BE556215A - - Google Patents
Info
- Publication number
- BE556215A BE556215A BE556215DA BE556215A BE 556215 A BE556215 A BE 556215A BE 556215D A BE556215D A BE 556215DA BE 556215 A BE556215 A BE 556215A
- Authority
- BE
- Belgium
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
- F01D11/14—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing
- F01D11/16—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing by self-adjusting means
- F01D11/18—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing by self-adjusting means using stator or rotor components with predetermined thermal response, e.g. selective insulation, thermal inertia, differential expansion
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB976056A GB806815A (en) | 1956-03-28 | 1956-03-28 | Turbine blade shroud rings |
Publications (1)
Publication Number | Publication Date |
---|---|
BE556215A true BE556215A (en) | 1957-04-15 |
Family
ID=9878254
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BE556215D BE556215A (en) | 1956-03-28 |
Country Status (4)
Country | Link |
---|---|
BE (1) | BE556215A (en) |
CH (1) | CH338328A (en) |
DE (1) | DE1116685B (en) |
GB (1) | GB806815A (en) |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1239889B (en) * | 1963-06-28 | 1967-05-03 | Licentia Gmbh | Inlet guide vane ring for axial turbines, in particular axial gas turbines, with radially resiliently pressed ring segments |
DE1286810B (en) * | 1963-11-19 | 1969-01-09 | Licentia Gmbh | Rotor blade radial gap cover ring of an axial turbine machine, in particular a gas turbine |
US3800864A (en) * | 1972-09-05 | 1974-04-02 | Gen Electric | Pin-fin cooling system |
FR2577281B1 (en) * | 1985-02-13 | 1987-03-20 | Snecma | TURBOMACHINE HOUSING ASSOCIATED WITH A DEVICE FOR ADJUSTING THE GAP BETWEEN MOBILE BLADES AND HOUSING |
US5127793A (en) * | 1990-05-31 | 1992-07-07 | General Electric Company | Turbine shroud clearance control assembly |
GB9815611D0 (en) | 1998-07-18 | 1998-09-16 | Rolls Royce Plc | Improvements in or relating to turbine cooling |
GB2395756B (en) | 2002-11-27 | 2006-02-08 | Rolls Royce Plc | Cooled turbine assembly |
FR2852053B1 (en) * | 2003-03-06 | 2007-12-28 | Snecma Moteurs | HIGH PRESSURE TURBINE FOR TURBOMACHINE |
RU2490478C2 (en) * | 2011-10-11 | 2013-08-20 | Открытое акционерное общество "Научно-производственное объединение "Сатурн" (ОАО "НПО "Сатурн") | Turbomachine stator |
RU2493388C1 (en) * | 2012-03-27 | 2013-09-20 | Открытое акционерное общество Конструкторско-производственное предприятие "Авиамотор" | Seal of gas turbine engine combustion chamber-to-stator joint |
CN111396137A (en) * | 2020-04-29 | 2020-07-10 | 北京动力机械研究所 | High-efficient axial compressor turbine suitable for inert mixed working medium |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB629770A (en) * | 1947-11-21 | 1949-09-28 | Napier & Son Ltd | Improvements in or relating to sealing rings for turbines |
DE852789C (en) * | 1951-02-08 | 1952-10-20 | Maschf Augsburg Nuernberg Ag | Guide vane carrier for axial turbines |
US2858104A (en) * | 1954-02-04 | 1958-10-28 | A V Roe Canada Ltd | Adjustable gas turbine shroud ring segments |
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0
- BE BE556215D patent/BE556215A/xx unknown
-
1956
- 1956-03-28 GB GB976056A patent/GB806815A/en not_active Expired
-
1957
- 1957-03-19 CH CH338328D patent/CH338328A/en unknown
- 1957-03-22 DE DEN13451A patent/DE1116685B/en active Pending
Also Published As
Publication number | Publication date |
---|---|
DE1116685B (en) | 1961-11-09 |
GB806815A (en) | 1958-12-31 |
CH338328A (en) | 1959-05-15 |