
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] => 4496123
[patent_doc_number] => 07913494
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-03-29
[patent_title] => 'Burner for combustion chamber and combustion method'
[patent_app_type] => utility
[patent_app_number] => 11/683614
[patent_app_country] => US
[patent_app_date] => 2007-03-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_no_of_words] => 3352
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/913/07913494.pdf
[firstpage_image] =>[orig_patent_app_number] => 11683614
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/683614 | Burner for combustion chamber and combustion method | Mar 7, 2007 | Issued |
Array
(
[id] => 4529650
[patent_doc_number] => 07874142
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-01-25
[patent_title] => 'Aeroengine thrust reverser'
[patent_app_type] => utility
[patent_app_number] => 11/715367
[patent_app_country] => US
[patent_app_date] => 2007-03-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/874/07874142.pdf
[firstpage_image] =>[orig_patent_app_number] => 11715367
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/715367 | Aeroengine thrust reverser | Mar 7, 2007 | Issued |
Array
(
[id] => 5004406
[patent_doc_number] => 20070201974
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-08-30
[patent_title] => 'NESTED CORE GAS TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 11/682077
[patent_app_country] => US
[patent_app_date] => 2007-03-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 47
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[patent_no_of_words] => 11486
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0201/20070201974.pdf
[firstpage_image] =>[orig_patent_app_number] => 11682077
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/682077 | NESTED CORE GAS TURBINE ENGINE | Mar 4, 2007 | Abandoned |
Array
(
[id] => 6549295
[patent_doc_number] => 20100058769
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-03-11
[patent_title] => 'FAN VARIABLE AREA NOZZLE FOR A GAS TURBINE ENGINE FAN NACELLE WITH DRIVE RING ACTUATION SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 12/521037
[patent_app_country] => US
[patent_app_date] => 2007-03-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 3873
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 2
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0058/20100058769.pdf
[firstpage_image] =>[orig_patent_app_number] => 12521037
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/521037 | Fan variable area nozzle for a gas turbine engine fan nacelle with drive ring actuation system | Mar 4, 2007 | Issued |
Array
(
[id] => 235426
[patent_doc_number] => 07594403
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2009-09-29
[patent_title] => 'Bleed off valve system'
[patent_app_type] => utility
[patent_app_number] => 11/706691
[patent_app_country] => US
[patent_app_date] => 2007-02-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 3418
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/594/07594403.pdf
[firstpage_image] =>[orig_patent_app_number] => 11706691
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/706691 | Bleed off valve system | Feb 14, 2007 | Issued |
Array
(
[id] => 99295
[patent_doc_number] => 07721549
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-05-25
[patent_title] => 'Fan variable area nozzle for a gas turbine engine fan nacelle with cam drive ring actuation system'
[patent_app_type] => utility
[patent_app_number] => 11/672589
[patent_app_country] => US
[patent_app_date] => 2007-02-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[patent_no_of_words] => 3438
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/721/07721549.pdf
[firstpage_image] =>[orig_patent_app_number] => 11672589
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/672589 | Fan variable area nozzle for a gas turbine engine fan nacelle with cam drive ring actuation system | Feb 7, 2007 | Issued |
Array
(
[id] => 4799410
[patent_doc_number] => 20080010997
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-01-17
[patent_title] => 'TURBINE ENGINE COMBUSTION CHAMBER WITH TANGENTIAL SLOTS'
[patent_app_type] => utility
[patent_app_number] => 11/670510
[patent_app_country] => US
[patent_app_date] => 2007-02-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 1749
[patent_no_of_claims] => 2
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0010/20080010997.pdf
[firstpage_image] =>[orig_patent_app_number] => 11670510
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/670510 | Turbine engine combustion chamber with tangential slots | Feb 1, 2007 | Issued |
Array
(
[id] => 5097549
[patent_doc_number] => 20070180809
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-08-09
[patent_title] => 'TURBINE ENGINE ANNULAR COMBUSTION CHAMBER WITH ALTERNATE FIXINGS'
[patent_app_type] => utility
[patent_app_number] => 11/670571
[patent_app_country] => US
[patent_app_date] => 2007-02-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2061
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[pdf_file] => publications/A1/0180/20070180809.pdf
[firstpage_image] =>[orig_patent_app_number] => 11670571
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/670571 | Turbine engine annular combustion chamber with alternate fixings | Feb 1, 2007 | Issued |
Array
(
[id] => 4544620
[patent_doc_number] => 07841186
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-11-30
[patent_title] => 'Inlet bleed heat and power augmentation for a gas turbine engine'
[patent_app_type] => utility
[patent_app_number] => 11/669257
[patent_app_country] => US
[patent_app_date] => 2007-01-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
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[patent_no_of_words] => 4811
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[pdf_file] => patents/07/841/07841186.pdf
[firstpage_image] =>[orig_patent_app_number] => 11669257
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/669257 | Inlet bleed heat and power augmentation for a gas turbine engine | Jan 30, 2007 | Issued |
Array
(
[id] => 6322180
[patent_doc_number] => 20100326043
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-12-30
[patent_title] => 'Expander cycle rocket engine nozzle'
[patent_app_type] => utility
[patent_app_number] => 11/700800
[patent_app_country] => US
[patent_app_date] => 2007-01-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 2441
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[pdf_file] => publications/A1/0326/20100326043.pdf
[firstpage_image] =>[orig_patent_app_number] => 11700800
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/700800 | Expander cycle rocket engine nozzle | Jan 30, 2007 | Abandoned |
Array
(
[id] => 4842183
[patent_doc_number] => 20080178590
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-07-31
[patent_title] => 'Integrated plant cooling system'
[patent_app_type] => utility
[patent_app_number] => 11/699290
[patent_app_country] => US
[patent_app_date] => 2007-01-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
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[pdf_file] => publications/A1/0178/20080178590.pdf
[firstpage_image] =>[orig_patent_app_number] => 11699290
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/699290 | Integrated plant cooling system | Jan 28, 2007 | Issued |
Array
(
[id] => 4439431
[patent_doc_number] => 07861509
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-01-04
[patent_title] => 'Methods and systems for gas turbine syngas warm-up with low emissions'
[patent_app_type] => utility
[patent_app_number] => 11/625990
[patent_app_country] => US
[patent_app_date] => 2007-01-23
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[pdf_file] => patents/07/861/07861509.pdf
[firstpage_image] =>[orig_patent_app_number] => 11625990
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/625990 | Methods and systems for gas turbine syngas warm-up with low emissions | Jan 22, 2007 | Issued |
Array
(
[id] => 4761794
[patent_doc_number] => 20080173003
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-07-24
[patent_title] => 'Flame stability enhancement'
[patent_app_type] => utility
[patent_app_number] => 11/654847
[patent_app_country] => US
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[patent_effective_date] => 0000-00-00
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[rel_patent_id] =>[rel_patent_doc_number] =>) 11/654847 | Flame stability enhancement | Jan 17, 2007 | Issued |
Array
(
[id] => 4807716
[patent_doc_number] => 20080171294
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[patent_kind] => A1
[patent_issue_date] => 2008-07-17
[patent_title] => 'Combustion systems with rotary fuel slingers'
[patent_app_type] => utility
[patent_app_number] => 11/653495
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[patent_app_date] => 2007-01-16
[patent_effective_date] => 0000-00-00
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[pdf_file] => publications/A1/0171/20080171294.pdf
[firstpage_image] =>[orig_patent_app_number] => 11653495
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/653495 | Combustion systems with rotary fuel slingers | Jan 15, 2007 | Issued |
Array
(
[id] => 5097568
[patent_doc_number] => 20070180828
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-08-09
[patent_title] => 'Combustor liners'
[patent_app_type] => utility
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[firstpage_image] =>[orig_patent_app_number] => 11652222
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/652222 | Combustor liners | Jan 10, 2007 | Issued |
Array
(
[id] => 40265
[patent_doc_number] => 07780152
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-08-24
[patent_title] => 'Direct combustion steam generator'
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[pdf_file] => patents/07/780/07780152.pdf
[firstpage_image] =>[orig_patent_app_number] => 11650980
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/650980 | Direct combustion steam generator | Jan 8, 2007 | Issued |
Array
(
[id] => 5184924
[patent_doc_number] => 20070163230
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[patent_kind] => A1
[patent_issue_date] => 2007-07-19
[patent_title] => 'CORE EXHAUST MIXER, HAVING A VARIABLE AREA, FOR TURBO-FAN JET ENGINES OF SUPERSONIC AIRCRAFT'
[patent_app_type] => utility
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[firstpage_image] =>[orig_patent_app_number] => 11620295
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/620295 | Core exhaust mixer, having a variable area, for turbo-fan jet engines of supersonic aircraft | Jan 4, 2007 | Issued |
Array
(
[id] => 6260354
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[patent_title] => 'Power generation system incorporating multiple Rankine cycles'
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Array
(
[id] => 49373
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[rel_patent_id] =>[rel_patent_doc_number] =>) 11/645367 | Non-linear fuel transfers for gas turbines | Dec 25, 2006 | Issued |
Array
(
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[patent_title] => 'Turbofan engine assembly and method of assembling same'
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[firstpage_image] =>[orig_patent_app_number] => 11614585
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/614585 | Turbofan engine assembly and method of assembling same | Dec 20, 2006 | Issued |