
William H. Rodriguez
Examiner (ID: 239, Phone: (571)272-4831 , Office: P/3741 )
| Most Active Art Unit | 3741 |
| Art Unit(s) | 3741, 3746 |
| Total Applications | 1832 |
| Issued Applications | 1604 |
| Pending Applications | 86 |
| Abandoned Applications | 161 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 7054820
[patent_doc_number] => 20050275992
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-12-15
[patent_title] => 'Radiation fan driving apparatus'
[patent_app_type] => utility
[patent_app_number] => 10/865917
[patent_app_country] => US
[patent_app_date] => 2004-06-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 2030
[patent_no_of_claims] => 7
[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/A1/0275/20050275992.pdf
[firstpage_image] =>[orig_patent_app_number] => 10865917
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/865917 | Radiation fan driving apparatus | Jun 13, 2004 | Issued |
Array
(
[id] => 7052932
[patent_doc_number] => 20050274103
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-12-15
[patent_title] => 'Gas turbine engine inlet with noise reduction features'
[patent_app_type] => utility
[patent_app_number] => 10/865025
[patent_app_country] => US
[patent_app_date] => 2004-06-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 19
[patent_figures_cnt] => 19
[patent_no_of_words] => 3903
[patent_no_of_claims] => 107
[patent_no_of_ind_claims] => 10
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0274/20050274103.pdf
[firstpage_image] =>[orig_patent_app_number] => 10865025
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/865025 | Gas turbine engine inlet with noise reduction features | Jun 9, 2004 | Abandoned |
Array
(
[id] => 7052946
[patent_doc_number] => 20050274117
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-12-15
[patent_title] => 'System & method for dumping surge flow into eductor primary nozzle for free turbine'
[patent_app_type] => utility
[patent_app_number] => 10/866398
[patent_app_country] => US
[patent_app_date] => 2004-06-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 12
[patent_no_of_words] => 4151
[patent_no_of_claims] => 32
[patent_no_of_ind_claims] => 6
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0274/20050274117.pdf
[firstpage_image] =>[orig_patent_app_number] => 10866398
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/866398 | System and method for dumping surge flow into eductor primary nozzle for free turbine | Jun 9, 2004 | Issued |
Array
(
[id] => 7052945
[patent_doc_number] => 20050274116
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-12-15
[patent_title] => 'Lean blowoff detection sensor'
[patent_app_type] => utility
[patent_app_number] => 10/865037
[patent_app_country] => US
[patent_app_date] => 2004-06-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 11
[patent_no_of_words] => 6012
[patent_no_of_claims] => 24
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 0
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0274/20050274116.pdf
[firstpage_image] =>[orig_patent_app_number] => 10865037
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/865037 | Lean blowoff detection sensor | Jun 9, 2004 | Issued |
Array
(
[id] => 7182305
[patent_doc_number] => 20050191197
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-09-01
[patent_title] => 'Hermetic compressor'
[patent_app_type] => utility
[patent_app_number] => 10/863437
[patent_app_country] => US
[patent_app_date] => 2004-06-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 2899
[patent_no_of_claims] => 8
[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/A1/0191/20050191197.pdf
[firstpage_image] =>[orig_patent_app_number] => 10863437
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/863437 | Hermetic compressor | Jun 7, 2004 | Issued |
Array
(
[id] => 777913
[patent_doc_number] => 06993916
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2006-02-07
[patent_title] => 'Burner tube and method for mixing air and gas in a gas turbine engine'
[patent_app_type] => utility
[patent_app_number] => 10/862427
[patent_app_country] => US
[patent_app_date] => 2004-06-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 8
[patent_no_of_words] => 4133
[patent_no_of_claims] => 22
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 149
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/993/06993916.pdf
[firstpage_image] =>[orig_patent_app_number] => 10862427
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/862427 | Burner tube and method for mixing air and gas in a gas turbine engine | Jun 7, 2004 | Issued |
Array
(
[id] => 7152119
[patent_doc_number] => 20050025645
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-02-03
[patent_title] => 'Debris evacuation apparatus and method for an oil pump'
[patent_app_type] => utility
[patent_app_number] => 10/862757
[patent_app_country] => US
[patent_app_date] => 2004-06-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
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[patent_no_of_words] => 1920
[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/A1/0025/20050025645.pdf
[firstpage_image] =>[orig_patent_app_number] => 10862757
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/862757 | Debris evacuation apparatus and method for an oil pump | Jun 6, 2004 | Issued |
Array
(
[id] => 7028779
[patent_doc_number] => 20050028526
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-02-10
[patent_title] => 'Burner for a gas-turbine combustion chamber'
[patent_app_type] => utility
[patent_app_number] => 10/860659
[patent_app_country] => US
[patent_app_date] => 2004-06-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2286
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 1
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0028/20050028526.pdf
[firstpage_image] =>[orig_patent_app_number] => 10860659
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/860659 | Burner for a gas-turbine combustion chamber | Jun 3, 2004 | Issued |
Array
(
[id] => 406584
[patent_doc_number] => 07284378
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2007-10-23
[patent_title] => 'Methods and apparatus for low emission gas turbine energy generation'
[patent_app_type] => utility
[patent_app_number] => 10/861257
[patent_app_country] => US
[patent_app_date] => 2004-06-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/284/07284378.pdf
[firstpage_image] =>[orig_patent_app_number] => 10861257
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/861257 | Methods and apparatus for low emission gas turbine energy generation | Jun 3, 2004 | Issued |
Array
(
[id] => 876452
[patent_doc_number] => 07353655
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2008-04-08
[patent_title] => 'Method and apparatus for achieving power augmentation in gas turbine using wet compression'
[patent_app_type] => utility
[patent_app_number] => 10/860329
[patent_app_country] => US
[patent_app_date] => 2004-06-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_no_of_words] => 6706
[patent_no_of_claims] => 21
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[pdf_file] => patents/07/353/07353655.pdf
[firstpage_image] =>[orig_patent_app_number] => 10860329
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/860329 | Method and apparatus for achieving power augmentation in gas turbine using wet compression | Jun 3, 2004 | Issued |
Array
(
[id] => 7215636
[patent_doc_number] => 20050076646
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-04-14
[patent_title] => 'Method and apparatus for achieving power augmentation in gas turbines using wet compression'
[patent_app_type] => utility
[patent_app_number] => 10/860328
[patent_app_country] => US
[patent_app_date] => 2004-06-04
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[pdf_file] => publications/A1/0076/20050076646.pdf
[firstpage_image] =>[orig_patent_app_number] => 10860328
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/860328 | Method and apparatus for achieving power augmentation in gas turbines using wet compression | Jun 3, 2004 | Issued |
Array
(
[id] => 851133
[patent_doc_number] => 07377114
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2008-05-27
[patent_title] => 'Turbine engine pulsed fuel injection utilizing stagger injector operation'
[patent_app_type] => utility
[patent_app_number] => 10/709877
[patent_app_country] => US
[patent_app_date] => 2004-06-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
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[pdf_file] => patents/07/377/07377114.pdf
[firstpage_image] =>[orig_patent_app_number] => 10709877
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/709877 | Turbine engine pulsed fuel injection utilizing stagger injector operation | Jun 1, 2004 | Issued |
Array
(
[id] => 7222499
[patent_doc_number] => 20050268613
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-12-08
[patent_title] => 'METHOD AND APPARATUS FOR COOLING COMBUSTOR LINER AND TRANSITION PIECE OF A GAS TURBINE'
[patent_app_type] => utility
[patent_app_number] => 10/709886
[patent_app_country] => US
[patent_app_date] => 2004-06-03
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[pdf_file] => publications/A1/0268/20050268613.pdf
[firstpage_image] =>[orig_patent_app_number] => 10709886
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/709886 | Method and apparatus for cooling combustor liner and transition piece of a gas turbine | May 31, 2004 | Issued |
Array
(
[id] => 789542
[patent_doc_number] => 06983601
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2006-01-10
[patent_title] => 'Method and apparatus for gas turbine engines'
[patent_app_type] => utility
[patent_app_number] => 10/856902
[patent_app_country] => US
[patent_app_date] => 2004-05-28
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[firstpage_image] =>[orig_patent_app_number] => 10856902
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/856902 | Method and apparatus for gas turbine engines | May 27, 2004 | Issued |
Array
(
[id] => 549619
[patent_doc_number] => 07464534
[patent_country] => US
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[patent_issue_date] => 2008-12-16
[patent_title] => 'Pulsed detonation engine'
[patent_app_type] => utility
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[firstpage_image] =>[orig_patent_app_number] => 10529556
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/529556 | Pulsed detonation engine | May 26, 2004 | Issued |
Array
(
[id] => 7229180
[patent_doc_number] => 20050138915
[patent_country] => US
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[patent_issue_date] => 2005-06-30
[patent_title] => 'TURBOMACHINE NOZZLE WITH NOISE REDUCTION'
[patent_app_type] => utility
[patent_app_number] => 10/853234
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[patent_app_date] => 2004-05-26
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[pdf_file] => publications/A1/0138/20050138915.pdf
[firstpage_image] =>[orig_patent_app_number] => 10853234
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/853234 | Turbomachine nozzle with noise reduction | May 25, 2004 | Issued |
Array
(
[id] => 501626
[patent_doc_number] => 07194853
[patent_country] => US
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[patent_issue_date] => 2007-03-27
[patent_title] => 'Pressurizer for a rocket engine'
[patent_app_type] => utility
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[firstpage_image] =>[orig_patent_app_number] => 10852761
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/852761 | Pressurizer for a rocket engine | May 24, 2004 | Issued |
Array
(
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[patent_title] => 'Method for operating a power plant by means of a CO2 process'
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Array
(
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[rel_patent_id] =>[rel_patent_doc_number] =>) 10/851188 | Gas turbine engine including stator vanes having variable camber and stagger configurations at different circumferential positions | May 23, 2004 | Issued |
Array
(
[id] => 7201283
[patent_doc_number] => 20050257530
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[patent_title] => 'Fuel-air mixing apparatus for reducing gas turbine combustor exhaust emissions'
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[firstpage_image] =>[orig_patent_app_number] => 10850871
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/850871 | Fuel-air mixing apparatus for reducing gas turbine combustor exhaust emissions | May 20, 2004 | Issued |