
Adam Wayne Brown
Examiner (ID: 2689, Phone: (571)270-3372 , Office: P/3745 )
| Most Active Art Unit | 3745 |
| Art Unit(s) | 3745 |
| Total Applications | 523 |
| Issued Applications | 367 |
| Pending Applications | 1 |
| Abandoned Applications | 155 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 10219334
[patent_doc_number] => 20150104327
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-04-16
[patent_title] => 'TURBINE ROTOR BLADES WITH TIP PORTION PARAPET WALL CAVITIES'
[patent_app_type] => utility
[patent_app_number] => 14/055568
[patent_app_country] => US
[patent_app_date] => 2013-10-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 5546
[patent_no_of_claims] => 20
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14055568
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/055568 | Turbine rotor blades with tip portion parapet wall cavities | Oct 15, 2013 | Issued |
Array
(
[id] => 12429789
[patent_doc_number] => 09976439
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2018-05-22
[patent_title] => Method for differentiating control failures in a system for controlling an actuator, in particular of a stator of a gas-turbine engine
[patent_app_type] => utility
[patent_app_number] => 14/437489
[patent_app_country] => US
[patent_app_date] => 2013-09-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14437489
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/437489 | Method for differentiating control failures in a system for controlling an actuator, in particular of a stator of a gas-turbine engine | Sep 23, 2013 | Issued |
Array
(
[id] => 9926986
[patent_doc_number] => 20150075179
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-03-19
[patent_title] => 'Systems and Methods for Modifying a Pressure Side on an Airfoil About a Trailing Edge'
[patent_app_type] => utility
[patent_app_number] => 14/031206
[patent_app_country] => US
[patent_app_date] => 2013-09-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14031206
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/031206 | Systems and methods for modifying a pressure side on an airfoil about a trailing edge | Sep 18, 2013 | Issued |
Array
(
[id] => 9930708
[patent_doc_number] => 20150078900
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-03-19
[patent_title] => 'TURBINE BLADE WITH AIRFOIL TIP HAVING CUTTING TIPS'
[patent_app_type] => utility
[patent_app_number] => 14/031457
[patent_app_country] => US
[patent_app_date] => 2013-09-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_no_of_words] => 2871
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/031457 | TURBINE BLADE WITH AIRFOIL TIP HAVING CUTTING TIPS | Sep 18, 2013 | Abandoned |
Array
(
[id] => 12099649
[patent_doc_number] => 09856739
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2018-01-02
[patent_title] => 'Turbine blades with tip portions having converging cooling holes'
[patent_app_type] => utility
[patent_app_number] => 14/030647
[patent_app_country] => US
[patent_app_date] => 2013-09-18
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/030647 | Turbine blades with tip portions having converging cooling holes | Sep 17, 2013 | Issued |
Array
(
[id] => 11881508
[patent_doc_number] => 09752672
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2017-09-05
[patent_title] => 'Transmission turbo machine'
[patent_app_type] => utility
[patent_app_number] => 14/030832
[patent_app_country] => US
[patent_app_date] => 2013-09-18
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14030832
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/030832 | Transmission turbo machine | Sep 17, 2013 | Issued |
Array
(
[id] => 9362558
[patent_doc_number] => 20140072431
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-03-13
[patent_title] => 'Multi-Part Modular Airfoil Section and Method of Attachment Between Parts'
[patent_app_type] => utility
[patent_app_number] => 14/021094
[patent_app_country] => US
[patent_app_date] => 2013-09-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
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[patent_no_of_words] => 12362
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14021094
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/021094 | Multi-part modular airfoil section and method of attachment between parts | Sep 8, 2013 | Issued |
Array
(
[id] => 10362400
[patent_doc_number] => 20150247406
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-09-03
[patent_title] => 'METHOD FOR ASSEMBLING AND DISASSEMBLING A ROTOR HAVING A NUMBER OF ROTOR COMPONENTS OF AN AXIAL FLOW TURBOMACHINE AND SUCH A ROTOR'
[patent_app_type] => utility
[patent_app_number] => 14/425016
[patent_app_country] => US
[patent_app_date] => 2013-09-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 3334
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14425016
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/425016 | METHOD FOR ASSEMBLING AND DISASSEMBLING A ROTOR HAVING A NUMBER OF ROTOR COMPONENTS OF AN AXIAL FLOW TURBOMACHINE AND SUCH A ROTOR | Sep 5, 2013 | Abandoned |
Array
(
[id] => 10777176
[patent_doc_number] => 20160123332
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-05-05
[patent_title] => 'ROTARY MACHINE'
[patent_app_type] => utility
[patent_app_number] => 14/898705
[patent_app_country] => US
[patent_app_date] => 2013-09-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14898705
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/898705 | Rotary machine | Sep 5, 2013 | Issued |
Array
(
[id] => 10313047
[patent_doc_number] => 20150198048
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-07-16
[patent_title] => 'METHOD FOR PRODUCING A STATOR BLADE AND STATOR BLADE'
[patent_app_type] => utility
[patent_app_number] => 14/415480
[patent_app_country] => US
[patent_app_date] => 2013-07-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_no_of_words] => 2785
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14415480
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/415480 | METHOD FOR PRODUCING A STATOR BLADE AND STATOR BLADE | Jul 14, 2013 | Abandoned |
Array
(
[id] => 10800023
[patent_doc_number] => 20160146181
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-05-26
[patent_title] => 'WING AND TURBINE CONFIGURATION FOR POWER PLANT'
[patent_app_type] => utility
[patent_app_number] => 14/904361
[patent_app_country] => US
[patent_app_date] => 2013-07-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14904361
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/904361 | Wing and turbine configuration for power plant | Jul 11, 2013 | Issued |
Array
(
[id] => 10282486
[patent_doc_number] => 20150167485
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-06-18
[patent_title] => 'SEALING ARRANGEMENT OF A STEAM TURBINE IN WHICH A SEALING LIQUID AND A VAPOR STEAM EXTRACTION SYSTEM ARE USED'
[patent_app_type] => utility
[patent_app_number] => 14/415387
[patent_app_country] => US
[patent_app_date] => 2013-06-17
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/415387 | Sealing arrangement of a steam turbine in which a sealing liquid and a vapor steam extraction system are used | Jun 16, 2013 | Issued |
Array
(
[id] => 9106962
[patent_doc_number] => 20130280094
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-10-24
[patent_title] => 'GAS TURBINE BLADE AND GAS TURBINE HAVING THE SAME'
[patent_app_type] => utility
[patent_app_number] => 13/919324
[patent_app_country] => US
[patent_app_date] => 2013-06-17
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/919324 | GAS TURBINE BLADE AND GAS TURBINE HAVING THE SAME | Jun 16, 2013 | Abandoned |
Array
(
[id] => 9195501
[patent_doc_number] => 20130334816
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-12-19
[patent_title] => 'Method for Operating a Wave Energy Converter for Converting Energy from a Wave Motion of a Fluid into another Form of Energy'
[patent_app_type] => utility
[patent_app_number] => 13/916320
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Array
(
[id] => 10966800
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[patent_title] => 'Methods and Systems for Blade Health Monitoring'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/916179 | Methods and systems for blade health monitoring | Jun 11, 2013 | Issued |
Array
(
[id] => 10274677
[patent_doc_number] => 20150159674
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-06-11
[patent_title] => 'TURBO COMPRESSOR SYSTEM HAVING AT LEAST TWO DRIVING MOTORS'
[patent_app_type] => utility
[patent_app_number] => 14/403377
[patent_app_country] => US
[patent_app_date] => 2013-05-27
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/403377 | TURBO COMPRESSOR SYSTEM HAVING AT LEAST TWO DRIVING MOTORS | May 26, 2013 | Abandoned |
Array
(
[id] => 10938703
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[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-11-20
[patent_title] => 'STATIC CORE TIE RODS'
[patent_app_type] => utility
[patent_app_number] => 13/893508
[patent_app_country] => US
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13893508
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/893508 | Static core tie rods | May 13, 2013 | Issued |
Array
(
[id] => 9338186
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[patent_title] => 'Propeller for an aircraft engine comprising means for reducing noise at middle and high frequencies and improving the acoustic perception'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/894076 | Propeller for an aircraft engine comprising means for reducing noise at middle and high frequencies and improving the acoustic perception | May 13, 2013 | Issued |
Array
(
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/893729 | Seal system including angular features for rotary machine components | May 13, 2013 | Issued |
Array
(
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[patent_title] => 'Centrifugal compressor with casing treatment for surge control'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/893675 | Centrifugal compressor with casing treatment for surge control | May 13, 2013 | Issued |