
Arun Goyal
Examiner (ID: 3798, Phone: (571)270-7622 , Office: P/3741 )
| Most Active Art Unit | 3741 |
| Art Unit(s) | 3741 |
| Total Applications | 678 |
| Issued Applications | 435 |
| Pending Applications | 4 |
| Abandoned Applications | 240 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 8998785
[patent_doc_number] => 20130219908
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-08-29
[patent_title] => 'GEARED TURBOFAN ARCHITECTURE FOR IMPROVED THRUST DENSITY'
[patent_app_type] => utility
[patent_app_number] => 13/483406
[patent_app_country] => US
[patent_app_date] => 2012-05-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 4625
[patent_no_of_claims] => 23
[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] => 13483406
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/483406 | GEARED TURBOFAN ARCHITECTURE FOR IMPROVED THRUST DENSITY | May 29, 2012 | Abandoned |
Array
(
[id] => 8919021
[patent_doc_number] => 08484942
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2013-07-16
[patent_title] => 'Planetary gear system arrangement with auxiliary oil system'
[patent_app_type] => utility
[patent_app_number] => 13/483657
[patent_app_country] => US
[patent_app_date] => 2012-05-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 11
[patent_no_of_words] => 3552
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 237
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13483657
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/483657 | Planetary gear system arrangement with auxiliary oil system | May 29, 2012 | Issued |
Array
(
[id] => 9067898
[patent_doc_number] => 20130259654
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-10-03
[patent_title] => 'GEARED ARCHITECTURE WITH SPEED CHANGE DEVICE FOR GAS TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 13/481006
[patent_app_country] => US
[patent_app_date] => 2012-05-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 11
[patent_no_of_words] => 4725
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 3
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13481006
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/481006 | GEARED ARCHITECTURE WITH SPEED CHANGE DEVICE FOR GAS TURBINE ENGINE | May 24, 2012 | Abandoned |
Array
(
[id] => 8492035
[patent_doc_number] => 20120291442
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-11-22
[patent_title] => 'WALL FOR A TURBOMACHINE COMBUSTION CHAMBER INCLUDING AN OPTIMISED ARRANGEMENT OF AIR INLET APERTURES'
[patent_app_type] => utility
[patent_app_number] => 13/475306
[patent_app_country] => US
[patent_app_date] => 2012-05-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2507
[patent_no_of_claims] => 7
[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] => 13475306
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/475306 | WALL FOR A TURBOMACHINE COMBUSTION CHAMBER INCLUDING AN OPTIMISED ARRANGEMENT OF AIR INLET APERTURES | May 17, 2012 | Abandoned |
Array
(
[id] => 11358134
[patent_doc_number] => 09534781
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2017-01-03
[patent_title] => 'System and method having multi-tube fuel nozzle with differential flow'
[patent_app_type] => utility
[patent_app_number] => 13/468988
[patent_app_country] => US
[patent_app_date] => 2012-05-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 13
[patent_no_of_words] => 11657
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 178
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13468988
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/468988 | System and method having multi-tube fuel nozzle with differential flow | May 9, 2012 | Issued |
Array
(
[id] => 8355555
[patent_doc_number] => 20120210719
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-08-23
[patent_title] => 'CERAMIC COMBUSTOR LINER PANEL FOR A GAS TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 13/463062
[patent_app_country] => US
[patent_app_date] => 2012-05-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2878
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13463062
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/463062 | Ceramic combustor liner panel for a gas turbine engine | May 2, 2012 | Issued |
Array
(
[id] => 9116897
[patent_doc_number] => 20130283819
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-10-31
[patent_title] => 'GEARED TURBOFAN WITH THREE TURBINES ALL CO-ROTATING'
[patent_app_type] => utility
[patent_app_number] => 13/459498
[patent_app_country] => US
[patent_app_date] => 2012-04-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2719
[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] =>[firstpage_image] =>[orig_patent_app_number] => 13459498
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/459498 | Geared turbofan with three turbines all co-rotating | Apr 29, 2012 | Issued |
Array
(
[id] => 8783080
[patent_doc_number] => 08429918
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-04-30
[patent_title] => 'Method for generating electrical energy wherein carbonaceous fuel is gasified'
[patent_app_type] => utility
[patent_app_number] => 13/458093
[patent_app_country] => US
[patent_app_date] => 2012-04-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 5226
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 110
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13458093
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/458093 | Method for generating electrical energy wherein carbonaceous fuel is gasified | Apr 26, 2012 | Issued |
Array
(
[id] => 9116890
[patent_doc_number] => 20130283812
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-10-31
[patent_title] => 'SYSTEMS AND METHODS FOR RECONDITIONING TURBINE ENGINES IN POWER GENERATION SYSTEMS'
[patent_app_type] => utility
[patent_app_number] => 13/455965
[patent_app_country] => US
[patent_app_date] => 2012-04-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 4827
[patent_no_of_claims] => 20
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13455965
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/455965 | Systems and methods for reconditioning turbine engines in power generation systems | Apr 24, 2012 | Issued |
Array
(
[id] => 9089999
[patent_doc_number] => 20130269310
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-10-17
[patent_title] => 'SYSTEMS AND APPARATUS RELATING TO REHEAT COMBUSTION TURBINE ENGINES WITH EXHAUST GAS RECIRCULATION'
[patent_app_type] => utility
[patent_app_number] => 13/444956
[patent_app_country] => US
[patent_app_date] => 2012-04-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 14
[patent_figures_cnt] => 14
[patent_no_of_words] => 18371
[patent_no_of_claims] => 33
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13444956
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/444956 | SYSTEMS AND APPARATUS RELATING TO REHEAT COMBUSTION TURBINE ENGINES WITH EXHAUST GAS RECIRCULATION | Apr 11, 2012 | Abandoned |
Array
(
[id] => 10636188
[patent_doc_number] => 09353682
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-05-31
[patent_title] => 'Methods, systems and apparatus relating to combustion turbine power plants with exhaust gas recirculation'
[patent_app_type] => utility
[patent_app_number] => 13/445003
[patent_app_country] => US
[patent_app_date] => 2012-04-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13445003
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/445003 | Methods, systems and apparatus relating to combustion turbine power plants with exhaust gas recirculation | Apr 11, 2012 | Issued |
Array
(
[id] => 8998789
[patent_doc_number] => 20130219913
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-08-29
[patent_title] => 'GEARED TURBOFAN GAS TURBINE ENGINE WITH RELIABILITY CHECK ON GEAR CONNECTION'
[patent_app_type] => utility
[patent_app_number] => 13/440085
[patent_app_country] => US
[patent_app_date] => 2012-04-05
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13440085
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/440085 | GEARED TURBOFAN GAS TURBINE ENGINE WITH RELIABILITY CHECK ON GEAR CONNECTION | Apr 4, 2012 | Abandoned |
Array
(
[id] => 9276621
[patent_doc_number] => 20140026589
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-01-30
[patent_title] => 'AIRCRAFT ENGINE'
[patent_app_type] => utility
[patent_app_number] => 14/110016
[patent_app_country] => US
[patent_app_date] => 2012-04-04
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14110016
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/110016 | Sealing arrangement of accessory to aircraft engine | Apr 3, 2012 | Issued |
Array
(
[id] => 9821802
[patent_doc_number] => 08931282
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-01-13
[patent_title] => 'Internal combustion engine'
[patent_app_type] => utility
[patent_app_number] => 13/438056
[patent_app_country] => US
[patent_app_date] => 2012-04-03
[patent_effective_date] => 0000-00-00
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/438056 | Internal combustion engine | Apr 2, 2012 | Issued |
Array
(
[id] => 9063513
[patent_doc_number] => 20130255269
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-10-03
[patent_title] => 'COMBUSTOR HAVING A BEVELED GROMMET'
[patent_app_type] => utility
[patent_app_number] => 13/437247
[patent_app_country] => US
[patent_app_date] => 2012-04-02
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13437247
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/437247 | Combustor having a beveled grommet | Apr 1, 2012 | Issued |
Array
(
[id] => 9063518
[patent_doc_number] => 20130255274
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-10-03
[patent_title] => 'GEARED ARCHITECTURE WITH SPEED CHANGE DEVICE FOR GAS TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 13/437448
[patent_app_country] => US
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13437448
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/437448 | GEARED ARCHITECTURE WITH SPEED CHANGE DEVICE FOR GAS TURBINE ENGINE | Apr 1, 2012 | Abandoned |
Array
(
[id] => 9063463
[patent_doc_number] => 20130255219
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[patent_issue_date] => 2013-10-03
[patent_title] => 'GEARED TURBOFAN WITH THREE CO-ROTATING TURBINES'
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[patent_app_number] => 13/437304
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/437304 | Geared turbofan with three co-rotating turbines | Apr 1, 2012 | Issued |
Array
(
[id] => 11750977
[patent_doc_number] => 09708982
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[patent_kind] => B2
[patent_issue_date] => 2017-07-18
[patent_title] => 'Method for mounting an aircraft engine on a pylon, and engine fastener for implementing said method'
[patent_app_type] => utility
[patent_app_number] => 14/110864
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/110864 | Method for mounting an aircraft engine on a pylon, and engine fastener for implementing said method | Mar 29, 2012 | Issued |
Array
(
[id] => 9063468
[patent_doc_number] => 20130255224
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[patent_title] => 'REVERSE CORE GEAR TURBOFAN'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/431048 | Reverse core gear turbofan | Mar 26, 2012 | Issued |
Array
(
[id] => 9302721
[patent_doc_number] => 20140041395
[patent_country] => US
[patent_kind] => A1
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[patent_title] => 'GAS TURBINE'
[patent_app_type] => utility
[patent_app_number] => 14/008513
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14008513
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/008513 | Gas turbine with improved blade and vane and flue gas diffuser | Mar 22, 2012 | Issued |