
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] => 7799260
[patent_doc_number] => 08127525
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-03-06
[patent_title] => 'System for dissipating energy in the event of a turbine shaft breaking in a gas turbine engine'
[patent_app_type] => utility
[patent_app_number] => 12/126407
[patent_app_country] => US
[patent_app_date] => 2008-05-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 2
[patent_no_of_words] => 1966
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 227
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/127/08127525.pdf
[firstpage_image] =>[orig_patent_app_number] => 12126407
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/126407 | System for dissipating energy in the event of a turbine shaft breaking in a gas turbine engine | May 22, 2008 | Issued |
Array
(
[id] => 6482682
[patent_doc_number] => 20100199627
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-08-12
[patent_title] => 'Gas Turbo Set and Method for Controlling a Gas Turbo Set'
[patent_app_type] => utility
[patent_app_number] => 12/601055
[patent_app_country] => US
[patent_app_date] => 2008-05-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 3174
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 2
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[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0199/20100199627.pdf
[firstpage_image] =>[orig_patent_app_number] => 12601055
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/601055 | Gas turbo set and method for controlling a gas turbo set | May 15, 2008 | Issued |
Array
(
[id] => 6497009
[patent_doc_number] => 20100218481
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-09-02
[patent_title] => 'TWO-PULSE ROCKET MOTOR'
[patent_app_type] => utility
[patent_app_number] => 12/599874
[patent_app_country] => US
[patent_app_date] => 2008-05-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 6077
[patent_no_of_claims] => 6
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[pdf_file] => publications/A1/0218/20100218481.pdf
[firstpage_image] =>[orig_patent_app_number] => 12599874
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/599874 | Two-pulse rocket motor | May 8, 2008 | Issued |
Array
(
[id] => 6236873
[patent_doc_number] => 20100132330
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-06-03
[patent_title] => 'METHOD AND APPARATUS FOR SUPPRESSING AEROENGINE CONTRAILS'
[patent_app_type] => utility
[patent_app_number] => 12/451503
[patent_app_country] => US
[patent_app_date] => 2008-04-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 3002
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 2
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0132/20100132330.pdf
[firstpage_image] =>[orig_patent_app_number] => 12451503
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/451503 | Method and apparatus for suppressing aeroengine contrails | Apr 27, 2008 | Issued |
Array
(
[id] => 5455116
[patent_doc_number] => 20090255268
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-10-15
[patent_title] => 'Divergent cooling thimbles for combustor liners and related method'
[patent_app_type] => utility
[patent_app_number] => 12/081167
[patent_app_country] => US
[patent_app_date] => 2008-04-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_no_of_words] => 1867
[patent_no_of_claims] => 17
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0255/20090255268.pdf
[firstpage_image] =>[orig_patent_app_number] => 12081167
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/081167 | Divergent cooling thimbles for combustor liners and related method | Apr 10, 2008 | Abandoned |
Array
(
[id] => 9164646
[patent_doc_number] => 08590316
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-11-26
[patent_title] => 'CMC mixer with structural outer cowling'
[patent_app_type] => utility
[patent_app_number] => 12/594874
[patent_app_country] => US
[patent_app_date] => 2008-04-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
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[patent_no_of_words] => 4095
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12594874
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/594874 | CMC mixer with structural outer cowling | Apr 7, 2008 | Issued |
Array
(
[id] => 5468381
[patent_doc_number] => 20090241547
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-10-01
[patent_title] => 'Gas turbine fuel injector for lower heating capacity fuels'
[patent_app_type] => utility
[patent_app_number] => 12/078407
[patent_app_country] => US
[patent_app_date] => 2008-03-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 5445
[patent_no_of_claims] => 20
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0241/20090241547.pdf
[firstpage_image] =>[orig_patent_app_number] => 12078407
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/078407 | Gas turbine fuel injector for lower heating capacity fuels | Mar 30, 2008 | Abandoned |
Array
(
[id] => 5306368
[patent_doc_number] => 20090013664
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-01-15
[patent_title] => 'Actuator Arrangement'
[patent_app_type] => utility
[patent_app_number] => 12/057497
[patent_app_country] => US
[patent_app_date] => 2008-03-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 1784
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 1
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0013/20090013664.pdf
[firstpage_image] =>[orig_patent_app_number] => 12057497
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/057497 | Thrust reverser and VAFN arrangement | Mar 27, 2008 | Issued |
Array
(
[id] => 4678845
[patent_doc_number] => 20080245071
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-10-09
[patent_title] => 'THERMAL POWER PLANT'
[patent_app_type] => utility
[patent_app_number] => 12/056805
[patent_app_country] => US
[patent_app_date] => 2008-03-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
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[patent_no_of_words] => 10993
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[pdf_file] => publications/A1/0245/20080245071.pdf
[firstpage_image] =>[orig_patent_app_number] => 12056805
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/056805 | THERMAL POWER PLANT | Mar 26, 2008 | Abandoned |
Array
(
[id] => 4678848
[patent_doc_number] => 20080245074
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-10-09
[patent_title] => 'Combustor of a gas turbine engine'
[patent_app_type] => utility
[patent_app_number] => 12/076087
[patent_app_country] => US
[patent_app_date] => 2008-03-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
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[patent_no_of_words] => 6281
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0245/20080245074.pdf
[firstpage_image] =>[orig_patent_app_number] => 12076087
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/076087 | Combustor of a gas turbine engine | Mar 12, 2008 | Issued |
Array
(
[id] => 5381957
[patent_doc_number] => 20090223201
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-09-10
[patent_title] => 'Methods of Injecting Diluent Into A Gas Turbine Assembly'
[patent_app_type] => utility
[patent_app_number] => 12/045497
[patent_app_country] => US
[patent_app_date] => 2008-03-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[pdf_file] => publications/A1/0223/20090223201.pdf
[firstpage_image] =>[orig_patent_app_number] => 12045497
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/045497 | Methods of Injecting Diluent Into A Gas Turbine Assembly | Mar 9, 2008 | Abandoned |
Array
(
[id] => 7769866
[patent_doc_number] => 08117847
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-02-21
[patent_title] => 'Hybrid missile propulsion system with reconfigurable multinozzle grid'
[patent_app_type] => utility
[patent_app_number] => 12/044227
[patent_app_country] => US
[patent_app_date] => 2008-03-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/117/08117847.pdf
[firstpage_image] =>[orig_patent_app_number] => 12044227
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/044227 | Hybrid missile propulsion system with reconfigurable multinozzle grid | Mar 6, 2008 | Issued |
Array
(
[id] => 5381983
[patent_doc_number] => 20090223227
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-09-10
[patent_title] => 'Combustion cap with crown mixing holes'
[patent_app_type] => utility
[patent_app_number] => 12/073407
[patent_app_country] => US
[patent_app_date] => 2008-03-05
[patent_effective_date] => 0000-00-00
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[pdf_file] => publications/A1/0223/20090223227.pdf
[firstpage_image] =>[orig_patent_app_number] => 12073407
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/073407 | Combustion cap with crown mixing holes | Mar 4, 2008 | Abandoned |
Array
(
[id] => 6181448
[patent_doc_number] => 20110167794
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-07-14
[patent_title] => 'Multi-Functional Pulse-Divided Rocket'
[patent_app_type] => utility
[patent_app_number] => 12/041797
[patent_app_country] => US
[patent_app_date] => 2008-03-04
[patent_effective_date] => 0000-00-00
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[pdf_file] => publications/A1/0167/20110167794.pdf
[firstpage_image] =>[orig_patent_app_number] => 12041797
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/041797 | Multi-functional pulse-divided rocket | Mar 3, 2008 | Issued |
Array
(
[id] => 8196828
[patent_doc_number] => 08186145
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-05-29
[patent_title] => 'Rocket nozzles for unconventional vehicles'
[patent_app_type] => utility
[patent_app_number] => 12/072487
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[pdf_file] => patents/08/186/08186145.pdf
[firstpage_image] =>[orig_patent_app_number] => 12072487
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/072487 | Rocket nozzles for unconventional vehicles | Feb 25, 2008 | Issued |
Array
(
[id] => 5388029
[patent_doc_number] => 20090205341
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[patent_kind] => A1
[patent_issue_date] => 2009-08-20
[patent_title] => 'GAS TURBINE ENGINE WITH TWIN TOWERSHAFT ACCESSORY GEARBOX'
[patent_app_type] => utility
[patent_app_number] => 12/033902
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[patent_app_date] => 2008-02-20
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[firstpage_image] =>[orig_patent_app_number] => 12033902
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/033902 | GAS TURBINE ENGINE WITH TWIN TOWERSHAFT ACCESSORY GEARBOX | Feb 19, 2008 | Abandoned |
Array
(
[id] => 5476582
[patent_doc_number] => 20090199563
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-08-13
[patent_title] => 'Scalable pyrospin combustor'
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[firstpage_image] =>[orig_patent_app_number] => 12069107
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/069107 | Scalable pyrospin combustor | Feb 6, 2008 | Abandoned |
Array
(
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[patent_title] => 'Method for automatic closed-loop control of one or more combustion temperatures in a gas turbine installation and method for determination of the water content in the working fluid of a gas turbine instalation'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/068337 | Method for automatic closed-loop control of one or more combustion temperatures in a gas turbine installation and method for determination of the water content in the working fluid of a gas turbine installation | Feb 4, 2008 | Issued |
Array
(
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[patent_title] => 'METHOD AND SYSTEM TO FACILITATE COMBINED CYCLE WORKING FLUID MODIFICATION AND COMBUSTION THEREOF'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/025437 | METHOD AND SYSTEM TO FACILITATE COMBINED CYCLE WORKING FLUID MODIFICATION AND COMBUSTION THEREOF | Feb 3, 2008 | Abandoned |
Array
(
[id] => 6578109
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[patent_issue_date] => 2010-01-07
[patent_title] => 'Method for producing fuel and power from a methane hydrate bed using a gas turbine engine'
[patent_app_type] => utility
[patent_app_number] => 12/012397
[patent_app_country] => US
[patent_app_date] => 2008-01-31
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/012397 | Method for producing fuel and power from a methane hydrate bed using a gas turbine engine | Jan 30, 2008 | Abandoned |