IT1045599B - Mezzi per ritenere palette su un disco struttura simile - Google Patents
Mezzi per ritenere palette su un disco struttura simileInfo
- Publication number
- IT1045599B IT1045599B IT28937/75A IT2893775A IT1045599B IT 1045599 B IT1045599 B IT 1045599B IT 28937/75 A IT28937/75 A IT 28937/75A IT 2893775 A IT2893775 A IT 2893775A IT 1045599 B IT1045599 B IT 1045599B
- Authority
- IT
- Italy
- Prior art keywords
- palette
- believe
- disc
- similar structure
- similar
- Prior art date
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
-
- 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
- F01D5/3007—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type
- F01D5/3015—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type with side plates
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB47904/74A GB1479332A (en) | 1974-11-06 | 1974-11-06 | Means for retaining blades to a disc or like structure |
Publications (1)
Publication Number | Publication Date |
---|---|
IT1045599B true IT1045599B (it) | 1980-06-10 |
Family
ID=10446671
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IT28937/75A IT1045599B (it) | 1974-11-06 | 1975-10-31 | Mezzi per ritenere palette su un disco struttura simile |
Country Status (6)
Country | Link |
---|---|
US (1) | US4019833A (it) |
JP (1) | JPS554930B2 (it) |
DE (1) | DE2549649C3 (it) |
FR (1) | FR2290570A1 (it) |
GB (1) | GB1479332A (it) |
IT (1) | IT1045599B (it) |
Families Citing this family (40)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2393931A1 (fr) * | 1977-06-08 | 1979-01-05 | Snecma | Dispositif de maintien des aubes d'un rotor |
JPS5699655U (it) * | 1979-12-21 | 1981-08-06 | ||
US4389161A (en) * | 1980-12-19 | 1983-06-21 | United Technologies Corporation | Locking of rotor blades on a rotor disk |
JPS62118033A (ja) * | 1985-11-04 | 1987-05-29 | ユナイテツド・テクノロジ−ズ・コ−ポレイシヨン | タ−ビンのデイスクとサイドプレ−トの組合体 |
US4701105A (en) * | 1986-03-10 | 1987-10-20 | United Technologies Corporation | Anti-rotation feature for a turbine rotor faceplate |
FR2603333B1 (fr) * | 1986-09-03 | 1990-07-20 | Snecma | Rotor de turbomachine comportant un moyen de verrouillage axial et d'etancheite d'aubes montees dans des brochages axiaux du disque et procede de montage |
DE3835932A1 (de) * | 1988-10-21 | 1990-04-26 | Mtu Muenchen Gmbh | Vorrichtung zur kuehlluftzufuehrung fuer gasturbinen-rotorschaufeln |
DE3934207A1 (de) * | 1989-10-13 | 1991-04-25 | Mtu Muenchen Gmbh | Anordnung zur befestigung von turboschaufeln |
FR2663997B1 (fr) * | 1990-06-27 | 1993-12-24 | Snecma | Dispositif de fixation d'une couronne de revolution sur un disque de turbomachine. |
FR2666623B1 (fr) * | 1990-09-11 | 1993-05-07 | Turbomeca | Roue de turbomachine a pales rapportees. |
US5275534A (en) * | 1991-10-30 | 1994-01-04 | General Electric Company | Turbine disk forward seal assembly |
US5211407A (en) * | 1992-04-30 | 1993-05-18 | General Electric Company | Compressor rotor cross shank leak seal for axial dovetails |
DE4438611C2 (de) * | 1994-10-28 | 1998-02-19 | Bmw Rolls Royce Gmbh | Radialverdichter oder Radialturbine mit einem Leitschaufeln aufweisenden Diffusor oder Turbinenleitkranz |
DE19960896A1 (de) | 1999-12-17 | 2001-06-28 | Rolls Royce Deutschland | Rückhaltevorrichtung für Rotorschaufeln einer Axialturbomaschine |
US6951448B2 (en) | 2002-04-16 | 2005-10-04 | United Technologies Corporation | Axial retention system and components thereof for a bladed rotor |
GB0423363D0 (en) * | 2004-10-21 | 2004-11-24 | Rolls Royce Plc | Rotor assembly retaining apparatus |
ES2321862T3 (es) * | 2006-09-25 | 2009-06-12 | Siemens Aktiengesellschaft | Rotor de turbina con placas de bloqueo y correspondiente procedimiento de montaje. |
EP1916389A1 (en) * | 2006-10-26 | 2008-04-30 | Siemens Aktiengesellschaft | Turbine blade assembly |
FR2918106B1 (fr) * | 2007-06-27 | 2011-05-06 | Snecma | Dispositif de retenue axiale d'aubes montees sur un disque de rotor de turbomachine. |
FR2928406A1 (fr) * | 2008-03-07 | 2009-09-11 | Snecma Sa | Dispositif de retenue axiale d'aubes montees sur un disque de rotor de turbomachine, disque de rotor et flasque de maintien d'un tel dispositif |
US8206119B2 (en) * | 2009-02-05 | 2012-06-26 | General Electric Company | Turbine coverplate systems |
US7980781B2 (en) * | 2009-02-20 | 2011-07-19 | Charles Edward Trice | Self locking mast assembly and method of making |
US20100232939A1 (en) * | 2009-03-12 | 2010-09-16 | General Electric Company | Machine Seal Assembly |
US8696320B2 (en) * | 2009-03-12 | 2014-04-15 | General Electric Company | Gas turbine having seal assembly with coverplate and seal |
US8419370B2 (en) * | 2009-06-25 | 2013-04-16 | Rolls-Royce Corporation | Retaining and sealing ring assembly |
US8469670B2 (en) * | 2009-08-27 | 2013-06-25 | Rolls-Royce Corporation | Fan assembly |
US8435006B2 (en) * | 2009-09-30 | 2013-05-07 | Rolls-Royce Corporation | Fan |
US8579538B2 (en) | 2010-07-30 | 2013-11-12 | United Technologies Corporation | Turbine engine coupling stack |
US8491267B2 (en) | 2010-08-27 | 2013-07-23 | Pratt & Whitney Canada Corp. | Retaining ring arrangement for a rotary assembly |
US8662845B2 (en) | 2011-01-11 | 2014-03-04 | United Technologies Corporation | Multi-function heat shield for a gas turbine engine |
US8840375B2 (en) | 2011-03-21 | 2014-09-23 | United Technologies Corporation | Component lock for a gas turbine engine |
US8727735B2 (en) * | 2011-06-30 | 2014-05-20 | General Electric Company | Rotor assembly and reversible turbine blade retainer therefor |
US8745881B2 (en) * | 2011-07-25 | 2014-06-10 | Bettcher Industries, Inc. | Power operated rotary knife |
US8752299B2 (en) * | 2012-02-29 | 2014-06-17 | Bettcher Industries, Inc. | Blade guide assembly for power operated rotary knife |
WO2014137435A2 (en) | 2013-03-05 | 2014-09-12 | Rolls-Royce North American Technologies, Inc. | Turbine segmented cover plate retention method |
US9945237B2 (en) * | 2013-03-15 | 2018-04-17 | United Technologies Corporation | Lock for retaining minidisks with rotors of a gas turbine engine |
GB201417038D0 (en) | 2014-09-26 | 2014-11-12 | Rolls Royce Plc | A bladed rotor arrangement |
KR102182102B1 (ko) | 2014-11-27 | 2020-11-23 | 한화에어로스페이스 주식회사 | 터빈 장치 |
EP3073052B1 (en) * | 2015-02-17 | 2018-01-24 | Rolls-Royce Corporation | Fan assembly |
US11168615B1 (en) * | 2020-08-25 | 2021-11-09 | Raytheon Technologies Corporation | Double ring axial sealing design |
Family Cites Families (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR960069A (it) * | 1947-04-02 | 1950-04-12 | ||
GB779059A (en) * | 1954-07-15 | 1957-07-17 | Rolls Royce | Improvements in or relating to axial-flow fluid machines, for example compressors orturbines of gas-turbine engines |
BE551145A (it) * | 1955-09-26 | |||
GB802476A (en) * | 1955-09-29 | 1958-10-08 | Rolls Royce | Improvements in or relating to rotors of axial-flow fluid machines for example compressors and turbines |
US2988324A (en) * | 1957-06-14 | 1961-06-13 | Napier & Son Ltd | Rotors for multi-stage axial flow compressors or turbines |
US2988325A (en) * | 1957-07-18 | 1961-06-13 | Rolls Royce | Rotary fluid machine with means supplying fluid to rotor blade passages |
GB928349A (en) * | 1960-12-06 | 1963-06-12 | Rolls Royce | Improvements in or relating to bladed rotors of fluid flow machines |
NL295165A (it) * | 1962-07-11 | |||
US3501249A (en) * | 1968-06-24 | 1970-03-17 | Westinghouse Electric Corp | Side plates for turbine blades |
US3572966A (en) * | 1969-01-17 | 1971-03-30 | Westinghouse Electric Corp | Seal plates for root cooled turbine rotor blades |
US3635586A (en) * | 1970-04-06 | 1972-01-18 | Rolls Royce | Method and apparatus for turbine blade cooling |
US3644058A (en) * | 1970-05-18 | 1972-02-22 | Westinghouse Electric Corp | Axial positioner and seal for turbine blades |
BE794573A (fr) * | 1972-02-02 | 1973-05-16 | Gen Electric | Dispositif de fixation d'aubes |
-
1974
- 1974-11-06 GB GB47904/74A patent/GB1479332A/en not_active Expired
-
1975
- 1975-10-31 IT IT28937/75A patent/IT1045599B/it active
- 1975-10-31 US US05/627,785 patent/US4019833A/en not_active Expired - Lifetime
- 1975-11-04 FR FR7533661A patent/FR2290570A1/fr active Granted
- 1975-11-05 DE DE2549649A patent/DE2549649C3/de not_active Expired
- 1975-11-06 JP JP13355775A patent/JPS554930B2/ja not_active Expired
Also Published As
Publication number | Publication date |
---|---|
DE2549649A1 (de) | 1976-05-20 |
US4019833A (en) | 1977-04-26 |
JPS5169709A (it) | 1976-06-16 |
DE2549649B2 (de) | 1978-09-07 |
FR2290570A1 (fr) | 1976-06-04 |
JPS554930B2 (it) | 1980-02-01 |
DE2549649C3 (de) | 1982-09-09 |
GB1479332A (en) | 1977-07-13 |
FR2290570B1 (it) | 1980-10-31 |
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