] => utility [patent_app_number] => 12/594874 [patent_app_country] => US [patent_app_date] => 2008-04-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 11 [patent_no_of_words] => 4095 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 142 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12594874 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/594874
CMC mixer with structural outer cowling Apr 7, 2008 Issued
Array ( [id] => 5468381 [patent_doc_number] => 20090241547 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-10-01 [patent_title] => 'Gas turbine fuel injector for lower heating capacity fuels' [patent_app_type] => utility [patent_app_number] => 12/078407 [patent_app_country] => US [patent_app_date] => 2008-03-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 5445 [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/A1/0241/20090241547.pdf [firstpage_image] =>[orig_patent_app_number] => 12078407 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/078407
Gas turbine fuel injector for lower heating capacity fuels Mar 30, 2008 Abandoned
Array ( [id] => 5306368 [patent_doc_number] => 20090013664 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-01-15 [patent_title] => 'Actuator Arrangement' [patent_app_type] => utility [patent_app_number] => 12/057497 [patent_app_country] => US [patent_app_date] => 2008-03-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 1784 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0013/20090013664.pdf [firstpage_image] =>[orig_patent_app_number] => 12057497 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/057497
Thrust reverser and VAFN arrangement Mar 27, 2008 Issued
Array ( [id] => 4678845 [patent_doc_number] => 20080245071 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-10-09 [patent_title] => 'THERMAL POWER PLANT' [patent_app_type] => utility [patent_app_number] => 12/056805 [patent_app_country] => US [patent_app_date] => 2008-03-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 10993 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0245/20080245071.pdf [firstpage_image] =>[orig_patent_app_number] => 12056805 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/056805
THERMAL POWER PLANT Mar 26, 2008 Abandoned
Array ( [id] => 4678848 [patent_doc_number] => 20080245074 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-10-09 [patent_title] => 'Combustor of a gas turbine engine' [patent_app_type] => utility [patent_app_number] => 12/076087 [patent_app_country] => US [patent_app_date] => 2008-03-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 11 [patent_no_of_words] => 6281 [patent_no_of_claims] => 7 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0245/20080245074.pdf [firstpage_image] =>[orig_patent_app_number] => 12076087 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/076087
Combustor of a gas turbine engine Mar 12, 2008 Issued
Array ( [id] => 5381957 [patent_doc_number] => 20090223201 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-09-10 [patent_title] => 'Methods of Injecting Diluent Into A Gas Turbine Assembly' [patent_app_type] => utility [patent_app_number] => 12/045497 [patent_app_country] => US [patent_app_date] => 2008-03-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 3322 [patent_no_of_claims] => 16 [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/A1/0223/20090223201.pdf [firstpage_image] =>[orig_patent_app_number] => 12045497 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/045497
Methods of Injecting Diluent Into A Gas Turbine Assembly Mar 9, 2008 Abandoned
Array ( [id] => 7769866 [patent_doc_number] => 08117847 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-02-21 [patent_title] => 'Hybrid missile propulsion system with reconfigurable multinozzle grid' [patent_app_type] => utility [patent_app_number] => 12/044227 [patent_app_country] => US [patent_app_date] => 2008-03-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 20 [patent_no_of_words] => 4388 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 117 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/08/117/08117847.pdf [firstpage_image] =>[orig_patent_app_number] => 12044227 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/044227
Hybrid missile propulsion system with reconfigurable multinozzle grid Mar 6, 2008 Issued
Array ( [id] => 5381983 [patent_doc_number] => 20090223227 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-09-10 [patent_title] => 'Combustion cap with crown mixing holes' [patent_app_type] => utility [patent_app_number] => 12/073407 [patent_app_country] => US [patent_app_date] => 2008-03-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 2346 [patent_no_of_claims] => 18 [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/A1/0223/20090223227.pdf [firstpage_image] =>[orig_patent_app_number] => 12073407 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/073407
Combustion cap with crown mixing holes Mar 4, 2008 Abandoned
Array ( [id] => 6181448 [patent_doc_number] => 20110167794 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-07-14 [patent_title] => 'Multi-Functional Pulse-Divided Rocket' [patent_app_type] => utility [patent_app_number] => 12/041797 [patent_app_country] => US [patent_app_date] => 2008-03-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 4678 [patent_no_of_claims] => 13 [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/A1/0167/20110167794.pdf [firstpage_image] =>[orig_patent_app_number] => 12041797 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/041797
Multi-functional pulse-divided rocket Mar 3, 2008 Issued
Array ( [id] => 8196828 [patent_doc_number] => 08186145 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-05-29 [patent_title] => 'Rocket nozzles for unconventional vehicles' [patent_app_type] => utility [patent_app_number] => 12/072487 [patent_app_country] => US [patent_app_date] => 2008-02-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 13 [patent_figures_cnt] => 14 [patent_no_of_words] => 3321 [patent_no_of_claims] => 3 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 160 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/08/186/08186145.pdf [firstpage_image] =>[orig_patent_app_number] => 12072487 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/072487
Rocket nozzles for unconventional vehicles Feb 25, 2008 Issued
Array ( [id] => 5388029 [patent_doc_number] => 20090205341 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-08-20 [patent_title] => 'GAS TURBINE ENGINE WITH TWIN TOWERSHAFT ACCESSORY GEARBOX' [patent_app_type] => utility [patent_app_number] => 12/033902 [patent_app_country] => US [patent_app_date] => 2008-02-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 1516 [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/A1/0205/20090205341.pdf [firstpage_image] =>[orig_patent_app_number] => 12033902 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/033902
GAS TURBINE ENGINE WITH TWIN TOWERSHAFT ACCESSORY GEARBOX Feb 19, 2008 Abandoned
Array ( [id] => 5476582 [patent_doc_number] => 20090199563 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-08-13 [patent_title] => 'Scalable pyrospin combustor' [patent_app_type] => utility [patent_app_number] => 12/069107 [patent_app_country] => US [patent_app_date] => 2008-02-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 5556 [patent_no_of_claims] => 24 [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/A1/0199/20090199563.pdf [firstpage_image] =>[orig_patent_app_number] => 12069107 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/069107
Scalable pyrospin combustor Feb 6, 2008 Abandoned
Array ( [id] => 6213638 [patent_doc_number] => 20100050591 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-03-04 [patent_title] => 'Method for automatic closed-loop control of one or more combustion temperatures in a gas turbine installation and method for determination of the water content in the working fluid of a gas turbine instalation' [patent_app_type] => utility [patent_app_number] => 12/068337 [patent_app_country] => US [patent_app_date] => 2008-02-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 4377 [patent_no_of_claims] => 28 [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/A1/0050/20100050591.pdf [firstpage_image] =>[orig_patent_app_number] => 12068337 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/068337
Method for automatic closed-loop control of one or more combustion temperatures in a gas turbine installation and method for determination of the water content in the working fluid of a gas turbine installation Feb 4, 2008 Issued
Array ( [id] => 5523733 [patent_doc_number] => 20090193809 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-08-06 [patent_title] => 'METHOD AND SYSTEM TO FACILITATE COMBINED CYCLE WORKING FLUID MODIFICATION AND COMBUSTION THEREOF' [patent_app_type] => utility [patent_app_number] => 12/025437 [patent_app_country] => US [patent_app_date] => 2008-02-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2963 [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/A1/0193/20090193809.pdf [firstpage_image] =>[orig_patent_app_number] => 12025437 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/025437
METHOD AND SYSTEM TO FACILITATE COMBINED CYCLE WORKING FLUID MODIFICATION AND COMBUSTION THEREOF Feb 3, 2008 Abandoned
Array ( [id] => 6578109 [patent_doc_number] => 20100000221 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-01-07 [patent_title] => 'Method for producing fuel and power from a methane hydrate bed using a gas turbine engine' [patent_app_type] => utility [patent_app_number] => 12/012397 [patent_app_country] => US [patent_app_date] => 2008-01-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 1109 [patent_no_of_claims] => 16 [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/A1/0000/20100000221.pdf [firstpage_image] =>[orig_patent_app_number] => 12012397 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/012397
Method for producing fuel and power from a methane hydrate bed using a gas turbine engine Jan 30, 2008 Abandoned
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