
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] => 5837099
[patent_doc_number] => 20060117757
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-06-08
[patent_title] => 'Fuel gas heating control equipment and gas turbine power generation facility provided with the fuel gas heating control equipment'
[patent_app_type] => utility
[patent_app_number] => 11/294542
[patent_app_country] => US
[patent_app_date] => 2005-12-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 6029
[patent_no_of_claims] => 13
[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/A1/0117/20060117757.pdf
[firstpage_image] =>[orig_patent_app_number] => 11294542
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/294542 | Fuel gas heating control equipment and gas turbine power generation facility provided with the fuel gas heating control equipment | Dec 5, 2005 | Issued |
Array
(
[id] => 5075955
[patent_doc_number] => 20070119179
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-05-31
[patent_title] => 'Opposed flow combustor'
[patent_app_type] => utility
[patent_app_number] => 11/291677
[patent_app_country] => US
[patent_app_date] => 2005-11-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2656
[patent_no_of_claims] => 33
[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/A1/0119/20070119179.pdf
[firstpage_image] =>[orig_patent_app_number] => 11291677
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/291677 | Opposed flow combustor | Nov 29, 2005 | Abandoned |
Array
(
[id] => 29009
[patent_doc_number] => 07788927
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-09-07
[patent_title] => 'Turbine engine fuel nozzles and methods of assembling the same'
[patent_app_type] => utility
[patent_app_number] => 11/290116
[patent_app_country] => US
[patent_app_date] => 2005-11-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 4
[patent_no_of_words] => 1710
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 135
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/788/07788927.pdf
[firstpage_image] =>[orig_patent_app_number] => 11290116
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/290116 | Turbine engine fuel nozzles and methods of assembling the same | Nov 29, 2005 | Issued |
Array
(
[id] => 5075925
[patent_doc_number] => 20070119149
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-05-31
[patent_title] => 'Hyperjet'
[patent_app_type] => utility
[patent_app_number] => 11/290330
[patent_app_country] => US
[patent_app_date] => 2005-11-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 3860
[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/A1/0119/20070119149.pdf
[firstpage_image] =>[orig_patent_app_number] => 11290330
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/290330 | Hyperjet | Nov 29, 2005 | Abandoned |
Array
(
[id] => 5075921
[patent_doc_number] => 20070119145
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-05-31
[patent_title] => 'Dirt separator for compressor diffuser in gas turbine engine'
[patent_app_type] => utility
[patent_app_number] => 11/289035
[patent_app_country] => US
[patent_app_date] => 2005-11-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 1467
[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/A1/0119/20070119145.pdf
[firstpage_image] =>[orig_patent_app_number] => 11289035
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/289035 | Dirt separator for compressor diffuser in gas turbine engine | Nov 28, 2005 | Issued |
Array
(
[id] => 280589
[patent_doc_number] => 07552582
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2009-06-30
[patent_title] => 'More electric aircraft power transfer systems and methods'
[patent_app_type] => utility
[patent_app_number] => 11/290745
[patent_app_country] => US
[patent_app_date] => 2005-11-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 6058
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 262
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/552/07552582.pdf
[firstpage_image] =>[orig_patent_app_number] => 11290745
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/290745 | More electric aircraft power transfer systems and methods | Nov 28, 2005 | Issued |
Array
(
[id] => 5075927
[patent_doc_number] => 20070119151
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-05-31
[patent_title] => 'Nozzle assembly for rocket and ramjet applications'
[patent_app_type] => utility
[patent_app_number] => 11/287297
[patent_app_country] => US
[patent_app_date] => 2005-11-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 2003
[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/A1/0119/20070119151.pdf
[firstpage_image] =>[orig_patent_app_number] => 11287297
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/287297 | Nozzle assembly for rocket and ramjet applications | Nov 27, 2005 | Issued |
Array
(
[id] => 5644746
[patent_doc_number] => 20060130478
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-06-22
[patent_title] => 'Wave rotor apparatus'
[patent_app_type] => utility
[patent_app_number] => 11/271483
[patent_app_country] => US
[patent_app_date] => 2005-11-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 27
[patent_figures_cnt] => 27
[patent_no_of_words] => 7524
[patent_no_of_claims] => 83
[patent_no_of_ind_claims] => 15
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0130/20060130478.pdf
[firstpage_image] =>[orig_patent_app_number] => 11271483
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/271483 | Wave rotor apparatus | Nov 10, 2005 | Issued |
Array
(
[id] => 5212643
[patent_doc_number] => 20070101723
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-05-10
[patent_title] => 'Methods and apparatus for a combustion turbine nitrogen purge system'
[patent_app_type] => utility
[patent_app_number] => 11/268041
[patent_app_country] => US
[patent_app_date] => 2005-11-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 7989
[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/A1/0101/20070101723.pdf
[firstpage_image] =>[orig_patent_app_number] => 11268041
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/268041 | Methods and apparatus for a combustion turbine nitrogen purge system | Nov 6, 2005 | Issued |
Array
(
[id] => 5212640
[patent_doc_number] => 20070101720
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-05-10
[patent_title] => 'Methods and apparatus for a combustion turbine fuel recirculation system and nitrogen purge system'
[patent_app_type] => utility
[patent_app_number] => 11/268247
[patent_app_country] => US
[patent_app_date] => 2005-11-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 8116
[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/A1/0101/20070101720.pdf
[firstpage_image] =>[orig_patent_app_number] => 11268247
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/268247 | Methods and apparatus for a combustion turbine fuel recirculation system and nitrogen purge system | Nov 6, 2005 | Issued |
Array
(
[id] => 5571879
[patent_doc_number] => 20090139238
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-06-04
[patent_title] => 'AIRFLOW DISTRIBUTION TO A LOW EMISSIONS COMBUSTOR'
[patent_app_type] => utility
[patent_app_number] => 11/262447
[patent_app_country] => US
[patent_app_date] => 2005-10-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2000
[patent_no_of_claims] => 20
[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/A1/0139/20090139238.pdf
[firstpage_image] =>[orig_patent_app_number] => 11262447
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/262447 | Airflow distribution to a low emissions combustor | Oct 27, 2005 | Issued |
Array
(
[id] => 5037139
[patent_doc_number] => 20070089421
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-04-26
[patent_title] => 'Assembly and method for cooling rear bearing and exhaust frame of gas turbine'
[patent_app_type] => utility
[patent_app_number] => 11/257153
[patent_app_country] => US
[patent_app_date] => 2005-10-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 1854
[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/A1/0089/20070089421.pdf
[firstpage_image] =>[orig_patent_app_number] => 11257153
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/257153 | Assembly and method for cooling rear bearing and exhaust frame of gas turbine | Oct 24, 2005 | Issued |
Array
(
[id] => 5037145
[patent_doc_number] => 20070089427
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-04-26
[patent_title] => 'Two-branch mixing passage and method to control combustor pulsations'
[patent_app_type] => utility
[patent_app_number] => 11/257264
[patent_app_country] => US
[patent_app_date] => 2005-10-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[patent_no_of_words] => 3702
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 4
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0089/20070089427.pdf
[firstpage_image] =>[orig_patent_app_number] => 11257264
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/257264 | Two-branch mixing passage and method to control combustor pulsations | Oct 23, 2005 | Abandoned |
Array
(
[id] => 5037146
[patent_doc_number] => 20070089428
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-04-26
[patent_title] => 'Gas turbine engine mixing duct and method to start the engine'
[patent_app_type] => utility
[patent_app_number] => 11/255339
[patent_app_country] => US
[patent_app_date] => 2005-10-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[patent_no_of_words] => 2685
[patent_no_of_claims] => 22
[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/A1/0089/20070089428.pdf
[firstpage_image] =>[orig_patent_app_number] => 11255339
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/255339 | Gas turbine engine mixing duct and method to start the engine | Oct 20, 2005 | Issued |
Array
(
[id] => 5740356
[patent_doc_number] => 20060086078
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-04-27
[patent_title] => 'Universal Carnot propulsion systems for turbo rocketry'
[patent_app_type] => utility
[patent_app_number] => 11/254421
[patent_app_country] => US
[patent_app_date] => 2005-10-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 16
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[patent_no_of_words] => 4223
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0086/20060086078.pdf
[firstpage_image] =>[orig_patent_app_number] => 11254421
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/254421 | Universal Carnot propulsion systems for turbo rocketry | Oct 19, 2005 | Abandoned |
Array
(
[id] => 4541183
[patent_doc_number] => 07836698
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-11-23
[patent_title] => 'Combustor with staged fuel premixer'
[patent_app_type] => utility
[patent_app_number] => 11/163483
[patent_app_country] => US
[patent_app_date] => 2005-10-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
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[patent_no_of_words] => 1647
[patent_no_of_claims] => 18
[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/07/836/07836698.pdf
[firstpage_image] =>[orig_patent_app_number] => 11163483
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/163483 | Combustor with staged fuel premixer | Oct 19, 2005 | Issued |
Array
(
[id] => 59912
[patent_doc_number] => 07762076
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-07-27
[patent_title] => 'Attachment of a ceramic combustor can'
[patent_app_type] => utility
[patent_app_number] => 11/254876
[patent_app_country] => US
[patent_app_date] => 2005-10-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
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[patent_no_of_words] => 2200
[patent_no_of_claims] => 16
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[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/762/07762076.pdf
[firstpage_image] =>[orig_patent_app_number] => 11254876
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/254876 | Attachment of a ceramic combustor can | Oct 19, 2005 | Issued |
Array
(
[id] => 4983333
[patent_doc_number] => 20070087892
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-04-19
[patent_title] => 'Gas turbine engine assembly and methods of assembling same'
[patent_app_type] => utility
[patent_app_number] => 11/253495
[patent_app_country] => US
[patent_app_date] => 2005-10-19
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0087/20070087892.pdf
[firstpage_image] =>[orig_patent_app_number] => 11253495
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/253495 | Gas turbine assembly and methods of assembling same | Oct 18, 2005 | Issued |
Array
(
[id] => 5072071
[patent_doc_number] => 20070012046
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-01-18
[patent_title] => 'GAS TURBINE INTERMEDIATE STRUCTURE AND A GAS TURBINE ENGINE COMPRISING THE INTERMEDIATE STRUCTURE'
[patent_app_type] => utility
[patent_app_number] => 11/163172
[patent_app_country] => US
[patent_app_date] => 2005-10-07
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0012/20070012046.pdf
[firstpage_image] =>[orig_patent_app_number] => 11163172
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/163172 | GAS TURBINE INTERMEDIATE STRUCTURE AND A GAS TURBINE ENGINE COMPRISING THE INTERMEDIATE STRUCTURE | Oct 6, 2005 | Abandoned |
Array
(
[id] => 207831
[patent_doc_number] => 07624578
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2009-12-01
[patent_title] => 'Method and apparatus for generating combustion products within a gas turbine engine'
[patent_app_type] => utility
[patent_app_number] => 11/241391
[patent_app_country] => US
[patent_app_date] => 2005-09-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[patent_no_of_words] => 2642
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/624/07624578.pdf
[firstpage_image] =>[orig_patent_app_number] => 11241391
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/241391 | Method and apparatus for generating combustion products within a gas turbine engine | Sep 29, 2005 | Issued |