FR1542561A - Turbomachinery blade attachment device - Google Patents
Turbomachinery blade attachment deviceInfo
- Publication number
- FR1542561A FR1542561A FR1542561DA FR1542561A FR 1542561 A FR1542561 A FR 1542561A FR 1542561D A FR1542561D A FR 1542561DA FR 1542561 A FR1542561 A FR 1542561A
- Authority
- FR
- France
- Prior art keywords
- attachment device
- blade attachment
- turbomachinery blade
- turbomachinery
- blade
- 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.)
- Active
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
- F01D5/12—Blades
- F01D5/22—Blade-to-blade connections, e.g. for damping vibrations
- F01D5/24—Blade-to-blade connections, e.g. for damping vibrations using wire or the like
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/71—Ceramic products containing macroscopic reinforcing agents
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/71—Ceramic products containing macroscopic reinforcing agents
- C04B35/78—Ceramic products containing macroscopic reinforcing agents containing non-metallic materials
- C04B35/80—Fibres, filaments, whiskers, platelets, or the like
- C04B35/82—Asbestos; Glass; Fused silica
-
- 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
- F01D5/12—Blades
- F01D5/22—Blade-to-blade connections, e.g. for damping vibrations
- F01D5/225—Blade-to-blade connections, e.g. for damping vibrations by shrouding
-
- 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
- F01D5/12—Blades
- F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
-
- 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
-
- 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
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
- F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Ceramic Engineering (AREA)
- Materials Engineering (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Manufacturing & Machinery (AREA)
- Structural Engineering (AREA)
- Organic Chemistry (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR113959 | 1967-07-07 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1542561A true FR1542561A (en) |
Family
ID=8634946
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1542561D Active FR1542561A (en) | 1967-07-07 | Turbomachinery blade attachment device |
Country Status (3)
Country | Link |
---|---|
US (1) | US3501247A (en) |
FR (1) | FR1542561A (en) |
GB (1) | GB1208507A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2697285A1 (en) * | 1992-10-28 | 1994-04-29 | Snecma | Locking system of blade tips. |
EP2706242A1 (en) * | 2012-09-11 | 2014-03-12 | Techspace Aero S.A. | Fixing of blades on an axial compressor drum |
Families Citing this family (24)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3985465A (en) * | 1975-06-25 | 1976-10-12 | United Technologies Corporation | Turbomachine with removable stator vane |
US4492517A (en) * | 1983-01-06 | 1985-01-08 | General Electric Company | Segmented inlet nozzle for gas turbine, and methods of installation |
IT1167241B (en) * | 1983-10-03 | 1987-05-13 | Nuovo Pignone Spa | IMPROVED SYSTEM FOR FIXING STATOR NOZZLES TO THE CASE OF A POWER TURBINE |
CH666722A5 (en) * | 1985-07-05 | 1988-08-15 | Bbc Brown Boveri & Cie | Vane ring of an axially flowed turbo machine. |
FR2585069B1 (en) * | 1985-07-16 | 1989-06-09 | Snecma | DEVICE FOR LIMITING THE ANGULAR DEFLECTION OF BLADES MOUNTED ON A TURBOMACHINE ROTOR DISC |
US4767273A (en) * | 1987-02-24 | 1988-08-30 | Westinghouse Electric Corp. | Apparatus and method for reducing blade flop in steam turbine |
EP0290783B1 (en) * | 1987-04-13 | 1991-07-17 | BBC Brown Boveri AG | Fastening of an end plate to the rotor blade of a turbo machine |
EP1548233B1 (en) * | 2003-12-18 | 2006-08-02 | Techspace Aero S.A. | Fastening device for stator blades and compressor stator stage comprising such a fastening device |
US7628578B2 (en) | 2005-09-12 | 2009-12-08 | Pratt & Whitney Canada Corp. | Vane assembly with improved vane roots |
US7637718B2 (en) * | 2005-09-12 | 2009-12-29 | Pratt & Whitney Canada Corp. | Vane assembly with outer grommets |
US7530782B2 (en) * | 2005-09-12 | 2009-05-12 | Pratt & Whitney Canada Corp. | Foreign object damage resistant vane assembly |
US7413400B2 (en) * | 2005-09-12 | 2008-08-19 | Pratt & Whitney Canada Corp. | Vane assembly with grommet |
DE602005024425D1 (en) | 2005-12-22 | 2010-12-09 | Techspace Aero Milmort | Bucket ring of a turbomachine, turbomachine with such a guide ring and vane |
US8696311B2 (en) | 2011-03-29 | 2014-04-15 | Pratt & Whitney Canada Corp. | Apparatus and method for gas turbine engine vane retention |
FR2995934B1 (en) * | 2012-09-24 | 2018-06-01 | Safran Aircraft Engines | AUBE FOR TURBOMACHINE RECTIFIER |
EP2735707B1 (en) * | 2012-11-27 | 2017-04-05 | Safran Aero Boosters SA | Axial turbomachine guide nozzle with segmented inner shroud and corresponding compressor |
US20140255194A1 (en) * | 2012-12-21 | 2014-09-11 | General Electric Company | Tip shrouds of turbine rotor blades and methods of manufacture related thereto |
CA2903730A1 (en) | 2013-03-08 | 2014-09-12 | Rolls-Royce North American Technologies, Inc. | Method for forming a gas turbine engine composite airfoil assembly and corresponding airfoil assembly |
US9840929B2 (en) | 2013-05-28 | 2017-12-12 | Pratt & Whitney Canada Corp. | Gas turbine engine vane assembly and method of mounting same |
WO2015147821A1 (en) * | 2014-03-27 | 2015-10-01 | Siemens Aktiengesellschaft | Stator vane support system within a gas turbine engine |
FR3051825B1 (en) * | 2016-05-27 | 2020-02-28 | Safran Aircraft Engines | TURBOMACHINE RECTIFIER, AND METHOD FOR CHANGING THE BLADE SETTING |
US10767502B2 (en) | 2016-12-23 | 2020-09-08 | Rolls-Royce Corporation | Composite turbine vane with three-dimensional fiber reinforcements |
US20190234222A1 (en) * | 2018-01-30 | 2019-08-01 | United Technologies Corporation | Angled vane slot |
CN112324520B (en) * | 2020-10-27 | 2022-08-30 | 中国船舶重工集团公司第七0三研究所 | Stationary blade ring structure of gas turbine |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB599391A (en) * | 1945-05-25 | 1948-03-11 | Power Jets Res & Dev Ltd | Improvements in and relating to axial flow compressors, turbines and the like machines |
US764451A (en) * | 1903-12-19 | 1904-07-05 | Gen Electric | Bucket construction for turbines. |
GB281032A (en) * | 1926-09-09 | 1927-12-01 | Karl Baumann | Improvements relating to elastic fluid turbines |
GB267405A (en) * | 1926-09-09 | 1927-03-17 | Charles Oliver | Improvements in or relating to shrouding for turbine blades and the like |
US1720754A (en) * | 1926-09-09 | 1929-07-16 | Westinghouse Electric & Mfg Co | Turbine-blade shrouding |
-
0
- FR FR1542561D patent/FR1542561A/en active Active
-
1968
- 1968-07-01 GB GB31338/68A patent/GB1208507A/en not_active Expired
- 1968-07-05 US US742658A patent/US3501247A/en not_active Expired - Lifetime
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2697285A1 (en) * | 1992-10-28 | 1994-04-29 | Snecma | Locking system of blade tips. |
US5399069A (en) * | 1992-10-28 | 1995-03-21 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" | Vane extremity locking system |
EP2706242A1 (en) * | 2012-09-11 | 2014-03-12 | Techspace Aero S.A. | Fixing of blades on an axial compressor drum |
US9598968B2 (en) | 2012-09-11 | 2017-03-21 | Safran Aero Boosters Sa | Attaching the blades to the drum of an axial turbocompressor |
Also Published As
Publication number | Publication date |
---|---|
US3501247A (en) | 1970-03-17 |
GB1208507A (en) | 1970-10-14 |
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