JP4559191B2 - 本体内部の亀裂を抑止するための方法及び装置 - Google Patents
本体内部の亀裂を抑止するための方法及び装置 Download PDFInfo
- Publication number
- JP4559191B2 JP4559191B2 JP2004321703A JP2004321703A JP4559191B2 JP 4559191 B2 JP4559191 B2 JP 4559191B2 JP 2004321703 A JP2004321703 A JP 2004321703A JP 2004321703 A JP2004321703 A JP 2004321703A JP 4559191 B2 JP4559191 B2 JP 4559191B2
- Authority
- JP
- Japan
- Prior art keywords
- plies
- assembly
- metal wire
- flap
- ply
- 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
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/06—Varying effective area of jet pipe or nozzle
- F02K1/12—Varying effective area of jet pipe or nozzle by means of pivoted flaps
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P6/00—Restoring or reconditioning objects
- B23P6/002—Repairing turbine components, e.g. moving or stationary blades, rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P6/00—Restoring or reconditioning objects
- B23P6/04—Repairing fractures or cracked metal parts or products, e.g. castings
- B23P6/045—Repairing fractures or cracked metal parts or products, e.g. castings of turbine components, e.g. moving or stationary blades, rotors, etc.
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/78—Other construction of jet pipes
- F02K1/80—Couplings or connections
- F02K1/805—Sealing devices therefor, e.g. for movable parts of jet pipes or nozzle flaps
-
- 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
- F05D2240/00—Components
- F05D2240/55—Seals
-
- 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
- F05D2300/00—Materials; Properties thereof
- F05D2300/20—Oxide or non-oxide ceramics
- F05D2300/21—Oxide ceramics
-
- 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
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Laminated Bodies (AREA)
- Gasket Seals (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US10/703,272 US7028462B2 (en) | 2003-11-07 | 2003-11-07 | Method and apparatus for arresting a crack within a body |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2005201241A JP2005201241A (ja) | 2005-07-28 |
| JP2005201241A5 JP2005201241A5 (enExample) | 2007-12-20 |
| JP4559191B2 true JP4559191B2 (ja) | 2010-10-06 |
Family
ID=34435567
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2004321703A Expired - Fee Related JP4559191B2 (ja) | 2003-11-07 | 2004-11-05 | 本体内部の亀裂を抑止するための方法及び装置 |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US7028462B2 (enExample) |
| EP (1) | EP1529950B1 (enExample) |
| JP (1) | JP4559191B2 (enExample) |
| CA (1) | CA2486024C (enExample) |
Families Citing this family (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7458221B1 (en) * | 2003-10-23 | 2008-12-02 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Variable area nozzle including a plurality of convexly vanes with a crowned contour, in a vane to vane sealing arrangement and with nonuniform lengths |
| US7310949B2 (en) * | 2003-11-07 | 2007-12-25 | General Electric Company | Method and apparatus for arresting a crack within a body |
| US8128100B2 (en) * | 2007-12-05 | 2012-03-06 | United Technologies Corporation | Laminate air seal for a gas turbine engine |
| US8122722B2 (en) * | 2008-02-29 | 2012-02-28 | General Electric Company | Exhaust nozzle seal with segmented basesheet disposed between side rails |
| US8715439B2 (en) | 2008-03-07 | 2014-05-06 | The Boeing Company | Method for making hybrid metal-ceramic matrix composite structures and structures made thereby |
| EP2571686A1 (en) * | 2010-05-17 | 2013-03-27 | General Electric Company | Ceramic matrix composite structures, components formed therewith, and methods of producing |
| WO2012082848A1 (en) * | 2010-12-15 | 2012-06-21 | Advanced Bionics Ag | Crack diversion planes in ceramic feedthroughs |
| US20160086275A1 (en) * | 2014-09-24 | 2016-03-24 | Sourcewater, Inc. | Computerized techniques for facilitating exchange of a water resource |
| US11035239B2 (en) | 2018-10-25 | 2021-06-15 | General Electric Company | Ceramic matrix composite turbine nozzle shell and method of assembly |
| US11174203B2 (en) | 2018-10-25 | 2021-11-16 | General Electric Company | Ceramic matrix composite turbine nozzle shell and method of assembly |
| US11845699B2 (en) * | 2021-09-07 | 2023-12-19 | Blue Origin, Llc | Methods for manufacturing coated composite materials |
Family Cites Families (22)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4530884A (en) | 1976-04-05 | 1985-07-23 | Brunswick Corporation | Ceramic-metal laminate |
| US4544098A (en) * | 1982-12-27 | 1985-10-01 | United Technologies Corporation | Cooled exhaust nozzle flaps |
| JPS6077178A (ja) * | 1983-09-30 | 1985-05-01 | 株式会社東芝 | 窒化物セラミックス接合体およびその製造方法 |
| DE3602132A1 (de) * | 1986-01-24 | 1987-07-30 | Glyco Metall Werke | Gleit- oder reibelement mit funktionsteil aus keramischem werkstoff mit eingelagertem stabilisator sowie verfahren zu seiner herstellung |
| US4780432A (en) | 1986-09-02 | 1988-10-25 | United Technologies Corporation | Controlled fiber distribution technique for glass matrix composites |
| US4837230A (en) | 1987-05-07 | 1989-06-06 | Kaiser Aerotech | Structural ceramic materials having refractory interface layers |
| US4994416A (en) | 1988-02-04 | 1991-02-19 | Martin Marietta Energy Systems, Inc. | Ceramic composites reinforced with modified silicon carbide whiskers and method for modifying the whiskers |
| US4916092A (en) | 1988-02-04 | 1990-04-10 | Martin Marietta Energy Systems, Inc. | Ceramic composites reinforced with modified silicon carbide whiskers |
| US4835831A (en) | 1988-07-15 | 1989-06-06 | Melton Sidney H | Method of providing a refractory covering to a furnace wall |
| US5137852A (en) | 1991-01-11 | 1992-08-11 | Rockwell International Corp. | High temperature ceramic composites |
| US6338906B1 (en) | 1992-09-17 | 2002-01-15 | Coorstek, Inc. | Metal-infiltrated ceramic seal |
| IL109085A (en) | 1993-04-05 | 1997-08-14 | Gen Electric | Nozzle seal assembly with removable baseplate |
| CA2137528C (en) | 1994-04-15 | 2001-07-03 | Peter E. D. Morgan | Ceramic composites having a weak bond interphase material selected from monazites and xenotimes |
| US5839663A (en) * | 1996-07-23 | 1998-11-24 | United Technologies Corporation | Gas turbine exhaust nozzle flap and flap seal apparatus |
| US5759663A (en) | 1996-10-31 | 1998-06-02 | Thorpe Products Company | Hard-faced insulating refractory fiber linings |
| JPH10168699A (ja) * | 1996-12-06 | 1998-06-23 | Toshiba Corp | 繊維複合材料およびその製造方法 |
| DE19800926A1 (de) * | 1998-01-13 | 1999-07-29 | Emitec Emissionstechnologie | Wabenkörperanordnung mit einer mindestens eine Metallfolie enthaltenden Zwischenschicht |
| JP2000026170A (ja) * | 1998-07-07 | 2000-01-25 | Ishikawajima Harima Heavy Ind Co Ltd | セラミックス複合材料 |
| US6240720B1 (en) * | 1999-09-09 | 2001-06-05 | General Electric Company | Hybrid-composite gas turbine exhaust nozzle compression link |
| EP1126221A1 (de) | 2000-02-17 | 2001-08-22 | Siemens Aktiengesellschaft | Gepolsterter Hitzeschildstein zur Auskleidung einer Gasturbinenbrennkammerwand |
| US6471469B2 (en) | 2000-11-30 | 2002-10-29 | General Electric Company | Methods and apparatus for sealing gas turbine engine variable nozzles |
| US20040242095A1 (en) | 2003-05-27 | 2004-12-02 | Amit Prakash | Composites reinforced by wire net or mesh for lightweight, strength and stiffness |
-
2003
- 2003-11-07 US US10/703,272 patent/US7028462B2/en not_active Expired - Lifetime
-
2004
- 2004-10-28 CA CA2486024A patent/CA2486024C/en not_active Expired - Fee Related
- 2004-11-04 EP EP04256838.6A patent/EP1529950B1/en not_active Expired - Lifetime
- 2004-11-05 JP JP2004321703A patent/JP4559191B2/ja not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| CA2486024A1 (en) | 2005-05-07 |
| EP1529950A1 (en) | 2005-05-11 |
| US7028462B2 (en) | 2006-04-18 |
| EP1529950B1 (en) | 2016-01-20 |
| CA2486024C (en) | 2010-10-05 |
| JP2005201241A (ja) | 2005-07-28 |
| US20050097892A1 (en) | 2005-05-12 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US11306617B2 (en) | Shroud for a gas turbine engine | |
| CN107044445B (zh) | 易碎的燃气涡轮发动机翼型件 | |
| US8118546B2 (en) | Grid ceramic matrix composite structure for gas turbine shroud ring segment | |
| CN104100304B (zh) | 涡轮机叶片组件 | |
| US7334997B2 (en) | Hybrid blisk | |
| US10060272B2 (en) | Turbine vane with load shield | |
| JP4559191B2 (ja) | 本体内部の亀裂を抑止するための方法及び装置 | |
| EP3517282B1 (en) | Composite component having t or l-joints and method for forming same | |
| US12297751B2 (en) | Turbine engine with composite airfoil having a non-metallic leading edge protective wrap | |
| JP6728287B2 (ja) | 複合材構成部品のための接触境界部および製作方法 | |
| US11028696B2 (en) | Ceramic matrix composite airfoil repair | |
| EP2519720B1 (en) | Integrated aero-engine flowpath structure | |
| JP4596389B2 (ja) | 本体内部の亀裂を抑止するための方法及び装置 | |
| EP3712382B1 (en) | Blade outer air seal assembly with wear liner | |
| US10018054B2 (en) | Fabrication of gas turbine engine components using multiple processing steps | |
| JP2005140116A (ja) | 本体の耐久性を向上させる方法及び装置 | |
| EP4454880A1 (en) | Ceramic matrix composite (cmc) component resistant to edge cracks | |
| CN120398574A (zh) | 陶瓷基复合材料部件修复以及接合 |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| A521 | Request for written amendment filed |
Free format text: JAPANESE INTERMEDIATE CODE: A523 Effective date: 20071102 |
|
| A621 | Written request for application examination |
Free format text: JAPANESE INTERMEDIATE CODE: A621 Effective date: 20071102 |
|
| A131 | Notification of reasons for refusal |
Free format text: JAPANESE INTERMEDIATE CODE: A131 Effective date: 20100309 |
|
| A521 | Request for written amendment filed |
Free format text: JAPANESE INTERMEDIATE CODE: A523 Effective date: 20100608 |
|
| RD02 | Notification of acceptance of power of attorney |
Free format text: JAPANESE INTERMEDIATE CODE: A7422 Effective date: 20100608 |
|
| RD04 | Notification of resignation of power of attorney |
Free format text: JAPANESE INTERMEDIATE CODE: A7424 Effective date: 20100608 |
|
| 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: 20100629 |
|
| 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: 20100722 |
|
| R150 | Certificate of patent or registration of utility model |
Ref document number: 4559191 Country of ref document: JP Free format text: JAPANESE INTERMEDIATE CODE: R150 Free format text: JAPANESE INTERMEDIATE CODE: R150 |
|
| FPAY | Renewal fee payment (event date is renewal date of database) |
Free format text: PAYMENT UNTIL: 20130730 Year of fee payment: 3 |
|
| 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 |
|
| R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
| LAPS | Cancellation because of no payment of annual fees |