GB1093312A - Improvements in or relating to turbine construction - Google Patents
Improvements in or relating to turbine constructionInfo
- Publication number
- GB1093312A GB1093312A GB1495/65A GB149565A GB1093312A GB 1093312 A GB1093312 A GB 1093312A GB 1495/65 A GB1495/65 A GB 1495/65A GB 149565 A GB149565 A GB 149565A GB 1093312 A GB1093312 A GB 1093312A
- Authority
- GB
- United Kingdom
- Prior art keywords
- ring
- lugs
- engaging
- slots
- casing
- 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
- 238000010276 construction Methods 0.000 title 1
- 239000012634 fragment Substances 0.000 abstract 3
- 229910000831 Steel Inorganic materials 0.000 abstract 1
- 238000010521 absorption reaction Methods 0.000 abstract 1
- 239000011152 fibreglass Substances 0.000 abstract 1
- 239000000463 material Substances 0.000 abstract 1
- 230000035515 penetration Effects 0.000 abstract 1
- 230000000717 retained effect Effects 0.000 abstract 1
- 125000006850 spacer group Chemical group 0.000 abstract 1
- 239000010959 steel Substances 0.000 abstract 1
- 238000011144 upstream manufacturing Methods 0.000 abstract 1
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
- F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
- F01D21/04—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position
- F01D21/045—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position special arrangements in stators or in rotors dealing with breaking-off of part of rotor
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 |
|---|---|---|---|
| US337905A US3243158A (en) | 1964-01-15 | 1964-01-15 | Turbine construction |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB1093312A true GB1093312A (en) | 1967-11-29 |
Family
ID=23322518
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB1495/65A Expired GB1093312A (en) | 1964-01-15 | 1965-01-13 | Improvements in or relating to turbine construction |
Country Status (8)
| Country | Link |
|---|---|
| US (1) | US3243158A (de) |
| BE (1) | BE658332A (de) |
| CH (1) | CH460450A (de) |
| DE (1) | DE1476916B2 (de) |
| FR (1) | FR1435869A (de) |
| GB (1) | GB1093312A (de) |
| NL (2) | NL6500415A (de) |
| SE (1) | SE305775B (de) |
Families Citing this family (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3295751A (en) * | 1965-04-21 | 1967-01-03 | United Aircraft Corp | Compressor stator shroud arrangement |
| US3387820A (en) * | 1965-05-24 | 1968-06-11 | Continental Aviat & Engineerin | Turbine engine construction |
| US3391904A (en) * | 1966-11-02 | 1968-07-09 | United Aircraft Corp | Optimum response tip seal |
| US3428129A (en) * | 1966-12-27 | 1969-02-18 | Mobil Oil Corp | Vertical fracture control |
| US3836279A (en) * | 1973-02-23 | 1974-09-17 | United Aircraft Corp | Seal means for blade and shroud |
| FR2452601A1 (fr) * | 1979-03-30 | 1980-10-24 | Snecma | Support amovible de revetement d'etancheite pour carter de soufflante de turboreacteur |
| DE3019920C2 (de) * | 1980-05-24 | 1982-12-30 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | Einrichtung zur äußeren Ummantelung der Laufschaufeln von Axialturbinen für Gasturbinentriebwerke |
| FR2574476B1 (fr) * | 1984-12-06 | 1987-01-02 | Snecma | Carter de retention pour soufflante de turboreacteur |
| US5395211A (en) * | 1994-01-14 | 1995-03-07 | United Technologies Corporation | Stator structure for a rotary machine |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR975879A (fr) * | 1948-12-06 | 1951-03-12 | Const Et D Equipements Mecaniq | Perfectionnement dans la construction des cylindres pour turbines à gaz |
| BE543281A (de) * | 1954-12-16 | |||
| GB868197A (en) * | 1956-09-28 | 1961-05-17 | Rolls Royce | Improvements in or relating to protective arrangements for use with rotating parts |
| US2987296A (en) * | 1957-12-02 | 1961-06-06 | Bendix Corp | Safety device for starter turbine |
| US3146992A (en) * | 1962-12-10 | 1964-09-01 | Gen Electric | Turbine shroud support structure |
-
0
- NL NL134135D patent/NL134135C/xx active
-
1964
- 1964-01-15 US US337905A patent/US3243158A/en not_active Expired - Lifetime
-
1965
- 1965-01-13 GB GB1495/65A patent/GB1093312A/en not_active Expired
- 1965-01-13 FR FR1722A patent/FR1435869A/fr not_active Expired
- 1965-01-14 CH CH53065A patent/CH460450A/fr unknown
- 1965-01-14 NL NL6500415A patent/NL6500415A/xx unknown
- 1965-01-15 SE SE524/65A patent/SE305775B/xx unknown
- 1965-01-15 BE BE658332D patent/BE658332A/xx unknown
- 1965-01-15 DE DE1965U0011371 patent/DE1476916B2/de active Pending
Also Published As
| Publication number | Publication date |
|---|---|
| CH460450A (fr) | 1968-07-31 |
| DE1476916A1 (de) | 1970-08-06 |
| DE1476916B2 (de) | 1970-11-26 |
| NL134135C (de) | |
| FR1435869A (fr) | 1966-04-22 |
| US3243158A (en) | 1966-03-29 |
| NL6500415A (de) | 1965-07-16 |
| BE658332A (de) | 1965-04-30 |
| SE305775B (de) | 1968-11-04 |
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