
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 number | Title of the application | Filing Date | Status |
|---|---|---|---|
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
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[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
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[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
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[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
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[patent_no_of_words] => 3511
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[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
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[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
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[patent_no_of_words] => 3533
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[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
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[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
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[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
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[patent_maintenance] => 1
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[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 |