
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] => 8373417
[patent_doc_number] => 08256203
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2012-09-04
[patent_title] => 'Rocket based combined cycle propulsion unit having external rocket thrusters'
[patent_app_type] => utility
[patent_app_number] => 12/021142
[patent_app_country] => US
[patent_app_date] => 2008-01-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 7
[patent_no_of_words] => 4879
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 6
[patent_words_short_claim] => 100
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12021142
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/021142 | Rocket based combined cycle propulsion unit having external rocket thrusters | Jan 27, 2008 | Issued |
Array
(
[id] => 4555015
[patent_doc_number] => 07827802
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-11-09
[patent_title] => 'Variable-section flow mixer for a double-flow turbojet for a supersonic airplane'
[patent_app_type] => utility
[patent_app_number] => 12/020242
[patent_app_country] => US
[patent_app_date] => 2008-01-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 6
[patent_no_of_words] => 2467
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 249
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/827/07827802.pdf
[firstpage_image] =>[orig_patent_app_number] => 12020242
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/020242 | Variable-section flow mixer for a double-flow turbojet for a supersonic airplane | Jan 24, 2008 | Issued |
Array
(
[id] => 4736103
[patent_doc_number] => 20080229755
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-09-25
[patent_title] => 'HUMID AIR TURBINE, HUMID AIR TURBINE CONTROL SYSTEM, AND HUMID AIR TURBINE CONTROL METHOD'
[patent_app_type] => utility
[patent_app_number] => 12/018574
[patent_app_country] => US
[patent_app_date] => 2008-01-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 4840
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 3
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0229/20080229755.pdf
[firstpage_image] =>[orig_patent_app_number] => 12018574
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/018574 | Humid air turbine, humid air turbine control system, and humid air turbine control method | Jan 22, 2008 | Issued |
Array
(
[id] => 4464123
[patent_doc_number] => 07942003
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-05-17
[patent_title] => 'Dual-injector fuel injector system'
[patent_app_type] => utility
[patent_app_number] => 12/018520
[patent_app_country] => US
[patent_app_date] => 2008-01-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 4297
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 94
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/942/07942003.pdf
[firstpage_image] =>[orig_patent_app_number] => 12018520
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/018520 | Dual-injector fuel injector system | Jan 22, 2008 | Issued |
Array
(
[id] => 4842197
[patent_doc_number] => 20080178604
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-07-31
[patent_title] => 'Process for Optimizing the Energy of a Combined Heat and Power Generation Site'
[patent_app_type] => utility
[patent_app_number] => 12/018328
[patent_app_country] => US
[patent_app_date] => 2008-01-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 1314
[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/A1/0178/20080178604.pdf
[firstpage_image] =>[orig_patent_app_number] => 12018328
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/018328 | Process for optimizing the energy of a combined heat and power generation site | Jan 22, 2008 | Issued |
Array
(
[id] => 7799287
[patent_doc_number] => 08127552
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-03-06
[patent_title] => 'Transition scrolls for use in turbine engine assemblies'
[patent_app_type] => utility
[patent_app_number] => 12/016360
[patent_app_country] => US
[patent_app_date] => 2008-01-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2850
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 88
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/127/08127552.pdf
[firstpage_image] =>[orig_patent_app_number] => 12016360
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/016360 | Transition scrolls for use in turbine engine assemblies | Jan 17, 2008 | Issued |
Array
(
[id] => 5443315
[patent_doc_number] => 20090044541
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-02-19
[patent_title] => 'APPARATUS AND METHOD FOR REDUCTION OF JET NOISE FROM SINGLE JETS'
[patent_app_type] => utility
[patent_app_number] => 12/013045
[patent_app_country] => US
[patent_app_date] => 2008-01-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 12
[patent_no_of_words] => 4457
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 3
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[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0044/20090044541.pdf
[firstpage_image] =>[orig_patent_app_number] => 12013045
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/013045 | Apparatus and method for reduction of jet noise from single jets | Jan 10, 2008 | Issued |
Array
(
[id] => 4541194
[patent_doc_number] => 07836700
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-11-23
[patent_title] => 'Apparatus and method for reduction of jet noise from turbofan engines having separate bypass and core flaws'
[patent_app_type] => utility
[patent_app_number] => 12/013060
[patent_app_country] => US
[patent_app_date] => 2008-01-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 15
[patent_figures_cnt] => 36
[patent_no_of_words] => 6241
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 130
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/836/07836700.pdf
[firstpage_image] =>[orig_patent_app_number] => 12013060
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/013060 | Apparatus and method for reduction of jet noise from turbofan engines having separate bypass and core flaws | Jan 10, 2008 | Issued |
Array
(
[id] => 7701479
[patent_doc_number] => 08087229
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-01-03
[patent_title] => 'Variable supersonic mach number air heater utilizing supersonic combustion'
[patent_app_type] => utility
[patent_app_number] => 11/970231
[patent_app_country] => US
[patent_app_date] => 2008-01-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 6370
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 298
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/087/08087229.pdf
[firstpage_image] =>[orig_patent_app_number] => 11970231
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/970231 | Variable supersonic mach number air heater utilizing supersonic combustion | Jan 6, 2008 | Issued |
Array
(
[id] => 6430341
[patent_doc_number] => 20100281868
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-11-11
[patent_title] => 'GAS TURBINE ENGINE COMBUSTER'
[patent_app_type] => utility
[patent_app_number] => 11/965880
[patent_app_country] => US
[patent_app_date] => 2007-12-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 1951
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 4
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0281/20100281868.pdf
[firstpage_image] =>[orig_patent_app_number] => 11965880
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/965880 | GAS TURBINE ENGINE COMBUSTER | Dec 27, 2007 | Abandoned |
Array
(
[id] => 5430853
[patent_doc_number] => 20090165438
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-07-02
[patent_title] => 'Pulse detonation engine'
[patent_app_type] => utility
[patent_app_number] => 12/005200
[patent_app_country] => US
[patent_app_date] => 2007-12-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 1597
[patent_no_of_claims] => 4
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0165/20090165438.pdf
[firstpage_image] =>[orig_patent_app_number] => 12005200
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/005200 | Pulse detonation engine | Dec 25, 2007 | Abandoned |
Array
(
[id] => 5541440
[patent_doc_number] => 20090151317
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-06-18
[patent_title] => 'GEARED COUNTER-ROTATING GAS TURBOFAN ENGINE'
[patent_app_type] => utility
[patent_app_number] => 11/955630
[patent_app_country] => US
[patent_app_date] => 2007-12-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[pdf_file] => publications/A1/0151/20090151317.pdf
[firstpage_image] =>[orig_patent_app_number] => 11955630
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/955630 | Geared counter-rotating gas turbofan engine | Dec 12, 2007 | Issued |
Array
(
[id] => 4862145
[patent_doc_number] => 20080141674
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-06-19
[patent_title] => 'DEFLECTOR FOR A COMBUSTION CHAMBER ENDWALL, COMBUSTION CHAMBER EQUIPPED THEREWITH AND TURBINE ENGINE COMPRISING THEM'
[patent_app_type] => utility
[patent_app_number] => 11/950880
[patent_app_country] => US
[patent_app_date] => 2007-12-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[pdf_file] => publications/A1/0141/20080141674.pdf
[firstpage_image] =>[orig_patent_app_number] => 11950880
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/950880 | Deflector for a combustion chamber endwall, combustion chamber equipped therewith and turbine engine comprising them | Dec 4, 2007 | Issued |
Array
(
[id] => 5560552
[patent_doc_number] => 20090133404
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-05-28
[patent_title] => 'SYSTEMS AND METHODS FOR COOLING GAS TURBINE ENGINE TRANSITION LINERS'
[patent_app_type] => utility
[patent_app_number] => 11/946364
[patent_app_country] => US
[patent_app_date] => 2007-11-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_no_of_words] => 2873
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[pdf_file] => publications/A1/0133/20090133404.pdf
[firstpage_image] =>[orig_patent_app_number] => 11946364
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/946364 | Systems and methods for cooling gas turbine engine transition liners | Nov 27, 2007 | Issued |
Array
(
[id] => 4484315
[patent_doc_number] => 07954327
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-06-07
[patent_title] => 'Chamber endwall, method of producing it, combustion chamber comprising it, and turbine engine equipped therewith'
[patent_app_type] => utility
[patent_app_number] => 11/945580
[patent_app_country] => US
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[pdf_file] => patents/07/954/07954327.pdf
[firstpage_image] =>[orig_patent_app_number] => 11945580
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/945580 | Chamber endwall, method of producing it, combustion chamber comprising it, and turbine engine equipped therewith | Nov 26, 2007 | Issued |
Array
(
[id] => 8338202
[patent_doc_number] => 08240121
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-08-14
[patent_title] => 'Retrofit dirt separator for gas turbine engine'
[patent_app_type] => utility
[patent_app_number] => 11/942962
[patent_app_country] => US
[patent_app_date] => 2007-11-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 11942962
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/942962 | Retrofit dirt separator for gas turbine engine | Nov 19, 2007 | Issued |
Array
(
[id] => 4514587
[patent_doc_number] => 07950215
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-05-31
[patent_title] => 'Sequential combustion firing system for a fuel system of a gas turbine engine'
[patent_app_type] => utility
[patent_app_number] => 11/942795
[patent_app_country] => US
[patent_app_date] => 2007-11-20
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[patent_drawing_sheets_cnt] => 2
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[pdf_file] => patents/07/950/07950215.pdf
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[rel_patent_id] =>[rel_patent_doc_number] =>) 11/942795 | Sequential combustion firing system for a fuel system of a gas turbine engine | Nov 19, 2007 | Issued |
Array
(
[id] => 4848278
[patent_doc_number] => 20080314019
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[patent_kind] => A1
[patent_issue_date] => 2008-12-25
[patent_title] => 'Engine cooling'
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[patent_app_number] => 11/984472
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[firstpage_image] =>[orig_patent_app_number] => 11984472
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/984472 | Engine cooling | Nov 18, 2007 | Issued |
Array
(
[id] => 49365
[patent_doc_number] => 07770396
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[patent_issue_date] => 2010-08-10
[patent_title] => 'System for vaporization of liquid fuels for combustion and method of use'
[patent_app_type] => utility
[patent_app_number] => 11/929675
[patent_app_country] => US
[patent_app_date] => 2007-10-30
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[pdf_file] => patents/07/770/07770396.pdf
[firstpage_image] =>[orig_patent_app_number] => 11929675
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/929675 | System for vaporization of liquid fuels for combustion and method of use | Oct 29, 2007 | Issued |
Array
(
[id] => 4647503
[patent_doc_number] => 20080034758
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-02-14
[patent_title] => 'Integrated Air Separation and Oxygen Fired Power Generation System'
[patent_app_type] => utility
[patent_app_number] => 11/876463
[patent_app_country] => US
[patent_app_date] => 2007-10-22
[patent_effective_date] => 0000-00-00
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[pdf_file] => publications/A1/0034/20080034758.pdf
[firstpage_image] =>[orig_patent_app_number] => 11876463
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/876463 | Integrated Air Separation and Oxygen Fired Power Generation System | Oct 21, 2007 | Abandoned |