Search

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 numberTitle of the applicationFiling DateStatus
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 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_figures_cnt] => 10 [patent_no_of_words] => 2458 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_figures_cnt] => 8 [patent_no_of_words] => 4818 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 66 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_figures_cnt] => 4 [patent_no_of_words] => 2394 [patent_no_of_claims] => 6 [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/A1/0230/20090230212.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 [patent_figures_cnt] => 13 [patent_no_of_words] => 4121 [patent_no_of_claims] => 32 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 80 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_figures_cnt] => 14 [patent_no_of_words] => 5216 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 174 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 4479 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 83 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [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 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 6729 [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/A1/0193/20090193788.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 [patent_figures_cnt] => 11 [patent_no_of_words] => 4957 [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/A1/0193/20090193786.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 [patent_figures_cnt] => 11 [patent_no_of_words] => 3857 [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/A1/0196/20090196733.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
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