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] => 4935260 [patent_doc_number] => 20080072572 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-03-27 [patent_title] => 'TURBOMACHINE FAN DUCT' [patent_app_type] => utility [patent_app_number] => 11/856297 [patent_app_country] => US [patent_app_date] => 2007-09-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 3409 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 7 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0072/20080072572.pdf [firstpage_image] =>[orig_patent_app_number] => 11856297 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/856297
Turbomachine fan duct Sep 16, 2007 Issued
Array ( [id] => 4929439 [patent_doc_number] => 20080000214 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-01-03 [patent_title] => 'METHOD FOR TUNING VALVES FOR PRIMARY AND SECONDARY FUEL CIRCUIT' [patent_app_type] => utility [patent_app_number] => 11/855638 [patent_app_country] => US [patent_app_date] => 2007-09-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 7369 [patent_no_of_claims] => 23 [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/A1/0000/20080000214.pdf [firstpage_image] =>[orig_patent_app_number] => 11855638 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/855638
Method for tuning valves for primary and secondary fuel circuit Sep 13, 2007 Issued
Array ( [id] => 5281312 [patent_doc_number] => 20090094985 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-04-16 [patent_title] => 'Non-Rectangular Resonator Devices Providing Enhanced Liner Cooling for Combustion Chamber' [patent_app_type] => utility [patent_app_number] => 11/855747 [patent_app_country] => US [patent_app_date] => 2007-09-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 5912 [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/A1/0094/20090094985.pdf [firstpage_image] =>[orig_patent_app_number] => 11855747 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/855747
Non-rectangular resonator devices providing enhanced liner cooling for combustion chamber Sep 13, 2007 Issued
Array ( [id] => 5448619 [patent_doc_number] => 20090064654 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-03-12 [patent_title] => 'Turbine engine with modulated combustion and reheat chambers' [patent_app_type] => utility [patent_app_number] => 11/898257 [patent_app_country] => US [patent_app_date] => 2007-09-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 1779 [patent_no_of_claims] => 19 [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/A1/0064/20090064654.pdf [firstpage_image] =>[orig_patent_app_number] => 11898257 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/898257
Turbine engine with modulated combustion and reheat chambers Sep 10, 2007 Abandoned
Array ( [id] => 9480735 [patent_doc_number] => 08726675 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-05-20 [patent_title] => 'Scalloped flexure ring' [patent_app_type] => utility [patent_app_number] => 11/851667 [patent_app_country] => US [patent_app_date] => 2007-09-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 9 [patent_no_of_words] => 2330 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 152 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 11851667 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/851667
Scalloped flexure ring Sep 6, 2007 Issued
Array ( [id] => 4603629 [patent_doc_number] => 07984607 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2011-07-26 [patent_title] => 'Gas turbine engine systems and related methods involving vane-blade count ratios greater than unity' [patent_app_type] => utility [patent_app_number] => 11/850787 [patent_app_country] => US [patent_app_date] => 2007-09-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 4 [patent_no_of_words] => 2156 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 81 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/984/07984607.pdf [firstpage_image] =>[orig_patent_app_number] => 11850787 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/850787
Gas turbine engine systems and related methods involving vane-blade count ratios greater than unity Sep 5, 2007 Issued
Array ( [id] => 5318352 [patent_doc_number] => 20090056342 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-03-05 [patent_title] => 'Methods and Systems for Gas Turbine Part-Load Operating Conditions' [patent_app_type] => utility [patent_app_number] => 11/849383 [patent_app_country] => US [patent_app_date] => 2007-09-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2126 [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/A1/0056/20090056342.pdf [firstpage_image] =>[orig_patent_app_number] => 11849383 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/849383
Methods and Systems for Gas Turbine Part-Load Operating Conditions Sep 3, 2007 Abandoned
Array ( [id] => 4632743 [patent_doc_number] => 08011188 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2011-09-06 [patent_title] => 'Augmentor with trapped vortex cavity pilot' [patent_app_type] => utility [patent_app_number] => 11/848587 [patent_app_country] => US [patent_app_date] => 2007-08-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 13 [patent_figures_cnt] => 14 [patent_no_of_words] => 5066 [patent_no_of_claims] => 29 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 139 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/08/011/08011188.pdf [firstpage_image] =>[orig_patent_app_number] => 11848587 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/848587
Augmentor with trapped vortex cavity pilot Aug 30, 2007 Issued
Array ( [id] => 4647823 [patent_doc_number] => 20080035078 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-02-14 [patent_title] => 'Method and device of turbine submerged combustion boiler' [patent_app_type] => utility [patent_app_number] => 11/881420 [patent_app_country] => US [patent_app_date] => 2007-07-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 2761 [patent_no_of_claims] => 8 [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/A1/0035/20080035078.pdf [firstpage_image] =>[orig_patent_app_number] => 11881420 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/881420
Method and device of turbine submerged combustion boiler Jul 27, 2007 Issued
Array ( [id] => 5381810 [patent_doc_number] => 20090223054 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-09-10 [patent_title] => 'FUEL NOZZLE FOR A GAS TURBINE ENGINE AND METHOD OF FABRICATING THE SAME' [patent_app_type] => utility [patent_app_number] => 11/828447 [patent_app_country] => US [patent_app_date] => 2007-07-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 5905 [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/A1/0223/20090223054.pdf [firstpage_image] =>[orig_patent_app_number] => 11828447 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/828447
Fuel nozzle assembly for a gas turbine engine Jul 25, 2007 Issued
Array ( [id] => 4736105 [patent_doc_number] => 20080229757 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-09-25 [patent_title] => 'Methods and systems for output variance and facilitation of maintenance of multiple gas turbine plants' [patent_app_type] => utility [patent_app_number] => 11/879317 [patent_app_country] => US [patent_app_date] => 2007-07-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 2680 [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/A1/0229/20080229757.pdf [firstpage_image] =>[orig_patent_app_number] => 11879317 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/879317
Methods and systems for output variance and facilitation of maintenance of multiple gas turbine plants Jul 16, 2007 Issued
Array ( [id] => 78083 [patent_doc_number] => 07743599 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2010-06-29 [patent_title] => 'System and apparatus for gas turbine engine lean blowout avoidance' [patent_app_type] => utility [patent_app_number] => 11/779127 [patent_app_country] => US [patent_app_date] => 2007-07-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 6508 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 127 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/743/07743599.pdf [firstpage_image] =>[orig_patent_app_number] => 11779127 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/779127
System and apparatus for gas turbine engine lean blowout avoidance Jul 16, 2007 Issued
Array ( [id] => 5293582 [patent_doc_number] => 20090008508 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-01-08 [patent_title] => 'VARIABLE CONTOUR NACELLE ASSEMBLY FOR A GAS TURBINE ENGINE' [patent_app_type] => utility [patent_app_number] => 11/772287 [patent_app_country] => US [patent_app_date] => 2007-07-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 3735 [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/A1/0008/20090008508.pdf [firstpage_image] =>[orig_patent_app_number] => 11772287 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/772287
Variable contour nacelle assembly for a gas turbine engine Jul 1, 2007 Issued
Array ( [id] => 5348637 [patent_doc_number] => 20090003998 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-01-01 [patent_title] => 'COMBUSTORS FOR USE IN TURBINE ENGINE ASSEMBLIES' [patent_app_type] => utility [patent_app_number] => 11/769077 [patent_app_country] => US [patent_app_date] => 2007-06-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 3135 [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/A1/0003/20090003998.pdf [firstpage_image] =>[orig_patent_app_number] => 11769077 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/769077
Combustors for use in turbine engine assemblies Jun 26, 2007 Issued
Array ( [id] => 4665999 [patent_doc_number] => 20080041059 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-02-21 [patent_title] => 'Radially staged RQL combustor with tangential fuel premixers' [patent_app_type] => utility [patent_app_number] => 11/820427 [patent_app_country] => US [patent_app_date] => 2007-06-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 5875 [patent_no_of_claims] => 7 [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/A1/0041/20080041059.pdf [firstpage_image] =>[orig_patent_app_number] => 11820427 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/820427
Radially staged RQL combustor with tangential fuel-air premixers Jun 18, 2007 Issued
Array ( [id] => 9045205 [patent_doc_number] => 08539753 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-09-24 [patent_title] => 'Hybrid rocket motor with annular, concentric solid fuel elements' [patent_app_type] => utility [patent_app_number] => 11/764677 [patent_app_country] => US [patent_app_date] => 2007-06-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 4 [patent_no_of_words] => 2134 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 165 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 11764677 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/764677
Hybrid rocket motor with annular, concentric solid fuel elements Jun 17, 2007 Issued
Array ( [id] => 4957808 [patent_doc_number] => 20080272232 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-11-06 [patent_title] => 'Jet Engine Exhaust Nozzle Flow Effector' [patent_app_type] => utility [patent_app_number] => 11/762827 [patent_app_country] => US [patent_app_date] => 2007-06-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 4192 [patent_no_of_claims] => 42 [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/A1/0272/20080272232.pdf [firstpage_image] =>[orig_patent_app_number] => 11762827 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/762827
Jet engine exhaust nozzle flow effector Jun 13, 2007 Issued
Array ( [id] => 5448624 [patent_doc_number] => 20090064659 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-03-12 [patent_title] => 'GAS TURBINE ENGINE WITH FAN VARIABLE AREA NOZZLE HAVING A ROTATIONAL VALVE SYSTEM' [patent_app_type] => utility [patent_app_number] => 11/755757 [patent_app_country] => US [patent_app_date] => 2007-05-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 2205 [patent_no_of_claims] => 18 [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/A1/0064/20090064659.pdf [firstpage_image] =>[orig_patent_app_number] => 11755757 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/755757
Gas turbine engine with fan variable area nozzle having a rotational valve system May 30, 2007 Issued
Array ( [id] => 4706955 [patent_doc_number] => 20080295481 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-12-04 [patent_title] => 'Fluidic vectoring for exhaust nozzle' [patent_app_type] => utility [patent_app_number] => 11/809297 [patent_app_country] => US [patent_app_date] => 2007-05-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 3693 [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/A1/0295/20080295481.pdf [firstpage_image] =>[orig_patent_app_number] => 11809297 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/809297
Fluidic vectoring for exhaust nozzle May 30, 2007 Issued
Array ( [id] => 4525671 [patent_doc_number] => 07870741 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2011-01-18 [patent_title] => 'Turbine engine valve assembly and method of assembling the same' [patent_app_type] => utility [patent_app_number] => 11/753907 [patent_app_country] => US [patent_app_date] => 2007-05-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 4628 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 141 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/870/07870741.pdf [firstpage_image] =>[orig_patent_app_number] => 11753907 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/753907
Turbine engine valve assembly and method of assembling the same May 24, 2007 Issued
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