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] => 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 [patent_figures_cnt] => 10 [patent_no_of_words] => 3310 [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/A1/0284/20110284660.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 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 2073 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 141 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [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 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 1340 [patent_no_of_claims] => 10 [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/A1/0122/20100122519.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 [patent_figures_cnt] => 8 [patent_no_of_words] => 6778 [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/A1/0162/20100162712.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 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 8 [patent_no_of_words] => 4588 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 206 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12589182 [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 [patent_app_date] => 2009-09-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 3 [patent_no_of_words] => 1911 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 67 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [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 [patent_figures_cnt] => 7 [patent_no_of_words] => 2632 [patent_no_of_claims] => 28 [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/A1/0067/20110067377.pdf [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 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 6 [patent_no_of_words] => 2135 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 3 [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] => 12553153 [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 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 5021 [patent_no_of_claims] => 16 [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/A1/0162/20110162387.pdf [firstpage_image] =>[orig_patent_app_number] => 13119291 [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 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 1559 [patent_no_of_claims] => 12 [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/A1/0038/20100038455.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 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-03-25 [patent_title] => 'Fuel supply system for a gas-turbine engine' [patent_app_type] => utility [patent_app_number] => 12/501602 [patent_app_country] => US [patent_app_date] => 2009-07-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 10 [patent_no_of_words] => 3112 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 286 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12501602 [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 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-12-17 [patent_title] => 'Methods and systems to thermally protect fuel nozzles in combustion systems' [patent_app_type] => utility [patent_app_number] => 12/495918 [patent_app_country] => US [patent_app_date] => 2009-07-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 5 [patent_no_of_words] => 4130 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 200 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12495918 [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 [patent_doc_number] => 20100326047 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-12-30 [patent_title] => 'SYSTEM AND METHOD FOR ASSEMBLING A THRUST REVERSER FOR A GAS TURBINE PROPULSION SYSTEM' [patent_app_type] => utility [patent_app_number] => 12/495248 [patent_app_country] => US [patent_app_date] => 2009-06-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 4422 [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/A1/0326/20100326047.pdf [firstpage_image] =>[orig_patent_app_number] => 12495248 [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 [patent_doc_number] => 20090320493 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-12-31 [patent_title] => 'METHOD FOR PRIMARY CONTROL OF A COMBINED GAS AND STEAM TURBINE ARRANGEMENT' [patent_app_type] => utility [patent_app_number] => 12/492959 [patent_app_country] => US [patent_app_date] => 2009-06-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 4632 [patent_no_of_claims] => 10 [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/A1/0320/20090320493.pdf [firstpage_image] =>[orig_patent_app_number] => 12492959 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/492959
Method for primary control of a combined gas and steam turbine arrangement Jun 25, 2009 Issued
Array ( [id] => 9689505 [patent_doc_number] => 08820085 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-09-02 [patent_title] => 'Lean fuel intake gas turbine system' [patent_app_type] => utility [patent_app_number] => 12/993398 [patent_app_country] => US [patent_app_date] => 2009-06-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 5476 [patent_no_of_claims] => 7 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 195 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12993398 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/993398
Lean fuel intake gas turbine system Jun 9, 2009 Issued
Array ( [id] => 6345843 [patent_doc_number] => 20100071377 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-03-25 [patent_title] => 'Combustor Apparatus for Use in a Gas Turbine Engine' [patent_app_type] => utility [patent_app_number] => 12/477397 [patent_app_country] => US [patent_app_date] => 2009-06-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 12 [patent_no_of_words] => 10127 [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/A1/0071/20100071377.pdf [firstpage_image] =>[orig_patent_app_number] => 12477397 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/477397
Combustor Apparatus for Use in a Gas Turbine Engine Jun 2, 2009 Abandoned
Array ( [id] => 8627762 [patent_doc_number] => 08359825 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-01-29 [patent_title] => 'Microjet creation and control of shock waves' [patent_app_type] => utility [patent_app_number] => 12/454587 [patent_app_country] => US [patent_app_date] => 2009-05-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 11 [patent_no_of_words] => 4541 [patent_no_of_claims] => 2 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 244 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12454587 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/454587
Microjet creation and control of shock waves May 19, 2009 Issued
Array ( [id] => 9955630 [patent_doc_number] => 09003812 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2015-04-14 [patent_title] => 'Supporting structure for a gas turbine engine' [patent_app_type] => utility [patent_app_number] => 13/319114 [patent_app_country] => US [patent_app_date] => 2009-05-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 11 [patent_no_of_words] => 5577 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 202 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13319114 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/319114
Supporting structure for a gas turbine engine May 7, 2009 Issued
Array ( [id] => 8662272 [patent_doc_number] => 08375726 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-02-19 [patent_title] => 'Combustor assembly in a gas turbine engine' [patent_app_type] => utility [patent_app_number] => 12/431302 [patent_app_country] => US [patent_app_date] => 2009-04-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 4 [patent_no_of_words] => 7539 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 196 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12431302 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/431302
Combustor assembly in a gas turbine engine Apr 27, 2009 Issued
Array ( [id] => 9748341 [patent_doc_number] => 08839805 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-09-23 [patent_title] => 'Passive boundary layer bleed system for nacelle inlet airflow control' [patent_app_type] => utility [patent_app_number] => 12/428582 [patent_app_country] => US [patent_app_date] => 2009-04-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 4 [patent_no_of_words] => 2508 [patent_no_of_claims] => 25 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 153 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12428582 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/428582
Passive boundary layer bleed system for nacelle inlet airflow control Apr 22, 2009 Issued
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