JP5698986B2 - ステータプラズマアクチュエータを用いた不安定性軽減システム - Google Patents
ステータプラズマアクチュエータを用いた不安定性軽減システム Download PDFInfo
- Publication number
- JP5698986B2 JP5698986B2 JP2010540908A JP2010540908A JP5698986B2 JP 5698986 B2 JP5698986 B2 JP 5698986B2 JP 2010540908 A JP2010540908 A JP 2010540908A JP 2010540908 A JP2010540908 A JP 2010540908A JP 5698986 B2 JP5698986 B2 JP 5698986B2
- Authority
- JP
- Japan
- Prior art keywords
- rotor
- instability
- gas turbine
- plasma actuator
- blade
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D27/00—Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
- F04D27/001—Testing thereof; Determination or simulation of flow characteristics; Stall or surge detection, e.g. condition monitoring
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D27/00—Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D27/00—Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
- F04D27/02—Surge control
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/40—Casings; Connections of working fluid
- F04D29/52—Casings; Connections of working fluid for axial pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/40—Casings; Connections of working fluid
- F04D29/52—Casings; Connections of working fluid for axial pumps
- F04D29/522—Casings; Connections of working fluid for axial pumps especially adapted for elastic fluid pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/40—Casings; Connections of working fluid
- F04D29/52—Casings; Connections of working fluid for axial pumps
- F04D29/522—Casings; Connections of working fluid for axial pumps especially adapted for elastic fluid pumps
- F04D29/526—Details of the casing section radially opposing blade tips
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2270/00—Control
- F05D2270/01—Purpose of the control system
- F05D2270/10—Purpose of the control system to cope with, or avoid, compressor flow instabilities
- F05D2270/101—Compressor surge or stall
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2270/00—Control
- F05D2270/01—Purpose of the control system
- F05D2270/17—Purpose of the control system to control boundary layer
- F05D2270/172—Purpose of the control system to control boundary layer by a plasma generator, e.g. control of ignition
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Control Of Positive-Displacement Air Blowers (AREA)
- Control Of Turbines (AREA)
- Supercharger (AREA)
- Non-Positive Displacement Air Blowers (AREA)
Description
Claims (7)
- (a)中心線軸(8)を有するロータハブ(39)の周囲に動翼(40)の列を有するロータ(12a)と、
(b)前記ロータ(12a)に軸方向に近接して配置されており、各々が静翼翼形(35)を有する、前記中心線軸(8)の周囲に配列された複数の静翼(31a)の列を有するステータ段(31)と、
(c)不安定性軽減システム(700)であって、
(c1)前記ロータ(12a)の動作中に前記ロータ(12a)における不安定性の発生を検出するための検出システム(500)であって、ロータ速度信号(506)を供給する手段、前記動翼(40)の先端(46)から半径方向外方に離れて配置された圧力センサ(502)から圧力信号(504)を供給する手段、並びに前記ロータ速度信号(506)及び圧力信号(504)を含む入力信号を受信し、安定性相関信号(512)を発生させることのできる相関プロセッサ(510)を備える検出システム(500)と、
(c2)前記ステータ段(31)の静翼(31a)の少なくとも1つに取り付けられた少なくとも1つのプラズマアクチュエータ(82)を備え、前記検出システム(500)が不安定性の発生を検出した場合に前記ロータ(12a)を安定化させる軽減システム(300)と、
(c3)前記検出システム(500)及び前記軽減システム(300)の動作を制御するための制御システム(74)であって、前記プラズマアクチュエータ(82)の第1電極(62)及び第2電極(64)に接続されたAC電源(70)の動作を制御する制御装置(72)を備える制御システム(74)と
を備える不安定性軽減システム(700)と
を備えるガスタービン圧縮システム。 - 前記検出システム(500)が、前記ロータ(12a)上に円周方向に配列された動翼(40)の列の先端(46)から半径方向外方に離間配置された静的要素(50)上に配置されたセンサ(502)を備える、請求項1に記載のガスタービン圧縮システム。
- 前記センサ(502)が、動翼(40)の先端(46)付近の場所における流動パラメータに対応する入力信号(504)を発生させることができる、請求項2に記載のガスタービン圧縮システム。
- 前記制御システム(74)が、制御装置(72)に不安定性制御信号(606)を送信することによって、前記制御装置(72)の動作を制御する不安定性制御システム(600)を備える、請求項1乃至請求項3のいずれか1項に記載のガスタービン圧縮システム。
- 前記制御装置(72)が、所定の周波数又は同相又は異相でのパルシングによって前記プラズマアクチュエータ(82)を制御する、請求項1乃至請求項4のいずれか1項に記載のガスタービン圧縮システム。
- 前記ステータ段(31)が入口案内翼(30)を備えており、前記プラズマアクチュエータ(82)が前記入口案内翼(30)上に取り付けられる、請求項1乃至請求項5のいずれか1項に記載のガスタービン圧縮システム。
- 前記プラズマアクチュエータ(82)が可動入口案内翼フラップ(32)上に取り付けられる、請求項6に記載のガスタービン圧縮システム。
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US11/966,503 US20090169363A1 (en) | 2007-12-28 | 2007-12-28 | Plasma Enhanced Stator |
US11/966,503 | 2007-12-28 | ||
PCT/US2008/088370 WO2009086481A1 (en) | 2007-12-28 | 2008-12-26 | Instability mitigation system using stator plasma actuators |
Publications (2)
Publication Number | Publication Date |
---|---|
JP2011508159A JP2011508159A (ja) | 2011-03-10 |
JP5698986B2 true JP5698986B2 (ja) | 2015-04-08 |
Family
ID=40457041
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2010540908A Expired - Fee Related JP5698986B2 (ja) | 2007-12-28 | 2008-12-26 | ステータプラズマアクチュエータを用いた不安定性軽減システム |
JP2010540907A Pending JP2011508158A (ja) | 2007-12-28 | 2008-12-26 | プラズマアクチュエータを備えた圧縮機及びガスタービンエンジン |
Family Applications After (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2010540907A Pending JP2011508158A (ja) | 2007-12-28 | 2008-12-26 | プラズマアクチュエータを備えた圧縮機及びガスタービンエンジン |
Country Status (6)
Country | Link |
---|---|
US (1) | US20090169363A1 (ja) |
JP (2) | JP5698986B2 (ja) |
CA (2) | CA2710003A1 (ja) |
DE (2) | DE112008003484T5 (ja) |
GB (2) | GB2468248A (ja) |
WO (2) | WO2009086481A1 (ja) |
Families Citing this family (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20100205928A1 (en) * | 2007-12-28 | 2010-08-19 | Moeckel Curtis W | Rotor stall sensor system |
US20100290906A1 (en) * | 2007-12-28 | 2010-11-18 | Moeckel Curtis W | Plasma sensor stall control system and turbomachinery diagnostics |
US8282336B2 (en) * | 2007-12-28 | 2012-10-09 | General Electric Company | Instability mitigation system |
US20090169356A1 (en) * | 2007-12-28 | 2009-07-02 | Aspi Rustom Wadia | Plasma Enhanced Compression System |
US8348592B2 (en) * | 2007-12-28 | 2013-01-08 | General Electric Company | Instability mitigation system using rotor plasma actuators |
US20100047060A1 (en) * | 2007-12-28 | 2010-02-25 | Aspi Rustom Wadia | Plasma Enhanced Compressor |
US8282337B2 (en) * | 2007-12-28 | 2012-10-09 | General Electric Company | Instability mitigation system using stator plasma actuators |
US20100047055A1 (en) * | 2007-12-28 | 2010-02-25 | Aspi Rustom Wadia | Plasma Enhanced Rotor |
US20100284785A1 (en) * | 2007-12-28 | 2010-11-11 | Aspi Rustom Wadia | Fan Stall Detection System |
US20100284795A1 (en) * | 2007-12-28 | 2010-11-11 | General Electric Company | Plasma Clearance Controlled Compressor |
US8317457B2 (en) * | 2007-12-28 | 2012-11-27 | General Electric Company | Method of operating a compressor |
US7984614B2 (en) * | 2008-11-17 | 2011-07-26 | Honeywell International Inc. | Plasma flow controlled diffuser system |
US20100172747A1 (en) * | 2009-01-08 | 2010-07-08 | General Electric Company | Plasma enhanced compressor duct |
US20100170224A1 (en) * | 2009-01-08 | 2010-07-08 | General Electric Company | Plasma enhanced booster and method of operation |
US8585356B2 (en) * | 2010-03-23 | 2013-11-19 | Siemens Energy, Inc. | Control of blade tip-to-shroud leakage in a turbine engine by directed plasma flow |
US8500404B2 (en) | 2010-04-30 | 2013-08-06 | Siemens Energy, Inc. | Plasma actuator controlled film cooling |
US20130180245A1 (en) * | 2012-01-12 | 2013-07-18 | General Electric Company | Gas turbine exhaust diffuser having plasma actuator |
US9359950B2 (en) | 2013-05-20 | 2016-06-07 | Honeywell International Inc. | Gas turbine engines having plasma flow-controlled intake systems |
EP2963241B1 (fr) * | 2014-06-30 | 2019-03-06 | Safran Aero Boosters SA | Élément de guidage de flux gazeux de turbomachine |
US10221720B2 (en) | 2014-09-03 | 2019-03-05 | Honeywell International Inc. | Structural frame integrated with variable-vectoring flow control for use in turbine systems |
US10371050B2 (en) * | 2014-12-23 | 2019-08-06 | Rolls-Royce Corporation | Gas turbine engine with rotor blade tip clearance flow control |
US10487679B2 (en) * | 2017-07-17 | 2019-11-26 | United Technologies Corporation | Method and apparatus for sealing components of a gas turbine engine with a dielectric barrier discharge plasma actuator |
JP7116541B2 (ja) * | 2017-11-30 | 2022-08-10 | 三菱重工業株式会社 | 回転機械の翼の状態の監視センサ及びセンサの位置調節方法 |
Family Cites Families (43)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2594042A (en) * | 1947-05-21 | 1952-04-22 | United Aircraft Corp | Boundary layer energizing means for annular diffusers |
US3300121A (en) * | 1965-02-24 | 1967-01-24 | Gen Motors Corp | Axial-flow compressor |
GB8610297D0 (en) * | 1986-04-28 | 1986-10-01 | Rolls Royce | Turbomachinery |
JPS6388300A (ja) * | 1986-10-02 | 1988-04-19 | Toshiba Corp | 軸流圧縮機のサ−ジング監視方法および装置 |
GB2245316B (en) * | 1990-06-21 | 1993-12-15 | Rolls Royce Plc | Improvements in shroud assemblies for turbine rotors |
AU4637293A (en) * | 1992-08-10 | 1994-03-03 | Dow Deutschland Inc. | Process and device for monitoring and for controlling of a compressor |
WO1999035893A2 (en) * | 1998-01-08 | 1999-07-15 | The University Of Tennessee Research Corporation | Paraelectric gas flow accelerator |
US6793455B2 (en) * | 2001-02-08 | 2004-09-21 | Georgia Tech Research Corporation | Method and apparatus for active control of surge in compressors |
US6438484B1 (en) * | 2001-05-23 | 2002-08-20 | General Electric Company | Method and apparatus for detecting and compensating for compressor surge in a gas turbine using remote monitoring and diagnostics |
JP2002364582A (ja) * | 2001-06-11 | 2002-12-18 | Ishikawajima Harima Heavy Ind Co Ltd | 軸流圧縮機におけるストール予知方法 |
FR2835019B1 (fr) * | 2002-01-22 | 2004-12-31 | Snecma Moteurs | Diffuseur pour moteur a turbine a gaz terrestre ou aeronautique |
US6619916B1 (en) * | 2002-02-28 | 2003-09-16 | General Electric Company | Methods and apparatus for varying gas turbine engine inlet air flow |
US6666017B2 (en) * | 2002-05-24 | 2003-12-23 | General Electric Company | Counterrotatable booster compressor assembly for a gas turbine engine |
US20040011917A1 (en) * | 2002-07-18 | 2004-01-22 | Saeks Richard E. | Shock wave modification via shock induced ion doping |
US6871487B2 (en) * | 2003-02-14 | 2005-03-29 | Kulite Semiconductor Products, Inc. | System for detecting and compensating for aerodynamic instabilities in turbo-jet engines |
US7334394B2 (en) * | 2003-09-02 | 2008-02-26 | The Ohio State University | Localized arc filament plasma actuators for noise mitigation and mixing enhancement |
US7183515B2 (en) * | 2004-12-20 | 2007-02-27 | Lockhead-Martin Corporation | Systems and methods for plasma jets |
US7159401B1 (en) * | 2004-12-23 | 2007-01-09 | Kulite Semiconductor Products, Inc. | System for detecting and compensating for aerodynamic instabilities in turbo-jet engines |
DE102006008864B4 (de) * | 2006-02-25 | 2013-08-22 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Strömungsflächenelement |
WO2007127245A2 (en) * | 2006-04-28 | 2007-11-08 | Johnson Controls Technology Company | Battery module assembly |
JP5060163B2 (ja) * | 2006-04-28 | 2012-10-31 | 株式会社東芝 | 翼 |
US7827803B1 (en) * | 2006-09-27 | 2010-11-09 | General Electric Company | Method and apparatus for an aerodynamic stability management system |
US7819626B2 (en) * | 2006-10-13 | 2010-10-26 | General Electric Company | Plasma blade tip clearance control |
US7766599B2 (en) * | 2006-10-31 | 2010-08-03 | General Electric Company | Plasma lifted boundary layer gas turbine engine vane |
US8006939B2 (en) * | 2006-11-22 | 2011-08-30 | Lockheed Martin Corporation | Over-wing traveling-wave axial flow plasma accelerator |
US7870720B2 (en) * | 2006-11-29 | 2011-01-18 | Lockheed Martin Corporation | Inlet electromagnetic flow control |
US7695241B2 (en) * | 2006-11-30 | 2010-04-13 | General Electric Company | Downstream plasma shielded film cooling |
US7588413B2 (en) * | 2006-11-30 | 2009-09-15 | General Electric Company | Upstream plasma shielded film cooling |
US7628585B2 (en) * | 2006-12-15 | 2009-12-08 | General Electric Company | Airfoil leading edge end wall vortex reducing plasma |
US7736123B2 (en) * | 2006-12-15 | 2010-06-15 | General Electric Company | Plasma induced virtual turbine airfoil trailing edge extension |
JP5004079B2 (ja) * | 2007-04-24 | 2012-08-22 | 独立行政法人産業技術総合研究所 | 表面プラズマアクチュエータ |
US20100047060A1 (en) * | 2007-12-28 | 2010-02-25 | Aspi Rustom Wadia | Plasma Enhanced Compressor |
US8348592B2 (en) * | 2007-12-28 | 2013-01-08 | General Electric Company | Instability mitigation system using rotor plasma actuators |
US8282337B2 (en) * | 2007-12-28 | 2012-10-09 | General Electric Company | Instability mitigation system using stator plasma actuators |
US20100284795A1 (en) * | 2007-12-28 | 2010-11-11 | General Electric Company | Plasma Clearance Controlled Compressor |
US8282336B2 (en) * | 2007-12-28 | 2012-10-09 | General Electric Company | Instability mitigation system |
US20100284785A1 (en) * | 2007-12-28 | 2010-11-11 | Aspi Rustom Wadia | Fan Stall Detection System |
US20090169356A1 (en) * | 2007-12-28 | 2009-07-02 | Aspi Rustom Wadia | Plasma Enhanced Compression System |
US8317457B2 (en) * | 2007-12-28 | 2012-11-27 | General Electric Company | Method of operating a compressor |
US8006497B2 (en) * | 2008-05-30 | 2011-08-30 | Honeywell International Inc. | Diffusers, diffusion systems, and methods for controlling airflow through diffusion systems |
US7984614B2 (en) * | 2008-11-17 | 2011-07-26 | Honeywell International Inc. | Plasma flow controlled diffuser system |
US20100172747A1 (en) * | 2009-01-08 | 2010-07-08 | General Electric Company | Plasma enhanced compressor duct |
US20100170224A1 (en) * | 2009-01-08 | 2010-07-08 | General Electric Company | Plasma enhanced booster and method of operation |
-
2007
- 2007-12-28 US US11/966,503 patent/US20090169363A1/en not_active Abandoned
-
2008
- 2008-12-26 JP JP2010540908A patent/JP5698986B2/ja not_active Expired - Fee Related
- 2008-12-26 DE DE112008003484T patent/DE112008003484T5/de not_active Ceased
- 2008-12-26 CA CA2710003A patent/CA2710003A1/en not_active Abandoned
- 2008-12-26 GB GB1010140A patent/GB2468248A/en not_active Withdrawn
- 2008-12-26 JP JP2010540907A patent/JP2011508158A/ja active Pending
- 2008-12-26 GB GB1010131.9A patent/GB2467507B/en not_active Expired - Fee Related
- 2008-12-26 CA CA2710000A patent/CA2710000A1/en not_active Abandoned
- 2008-12-26 WO PCT/US2008/088370 patent/WO2009086481A1/en active Application Filing
- 2008-12-26 DE DE112008003483T patent/DE112008003483T5/de not_active Withdrawn
- 2008-12-26 WO PCT/US2008/088369 patent/WO2009086480A1/en active Application Filing
Also Published As
Publication number | Publication date |
---|---|
GB201010131D0 (en) | 2010-07-21 |
GB201010140D0 (en) | 2010-07-21 |
GB2468248A (en) | 2010-09-01 |
GB2467507B (en) | 2012-12-05 |
GB2467507A (en) | 2010-08-04 |
US20090169363A1 (en) | 2009-07-02 |
CA2710003A1 (en) | 2009-07-09 |
DE112008003483T5 (de) | 2010-12-23 |
JP2011508159A (ja) | 2011-03-10 |
CA2710000A1 (en) | 2009-07-09 |
JP2011508158A (ja) | 2011-03-10 |
WO2009086481A1 (en) | 2009-07-09 |
WO2009086480A1 (en) | 2009-07-09 |
DE112008003484T5 (de) | 2010-10-21 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
JP5698986B2 (ja) | ステータプラズマアクチュエータを用いた不安定性軽減システム | |
JP5518738B2 (ja) | ロータプラズマアクチュエータを使用する不安定性緩和システム | |
JP5410447B2 (ja) | ロータ用の不安定性緩和システム | |
US8282337B2 (en) | Instability mitigation system using stator plasma actuators | |
JP2011508154A (ja) | プラズマアクチュエータを備えた圧縮機およびガスタービンエンジン | |
US20090169356A1 (en) | Plasma Enhanced Compression System | |
JP5550563B2 (ja) | 圧縮機を動作させる方法 | |
JP2011508155A (ja) | ファンの失速検出システム | |
US20100284795A1 (en) | Plasma Clearance Controlled Compressor | |
US20100047060A1 (en) | Plasma Enhanced Compressor | |
US20100290906A1 (en) | Plasma sensor stall control system and turbomachinery diagnostics | |
WO2011133293A1 (en) | Fan stall detection system | |
US20100205928A1 (en) | Rotor stall sensor system |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
A621 | Written request for application examination |
Free format text: JAPANESE INTERMEDIATE CODE: A621 Effective date: 20111216 |
|
A977 | Report on retrieval |
Free format text: JAPANESE INTERMEDIATE CODE: A971007 Effective date: 20130424 |
|
A131 | Notification of reasons for refusal |
Free format text: JAPANESE INTERMEDIATE CODE: A131 Effective date: 20130507 |
|
A601 | Written request for extension of time |
Free format text: JAPANESE INTERMEDIATE CODE: A601 Effective date: 20130807 |
|
A602 | Written permission of extension of time |
Free format text: JAPANESE INTERMEDIATE CODE: A602 Effective date: 20130814 |
|
A601 | Written request for extension of time |
Free format text: JAPANESE INTERMEDIATE CODE: A601 Effective date: 20130906 |
|
A602 | Written permission of extension of time |
Free format text: JAPANESE INTERMEDIATE CODE: A602 Effective date: 20130913 |
|
A601 | Written request for extension of time |
Free format text: JAPANESE INTERMEDIATE CODE: A601 Effective date: 20131007 |
|
A602 | Written permission of extension of time |
Free format text: JAPANESE INTERMEDIATE CODE: A602 Effective date: 20131015 |
|
A02 | Decision of refusal |
Free format text: JAPANESE INTERMEDIATE CODE: A02 Effective date: 20140513 |
|
A521 | Request for written amendment filed |
Free format text: JAPANESE INTERMEDIATE CODE: A523 Effective date: 20140912 |
|
A911 | Transfer to examiner for re-examination before appeal (zenchi) |
Free format text: JAPANESE INTERMEDIATE CODE: A911 Effective date: 20141104 |
|
TRDD | Decision of grant or rejection written | ||
A01 | Written decision to grant a patent or to grant a registration (utility model) |
Free format text: JAPANESE INTERMEDIATE CODE: A01 Effective date: 20150120 |
|
A61 | First payment of annual fees (during grant procedure) |
Free format text: JAPANESE INTERMEDIATE CODE: A61 Effective date: 20150216 |
|
R150 | Certificate of patent or registration of utility model |
Ref document number: 5698986 Country of ref document: JP Free format text: JAPANESE INTERMEDIATE CODE: R150 |
|
LAPS | Cancellation because of no payment of annual fees |