
Sarai E. Butler
Examiner (ID: 57, Phone: (571)270-3823 , Office: P/2114 )
| Most Active Art Unit | 2114 |
| Art Unit(s) | 2114 |
| Total Applications | 1376 |
| Issued Applications | 1205 |
| Pending Applications | 61 |
| Abandoned Applications | 137 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 10423434
[patent_doc_number] => 20150308445
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-10-29
[patent_title] => 'GAS TURBINE ENGINE AND BUFFER SYSTEM THEREFOR'
[patent_app_type] => utility
[patent_app_number] => 14/692457
[patent_app_country] => US
[patent_app_date] => 2015-04-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14692457
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/692457 | GAS TURBINE ENGINE AND BUFFER SYSTEM THEREFOR | Apr 20, 2015 | Abandoned |
Array
(
[id] => 13894517
[patent_doc_number] => 10199816
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2019-02-05
[patent_title] => Wind turbine rotor blade having a lightning receptor base and method for making the same
[patent_app_type] => utility
[patent_app_number] => 14/680964
[patent_app_country] => US
[patent_app_date] => 2015-04-07
[patent_effective_date] => 0000-00-00
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/680964 | Wind turbine rotor blade having a lightning receptor base and method for making the same | Apr 6, 2015 | Issued |
Array
(
[id] => 10390676
[patent_doc_number] => 20150275683
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-10-01
[patent_title] => 'Guide vane ring ,guide vane, inner ring and turbomachine'
[patent_app_type] => utility
[patent_app_number] => 14/672333
[patent_app_country] => US
[patent_app_date] => 2015-03-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_no_of_words] => 3935
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/672333 | Guide vane ring, guide vane, inner ring and turbomachine | Mar 29, 2015 | Issued |
Array
(
[id] => 10390837
[patent_doc_number] => 20150275844
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-10-01
[patent_title] => 'HYDRAULIC TURBINE SYSTEM WITH AUXILIARY NOZZLES'
[patent_app_type] => utility
[patent_app_number] => 14/670231
[patent_app_country] => US
[patent_app_date] => 2015-03-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/670231 | HYDRAULIC TURBINE SYSTEM WITH AUXILIARY NOZZLES | Mar 25, 2015 | Abandoned |
Array
(
[id] => 11055007
[patent_doc_number] => 20160251969
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-09-01
[patent_title] => 'GAS TURBINE ENGINE AIRFOIL'
[patent_app_type] => utility
[patent_app_number] => 14/634006
[patent_app_country] => US
[patent_app_date] => 2015-02-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/634006 | Gas turbine engine airfoil | Feb 26, 2015 | Issued |
Array
(
[id] => 13237945
[patent_doc_number] => 10132166
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2018-11-20
[patent_title] => Engine component
[patent_app_type] => utility
[patent_app_number] => 14/633167
[patent_app_country] => US
[patent_app_date] => 2015-02-27
[patent_effective_date] => 0000-00-00
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/633167 | Engine component | Feb 26, 2015 | Issued |
Array
(
[id] => 14006547
[patent_doc_number] => 10221716
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2019-03-05
[patent_title] => Turbine abradable layer with inclined angle surface ridge or groove pattern
[patent_app_type] => utility
[patent_app_number] => 15/118996
[patent_app_country] => US
[patent_app_date] => 2015-02-18
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15118996
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/118996 | Turbine abradable layer with inclined angle surface ridge or groove pattern | Feb 17, 2015 | Issued |
Array
(
[id] => 10149682
[patent_doc_number] => 09181961
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2015-11-10
[patent_title] => 'Compressor intake noise prevention by choking flow with duct geometry'
[patent_app_type] => utility
[patent_app_number] => 14/623897
[patent_app_country] => US
[patent_app_date] => 2015-02-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[patent_no_of_words] => 3961
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14623897
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/623897 | Compressor intake noise prevention by choking flow with duct geometry | Feb 16, 2015 | Issued |
Array
(
[id] => 11312581
[patent_doc_number] => 20160348691
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-12-01
[patent_title] => 'GAS TURBINE ENGINE AIRFOIL'
[patent_app_type] => utility
[patent_app_number] => 15/114922
[patent_app_country] => US
[patent_app_date] => 2015-02-12
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/114922 | Gas turbine engine airfoil | Feb 11, 2015 | Issued |
Array
(
[id] => 11018746
[patent_doc_number] => 20160215700
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-07-28
[patent_title] => 'INNER FIXED STRUCTURE ACOUSTIC PANEL WITH DIRECTIONAL PERFORATIONS'
[patent_app_type] => utility
[patent_app_number] => 14/604233
[patent_app_country] => US
[patent_app_date] => 2015-01-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14604233
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/604233 | INNER FIXED STRUCTURE ACOUSTIC PANEL WITH DIRECTIONAL PERFORATIONS | Jan 22, 2015 | |
Array
(
[id] => 10240266
[patent_doc_number] => 20150125261
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-05-07
[patent_title] => 'VALVE SEQUENCING SYSTEM AND METHOD FOR CONTROLLING TURBOMACHINE ACOUSTIC SIGNATURE'
[patent_app_type] => utility
[patent_app_number] => 14/597333
[patent_app_country] => US
[patent_app_date] => 2015-01-15
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14597333
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/597333 | Valve sequencing system and method for controlling turbomachine acoustic signature | Jan 14, 2015 | Issued |
Array
(
[id] => 11364852
[patent_doc_number] => 20170002832
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-01-05
[patent_title] => 'VACUUM PUMP'
[patent_app_type] => utility
[patent_app_number] => 15/115094
[patent_app_country] => US
[patent_app_date] => 2015-01-08
[patent_effective_date] => 0000-00-00
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/115094 | Vacuum pump | Jan 7, 2015 | Issued |
Array
(
[id] => 10225615
[patent_doc_number] => 20150110607
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-04-23
[patent_title] => 'VARIABLE NOZZLE UNIT AND VARIABLE GEOMETRY SYSTEM TURBOCHARGER'
[patent_app_type] => utility
[patent_app_number] => 14/589316
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14589316
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/589316 | Variable nozzle unit and variable geometry system turbocharger | Jan 4, 2015 | Issued |
Array
(
[id] => 10313063
[patent_doc_number] => 20150198065
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-07-16
[patent_title] => 'TURBOMACHINE ASSEMBLY COMPRISING TWO BODIES AND MEANS FOR GUIDING A FLUID FLOWING FROM ONE BODY TO THE OTHER'
[patent_app_type] => utility
[patent_app_number] => 14/583910
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14583910
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/583910 | Turbomachine assembly comprising two bodies and means for guiding a fluid flowing from one body to the other | Dec 28, 2014 | Issued |
Array
(
[id] => 10299536
[patent_doc_number] => 20150184535
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-07-02
[patent_title] => 'ACTIVE SYNCHRONIZING RING'
[patent_app_type] => utility
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/576858 | Active synchronizing ring | Dec 18, 2014 | Issued |
Array
(
[id] => 10821613
[patent_doc_number] => 20160167777
[patent_country] => US
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[patent_issue_date] => 2016-06-16
[patent_title] => 'ROTOR ASSEMBLY APPARATUS'
[patent_app_type] => utility
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/570709 | Rotor assembly apparatus | Dec 14, 2014 | Issued |
Array
(
[id] => 10233027
[patent_doc_number] => 20150118021
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[patent_kind] => A1
[patent_issue_date] => 2015-04-30
[patent_title] => 'ROTARY PUMP WITH THRUST BEARINGS'
[patent_app_type] => utility
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/567194 | Rotary pump with thrust bearings | Dec 10, 2014 | Issued |
Array
(
[id] => 13637703
[patent_doc_number] => 09845808
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[patent_issue_date] => 2017-12-19
[patent_title] => Spherical sleeve and bushing bearing for centrifugal pump stage
[patent_app_type] => utility
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/565543 | Spherical sleeve and bushing bearing for centrifugal pump stage | Dec 9, 2014 | Issued |
Array
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Array
(
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/559527 | Aircraft gas turbine having a core engine casing with cooling-air tubes | Dec 2, 2014 | Issued |