JP4520306B2 - 遷音速巡航用の航空機 - Google Patents
遷音速巡航用の航空機 Download PDFInfo
- Publication number
- JP4520306B2 JP4520306B2 JP2004551807A JP2004551807A JP4520306B2 JP 4520306 B2 JP4520306 B2 JP 4520306B2 JP 2004551807 A JP2004551807 A JP 2004551807A JP 2004551807 A JP2004551807 A JP 2004551807A JP 4520306 B2 JP4520306 B2 JP 4520306B2
- Authority
- JP
- Japan
- Prior art keywords
- wing
- leading edge
- aircraft
- fuselage
- tail
- 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
- 230000007704 transition Effects 0.000 claims description 6
- 230000007423 decrease Effects 0.000 claims description 4
- 230000002028 premature Effects 0.000 claims description 2
- 238000007373 indentation Methods 0.000 abstract 1
- 230000000694 effects Effects 0.000 description 4
- 230000003247 decreasing effect Effects 0.000 description 2
- 230000002349 favourable effect Effects 0.000 description 2
- 230000002596 correlated effect Effects 0.000 description 1
- 230000003111 delayed effect Effects 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C30/00—Supersonic type aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/10—Shape of wings
- B64C3/14—Aerofoil profile
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/10—Shape of wings
- B64C3/14—Aerofoil profile
- B64C2003/146—Aerofoil profile comprising leading edges of particular shape
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/10—Drag reduction
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Toys (AREA)
- Exhaust Silencers (AREA)
- Structure Of Belt Conveyors (AREA)
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
- Tires In General (AREA)
- Motorcycle And Bicycle Frame (AREA)
Description
一方、最新鋭の戦闘機は、超音速ダッシュ能力をも有するようにするために、妥協の産物として、もっと薄い翼形、典型的には約3〜5%t/cの翼形を有し、それに合わせて前縁も後退しているが、アスペクト比は低く(3対5)、後縁はほとんど後退していない。
a)鋭さを落とした翼前縁近傍にキャンバ(Camber:下向き湾曲)を有する翼と、
b)翼側に沿って長さ方向に設けたくびれを有する胴体とを含む航空機を提供することにある。
・現在の亜音速巡航翼よりもかなり薄くて、2〜4%のt/cで現在の戦闘機と同様か或いはそれよりも薄いということ。
・現在の戦闘機よりも前縁後退角がかなり緩くて、後退角は大体20度以下で、Tracyが以前に特許権を取得した層流超音速翼と同様か或いはそれよりも小さいということ。
・前縁の鋭さをわずかに落としてあり、特に、(従来のTracy特許の鋭利でほぼ両凸面状の超音速翼形と比較して)、キャンバ(camber)を付けて成形された翼形となっていること。
重量と巡航効率との妥協策として、低から中のアスペクト比であること。
・「エリア・ルール(area-ruled)」胴体に関連して局部的に厚くした内側部分。
・低横流れおよび広範な領域にわたる有利な翼弦方向圧力勾配の結果として、従来の後退翼で可能なよりも、かなり広範囲にわたり層流が存在することによる表面摩擦の低下。
・圧縮性抗力上昇の発生が、典型的なもっと厚い後退翼や三角翼の場合に対するよりも、相当に薄い非後退翼により、更に高い亜音速マッハ数まで「遅らされる」ということ。
・たとえ後退翼が等しいアスペクト比を有するとした場合でも、本発明の非後退翼は、後退翼よりも小さい迎角とすることで離発着性能を向上したこと。
図6に示すように、分析によると、本発明による翼は、マッハ0.9〜1.0間の高亜音速範囲で、現行の後退翼よりかなり優れた「抗力特性 対 マッハ数」を有することがわかっている。
Claims (8)
- 翼及び胴体を有する遷音速巡航のための航空機であって、前記翼は前縁後退角を有し、 前記胴体は翼側に沿って長さ方向に細長く外側に凹状のくびれを有し、
a)前記翼は、翼長方向平均として、3%未満の最大翼厚対翼弦比を有し、
b)前記翼は、そのほぼ全長にわたって鋭さを落とした前縁又はその近傍にキャンバを有し、翼長方向の場所における該落とした鋭さは、前記場所での最大翼形翼厚の1/2%〜3%であり、
c)前記翼は、その大部分にわたって横流れ不安定性(crossflow instability)が臨界未満レベルにまで減じられるように、20度未満の前縁後退角を有する、ことを特徴とする航空機。 - 翼付け根から翼外側先端部の長さまでの前記場所において、前記最大翼厚対翼弦比が3.5〜1.5%で変化することを特徴とする請求項1に記載の航空機。
- 前記翼の厚さは、前記場所で、最大翼厚のゾーンから前方及び後方に徐々に減少し、前記翼は先端を鈍化させた前縁から生ずる滑らかで有利な圧力勾配を、亜音速設計飛行条件で可能な限り翼面に沿って後方位置まで維持するように設計してある凸面状になる上、下翼面を有することを特徴とする請求項2に記載の航空機。
- 前記翼は、設計飛行条件で早期境界層遷移を生じさせないレベルに、横流れ圧力勾配(crossflow pressure gradients)を制限するのに必要とするような前縁後退角を有することを特徴とする請求項1乃至3のいずれかに記載の航空機。
- 前記くびれを含んだ胴体の各々の側部に位置する前記翼は、全体的に台形の形態を有することを特徴とする請求項1乃至4のいずれかに記載の航空機。
- 前記胴体は、翼前縁の胴体側端部近傍の位置で幅w1を有し、後縁端部の胴体側端部近傍の位置で幅w2を有し、w1>w2であることを特徴とする請求項1乃至5のいずれかに記載の航空機。
- 前記胴体の後端に尾翼を含み、該胴体の相対向する両側に、前記翼と前記尾翼の間に位置して、エンジン・ナセル(エンジン室)があることを特徴とする請求項1乃至6のいずれかに記載の航空機。
- 前記尾翼は、左尾翼と右尾翼とを含み、それら左右の尾翼は、最大翼厚ゾーンから前方および後方へ厚さを徐々に減じており、全体的に凸面状の上、下尾翼面が、先端を鈍化させた前縁から生ずる滑らかで有利な圧力勾配を、亜音速設計飛行条件で可能な限り尾翼表面に沿って後方位置まで維持するように設計してあることを特徴とする請求項8に記載の航空機。
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US42403902P | 2002-11-07 | 2002-11-07 | |
US10/693,411 US7000870B2 (en) | 2002-11-07 | 2003-10-23 | Laminar flow wing for transonic cruise |
PCT/US2003/035393 WO2004043780A2 (en) | 2002-11-07 | 2003-11-06 | Laminar flow wing for transonic cruise |
Publications (2)
Publication Number | Publication Date |
---|---|
JP2006517162A JP2006517162A (ja) | 2006-07-20 |
JP4520306B2 true JP4520306B2 (ja) | 2010-08-04 |
Family
ID=32314520
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2004551807A Expired - Fee Related JP4520306B2 (ja) | 2002-11-07 | 2003-11-06 | 遷音速巡航用の航空機 |
Country Status (9)
Country | Link |
---|---|
US (1) | US7000870B2 (ja) |
EP (1) | EP1583690B1 (ja) |
JP (1) | JP4520306B2 (ja) |
AT (1) | ATE455034T1 (ja) |
AU (1) | AU2003287542B2 (ja) |
BR (1) | BR0316038B1 (ja) |
CA (1) | CA2503270C (ja) |
DE (1) | DE60331004D1 (ja) |
WO (1) | WO2004043780A2 (ja) |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20060289679A1 (en) * | 2005-06-27 | 2006-12-28 | Johnson Kaj A | Modular sprayer |
US8272594B2 (en) * | 2009-10-26 | 2012-09-25 | Aerion Corporation | Laminar flow wing optimized for supersonic cruise aircraft |
US8317128B2 (en) * | 2009-10-26 | 2012-11-27 | Aerion Corporation | Laminar flow wing optimized for transonic cruise aircraft |
US8448893B2 (en) * | 2009-10-26 | 2013-05-28 | Aerion Corporation | Laminar flow wing optimized for transonic cruise aircraft |
CN104897006A (zh) * | 2015-04-24 | 2015-09-09 | 江西洪都航空工业集团有限责任公司 | 一种靶机气动布局 |
CN106828875B (zh) * | 2016-12-27 | 2018-11-16 | 西北工业大学 | 一种适用于通用飞行器偏重爬升特性的层流翼型 |
EP3348470B1 (en) * | 2017-01-16 | 2019-03-06 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Airplane or vehicle with configuration of a t junction of a flow obstacle on a wall bounding a flow |
CN107444612B (zh) * | 2017-08-15 | 2023-04-18 | 中国空气动力研究与发展中心高速空气动力研究所 | 一种λ机翼飞翼布局无人飞行器的变机翼前缘装置 |
JP7038404B2 (ja) * | 2017-12-12 | 2022-03-18 | 国立研究開発法人宇宙航空研究開発機構 | 遷音速翼型、翼及び航空機 |
DE102019129998B4 (de) * | 2019-11-07 | 2022-04-28 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Flugzeug mit Strahltriebwerken oberhalb der Tragflügel und mit einer lokalen Erweiterung des Rumpfs zur Reduktion aerodynamischer Widerstände bei transsonischen Fluggeschwindigkeiten |
JP7015582B2 (ja) * | 2020-09-03 | 2022-02-03 | 国立研究開発法人宇宙航空研究開発機構 | 翼及び航空機 |
Family Cites Families (45)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2709052A (en) * | 1952-04-15 | 1955-05-24 | Charles J Fletcher | Spanwise flow control of fluid swept lifting surfaces |
US2997256A (en) * | 1955-01-14 | 1961-08-22 | James H Walker | Supersonic aircraft |
US2874922A (en) * | 1956-08-24 | 1959-02-24 | Richard T Whitcomb | Fuselage shaping to reduce the strength of shock waves about airplanes at transonic and supersonic speeds |
US4050651A (en) * | 1976-06-24 | 1977-09-27 | The Gates Rubber Company | Wing and reduced airspeed system for jet aircraft |
US4280815A (en) * | 1979-06-18 | 1981-07-28 | Technicon Instruments Corporation | Electrochemiluminescent immunoassay and apparatus therefor |
US4652533A (en) * | 1983-04-28 | 1987-03-24 | Pandex Laboratories, Inc. | Method of solid phase immunoassay incorporating a luminescent label |
US4826759A (en) * | 1984-10-04 | 1989-05-02 | Bio-Metric Systems, Inc. | Field assay for ligands |
US5238808A (en) * | 1984-10-31 | 1993-08-24 | Igen, Inc. | Luminescent metal chelate labels and means for detection |
US5221605A (en) * | 1984-10-31 | 1993-06-22 | Igen, Inc. | Luminescent metal chelate labels and means for detection |
US5310687A (en) * | 1984-10-31 | 1994-05-10 | Igen, Inc. | Luminescent metal chelate labels and means for detection |
US4663230A (en) * | 1984-12-06 | 1987-05-05 | Hyperion Catalysis International, Inc. | Carbon fibrils, method for producing same and compositions containing same |
US5165909A (en) * | 1984-12-06 | 1992-11-24 | Hyperion Catalysis Int'l., Inc. | Carbon fibrils and method for producing same |
US5171560A (en) * | 1984-12-06 | 1992-12-15 | Hyperion Catalysis International | Carbon fibrils, method for producing same, and encapsulated catalyst |
US5468606A (en) * | 1989-09-18 | 1995-11-21 | Biostar, Inc. | Devices for detection of an analyte based upon light interference |
US5591581A (en) * | 1986-04-30 | 1997-01-07 | Igen, Inc. | Electrochemiluminescent rhenium moieties and methods for their use |
US5147806A (en) * | 1988-04-29 | 1992-09-15 | Igen, Inc. | Method and apparatus for conducting electrochemiluminescence measurements |
CA1320713C (en) * | 1987-09-03 | 1993-07-27 | Harry Stephen Wainauski | Airfoiled blade |
US4891321A (en) * | 1987-10-21 | 1990-01-02 | Hubscher Thomas T | Apparatus for performing determinations of immune reactants in biological fluids |
US5308754A (en) * | 1988-03-21 | 1994-05-03 | Kankare Jouko J | Electrogenerated luminescence in solution |
US5093268A (en) * | 1988-04-28 | 1992-03-03 | Igen, Inc. | Apparatus for conducting a plurality of simultaneous measurements of electrochemiluminescent phenomena |
US5061445A (en) * | 1988-11-03 | 1991-10-29 | Igen, Inc. | Apparatus for conducting measurements of electrochemiluminescent phenomena |
US5247243A (en) * | 1988-11-03 | 1993-09-21 | Igen, Inc. | Method and apparatus for conducting electrochemiluminescent measurements |
US5068088A (en) * | 1988-11-03 | 1991-11-26 | Igen, Inc. | Method and apparatus for conducting electrochemiluminescent measurements |
US5296191A (en) * | 1988-11-03 | 1994-03-22 | Igen, Inc. | Method and apparatus for conducting electrochemiluminescent measurements |
SE8804074D0 (sv) * | 1988-11-10 | 1988-11-10 | Pharmacia Ab | Sensorenhet och dess anvaendning i biosensorsystem |
JP2863192B2 (ja) * | 1989-04-19 | 1999-03-03 | ハイピリオン・カタリシス・インターナシヨナル・インコーポレイテツド | 熱可塑性エラストマー組成物 |
JP3029115B2 (ja) * | 1989-07-21 | 2000-04-04 | ハイピリオン・カタリシス・インターナショナル・インコーポレイテッド | 導電性シート |
US5098771A (en) * | 1989-07-27 | 1992-03-24 | Hyperion Catalysis International | Conductive coatings and inks |
US5110693A (en) * | 1989-09-28 | 1992-05-05 | Hyperion Catalysis International | Electrochemical cell |
US5324457A (en) * | 1989-10-02 | 1994-06-28 | Board Of Regents, The University Of Tx System | Devices and methods for generating electrogenerated chemiluminescence |
US5189549A (en) * | 1990-02-26 | 1993-02-23 | Molecular Displays, Inc. | Electrochromic, electroluminescent and electrochemiluminescent displays |
GB2244135B (en) * | 1990-05-04 | 1994-07-13 | Gen Electric Co Plc | Sensor devices |
US5776672A (en) * | 1990-09-28 | 1998-07-07 | Kabushiki Kaisha Toshiba | Gene detection method |
JPH0534345A (ja) * | 1991-02-19 | 1993-02-09 | Tdk Corp | 化学発光を利用する抗原・抗体の測定方法 |
US5418171A (en) * | 1991-03-28 | 1995-05-23 | Meiji Seika Kabushiki Kaisha | Method for detecting a target analyte in a sample |
US5340716A (en) * | 1991-06-20 | 1994-08-23 | Snytex (U.S.A.) Inc. | Assay method utilizing photoactivated chemiluminescent label |
US6149101A (en) * | 1991-07-08 | 2000-11-21 | Tracy; Richard R. | Aircraft wing and fuselage contours |
US5322242A (en) * | 1991-07-08 | 1994-06-21 | Tracy Richard R | High efficiency, supersonic aircraft |
US5897076A (en) * | 1991-07-08 | 1999-04-27 | Tracy; Richard R. | High-efficiency, supersonic aircraft |
US5632957A (en) * | 1993-11-01 | 1997-05-27 | Nanogen | Molecular biological diagnostic systems including electrodes |
US5466416A (en) * | 1993-05-14 | 1995-11-14 | Ghaed; Ali | Apparatus and methods for carrying out electrochemiluminescence test measurements |
US5527710A (en) * | 1994-12-02 | 1996-06-18 | Igen, Inc. | Rate measurements of biomolecular reactions using electrochemiluminescence |
US5842666A (en) * | 1997-02-21 | 1998-12-01 | Northrop Grumman Coporation | Laminar supersonic transport aircraft |
US6413783B1 (en) * | 1997-09-18 | 2002-07-02 | Meso Scale Technologies, Llc | Assay sonication apparatus and methodology |
CA2474552C (en) * | 2002-01-30 | 2011-07-26 | Gulfstream Aerospace Corporation | Fuselage shaping and inclusion of spike on a supersonic aircraft for controlling and reducing sonic boom |
-
2003
- 2003-10-23 US US10/693,411 patent/US7000870B2/en not_active Expired - Lifetime
- 2003-11-06 EP EP03781784A patent/EP1583690B1/en not_active Expired - Lifetime
- 2003-11-06 AT AT03781784T patent/ATE455034T1/de not_active IP Right Cessation
- 2003-11-06 AU AU2003287542A patent/AU2003287542B2/en not_active Ceased
- 2003-11-06 CA CA2503270A patent/CA2503270C/en not_active Expired - Fee Related
- 2003-11-06 BR BRPI0316038-6B1A patent/BR0316038B1/pt not_active IP Right Cessation
- 2003-11-06 WO PCT/US2003/035393 patent/WO2004043780A2/en active Application Filing
- 2003-11-06 JP JP2004551807A patent/JP4520306B2/ja not_active Expired - Fee Related
- 2003-11-06 DE DE60331004T patent/DE60331004D1/de not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
BR0316038A (pt) | 2005-09-13 |
ATE455034T1 (de) | 2010-01-15 |
EP1583690A2 (en) | 2005-10-12 |
EP1583690A4 (en) | 2009-02-18 |
AU2003287542B2 (en) | 2009-07-02 |
EP1583690B1 (en) | 2010-01-13 |
WO2004043780A2 (en) | 2004-05-27 |
US20040129837A1 (en) | 2004-07-08 |
DE60331004D1 (de) | 2010-03-04 |
CA2503270A1 (en) | 2004-05-27 |
JP2006517162A (ja) | 2006-07-20 |
CA2503270C (en) | 2011-05-17 |
BR0316038B1 (pt) | 2013-06-25 |
WO2004043780A3 (en) | 2005-08-18 |
US7000870B2 (en) | 2006-02-21 |
AU2003287542A1 (en) | 2004-06-03 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
JP5992332B2 (ja) | 超音速及び高亜音速巡航航空機の為に最適化された層流流れ翼 | |
JP2624785B2 (ja) | 航空機の回転翼の羽根 | |
US7946535B2 (en) | Highly efficient supersonic laminar flow wing | |
US4867394A (en) | Compression pylon | |
JP4520306B2 (ja) | 遷音速巡航用の航空機 | |
JPH0380680B2 (ja) | ||
US8317128B2 (en) | Laminar flow wing optimized for transonic cruise aircraft | |
US5901925A (en) | Serrated-planform lifting-surfaces | |
JP3980775B2 (ja) | 飛行機の造波抵抗低減方法 | |
JP4237981B2 (ja) | 飛行機の主翼構造体 | |
JP4237980B2 (ja) | 飛行機の主翼用層流翼型 | |
US5205715A (en) | Helicopter rotor blades | |
CN113044205A (zh) | 可变机翼前缘弯度 | |
US2967030A (en) | Boundary-layer control means for lifting wings | |
EP0103478A1 (en) | Airfoil | |
JP4676633B2 (ja) | 回転翼航空機の回転翼羽根 | |
US6857599B2 (en) | Highly swept canard with low sweep wing supersonic aircraft configuration | |
US6592072B1 (en) | Spanwise tailoring of divergent trailing edge wings | |
CA2350161A1 (en) | Airfoil suitable for forward and reverse flow | |
CA2431383C (en) | Spanwise tailoring of a trailing edge wedge to a wing | |
CN111003143B (zh) | 飞机的机翼及包括该机翼的飞机 | |
JP3130698B2 (ja) | 無尾翼航空機の翼形状 | |
EP0120009A1 (en) | SHOCK WAVE RELEASING GONDOLA TO SEPARATE CURRENTS. |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
A521 | Request for written amendment filed |
Free format text: JAPANESE INTERMEDIATE CODE: A523 Effective date: 20060320 |
|
A521 | Request for written amendment filed |
Free format text: JAPANESE INTERMEDIATE CODE: A821 Effective date: 20060516 |
|
A621 | Written request for application examination |
Free format text: JAPANESE INTERMEDIATE CODE: A621 Effective date: 20061002 |
|
A977 | Report on retrieval |
Free format text: JAPANESE INTERMEDIATE CODE: A971007 Effective date: 20090415 |
|
A131 | Notification of reasons for refusal |
Free format text: JAPANESE INTERMEDIATE CODE: A131 Effective date: 20090512 |
|
RD02 | Notification of acceptance of power of attorney |
Free format text: JAPANESE INTERMEDIATE CODE: A7422 Effective date: 20090717 |
|
A521 | Request for written amendment filed |
Free format text: JAPANESE INTERMEDIATE CODE: A523 Effective date: 20090807 |
|
A131 | Notification of reasons for refusal |
Free format text: JAPANESE INTERMEDIATE CODE: A131 Effective date: 20091028 |
|
A601 | Written request for extension of time |
Free format text: JAPANESE INTERMEDIATE CODE: A601 Effective date: 20100125 |
|
A602 | Written permission of extension of time |
Free format text: JAPANESE INTERMEDIATE CODE: A602 Effective date: 20100201 |
|
A601 | Written request for extension of time |
Free format text: JAPANESE INTERMEDIATE CODE: A601 Effective date: 20100226 |
|
A521 | Request for written amendment filed |
Free format text: JAPANESE INTERMEDIATE CODE: A523 Effective date: 20100305 |
|
A602 | Written permission of extension of time |
Free format text: JAPANESE INTERMEDIATE CODE: A602 Effective date: 20100305 |
|
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: 20100421 |
|
A01 | Written decision to grant a patent or to grant a registration (utility model) |
Free format text: JAPANESE INTERMEDIATE CODE: A01 |
|
A61 | First payment of annual fees (during grant procedure) |
Free format text: JAPANESE INTERMEDIATE CODE: A61 Effective date: 20100520 |
|
FPAY | Renewal fee payment (event date is renewal date of database) |
Free format text: PAYMENT UNTIL: 20130528 Year of fee payment: 3 |
|
R150 | Certificate of patent or registration of utility model |
Ref document number: 4520306 Country of ref document: JP Free format text: JAPANESE INTERMEDIATE CODE: R150 Free format text: JAPANESE INTERMEDIATE CODE: R150 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
S111 | Request for change of ownership or part of ownership |
Free format text: JAPANESE INTERMEDIATE CODE: R313113 |
|
R350 | Written notification of registration of transfer |
Free format text: JAPANESE INTERMEDIATE CODE: R350 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
LAPS | Cancellation because of no payment of annual fees |