
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] => 5548847
[patent_doc_number] => 20090282833
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-11-19
[patent_title] => 'Method and apparatus for cooling and dilution tuning a gas turbine combustor liner and transition piece interface'
[patent_app_type] => utility
[patent_app_number] => 12/153020
[patent_app_country] => US
[patent_app_date] => 2008-05-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 2365
[patent_no_of_claims] => 18
[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/A1/0282/20090282833.pdf
[firstpage_image] =>[orig_patent_app_number] => 12153020
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/153020 | Method and apparatus for cooling and dilution tuning a gas turbine combustor liner and transition piece interface | May 12, 2008 | Issued |
Array
(
[id] => 5460243
[patent_doc_number] => 20090320443
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-12-31
[patent_title] => 'Propulsion system, opposing grains rocket engine, and method for controlling the burn rate of solid propellant grains'
[patent_app_type] => utility
[patent_app_number] => 12/151900
[patent_app_country] => US
[patent_app_date] => 2008-05-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 12
[patent_no_of_words] => 9477
[patent_no_of_claims] => 24
[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/A1/0320/20090320443.pdf
[firstpage_image] =>[orig_patent_app_number] => 12151900
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/151900 | Propulsion system, opposing grains rocket engine, and method for controlling the burn rate of solid propellant grains | May 8, 2008 | Issued |
Array
(
[id] => 5482356
[patent_doc_number] => 20090272121
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-11-05
[patent_title] => 'GAS TURBINE AIRCRAFT ENGINE WITH POWER VARIABILITY'
[patent_app_type] => utility
[patent_app_number] => 12/114962
[patent_app_country] => US
[patent_app_date] => 2008-05-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 1701
[patent_no_of_claims] => 13
[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/A1/0272/20090272121.pdf
[firstpage_image] =>[orig_patent_app_number] => 12114962
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/114962 | Gas turbine aircraft engine with power variability | May 4, 2008 | Issued |
Array
(
[id] => 5554472
[patent_doc_number] => 20090266049
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-10-29
[patent_title] => 'METHODS AND SYSTEMS FOR PROPELLING A VEHICLE'
[patent_app_type] => utility
[patent_app_number] => 12/111562
[patent_app_country] => US
[patent_app_date] => 2008-04-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 4985
[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/A1/0266/20090266049.pdf
[firstpage_image] =>[orig_patent_app_number] => 12111562
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/111562 | Rocket motor having a catalytic hydroxylammonium (HAN) decomposer and method for combusting the decomposed HAN-based propellant | Apr 28, 2008 | Issued |
Array
(
[id] => 138782
[patent_doc_number] => 07685803
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-03-30
[patent_title] => 'Gas turbine system for injecting a mixture of high value hydrocarbons plural distinct fuels into the gas turbine combustion chamber'
[patent_app_type] => utility
[patent_app_number] => 12/110497
[patent_app_country] => US
[patent_app_date] => 2008-04-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 3424
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 172
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/685/07685803.pdf
[firstpage_image] =>[orig_patent_app_number] => 12110497
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/110497 | Gas turbine system for injecting a mixture of high value hydrocarbons plural distinct fuels into the gas turbine combustion chamber | Apr 27, 2008 | Issued |
Array
(
[id] => 7736261
[patent_doc_number] => 08104284
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-01-31
[patent_title] => 'Combustor and a fuel supply method for the combustor'
[patent_app_type] => utility
[patent_app_number] => 12/108162
[patent_app_country] => US
[patent_app_date] => 2008-04-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 27
[patent_figures_cnt] => 32
[patent_no_of_words] => 8823
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 128
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/104/08104284.pdf
[firstpage_image] =>[orig_patent_app_number] => 12108162
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/108162 | Combustor and a fuel supply method for the combustor | Apr 22, 2008 | Issued |
Array
(
[id] => 4637792
[patent_doc_number] => 08015815
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-09-13
[patent_title] => 'Fuel injector nozzles, with labyrinth grooves, for gas turbine engines'
[patent_app_type] => utility
[patent_app_number] => 12/105770
[patent_app_country] => US
[patent_app_date] => 2008-04-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 9
[patent_no_of_words] => 4839
[patent_no_of_claims] => 23
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 127
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/015/08015815.pdf
[firstpage_image] =>[orig_patent_app_number] => 12105770
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/105770 | Fuel injector nozzles, with labyrinth grooves, for gas turbine engines | Apr 17, 2008 | Issued |
Array
(
[id] => 5492312
[patent_doc_number] => 20090260340
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-10-22
[patent_title] => 'Combustor of a Turbine, a Method of Retro-Fitting a Combustor of a Turbine and a Method of Building a Combustor of a Turbine'
[patent_app_type] => utility
[patent_app_number] => 12/104952
[patent_app_country] => US
[patent_app_date] => 2008-04-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2780
[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/A1/0260/20090260340.pdf
[firstpage_image] =>[orig_patent_app_number] => 12104952
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/104952 | Combustor of a Turbine, a Method of Retro-Fitting a Combustor of a Turbine and a Method of Building a Combustor of a Turbine | Apr 16, 2008 | Abandoned |
Array
(
[id] => 4434422
[patent_doc_number] => 07926292
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-04-19
[patent_title] => 'Partial oxidation gas turbine cooling'
[patent_app_type] => utility
[patent_app_number] => 12/051082
[patent_app_country] => US
[patent_app_date] => 2008-03-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 2493
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 113
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/926/07926292.pdf
[firstpage_image] =>[orig_patent_app_number] => 12051082
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/051082 | Partial oxidation gas turbine cooling | Mar 18, 2008 | Issued |
Array
(
[id] => 5344907
[patent_doc_number] => 20090000268
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-01-01
[patent_title] => 'THERMONUCLEAR PLASMA REACTOR FOR ROCKET THRUST AND ELECTRICAL GENERATION'
[patent_app_type] => utility
[patent_app_number] => 12/051110
[patent_app_country] => US
[patent_app_date] => 2008-03-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 6088
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 3
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0000/20090000268.pdf
[firstpage_image] =>[orig_patent_app_number] => 12051110
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/051110 | THERMONUCLEAR PLASMA REACTOR FOR ROCKET THRUST AND ELECTRICAL GENERATION | Mar 18, 2008 | Abandoned |
Array
(
[id] => 202095
[patent_doc_number] => 07628018
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2009-12-08
[patent_title] => 'Single stage dual-entry centriafugal compressor, radial turbine gas generator'
[patent_app_type] => utility
[patent_app_number] => 12/073980
[patent_app_country] => US
[patent_app_date] => 2008-03-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 3517
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 190
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/628/07628018.pdf
[firstpage_image] =>[orig_patent_app_number] => 12073980
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/073980 | Single stage dual-entry centriafugal compressor, radial turbine gas generator | Mar 11, 2008 | Issued |
Array
(
[id] => 5529481
[patent_doc_number] => 20090229269
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-09-17
[patent_title] => 'Lean direct injection combustion system'
[patent_app_type] => utility
[patent_app_number] => 12/073939
[patent_app_country] => US
[patent_app_date] => 2008-03-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
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[patent_no_of_words] => 2458
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0229/20090229269.pdf
[firstpage_image] =>[orig_patent_app_number] => 12073939
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/073939 | Lean direct injection combustion system | Mar 11, 2008 | Issued |
Array
(
[id] => 4434384
[patent_doc_number] => 07926282
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-04-19
[patent_title] => 'Pure air blast fuel injector'
[patent_app_type] => utility
[patent_app_number] => 12/041820
[patent_app_country] => US
[patent_app_date] => 2008-03-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[patent_no_of_words] => 4818
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/926/07926282.pdf
[firstpage_image] =>[orig_patent_app_number] => 12041820
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/041820 | Pure air blast fuel injector | Mar 3, 2008 | Issued |
Array
(
[id] => 5530424
[patent_doc_number] => 20090230212
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-09-17
[patent_title] => 'Pintle-Controlled Propulsion System With External Ring Actuator'
[patent_app_type] => utility
[patent_app_number] => 12/041810
[patent_app_country] => US
[patent_app_date] => 2008-03-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_no_of_words] => 2394
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0230/20090230212.pdf
[firstpage_image] =>[orig_patent_app_number] => 12041810
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/041810 | Pintle-controlled propulsion system with external ring actuator | Mar 3, 2008 | Issued |
Array
(
[id] => 7794018
[patent_doc_number] => 08122722
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-02-28
[patent_title] => 'Exhaust nozzle seal with segmented basesheet disposed between side rails'
[patent_app_type] => utility
[patent_app_number] => 12/040324
[patent_app_country] => US
[patent_app_date] => 2008-02-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
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[patent_no_of_words] => 4121
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/122/08122722.pdf
[firstpage_image] =>[orig_patent_app_number] => 12040324
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/040324 | Exhaust nozzle seal with segmented basesheet disposed between side rails | Feb 28, 2008 | Issued |
Array
(
[id] => 7722866
[patent_doc_number] => 08096132
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-01-17
[patent_title] => 'Air-cooled swirlerhead'
[patent_app_type] => utility
[patent_app_number] => 12/034064
[patent_app_country] => US
[patent_app_date] => 2008-02-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
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[patent_no_of_words] => 5216
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/096/08096132.pdf
[firstpage_image] =>[orig_patent_app_number] => 12034064
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/034064 | Air-cooled swirlerhead | Feb 19, 2008 | Issued |
Array
(
[id] => 4503886
[patent_doc_number] => 07908863
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-03-22
[patent_title] => 'Fuel nozzle for a gas turbine engine and method for fabricating the same'
[patent_app_type] => utility
[patent_app_number] => 12/069870
[patent_app_country] => US
[patent_app_date] => 2008-02-12
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[pdf_file] => patents/07/908/07908863.pdf
[firstpage_image] =>[orig_patent_app_number] => 12069870
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/069870 | Fuel nozzle for a gas turbine engine and method for fabricating the same | Feb 11, 2008 | Issued |
Array
(
[id] => 5523712
[patent_doc_number] => 20090193788
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-08-06
[patent_title] => 'METHODS AND APPARATUS FOR OPERATING GAS TURBINE ENGINE SYSTEMS'
[patent_app_type] => utility
[patent_app_number] => 12/026230
[patent_app_country] => US
[patent_app_date] => 2008-02-05
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[pdf_file] => publications/A1/0193/20090193788.pdf
[firstpage_image] =>[orig_patent_app_number] => 12026230
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/026230 | Methods and apparatus for operating gas turbine engine systems | Feb 4, 2008 | Issued |
Array
(
[id] => 5523710
[patent_doc_number] => 20090193786
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-08-06
[patent_title] => 'System And Method Of Continuous Detonation In A Gas Turbine Engine'
[patent_app_type] => utility
[patent_app_number] => 12/024592
[patent_app_country] => US
[patent_app_date] => 2008-02-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
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[pdf_file] => publications/A1/0193/20090193786.pdf
[firstpage_image] =>[orig_patent_app_number] => 12024592
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/024592 | System and method of continuous detonation in a gas turbine engine | Jan 31, 2008 | Issued |
Array
(
[id] => 5526656
[patent_doc_number] => 20090196733
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-08-06
[patent_title] => 'Rotary Pressure Rise Combustor For A Gas Turbine Engine'
[patent_app_type] => utility
[patent_app_number] => 12/024528
[patent_app_country] => US
[patent_app_date] => 2008-02-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0196/20090196733.pdf
[firstpage_image] =>[orig_patent_app_number] => 12024528
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/024528 | Rotary pressure rise combustor for a gas turbine engine | Jan 31, 2008 | Issued |