
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] => 7665521
[patent_doc_number] => 20110314790
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-12-29
[patent_title] => 'HYBRID PROPULSION SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 12/404977
[patent_app_country] => US
[patent_app_date] => 2009-03-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 6249
[patent_no_of_claims] => 16
[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] =>[firstpage_image] =>[orig_patent_app_number] => 12404977
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/404977 | Hybrid propulsion system | Mar 15, 2009 | Issued |
Array
(
[id] => 6600797
[patent_doc_number] => 20100223929
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-09-09
[patent_title] => 'SYSTEM FOR FUEL INJECTION IN A TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 12/397240
[patent_app_country] => US
[patent_app_date] => 2009-03-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 4900
[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/A1/0223/20100223929.pdf
[firstpage_image] =>[orig_patent_app_number] => 12397240
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/397240 | Fuel nozzle liquid cartridge including a fuel insert | Mar 2, 2009 | Issued |
Array
(
[id] => 8230971
[patent_doc_number] => 08196409
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-06-12
[patent_title] => 'Gas turbine engine fuel supply arrangement using plural distinct fuels'
[patent_app_type] => utility
[patent_app_number] => 12/370759
[patent_app_country] => US
[patent_app_date] => 2009-02-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 5156
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 199
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/196/08196409.pdf
[firstpage_image] =>[orig_patent_app_number] => 12370759
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/370759 | Gas turbine engine fuel supply arrangement using plural distinct fuels | Feb 12, 2009 | Issued |
Array
(
[id] => 8384139
[patent_doc_number] => 08261529
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-09-11
[patent_title] => 'Gas turbine combustor and gaseous fuel supply method for gas turbine combustor'
[patent_app_type] => utility
[patent_app_number] => 12/370236
[patent_app_country] => US
[patent_app_date] => 2009-02-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 9
[patent_no_of_words] => 4406
[patent_no_of_claims] => 3
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 161
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12370236
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/370236 | Gas turbine combustor and gaseous fuel supply method for gas turbine combustor | Feb 11, 2009 | Issued |
Array
(
[id] => 6306760
[patent_doc_number] => 20100192582
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-08-05
[patent_title] => 'COMBUSTOR NOZZLE'
[patent_app_type] => utility
[patent_app_number] => 12/365539
[patent_app_country] => US
[patent_app_date] => 2009-02-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 12
[patent_no_of_words] => 3093
[patent_no_of_claims] => 13
[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/A1/0192/20100192582.pdf
[firstpage_image] =>[orig_patent_app_number] => 12365539
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/365539 | COMBUSTOR NOZZLE | Feb 3, 2009 | Abandoned |
Array
(
[id] => 4428348
[patent_doc_number] => 07966821
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-06-28
[patent_title] => 'Reduced exhaust emissions gas turbine engine combustor'
[patent_app_type] => utility
[patent_app_number] => 12/361345
[patent_app_country] => US
[patent_app_date] => 2009-01-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 5
[patent_no_of_words] => 3583
[patent_no_of_claims] => 2
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 231
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/966/07966821.pdf
[firstpage_image] =>[orig_patent_app_number] => 12361345
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/361345 | Reduced exhaust emissions gas turbine engine combustor | Jan 27, 2009 | Issued |
Array
(
[id] => 6422871
[patent_doc_number] => 20100186387
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-07-29
[patent_title] => 'Soot Reduction By Combustor Conditioning'
[patent_app_type] => utility
[patent_app_number] => 12/358635
[patent_app_country] => US
[patent_app_date] => 2009-01-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 4817
[patent_no_of_claims] => 27
[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/A1/0186/20100186387.pdf
[firstpage_image] =>[orig_patent_app_number] => 12358635
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/358635 | Soot reduction by combustor conditioning | Jan 22, 2009 | Issued |
Array
(
[id] => 8144746
[patent_doc_number] => 08161750
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-04-24
[patent_title] => 'Fuel nozzle for a turbomachine'
[patent_app_type] => utility
[patent_app_number] => 12/355263
[patent_app_country] => US
[patent_app_date] => 2009-01-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 7
[patent_no_of_words] => 2435
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 108
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/161/08161750.pdf
[firstpage_image] =>[orig_patent_app_number] => 12355263
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/355263 | Fuel nozzle for a turbomachine | Jan 15, 2009 | Issued |
Array
(
[id] => 4503746
[patent_doc_number] => 07908842
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-03-22
[patent_title] => 'Method for operating a gas turbine, method of operation of a combined cycle power plant, and combined cycle power plant'
[patent_app_type] => utility
[patent_app_number] => 12/326519
[patent_app_country] => US
[patent_app_date] => 2008-12-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 3061
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 165
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/908/07908842.pdf
[firstpage_image] =>[orig_patent_app_number] => 12326519
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/326519 | Method for operating a gas turbine, method of operation of a combined cycle power plant, and combined cycle power plant | Dec 1, 2008 | Issued |
Array
(
[id] => 4439437
[patent_doc_number] => 07861510
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2011-01-04
[patent_title] => 'Ceramic regenerator for a gas turbine engine'
[patent_app_type] => utility
[patent_app_number] => 12/276322
[patent_app_country] => US
[patent_app_date] => 2008-11-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 5
[patent_no_of_words] => 2962
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 139
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/861/07861510.pdf
[firstpage_image] =>[orig_patent_app_number] => 12276322
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/276322 | Ceramic regenerator for a gas turbine engine | Nov 21, 2008 | Issued |
Array
(
[id] => 6376512
[patent_doc_number] => 20100175364
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-07-15
[patent_title] => 'INTEGRATED COAL GASIFICATION COMBINED CYCLE FACILITY'
[patent_app_type] => utility
[patent_app_number] => 12/452352
[patent_app_country] => US
[patent_app_date] => 2008-11-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 8994
[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/A1/0175/20100175364.pdf
[firstpage_image] =>[orig_patent_app_number] => 12452352
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/452352 | Integrated coal gasification combined cycle facility | Nov 5, 2008 | Issued |
Array
(
[id] => 11481296
[patent_doc_number] => 09587832
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2017-03-07
[patent_title] => 'Structures with adaptive cooling'
[patent_app_type] => utility
[patent_app_number] => 12/286705
[patent_app_country] => US
[patent_app_date] => 2008-10-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 1557
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 163
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12286705
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/286705 | Structures with adaptive cooling | Sep 30, 2008 | Issued |
Array
(
[id] => 7757937
[patent_doc_number] => 08113005
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-02-14
[patent_title] => 'Jet engine with detachably arranged generator unit'
[patent_app_type] => utility
[patent_app_number] => 12/243625
[patent_app_country] => US
[patent_app_date] => 2008-10-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 5
[patent_no_of_words] => 3383
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 143
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/113/08113005.pdf
[firstpage_image] =>[orig_patent_app_number] => 12243625
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/243625 | Jet engine with detachably arranged generator unit | Sep 30, 2008 | Issued |
Array
(
[id] => 8292493
[patent_doc_number] => 08220269
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-07-17
[patent_title] => 'Combustor for a gas turbine engine with effusion cooled baffle'
[patent_app_type] => utility
[patent_app_number] => 12/241199
[patent_app_country] => US
[patent_app_date] => 2008-09-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 3
[patent_no_of_words] => 1876
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 111
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12241199
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/241199 | Combustor for a gas turbine engine with effusion cooled baffle | Sep 29, 2008 | Issued |
Array
(
[id] => 8292505
[patent_doc_number] => 08220271
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-07-17
[patent_title] => 'Fuel lance for a gas turbine engine including outer helical grooves'
[patent_app_type] => utility
[patent_app_number] => 12/241223
[patent_app_country] => US
[patent_app_date] => 2008-09-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 6
[patent_no_of_words] => 2729
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 125
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12241223
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/241223 | Fuel lance for a gas turbine engine including outer helical grooves | Sep 29, 2008 | Issued |
Array
(
[id] => 6352722
[patent_doc_number] => 20100077769
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-04-01
[patent_title] => 'STARTER DRIVE ASSEMBLY AND METHOD OF STARTING A GAS TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 12/240516
[patent_app_country] => US
[patent_app_date] => 2008-09-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 3911
[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/A1/0077/20100077769.pdf
[firstpage_image] =>[orig_patent_app_number] => 12240516
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/240516 | STARTER DRIVE ASSEMBLY AND METHOD OF STARTING A GAS TURBINE ENGINE | Sep 28, 2008 | Abandoned |
Array
(
[id] => 8185312
[patent_doc_number] => 08181444
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-05-22
[patent_title] => 'Solid propellant rocket motor with notched annular fuel'
[patent_app_type] => utility
[patent_app_number] => 12/240223
[patent_app_country] => US
[patent_app_date] => 2008-09-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 5
[patent_no_of_words] => 2218
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 81
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/181/08181444.pdf
[firstpage_image] =>[orig_patent_app_number] => 12240223
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/240223 | Solid propellant rocket motor with notched annular fuel | Sep 28, 2008 | Issued |
Array
(
[id] => 5443313
[patent_doc_number] => 20090044539
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-02-19
[patent_title] => 'FUEL LANCE FOR A GAS TURBINE INSTALLATION AND A METHOD FOR OPERATING A FUEL LANCE'
[patent_app_type] => utility
[patent_app_number] => 12/240268
[patent_app_country] => US
[patent_app_date] => 2008-09-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2770
[patent_no_of_claims] => 17
[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/A1/0044/20090044539.pdf
[firstpage_image] =>[orig_patent_app_number] => 12240268
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/240268 | Fuel lance for a gas turbine installation and a method for operating a fuel lance | Sep 28, 2008 | Issued |
Array
(
[id] => 8396524
[patent_doc_number] => 08266889
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-09-18
[patent_title] => 'Gas turbine engine fan bleed heat exchanger system'
[patent_app_type] => utility
[patent_app_number] => 12/240359
[patent_app_country] => US
[patent_app_date] => 2008-09-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 8
[patent_no_of_words] => 2269
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 158
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12240359
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/240359 | Gas turbine engine fan bleed heat exchanger system | Sep 28, 2008 | Issued |
Array
(
[id] => 7708089
[patent_doc_number] => 08091367
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-01-10
[patent_title] => 'Combustor with improved cooling holes arrangement'
[patent_app_type] => utility
[patent_app_number] => 12/239218
[patent_app_country] => US
[patent_app_date] => 2008-09-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2555
[patent_no_of_claims] => 21
[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/08/091/08091367.pdf
[firstpage_image] =>[orig_patent_app_number] => 12239218
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/239218 | Combustor with improved cooling holes arrangement | Sep 25, 2008 | Issued |