
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] => 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
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[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
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[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
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[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
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[patent_no_of_words] => 2330
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[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
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[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
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[patent_no_of_words] => 2126
[patent_no_of_claims] => 21
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[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
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[patent_no_of_words] => 5066
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[patent_maintenance] => 1
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[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
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[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
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[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
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[patent_no_of_words] => 2680
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[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
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[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
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[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
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[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
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[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
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[patent_app_date] => 2007-06-18
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[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
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[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
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[patent_title] => 'GAS TURBINE ENGINE WITH FAN VARIABLE AREA NOZZLE HAVING A ROTATIONAL VALVE SYSTEM'
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[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
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[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
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[patent_title] => 'Turbine engine valve assembly and method of assembling the same'
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[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 |