
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] => 5460298
[patent_doc_number] => 20090320498
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-12-31
[patent_title] => 'COOLING AIR BLEED DEVICE IN A TURBOMACHINE'
[patent_app_type] => utility
[patent_app_number] => 12/490962
[patent_app_country] => US
[patent_app_date] => 2009-06-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
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[firstpage_image] =>[orig_patent_app_number] => 12490962
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/490962 | Cooling air bleed device in a turbomachine | Jun 23, 2009 | Issued |
Array
(
[id] => 5460297
[patent_doc_number] => 20090320497
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-12-31
[patent_title] => 'COOLING AIR BLEED DEVICE IN A TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 12/489844
[patent_app_country] => US
[patent_app_date] => 2009-06-23
[patent_effective_date] => 0000-00-00
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[firstpage_image] =>[orig_patent_app_number] => 12489844
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/489844 | Cooling air bleed device in a turbine engine | Jun 22, 2009 | Issued |
Array
(
[id] => 8723634
[patent_doc_number] => 08402743
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-03-26
[patent_title] => 'Actuating of a thrust reverser in a turbomachine'
[patent_app_type] => utility
[patent_app_number] => 12/489830
[patent_app_country] => US
[patent_app_date] => 2009-06-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/489830 | Actuating of a thrust reverser in a turbomachine | Jun 22, 2009 | Issued |
Array
(
[id] => 8687872
[patent_doc_number] => 08387393
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-03-05
[patent_title] => 'Flashback resistant fuel injection system'
[patent_app_type] => utility
[patent_app_number] => 12/489775
[patent_app_country] => US
[patent_app_date] => 2009-06-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/489775 | Flashback resistant fuel injection system | Jun 22, 2009 | Issued |
Array
(
[id] => 9259983
[patent_doc_number] => 20130341912
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-12-26
[patent_title] => 'FUEL INJECTOR BEARING PLATE ASSEMBLY AND SWIRLER ASSEMBLY'
[patent_app_type] => utility
[patent_app_number] => 12/482513
[patent_app_country] => US
[patent_app_date] => 2009-06-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/482513 | Fuel injector bearing plate assembly and swirler assembly | Jun 10, 2009 | Issued |
Array
(
[id] => 8456045
[patent_doc_number] => 08291706
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-10-23
[patent_title] => 'Fuel injector bearing plate assembly and swirler assembly'
[patent_app_type] => utility
[patent_app_number] => 12/482516
[patent_app_country] => US
[patent_app_date] => 2009-06-11
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12482516
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/482516 | Fuel injector bearing plate assembly and swirler assembly | Jun 10, 2009 | Issued |
Array
(
[id] => 9549901
[patent_doc_number] => 08756935
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-06-24
[patent_title] => 'Gas turbine engine combustion chamber comprising CMC deflectors'
[patent_app_type] => utility
[patent_app_number] => 12/997266
[patent_app_country] => US
[patent_app_date] => 2009-06-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12997266
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/997266 | Gas turbine engine combustion chamber comprising CMC deflectors | Jun 9, 2009 | Issued |
Array
(
[id] => 9084235
[patent_doc_number] => 08555650
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-10-15
[patent_title] => 'Combustion device for annular injection of a premixed gas and method for controlling the combustion device'
[patent_app_type] => utility
[patent_app_number] => 12/993233
[patent_app_country] => US
[patent_app_date] => 2009-05-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12993233
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/993233 | Combustion device for annular injection of a premixed gas and method for controlling the combustion device | May 21, 2009 | Issued |
Array
(
[id] => 6252719
[patent_doc_number] => 20100293954
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-11-25
[patent_title] => 'METHOD AND APPARATUS FOR COMBUSTOR NOZZLE WITH FLAMEHOLDING PROTECTION'
[patent_app_type] => utility
[patent_app_number] => 12/469910
[patent_app_country] => US
[patent_app_date] => 2009-05-21
[patent_effective_date] => 0000-00-00
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[pdf_file] => publications/A1/0293/20100293954.pdf
[firstpage_image] =>[orig_patent_app_number] => 12469910
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/469910 | Method and apparatus for combustor nozzle with flameholding protection | May 20, 2009 | Issued |
Array
(
[id] => 9975511
[patent_doc_number] => 09021811
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-05-05
[patent_title] => 'Gas turbine swirler including a vortex generator device and fuel injection openings arranged between adjacent vanes'
[patent_app_type] => utility
[patent_app_number] => 13/266297
[patent_app_country] => US
[patent_app_date] => 2009-05-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13266297
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/266297 | Gas turbine swirler including a vortex generator device and fuel injection openings arranged between adjacent vanes | May 4, 2009 | Issued |
Array
(
[id] => 8361792
[patent_doc_number] => 08250848
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-08-28
[patent_title] => 'Steam turbine power system and method of assembling the same'
[patent_app_type] => utility
[patent_app_number] => 12/436030
[patent_app_country] => US
[patent_app_date] => 2009-05-05
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12436030
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/436030 | Steam turbine power system and method of assembling the same | May 4, 2009 | Issued |
Array
(
[id] => 8384138
[patent_doc_number] => 08261530
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-09-11
[patent_title] => 'Cambered aero-engine inlet'
[patent_app_type] => utility
[patent_app_number] => 12/434290
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12434290
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/434290 | Cambered aero-engine inlet | Apr 30, 2009 | Issued |
Array
(
[id] => 6408323
[patent_doc_number] => 20100275614
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-11-04
[patent_title] => 'STRUCTURAL REINFORCEMENT STRUT FOR GAS TURBINE CASE'
[patent_app_type] => utility
[patent_app_number] => 12/433250
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[firstpage_image] =>[orig_patent_app_number] => 12433250
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/433250 | Structural reinforcement strut for gas turbine case | Apr 29, 2009 | Issued |
Array
(
[id] => 5476544
[patent_doc_number] => 20090199535
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-08-13
[patent_title] => 'ANTI-ICING APPARATUS AND METHOD FOR AERO-ENGINE NOSE CONE'
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[patent_app_number] => 12/429230
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[pdf_file] => publications/A1/0199/20090199535.pdf
[firstpage_image] =>[orig_patent_app_number] => 12429230
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/429230 | Anti-icing apparatus and method for aero-engine nose cone | Apr 23, 2009 | Issued |
Array
(
[id] => 5298838
[patent_doc_number] => 20090293490
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[patent_issue_date] => 2009-12-03
[patent_title] => 'Combustor wall with improved cooling'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/385870 | Combustor wall with improved cooling | Apr 21, 2009 | Abandoned |
Array
(
[id] => 8444391
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[patent_kind] => B2
[patent_issue_date] => 2012-10-16
[patent_title] => 'Jet engine with at least one emergency drive unit'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/385520 | Jet engine with at least one emergency drive unit | Apr 8, 2009 | Issued |
Array
(
[id] => 8456048
[patent_doc_number] => 08291710
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-10-23
[patent_title] => 'Gas turbine engine exhaust nozzle having a composite article having a shape memory material member'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/419450 | Gas turbine engine exhaust nozzle having a composite article having a shape memory material member | Apr 6, 2009 | Issued |
Array
(
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[patent_issue_date] => 2010-03-18
[patent_title] => 'TRANSLATING VARIABLE AREA FAN NOZZLE WITH SPLIT BEAVERTAIL FAIRINGS'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/419080 | Translating variable area fan nozzle with split beavertail fairings | Apr 5, 2009 | Issued |
Array
(
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Array
(
[id] => 50428
[patent_doc_number] => 07765790
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[patent_title] => 'Stationary mechanical engines and subsonic jet engines using supersonic gas turbines'
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[pdf_file] => patents/07/765/07765790.pdf
[firstpage_image] =>[orig_patent_app_number] => 12411248
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/411248 | Stationary mechanical engines and subsonic jet engines using supersonic gas turbines | Mar 24, 2009 | Issued |