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] => 302400 [patent_doc_number] => 07533533 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2009-05-19 [patent_title] => 'Jet engine with a variable section nozzle of which at least one flap pivots about a pin, pins for flaps' [patent_app_type] => utility [patent_app_number] => 11/236576 [patent_app_country] => US [patent_app_date] => 2005-09-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 5 [patent_no_of_words] => 3174 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 104 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/533/07533533.pdf [firstpage_image] =>[orig_patent_app_number] => 11236576 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/236576
Jet engine with a variable section nozzle of which at least one flap pivots about a pin, pins for flaps Sep 27, 2005 Issued
Array ( [id] => 5013196 [patent_doc_number] => 20070256404 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-11-08 [patent_title] => 'Method of adjusting a triggering clearance and a trigger' [patent_app_type] => utility [patent_app_number] => 11/234180 [patent_app_country] => US [patent_app_date] => 2005-09-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 4239 [patent_no_of_claims] => 25 [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/A1/0256/20070256404.pdf [firstpage_image] =>[orig_patent_app_number] => 11234180 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/234180
Method of adjusting a triggering clearance and a trigger Sep 25, 2005 Issued
Array ( [id] => 273040 [patent_doc_number] => 07559203 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2009-07-14 [patent_title] => 'Cooled support boss for a combustor in a gas turbine engine' [patent_app_type] => utility [patent_app_number] => 11/227285 [patent_app_country] => US [patent_app_date] => 2005-09-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 4 [patent_no_of_words] => 1551 [patent_no_of_claims] => 5 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 116 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/559/07559203.pdf [firstpage_image] =>[orig_patent_app_number] => 11227285 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/227285
Cooled support boss for a combustor in a gas turbine engine Sep 15, 2005 Issued
Array ( [id] => 5897026 [patent_doc_number] => 20060042259 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-03-02 [patent_title] => 'Combined-cycle power plant and steam thermal power plant' [patent_app_type] => utility [patent_app_number] => 11/213724 [patent_app_country] => US [patent_app_date] => 2005-08-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 3963 [patent_no_of_claims] => 9 [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/A1/0042/20060042259.pdf [firstpage_image] =>[orig_patent_app_number] => 11213724 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/213724
Combined-cycle power plant and steam thermal power plant Aug 29, 2005 Abandoned
Array ( [id] => 5151064 [patent_doc_number] => 20070033945 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-02-15 [patent_title] => 'Gas turbine system and method of operation' [patent_app_type] => utility [patent_app_number] => 11/201497 [patent_app_country] => US [patent_app_date] => 2005-08-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 4618 [patent_no_of_claims] => 35 [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/A1/0033/20070033945.pdf [firstpage_image] =>[orig_patent_app_number] => 11201497 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/201497
Gas turbine system and method of operation Aug 9, 2005 Abandoned
Array ( [id] => 5151040 [patent_doc_number] => 20070033921 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-02-15 [patent_title] => 'Aircraft engine exhaust flap curved strut slot' [patent_app_type] => utility [patent_app_number] => 11/200895 [patent_app_country] => US [patent_app_date] => 2005-08-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 2879 [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/A1/0033/20070033921.pdf [firstpage_image] =>[orig_patent_app_number] => 11200895 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/200895
Aircraft engine exhaust flap curved strut slot Aug 9, 2005 Issued
Array ( [id] => 5151065 [patent_doc_number] => 20070033946 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-02-15 [patent_title] => 'Helicopter defense system and method' [patent_app_type] => utility [patent_app_number] => 11/199267 [patent_app_country] => US [patent_app_date] => 2005-08-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 1431 [patent_no_of_claims] => 6 [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/A1/0033/20070033946.pdf [firstpage_image] =>[orig_patent_app_number] => 11199267 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/199267
Helicopter defense system and method Aug 8, 2005 Abandoned
Array ( [id] => 5049259 [patent_doc_number] => 20070029803 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-02-08 [patent_title] => 'Machine for transferring power and producing electricity in a jet engine' [patent_app_type] => utility [patent_app_number] => 11/197689 [patent_app_country] => US [patent_app_date] => 2005-08-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 989 [patent_no_of_claims] => 1 [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/A1/0029/20070029803.pdf [firstpage_image] =>[orig_patent_app_number] => 11197689 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/197689
Machine for transferring power and producing electricity in a jet engine Aug 3, 2005 Abandoned
Array ( [id] => 368691 [patent_doc_number] => 07475547 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2009-01-13 [patent_title] => 'Convergent turbojet exhaust nozzle' [patent_app_type] => utility [patent_app_number] => 11/188739 [patent_app_country] => US [patent_app_date] => 2005-07-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 8 [patent_no_of_words] => 2031 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 112 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/475/07475547.pdf [firstpage_image] =>[orig_patent_app_number] => 11188739 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/188739
Convergent turbojet exhaust nozzle Jul 25, 2005 Issued
Array ( [id] => 266282 [patent_doc_number] => 07565803 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2009-07-28 [patent_title] => 'Swirler arrangement for mixer assembly of a gas turbine engine combustor having shaped passages' [patent_app_type] => utility [patent_app_number] => 11/188595 [patent_app_country] => US [patent_app_date] => 2005-07-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 22 [patent_figures_cnt] => 23 [patent_no_of_words] => 7893 [patent_no_of_claims] => 27 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 110 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/565/07565803.pdf [firstpage_image] =>[orig_patent_app_number] => 11188595 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/188595
Swirler arrangement for mixer assembly of a gas turbine engine combustor having shaped passages Jul 24, 2005 Issued
Array ( [id] => 5651616 [patent_doc_number] => 20060137351 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-06-29 [patent_title] => 'Wall structure for limiting a hot gas path' [patent_app_type] => utility [patent_app_number] => 11/188404 [patent_app_country] => US [patent_app_date] => 2005-07-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 3719 [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/A1/0137/20060137351.pdf [firstpage_image] =>[orig_patent_app_number] => 11188404 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/188404
Wall structure for limiting a hot gas path Jul 24, 2005 Abandoned
Array ( [id] => 5048051 [patent_doc_number] => 20070028595 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-02-08 [patent_title] => 'High pressure gas turbine engine having reduced emissions' [patent_app_type] => utility [patent_app_number] => 11/188483 [patent_app_country] => US [patent_app_date] => 2005-07-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 5723 [patent_no_of_claims] => 36 [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/A1/0028/20070028595.pdf [firstpage_image] =>[orig_patent_app_number] => 11188483 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/188483
High pressure gas turbine engine having reduced emissions Jul 24, 2005 Abandoned
Array ( [id] => 5238717 [patent_doc_number] => 20070017207 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-01-25 [patent_title] => 'Combined Cycle Power Plant' [patent_app_type] => utility [patent_app_number] => 11/161137 [patent_app_country] => US [patent_app_date] => 2005-07-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 2645 [patent_no_of_claims] => 19 [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/A1/0017/20070017207.pdf [firstpage_image] =>[orig_patent_app_number] => 11161137 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/161137
Combined Cycle Power Plant Jul 24, 2005 Abandoned
Array ( [id] => 249642 [patent_doc_number] => 07581396 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2009-09-01 [patent_title] => 'Mixer assembly for combustor of a gas turbine engine having a plurality of counter-rotating swirlers' [patent_app_type] => utility [patent_app_number] => 11/188596 [patent_app_country] => US [patent_app_date] => 2005-07-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 39 [patent_figures_cnt] => 48 [patent_no_of_words] => 15915 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 193 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/581/07581396.pdf [firstpage_image] =>[orig_patent_app_number] => 11188596 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/188596
Mixer assembly for combustor of a gas turbine engine having a plurality of counter-rotating swirlers Jul 24, 2005 Issued
Array ( [id] => 98656 [patent_doc_number] => 07726134 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2010-06-01 [patent_title] => 'Method and apparatus for performing gas turbine engine maintenance' [patent_app_type] => utility [patent_app_number] => 11/184230 [patent_app_country] => US [patent_app_date] => 2005-07-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 3511 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 232 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/726/07726134.pdf [firstpage_image] =>[orig_patent_app_number] => 11184230 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/184230
Method and apparatus for performing gas turbine engine maintenance Jul 18, 2005 Issued
Array ( [id] => 5602159 [patent_doc_number] => 20060292504 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-12-28 [patent_title] => 'After-burner chamber with secure ignition' [patent_app_type] => utility [patent_app_number] => 11/181924 [patent_app_country] => US [patent_app_date] => 2005-07-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 1934 [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/A1/0292/20060292504.pdf [firstpage_image] =>[orig_patent_app_number] => 11181924 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/181924
After-burner chamber with secure ignition Jul 14, 2005 Abandoned
Array ( [id] => 5853495 [patent_doc_number] => 20060225428 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-10-12 [patent_title] => 'Dual fuel combined cycle power plant' [patent_app_type] => utility [patent_app_number] => 11/176163 [patent_app_country] => US [patent_app_date] => 2005-07-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 3533 [patent_no_of_claims] => 14 [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/A1/0225/20060225428.pdf [firstpage_image] =>[orig_patent_app_number] => 11176163 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/176163
Dual fuel combined cycle power plant Jul 6, 2005 Abandoned
Array ( [id] => 5138038 [patent_doc_number] => 20070000254 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-01-04 [patent_title] => 'Gas turbine combustor' [patent_app_type] => utility [patent_app_number] => 11/173655 [patent_app_country] => US [patent_app_date] => 2005-07-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2798 [patent_no_of_claims] => 21 [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/A1/0000/20070000254.pdf [firstpage_image] =>[orig_patent_app_number] => 11173655 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/173655
Controlled pilot oxidizer for a gas turbine combustor Jun 30, 2005 Issued
Array ( [id] => 294883 [patent_doc_number] => 07540143 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2009-06-02 [patent_title] => 'Boiler and pressure balls monopropellant thermal rocket engine' [patent_app_type] => utility [patent_app_number] => 11/172665 [patent_app_country] => US [patent_app_date] => 2005-06-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 11 [patent_no_of_words] => 3205 [patent_no_of_claims] => 13 [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] => patents/07/540/07540143.pdf [firstpage_image] =>[orig_patent_app_number] => 11172665 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/172665
Boiler and pressure balls monopropellant thermal rocket engine Jun 29, 2005 Issued
Array ( [id] => 5238735 [patent_doc_number] => 20070017225 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-01-25 [patent_title] => 'Combustion transition duct providing stage 1 tangential turning for turbine engines' [patent_app_type] => utility [patent_app_number] => 11/167464 [patent_app_country] => US [patent_app_date] => 2005-06-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 7109 [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/A1/0017/20070017225.pdf [firstpage_image] =>[orig_patent_app_number] => 11167464 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/167464
Combustion transition duct providing stage 1 tangential turning for turbine engines Jun 26, 2005 Issued
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