
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] => 10492010
[patent_doc_number] => 20150377032
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-12-31
[patent_title] => 'GAS TURBINE ENGINE COMPONENT WITH COMBINED MATE FACE AND PLATFORM COOLING'
[patent_app_type] => utility
[patent_app_number] => 14/766190
[patent_app_country] => US
[patent_app_date] => 2014-02-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 4795
[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] =>[firstpage_image] =>[orig_patent_app_number] => 14766190
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/766190 | Gas turbine engine component with combined mate face and platform cooling | Feb 6, 2014 | Issued |
Array
(
[id] => 14032359
[patent_doc_number] => 10227923
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2019-03-12
[patent_title] => System for preventing icing on an aircraft surface using a plasma actuator
[patent_app_type] => utility
[patent_app_number] => 14/765744
[patent_app_country] => US
[patent_app_date] => 2014-02-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 5
[patent_no_of_words] => 3144
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 420
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14765744
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/765744 | System for preventing icing on an aircraft surface using a plasma actuator | Feb 2, 2014 | Issued |
Array
(
[id] => 11549371
[patent_doc_number] => 09618208
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2017-04-11
[patent_title] => 'Lean azimuthal flame combustor'
[patent_app_type] => utility
[patent_app_number] => 14/143589
[patent_app_country] => US
[patent_app_date] => 2013-12-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 7
[patent_no_of_words] => 3275
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 54
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14143589
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/143589 | Lean azimuthal flame combustor | Dec 29, 2013 | Issued |
Array
(
[id] => 9698436
[patent_doc_number] => 20140248121
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-09-04
[patent_title] => 'AIRCRAFT POWER SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 14/140959
[patent_app_country] => US
[patent_app_date] => 2013-12-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 3901
[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] =>[firstpage_image] =>[orig_patent_app_number] => 14140959
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/140959 | Aircraft power system | Dec 25, 2013 | Issued |
Array
(
[id] => 10957182
[patent_doc_number] => 20140360205
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-12-11
[patent_title] => 'GAS TURBINE ENGINE AND ELECTRICAL SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 14/135567
[patent_app_country] => US
[patent_app_date] => 2013-12-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 8236
[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] =>[firstpage_image] =>[orig_patent_app_number] => 14135567
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/135567 | Gas turbine engine and electrical system | Dec 18, 2013 | Issued |
Array
(
[id] => 10949296
[patent_doc_number] => 20140352317
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-12-04
[patent_title] => 'INTERCOOLED GAS TURBINE WITH CLOSED COMBINED POWER CYCLE'
[patent_app_type] => utility
[patent_app_number] => 14/134427
[patent_app_country] => US
[patent_app_date] => 2013-12-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2493
[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] =>[firstpage_image] =>[orig_patent_app_number] => 14134427
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/134427 | Intercooled gas turbine with closed combined power cycle | Dec 18, 2013 | Issued |
Array
(
[id] => 10282981
[patent_doc_number] => 20150167979
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-06-18
[patent_title] => 'FIRST STAGE NOZZLE OR TRANSITION NOZZLE CONFIGURED TO PROMOTE MIXING OF RESPECTIVE COMBUSTION STREAMS DOWNSTREAM THEREOF BEFORE ENTRY INTO A FIRST STAGE BUCKET OF A TURBINE'
[patent_app_type] => utility
[patent_app_number] => 14/109418
[patent_app_country] => US
[patent_app_date] => 2013-12-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 2347
[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] =>[firstpage_image] =>[orig_patent_app_number] => 14109418
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/109418 | FIRST STAGE NOZZLE OR TRANSITION NOZZLE CONFIGURED TO PROMOTE MIXING OF RESPECTIVE COMBUSTION STREAMS DOWNSTREAM THEREOF BEFORE ENTRY INTO A FIRST STAGE BUCKET OF A TURBINE | Dec 16, 2013 | Abandoned |
Array
(
[id] => 9788346
[patent_doc_number] => 20150000291
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-01-01
[patent_title] => 'GAS TURBINE ENGINE COMBUSTOR HEAT EXCHANGER'
[patent_app_type] => utility
[patent_app_number] => 14/109685
[patent_app_country] => US
[patent_app_date] => 2013-12-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2318
[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] =>[firstpage_image] =>[orig_patent_app_number] => 14109685
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/109685 | GAS TURBINE ENGINE COMBUSTOR HEAT EXCHANGER | Dec 16, 2013 | Abandoned |
Array
(
[id] => 13118669
[patent_doc_number] => 10077681
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2018-09-18
[patent_title] => Compliant heat shield liner hanger assembly for gas turbine engines
[patent_app_type] => utility
[patent_app_number] => 14/759623
[patent_app_country] => US
[patent_app_date] => 2013-12-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 25
[patent_no_of_words] => 5745
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 6
[patent_words_short_claim] => 164
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14759623
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/759623 | Compliant heat shield liner hanger assembly for gas turbine engines | Dec 12, 2013 | Issued |
Array
(
[id] => 14058973
[patent_doc_number] => 10233771
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2019-03-19
[patent_title] => System and method for preventing an emergency over-speed condition in a rotating machine
[patent_app_type] => utility
[patent_app_number] => 14/097958
[patent_app_country] => US
[patent_app_date] => 2013-12-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 6
[patent_no_of_words] => 5655
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 222
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14097958
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/097958 | System and method for preventing an emergency over-speed condition in a rotating machine | Dec 4, 2013 | Issued |
Array
(
[id] => 11320003
[patent_doc_number] => 09518742
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-12-13
[patent_title] => 'Premixer assembly for mixing air and fuel for combustion'
[patent_app_type] => utility
[patent_app_number] => 14/094098
[patent_app_country] => US
[patent_app_date] => 2013-12-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 10
[patent_no_of_words] => 3592
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 164
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14094098
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/094098 | Premixer assembly for mixing air and fuel for combustion | Dec 1, 2013 | Issued |
Array
(
[id] => 9513944
[patent_doc_number] => 20140150436
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-06-05
[patent_title] => 'GAS TURBINE PART COMPRISING A NEAR WALL COOLING ARRANGEMENT'
[patent_app_type] => utility
[patent_app_number] => 14/091621
[patent_app_country] => US
[patent_app_date] => 2013-11-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2962
[patent_no_of_claims] => 12
[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] =>[firstpage_image] =>[orig_patent_app_number] => 14091621
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/091621 | Gas turbine part comprising a near wall cooling arrangement | Nov 26, 2013 | Issued |
Array
(
[id] => 11773976
[patent_doc_number] => 09382841
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-07-05
[patent_title] => 'Aircraft environmental control system selectively powered by three bleed ports'
[patent_app_type] => utility
[patent_app_number] => 14/088557
[patent_app_country] => US
[patent_app_date] => 2013-11-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 6
[patent_no_of_words] => 3662
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 292
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14088557
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/088557 | Aircraft environmental control system selectively powered by three bleed ports | Nov 24, 2013 | Issued |
Array
(
[id] => 12451098
[patent_doc_number] => 09982890
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2018-05-29
[patent_title] => Combustor dome heat shield
[patent_app_type] => utility
[patent_app_number] => 14/085011
[patent_app_country] => US
[patent_app_date] => 2013-11-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 8
[patent_no_of_words] => 2753
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 164
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14085011
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/085011 | Combustor dome heat shield | Nov 19, 2013 | Issued |
Array
(
[id] => 10492463
[patent_doc_number] => 20150377485
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-12-31
[patent_title] => 'COMBUSTION INSTABILITY CONTROL DEVICE AND CONTROL METHOD FOR SAME'
[patent_app_type] => utility
[patent_app_number] => 14/772288
[patent_app_country] => US
[patent_app_date] => 2013-11-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 3798
[patent_no_of_claims] => 8
[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] =>[firstpage_image] =>[orig_patent_app_number] => 14772288
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/772288 | Combustion instability control method | Nov 19, 2013 | Issued |
Array
(
[id] => 14949713
[patent_doc_number] => 10436117
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2019-10-08
[patent_title] => Carbureted fuel injection system for a gas turbine engine
[patent_app_type] => utility
[patent_app_number] => 14/083040
[patent_app_country] => US
[patent_app_date] => 2013-11-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 7
[patent_no_of_words] => 3218
[patent_no_of_claims] => 14
[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] =>[firstpage_image] =>[orig_patent_app_number] => 14083040
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/083040 | Carbureted fuel injection system for a gas turbine engine | Nov 17, 2013 | Issued |
Array
(
[id] => 11613110
[patent_doc_number] => 09650961
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2017-05-16
[patent_title] => 'Gas turbine combustor including burner having plural gaseous fuel manifolds'
[patent_app_type] => utility
[patent_app_number] => 14/081609
[patent_app_country] => US
[patent_app_date] => 2013-11-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 5
[patent_no_of_words] => 2554
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 363
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14081609
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/081609 | Gas turbine combustor including burner having plural gaseous fuel manifolds | Nov 14, 2013 | Issued |
Array
(
[id] => 9474018
[patent_doc_number] => 20140131481
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-05-15
[patent_title] => 'THREADED ROD FOR SYSTEM FOR DEPLOYING A DEPLOYABLE DIVERGENT SEGMENT OF A THRUSTER'
[patent_app_type] => utility
[patent_app_number] => 14/080009
[patent_app_country] => US
[patent_app_date] => 2013-11-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2247
[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] =>[firstpage_image] =>[orig_patent_app_number] => 14080009
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/080009 | Threaded rod for system for deploying a deployable divergent segment of a thruster | Nov 13, 2013 | Issued |
Array
(
[id] => 12247869
[patent_doc_number] => 09920639
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2018-03-20
[patent_title] => 'Gas turbine combustion chamber having a flow sleeve with a plurality of integrated segments'
[patent_app_type] => utility
[patent_app_number] => 14/079920
[patent_app_country] => US
[patent_app_date] => 2013-11-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 10
[patent_no_of_words] => 2093
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 348
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14079920
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/079920 | Gas turbine combustion chamber having a flow sleeve with a plurality of integrated segments | Nov 13, 2013 | Issued |
Array
(
[id] => 9459245
[patent_doc_number] => 20140123670
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-05-08
[patent_title] => 'GAS TURBINE BURNER'
[patent_app_type] => utility
[patent_app_number] => 14/074292
[patent_app_country] => US
[patent_app_date] => 2013-11-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 3857
[patent_no_of_claims] => 3
[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] =>[firstpage_image] =>[orig_patent_app_number] => 14074292
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/074292 | Method for operating a gas turbine burner with a swirl generator | Nov 6, 2013 | Issued |