GB2111889B - A method of increasing the reliability of creep-loaded components in particular turbine blades - Google Patents
A method of increasing the reliability of creep-loaded components in particular turbine bladesInfo
- Publication number
- GB2111889B GB2111889B GB08232519A GB8232519A GB2111889B GB 2111889 B GB2111889 B GB 2111889B GB 08232519 A GB08232519 A GB 08232519A GB 8232519 A GB8232519 A GB 8232519A GB 2111889 B GB2111889 B GB 2111889B
- Authority
- GB
- United Kingdom
- Prior art keywords
- creep
- reliability
- increasing
- turbine blades
- loaded components
- 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
Links
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F3/00—Changing the physical structure of non-ferrous metals or alloys by special physical methods, e.g. treatment with neutrons
Landscapes
- Chemical & Material Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19813145941 DE3145941C2 (en) | 1981-11-20 | 1981-11-20 | Process for increasing the reliability of coated components of turbomachinery that are already subject to creep stress |
Publications (2)
Publication Number | Publication Date |
---|---|
GB2111889A GB2111889A (en) | 1983-07-13 |
GB2111889B true GB2111889B (en) | 1985-10-23 |
Family
ID=6146760
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB08232519A Expired GB2111889B (en) | 1981-11-20 | 1982-11-15 | A method of increasing the reliability of creep-loaded components in particular turbine blades |
Country Status (3)
Country | Link |
---|---|
DE (1) | DE3145941C2 (en) |
FR (1) | FR2516943A1 (en) |
GB (1) | GB2111889B (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2550055C2 (en) * | 2013-04-30 | 2015-05-10 | Общество с ограниченной ответственностью "Производственное предприятие Турбинаспецсервис" | Reconditioning of gas turbine plant including nozzle blades from nickel or cobalt alloys composed of multibank structure |
RU2760895C1 (en) * | 2021-03-10 | 2021-12-01 | Акционерное общество "ОДК-Климов" | Method for restoring the cyclic durability of disks of aircraft gas turbine engines |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2620735A1 (en) * | 1987-09-19 | 1989-03-24 | Motoren Turbinen Union | Process for the heat treatment of structural components made of nickel-based foundry alloys |
US4975124A (en) * | 1989-02-06 | 1990-12-04 | United Technologies Corporation | Process for densifying castings |
DE19853285C1 (en) * | 1998-11-19 | 2000-06-15 | Karlsruhe Forschzent | Process for producing a protective layer on a martensitic steel and use of the steel provided with the protective layer |
CN110026478B (en) * | 2019-04-30 | 2024-05-03 | 中国民用航空飞行学院 | Method and device for vibration creep composite aging incremental forming based on pneumatic loading |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3758347A (en) * | 1970-12-21 | 1973-09-11 | Gen Electric | Method for improving a metal casting |
-
1981
- 1981-11-20 DE DE19813145941 patent/DE3145941C2/en not_active Expired
-
1982
- 1982-10-25 FR FR8217832A patent/FR2516943A1/en active Granted
- 1982-11-15 GB GB08232519A patent/GB2111889B/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2550055C2 (en) * | 2013-04-30 | 2015-05-10 | Общество с ограниченной ответственностью "Производственное предприятие Турбинаспецсервис" | Reconditioning of gas turbine plant including nozzle blades from nickel or cobalt alloys composed of multibank structure |
RU2760895C1 (en) * | 2021-03-10 | 2021-12-01 | Акционерное общество "ОДК-Климов" | Method for restoring the cyclic durability of disks of aircraft gas turbine engines |
Also Published As
Publication number | Publication date |
---|---|
FR2516943B3 (en) | 1985-02-15 |
DE3145941A1 (en) | 1983-06-01 |
DE3145941C2 (en) | 1983-12-01 |
GB2111889A (en) | 1983-07-13 |
FR2516943A1 (en) | 1983-05-27 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
746 | Register noted 'licences of right' (sect. 46/1977) | ||
PE20 | Patent expired after termination of 20 years |
Effective date: 20021114 |