JP2010540322A - 翼フェアリングの製造および取り付け方法 - Google Patents
翼フェアリングの製造および取り付け方法 Download PDFInfo
- Publication number
- JP2010540322A JP2010540322A JP2010527067A JP2010527067A JP2010540322A JP 2010540322 A JP2010540322 A JP 2010540322A JP 2010527067 A JP2010527067 A JP 2010527067A JP 2010527067 A JP2010527067 A JP 2010527067A JP 2010540322 A JP2010540322 A JP 2010540322A
- Authority
- JP
- Japan
- Prior art keywords
- composite
- fairing
- tiles
- aircraft
- sheet
- 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.)
- Granted
Links
- 238000000034 method Methods 0.000 title claims abstract description 33
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 27
- 239000002131 composite material Substances 0.000 claims abstract description 210
- 239000000945 filler Substances 0.000 claims abstract description 18
- 239000000565 sealant Substances 0.000 claims description 3
- 239000010410 layer Substances 0.000 description 31
- 238000001723 curing Methods 0.000 description 16
- 238000013461 design Methods 0.000 description 14
- 238000009434 installation Methods 0.000 description 11
- 239000000463 material Substances 0.000 description 11
- 238000012423 maintenance Methods 0.000 description 10
- 239000000853 adhesive Substances 0.000 description 8
- 230000001070 adhesive effect Effects 0.000 description 8
- 238000010586 diagram Methods 0.000 description 8
- 239000004744 fabric Substances 0.000 description 7
- 239000011440 grout Substances 0.000 description 6
- 230000015572 biosynthetic process Effects 0.000 description 5
- 239000006260 foam Substances 0.000 description 5
- 230000008569 process Effects 0.000 description 5
- 238000009420 retrofitting Methods 0.000 description 4
- 238000005520 cutting process Methods 0.000 description 3
- 239000002828 fuel tank Substances 0.000 description 3
- 238000012986 modification Methods 0.000 description 3
- 230000004048 modification Effects 0.000 description 3
- 230000008859 change Effects 0.000 description 2
- 238000005553 drilling Methods 0.000 description 2
- 239000000446 fuel Substances 0.000 description 2
- 238000011900 installation process Methods 0.000 description 2
- 230000010354 integration Effects 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 239000004033 plastic Substances 0.000 description 2
- 229920003023 plastic Polymers 0.000 description 2
- 238000002360 preparation method Methods 0.000 description 2
- 239000012783 reinforcing fiber Substances 0.000 description 2
- 238000007789 sealing Methods 0.000 description 2
- 235000015842 Hesperis Nutrition 0.000 description 1
- 229910000997 High-speed steel Inorganic materials 0.000 description 1
- 235000012633 Iberis amara Nutrition 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 238000004140 cleaning Methods 0.000 description 1
- 239000012792 core layer Substances 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000010894 electron beam technology Methods 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- -1 for example Substances 0.000 description 1
- 239000003292 glue Substances 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 230000008520 organization Effects 0.000 description 1
- 239000003973 paint Substances 0.000 description 1
- 230000000135 prohibitive effect Effects 0.000 description 1
- 238000009419 refurbishment Methods 0.000 description 1
- 230000008439 repair process Effects 0.000 description 1
- 239000011347 resin Substances 0.000 description 1
- 229920005989 resin Polymers 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
- 238000001029 thermal curing Methods 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/26—Attaching the wing or tail units or stabilising surfaces
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C7/00—Structures or fairings not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/10—Manufacturing or assembling aircraft, e.g. jigs therefor
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/06—Fibrous reinforcements only
- B29C70/08—Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers
- B29C70/086—Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers and with one or more layers of pure plastics material, e.g. foam layers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
- B29K2105/04—Condition, form or state of moulded material or of the material to be shaped cellular or porous
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
- B29K2105/06—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
- B29K2105/08—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts of continuous length, e.g. cords, rovings, mats, fabrics, strands or yarns
- B29K2105/0809—Fabrics
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
- B29L2031/3076—Aircrafts
-
- 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
- Y02T50/40—Weight reduction
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
- Y10T428/24802—Discontinuous or differential coating, impregnation or bond [e.g., artwork, printing, retouched photograph, etc.]
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
- Y10T428/24802—Discontinuous or differential coating, impregnation or bond [e.g., artwork, printing, retouched photograph, etc.]
- Y10T428/24851—Intermediate layer is discontinuous or differential
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Mechanical Engineering (AREA)
- Transportation (AREA)
- Laminated Bodies (AREA)
- Moulding By Coating Moulds (AREA)
Abstract
Description
Claims (10)
- 航空機に複合フェアリングを設置する方法であって、
複合フェアリングの形態を有する複合シートを形成すること、
間に空間が存在する複数の硬化した複合タイルを複合シートから作成すること、
複合フェアリングを航空機の表面に取り付けること、および
複数の複合タイルの間の空間に可撓性充填材を充填すること
を含む方法。 - 前記充填する工程が、
複合フェアリングを航空機の表面に取り付けた後に、複数の複合タイルの間の空間に可撓性充填材を充填することを含む請求項1に記載の方法。 - 複数の複合タイルのうちの各複合タイルが、第1の複合層と、第1の複合層上のコアと、コア上の第2の複合層とを有する請求項1に記載の方法。
- 前記取り付ける工程の前に、前記充填する工程を行うことをさらに含む請求項1に記載の方法。
- フェアリングを製造する方法であって、
フェアリングの形状の複合シートを形成すること、
複合シートから複数の複合タイルを形成して、フェアリングのアセンブリを形成すること、および、
複数の複合タイルを硬化させて、フェアリングを形成することを含む方法。 - 輸送手段の表面にフェアリングを設置することをさらに含む請求項5に記載の方法。
- 前記形成する工程が、
複合シートを分割して、複数の別個のタイルを形成すること、および、
複合層に複数の別個のタイルを取り付けて、複数の複合タイルを形成すること
を含む請求項5に記載の方法。 - フェアリングの外形を有する複合層と、
フェアリングの形状の前記複合層に接合されており、間に空間が存在する複数の複合タイルと
を含む装置。 - 前記複数の複合タイルの間の空間に位置している可撓性充填材
をさらに含む請求項8に記載の装置。 - 前記複数の複合タイルと前記可撓性充填材との上に位置しているシーラント
をさらに含む請求項8に記載の装置。
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US11/861,024 | 2007-09-25 | ||
US11/861,024 US7998392B2 (en) | 2007-09-25 | 2007-09-25 | Method for manufacturing and attachment of wing fairings |
PCT/US2008/077253 WO2009042549A2 (en) | 2007-09-25 | 2008-09-22 | Method for manufacturing and attachment of wing fairings |
Publications (2)
Publication Number | Publication Date |
---|---|
JP2010540322A true JP2010540322A (ja) | 2010-12-24 |
JP5480810B2 JP5480810B2 (ja) | 2014-04-23 |
Family
ID=39942964
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2010527067A Expired - Fee Related JP5480810B2 (ja) | 2007-09-25 | 2008-09-22 | 翼フェアリングの製造および取り付け方法 |
Country Status (5)
Country | Link |
---|---|
US (2) | US7998392B2 (ja) |
EP (1) | EP2190735B1 (ja) |
JP (1) | JP5480810B2 (ja) |
CN (1) | CN101868406B (ja) |
WO (1) | WO2009042549A2 (ja) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7998392B2 (en) * | 2007-09-25 | 2011-08-16 | The Boeing Company | Method for manufacturing and attachment of wing fairings |
US9937965B1 (en) | 2015-12-09 | 2018-04-10 | Airodyne Industries, Inc. | Collapsible roof fairing |
US10766600B2 (en) * | 2017-07-28 | 2020-09-08 | The Boeing Company | Articulation assemblies for retracting aircraft flap support fairings and related methods |
CN108860571B (zh) * | 2018-07-26 | 2023-09-29 | 成都飞机工业(集团)有限责任公司 | 一种飞机翼身整流罩及其构建方法 |
CN110439707B (zh) * | 2019-07-26 | 2021-10-01 | 中国航发沈阳发动机研究所 | 一种飞机尾部弹性片组件 |
US11407529B1 (en) * | 2019-10-22 | 2022-08-09 | Northrop Grumman Systems Corporation | Aircraft retrofit system |
Citations (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2997262A (en) * | 1960-01-21 | 1961-08-22 | Gen Dynamics Corp | Aircraft wing structure |
US3177273A (en) * | 1961-03-28 | 1965-04-06 | Minnesota Mining & Mfg | Method for making a ceramic tile faced panel |
US4124732A (en) * | 1975-03-05 | 1978-11-07 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Thermal insulation attaching means |
JPS59114141A (ja) * | 1982-12-17 | 1984-07-02 | ダイムラ−−ベンツ・アクチエンゲゼルシヤフト | 乗用車および貨物乗用車用空気力学的飾り外張り |
US4508774A (en) * | 1983-03-15 | 1985-04-02 | Basf Aktiengesellschaft | Cellular, molded polyurethane parts, process for their preparation by thermoforming of polyester-urethane foam and their use |
JPH0319943U (ja) * | 1989-03-29 | 1991-02-27 | ||
JPH0687499A (ja) * | 1992-04-23 | 1994-03-29 | Aerospat Soc Natl Ind | 物体を熱的に保護する装置および熱的シールド |
JPH10246391A (ja) * | 1997-03-05 | 1998-09-14 | Natl Space Dev Agency Japan<Nasda> | 耐圧縮型可撓断熱材 |
US6173807B1 (en) * | 1998-04-13 | 2001-01-16 | The Boeing Company | Engine nacelle acoustic panel with integral wedge fairings and an integral forward ring |
US20060083902A1 (en) * | 2003-04-30 | 2006-04-20 | Jarosz Dennis P | Resilient floor tile and method for making same |
EP1834873A1 (en) * | 2006-03-16 | 2007-09-19 | Eads Construcciones Aeronauticas S.A. | Elastic pre-deformed fairings for aircraft |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3352741A (en) * | 1963-12-13 | 1967-11-14 | Hicks & Otis Prints Inc | Contoured ornamentation of laminated resilient materials |
US5080306A (en) | 1989-10-10 | 1992-01-14 | General Dynamics Corporation, Space Systems Division | Multi-layer stitched blanket insulation |
FR2703323B1 (fr) * | 1993-04-01 | 1995-06-30 | Europ Propulsion | Dispositif de protection thermique, notamment pour engin aerospatial. |
US7325771B2 (en) | 2004-09-23 | 2008-02-05 | The Boeing Company | Splice joints for composite aircraft fuselages and other structures |
US7416401B2 (en) * | 2005-06-13 | 2008-08-26 | The Boeing Company | Lightweight composite fairing bar and method for manufacturing the same |
US7998392B2 (en) * | 2007-09-25 | 2011-08-16 | The Boeing Company | Method for manufacturing and attachment of wing fairings |
-
2007
- 2007-09-25 US US11/861,024 patent/US7998392B2/en not_active Expired - Fee Related
-
2008
- 2008-09-22 CN CN2008801167071A patent/CN101868406B/zh active Active
- 2008-09-22 JP JP2010527067A patent/JP5480810B2/ja not_active Expired - Fee Related
- 2008-09-22 WO PCT/US2008/077253 patent/WO2009042549A2/en active Application Filing
- 2008-09-22 EP EP08834217.5A patent/EP2190735B1/en active Active
-
2011
- 2011-05-11 US US13/105,572 patent/US8545211B2/en active Active
Patent Citations (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2997262A (en) * | 1960-01-21 | 1961-08-22 | Gen Dynamics Corp | Aircraft wing structure |
US3177273A (en) * | 1961-03-28 | 1965-04-06 | Minnesota Mining & Mfg | Method for making a ceramic tile faced panel |
US4124732A (en) * | 1975-03-05 | 1978-11-07 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Thermal insulation attaching means |
JPS59114141A (ja) * | 1982-12-17 | 1984-07-02 | ダイムラ−−ベンツ・アクチエンゲゼルシヤフト | 乗用車および貨物乗用車用空気力学的飾り外張り |
US4508774A (en) * | 1983-03-15 | 1985-04-02 | Basf Aktiengesellschaft | Cellular, molded polyurethane parts, process for their preparation by thermoforming of polyester-urethane foam and their use |
JPH0319943U (ja) * | 1989-03-29 | 1991-02-27 | ||
JPH0687499A (ja) * | 1992-04-23 | 1994-03-29 | Aerospat Soc Natl Ind | 物体を熱的に保護する装置および熱的シールド |
JPH10246391A (ja) * | 1997-03-05 | 1998-09-14 | Natl Space Dev Agency Japan<Nasda> | 耐圧縮型可撓断熱材 |
US6173807B1 (en) * | 1998-04-13 | 2001-01-16 | The Boeing Company | Engine nacelle acoustic panel with integral wedge fairings and an integral forward ring |
US20060083902A1 (en) * | 2003-04-30 | 2006-04-20 | Jarosz Dennis P | Resilient floor tile and method for making same |
EP1834873A1 (en) * | 2006-03-16 | 2007-09-19 | Eads Construcciones Aeronauticas S.A. | Elastic pre-deformed fairings for aircraft |
Also Published As
Publication number | Publication date |
---|---|
WO2009042549A2 (en) | 2009-04-02 |
JP5480810B2 (ja) | 2014-04-23 |
WO2009042549A3 (en) | 2009-06-18 |
CN101868406A (zh) | 2010-10-20 |
EP2190735A2 (en) | 2010-06-02 |
US20110212310A1 (en) | 2011-09-01 |
US8545211B2 (en) | 2013-10-01 |
US20090078825A1 (en) | 2009-03-26 |
EP2190735B1 (en) | 2016-05-04 |
CN101868406B (zh) | 2013-12-04 |
US7998392B2 (en) | 2011-08-16 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
McIlhagger et al. | Manufacturing processes for composite materials and components for aerospace applications | |
US11897191B2 (en) | Lattice reinforced radius filler | |
JP5480810B2 (ja) | 翼フェアリングの製造および取り付け方法 | |
EP2546149B1 (en) | Large area repair of composite aircraft | |
JP6505997B2 (ja) | 幾何学形状充填材要素を有するラミネート複合角部充填材およびそれを形成する方法 | |
CA2838229C (en) | Rapid fabrication of a composite part | |
KR102307891B1 (ko) | 접혀진 복합재 필러 | |
US20160101576A1 (en) | Method for manufacturing a fibre composite component, fibre composite component, and structural component for an aircraft or spacecraft | |
EP3434459B1 (en) | Slip sheet with compensation surface | |
CN103569348B (zh) | 用于交通工具的整体复合结构 | |
JP7144174B2 (ja) | 高度に積載された一次および二次構造部品の修理のための構造的な予備硬化修理パッチ | |
Bekhmetiev et al. | The study of the use of polymer composite materials in the mass and eco-friendly production of aircraft structural elements | |
Penela Guerrero | Mechanical Design, Analysis, and Manufacturing of Wind Tunnel Model and Support Structure | |
US10059068B2 (en) | Composite structure and method of forming thereof |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
A621 | Written request for application examination |
Free format text: JAPANESE INTERMEDIATE CODE: A621 Effective date: 20110624 |
|
A977 | Report on retrieval |
Free format text: JAPANESE INTERMEDIATE CODE: A971007 Effective date: 20130115 |
|
A131 | Notification of reasons for refusal |
Free format text: JAPANESE INTERMEDIATE CODE: A131 Effective date: 20130129 |
|
A521 | Request for written amendment filed |
Free format text: JAPANESE INTERMEDIATE CODE: A523 Effective date: 20130308 |
|
A131 | Notification of reasons for refusal |
Free format text: JAPANESE INTERMEDIATE CODE: A131 Effective date: 20130528 |
|
A521 | Request for written amendment filed |
Free format text: JAPANESE INTERMEDIATE CODE: A523 Effective date: 20130809 |
|
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: 20140128 |
|
A61 | First payment of annual fees (during grant procedure) |
Free format text: JAPANESE INTERMEDIATE CODE: A61 Effective date: 20140214 |
|
R150 | Certificate of patent or registration of utility model |
Ref document number: 5480810 Country of ref document: JP 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 |
|
LAPS | Cancellation because of no payment of annual fees |