
Benjamin S. Fields
Examiner (ID: 4456, Phone: (571)272-9734 , Office: P/3623 )
| Most Active Art Unit | 3684 |
| Art Unit(s) | 3624, 3623, 3692, 3684 |
| Total Applications | 372 |
| Issued Applications | 203 |
| Pending Applications | 0 |
| Abandoned Applications | 170 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 5961404
[patent_doc_number] => 20110146292
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-06-23
[patent_title] => 'METHOD FOR STARTING A TURBOMACHINE'
[patent_app_type] => utility
[patent_app_number] => 12/646101
[patent_app_country] => US
[patent_app_date] => 2009-12-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 4523
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0146/20110146292.pdf
[firstpage_image] =>[orig_patent_app_number] => 12646101
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/646101 | METHOD FOR STARTING A TURBOMACHINE | Dec 22, 2009 | Abandoned |
Array
(
[id] => 6384563
[patent_doc_number] => 20100162720
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-07-01
[patent_title] => 'GAS TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 12/646018
[patent_app_country] => US
[patent_app_date] => 2009-12-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[patent_no_of_words] => 13577
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[pdf_file] => publications/A1/0162/20100162720.pdf
[firstpage_image] =>[orig_patent_app_number] => 12646018
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/646018 | GAS TURBINE ENGINE | Dec 22, 2009 | Abandoned |
Array
(
[id] => 7582970
[patent_doc_number] => 20110277480
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-11-17
[patent_title] => 'SYSTEM AND METHOD FOR WASHING AND PURGING THE LIQUID FUEL SYSTEM OF A TURBINE WITH WATER'
[patent_app_type] => utility
[patent_app_number] => 13/127902
[patent_app_country] => US
[patent_app_date] => 2009-11-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
[patent_figures_cnt] => 13
[patent_no_of_words] => 4559
[patent_no_of_claims] => 15
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0277/20110277480.pdf
[firstpage_image] =>[orig_patent_app_number] => 13127902
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/127902 | System and method for washing and purging the liquid fuel system of a turbine with water | Nov 4, 2009 | Issued |
Array
(
[id] => 7477918
[patent_doc_number] => 20110247338
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-10-13
[patent_title] => 'FUEL LANCE FOR A BURNER'
[patent_app_type] => utility
[patent_app_number] => 13/133741
[patent_app_country] => US
[patent_app_date] => 2009-11-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[pdf_file] => publications/A1/0247/20110247338.pdf
[firstpage_image] =>[orig_patent_app_number] => 13133741
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/133741 | Fuel lance for A burner | Nov 4, 2009 | Issued |
Array
(
[id] => 6025645
[patent_doc_number] => 20110079018
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-04-07
[patent_title] => 'BLEED AIR TRANSFER TUBE'
[patent_app_type] => utility
[patent_app_number] => 12/571686
[patent_app_country] => US
[patent_app_date] => 2009-10-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
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[patent_no_of_words] => 3494
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[pdf_file] => publications/A1/0079/20110079018.pdf
[firstpage_image] =>[orig_patent_app_number] => 12571686
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/571686 | Bleed air transfer tube | Sep 30, 2009 | Issued |
Array
(
[id] => 6017784
[patent_doc_number] => 20110047959
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-03-03
[patent_title] => 'AIR PARTICLE SEPARATOR FOR A GAS TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 12/552490
[patent_app_country] => US
[patent_app_date] => 2009-09-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_no_of_words] => 3280
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[pdf_file] => publications/A1/0047/20110047959.pdf
[firstpage_image] =>[orig_patent_app_number] => 12552490
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/552490 | Air particle separator for a gas turbine engine | Sep 1, 2009 | Issued |
Array
(
[id] => 6017978
[patent_doc_number] => 20110048023
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-03-03
[patent_title] => 'FUEL NOZZLE SWIRLER ASSEMBLY'
[patent_app_type] => utility
[patent_app_number] => 12/552380
[patent_app_country] => US
[patent_app_date] => 2009-09-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_no_of_words] => 1995
[patent_no_of_claims] => 12
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0048/20110048023.pdf
[firstpage_image] =>[orig_patent_app_number] => 12552380
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/552380 | Fuel nozzle swirler assembly | Sep 1, 2009 | Issued |
Array
(
[id] => 6017976
[patent_doc_number] => 20110048022
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-03-03
[patent_title] => 'SYSTEM AND METHOD FOR COMBUSTION DYNAMICS CONTROL OF GAS TURBINE'
[patent_app_type] => utility
[patent_app_number] => 12/550354
[patent_app_country] => US
[patent_app_date] => 2009-08-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_no_of_words] => 1875
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[pdf_file] => publications/A1/0048/20110048022.pdf
[firstpage_image] =>[orig_patent_app_number] => 12550354
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/550354 | SYSTEM AND METHOD FOR COMBUSTION DYNAMICS CONTROL OF GAS TURBINE | Aug 28, 2009 | Abandoned |
Array
(
[id] => 6314896
[patent_doc_number] => 20100242437
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-09-30
[patent_title] => 'FUEL-COOLED FLEXIBLE HEAT EXCHANGER WITH THERMOELECTRIC DEVICE COMPRESSION'
[patent_app_type] => utility
[patent_app_number] => 12/550106
[patent_app_country] => US
[patent_app_date] => 2009-08-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[patent_no_of_words] => 3351
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[pdf_file] => publications/A1/0242/20100242437.pdf
[firstpage_image] =>[orig_patent_app_number] => 12550106
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/550106 | Fuel-cooled flexible heat exchanger with thermoelectric device compression | Aug 27, 2009 | Issued |
Array
(
[id] => 6315051
[patent_doc_number] => 20100242486
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-09-30
[patent_title] => 'FUEL-COOLED HEAT EXCHANGER WITH THERMOELECTRIC DEVICE COMPRESSION'
[patent_app_type] => utility
[patent_app_number] => 12/550150
[patent_app_country] => US
[patent_app_date] => 2009-08-28
[patent_effective_date] => 0000-00-00
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[pdf_file] => publications/A1/0242/20100242486.pdf
[firstpage_image] =>[orig_patent_app_number] => 12550150
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/550150 | Fuel-cooled heat exchanger with thermoelectric device compression | Aug 27, 2009 | Issued |
Array
(
[id] => 6213639
[patent_doc_number] => 20100050592
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-03-04
[patent_title] => 'Continuous Detonation Wave Engine'
[patent_app_type] => utility
[patent_app_number] => 12/545309
[patent_app_country] => US
[patent_app_date] => 2009-08-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
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[pdf_file] => publications/A1/0050/20100050592.pdf
[firstpage_image] =>[orig_patent_app_number] => 12545309
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/545309 | Continuous detonation wave engine with quenching structure | Aug 20, 2009 | Issued |
Array
(
[id] => 9452913
[patent_doc_number] => 08713910
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-05-06
[patent_title] => 'Integrated thrust reverser/pylon assembly'
[patent_app_type] => utility
[patent_app_number] => 12/533334
[patent_app_country] => US
[patent_app_date] => 2009-07-31
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/533334 | Integrated thrust reverser/pylon assembly | Jul 30, 2009 | Issued |
Array
(
[id] => 6143371
[patent_doc_number] => 20110016880
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-01-27
[patent_title] => 'RETAINER FOR SUSPENDED THERMAL PROTECTION ELEMENTS IN A GAS TURBINE ENGINE'
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[patent_app_number] => 12/510216
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[firstpage_image] =>[orig_patent_app_number] => 12510216
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/510216 | Retainer for suspended thermal protection elements in a gas turbine engine | Jul 26, 2009 | Issued |
Array
(
[id] => 5938466
[patent_doc_number] => 20110100007
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-05-05
[patent_title] => 'POWER RECOVERY'
[patent_app_type] => utility
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[firstpage_image] =>[orig_patent_app_number] => 12990984
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/990984 | POWER RECOVERY | May 5, 2009 | Abandoned |
Array
(
[id] => 6315057
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[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-09-30
[patent_title] => 'Systems, Methods, and Apparatus for Modifying Power Output and Efficiency of a Combined Cycle Power Plant'
[patent_app_type] => utility
[patent_app_number] => 12/414953
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Array
(
[id] => 6546653
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[patent_title] => 'Gas turbine engine'
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[firstpage_image] =>[orig_patent_app_number] => 12381958
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/381958 | Gas turbine engine | Mar 15, 2009 | Abandoned |
Array
(
[id] => 6244700
[patent_doc_number] => 20100024434
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-02-04
[patent_title] => 'Gas turbine engine arrangement'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/379594 | Gas turbine engine arrangement | Feb 24, 2009 | Issued |
Array
(
[id] => 5418650
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[patent_title] => 'COMBINED CYCLE POWER PLANT WITH RESERVES CAPABILITY'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/331824 | COMBINED CYCLE POWER PLANT WITH RESERVES CAPABILITY | Dec 9, 2008 | Abandoned |
Array
(
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[patent_issue_date] => 2010-09-30
[patent_title] => 'AIR INTAKE STRUCTURE TO BE MOUNTED UPSTREAM OF A NACELLE MIDDLE STRUCTURE FOR AIRCRAFT ENGINE, AND NACELLE EQUIPPED WITH SUCH AIR INTAKE STRUCTURE'
[patent_app_type] => utility
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[firstpage_image] =>[orig_patent_app_number] => 12681994
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/681994 | Air intake structure to be mounted upstream of a nacelle middle structure for aircraft engine, and nacelle equipped with such air intake structure | Aug 27, 2008 | Issued |
Array
(
[id] => 6236966
[patent_doc_number] => 20100132375
[patent_country] => US
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[patent_issue_date] => 2010-06-03
[patent_title] => 'ATTACHMENT STRUCTURE OF COMBUSTION OSCILLATION DETECTING DEVICE'
[patent_app_type] => utility
[patent_app_number] => 12/519574
[patent_app_country] => US
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[firstpage_image] =>[orig_patent_app_number] => 12519574
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/519574 | Attachment structure of combustion oscillation detecting device | Jun 3, 2008 | Issued |