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] => 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 [patent_figures_cnt] => 11 [patent_no_of_words] => 3352 [patent_no_of_claims] => 4 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 241 [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 [patent_figures_cnt] => 7 [patent_no_of_words] => 3323 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 131 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_figures_cnt] => 47 [patent_no_of_words] => 11486 [patent_no_of_claims] => 4 [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/A1/0201/20070201974.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 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 100 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_figures_cnt] => 15 [patent_no_of_words] => 3438 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 78 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [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/A1/0010/20080010997.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 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 5 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [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 [patent_figures_cnt] => 12 [patent_no_of_words] => 4811 [patent_no_of_claims] => 24 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 116 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [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 [patent_no_of_claims] => 25 [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/A1/0326/20100326043.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 [patent_figures_cnt] => 9 [patent_no_of_words] => 3272 [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/A1/0178/20080178590.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 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 2224 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 53 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [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 [patent_app_date] => 2007-01-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2168 [patent_no_of_claims] => 16 [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/A1/0173/20080173003.pdf [firstpage_image] =>[orig_patent_app_number] => 11654847 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/654847
Flame stability enhancement Jan 17, 2007 Issued
Array ( [id] => 4807716 [patent_doc_number] => 20080171294 [patent_country] => US [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 [patent_app_country] => US [patent_app_date] => 2007-01-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 3379 [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/A1/0171/20080171294.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 [patent_app_number] => 11/652222 [patent_app_country] => US [patent_app_date] => 2007-01-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 3166 [patent_no_of_claims] => 15 [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/A1/0180/20070180828.pdf [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' [patent_app_type] => utility [patent_app_number] => 11/650980 [patent_app_country] => US [patent_app_date] => 2007-01-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 9 [patent_no_of_words] => 5055 [patent_no_of_claims] => 35 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 96 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [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 [patent_country] => US [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 [patent_app_number] => 11/620295 [patent_app_country] => US [patent_app_date] => 2007-01-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 2097 [patent_no_of_claims] => 5 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0163/20070163230.pdf [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 [patent_doc_number] => 20100251729 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-10-07 [patent_title] => 'Power generation system incorporating multiple Rankine cycles' [patent_app_type] => utility [patent_app_number] => 11/649572 [patent_app_country] => US [patent_app_date] => 2007-01-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 5422 [patent_no_of_claims] => 23 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0251/20100251729.pdf [firstpage_image] =>[orig_patent_app_number] => 11649572 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/649572
Power generation system incorporating multiple Rankine cycles Jan 3, 2007 Issued
Array ( [id] => 49373 [patent_doc_number] => 07770400 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2010-08-10 [patent_title] => 'Non-linear fuel transfers for gas turbines' [patent_app_type] => utility [patent_app_number] => 11/645367 [patent_app_country] => US [patent_app_date] => 2006-12-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 12 [patent_no_of_words] => 6639 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 134 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/770/07770400.pdf [firstpage_image] =>[orig_patent_app_number] => 11645367 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/645367
Non-linear fuel transfers for gas turbines Dec 25, 2006 Issued
Array ( [id] => 108325 [patent_doc_number] => 07716914 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2010-05-18 [patent_title] => 'Turbofan engine assembly and method of assembling same' [patent_app_type] => utility [patent_app_number] => 11/614585 [patent_app_country] => US [patent_app_date] => 2006-12-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 3170 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 119 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/716/07716914.pdf [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
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