GB1061217A - An arrangement for damping vibrations in members which are subject to undesired vibration in use - Google Patents
An arrangement for damping vibrations in members which are subject to undesired vibration in useInfo
- Publication number
- GB1061217A GB1061217A GB4097464A GB4097464A GB1061217A GB 1061217 A GB1061217 A GB 1061217A GB 4097464 A GB4097464 A GB 4097464A GB 4097464 A GB4097464 A GB 4097464A GB 1061217 A GB1061217 A GB 1061217A
- Authority
- GB
- United Kingdom
- Prior art keywords
- sheath
- core
- subject
- members
- arrangement
- 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
-
- 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
- F01D5/14—Form or construction
- F01D5/16—Form or construction for counteracting blade vibration
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P15/00—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
- B23P15/04—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass turbine or like blades from several pieces
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
1,061,217. Making turbine and like blades. ROLLS-ROYCE Ltd. Sept. 30, 1965 [Oct. 7, 1964], No. 40974/64. Heading B3A. [Also in Divisions F1 and F2] A method of making a member, such as a turbine blade, subject in use to undesired vibrations comprises the steps of fitting an insert into a hollow slug, forging the resultant compound block to form a member comprising a sheath 12 and a core 15, and cooling the member to a temperature at which the core is separated from the sheath by a small space 19 which is filled with lubricant, any vibration of the member then being damped by friction resulting from relative movement between the sheath and the core. The core and the sheath may be made of the same material, or of materials having different coefficients of expansion.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB4097464A GB1061217A (en) | 1964-10-07 | 1964-10-07 | An arrangement for damping vibrations in members which are subject to undesired vibration in use |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB4097464A GB1061217A (en) | 1964-10-07 | 1964-10-07 | An arrangement for damping vibrations in members which are subject to undesired vibration in use |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1061217A true GB1061217A (en) | 1967-03-08 |
Family
ID=10417518
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB4097464A Expired GB1061217A (en) | 1964-10-07 | 1964-10-07 | An arrangement for damping vibrations in members which are subject to undesired vibration in use |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB1061217A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2474095A1 (en) * | 1980-01-17 | 1981-07-24 | Rolls Royce | VIBRATION DAMPING DEVICE FOR MOBILE BLADES OF A GAS TURBINE ENGINE |
GB2142387A (en) * | 1983-07-02 | 1985-01-16 | Rolls Royce | An aerofoil for a gas turbine engine |
US7794210B2 (en) | 2006-07-29 | 2010-09-14 | Rolls-Royce Plc | Turbomachine blade |
-
1964
- 1964-10-07 GB GB4097464A patent/GB1061217A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2474095A1 (en) * | 1980-01-17 | 1981-07-24 | Rolls Royce | VIBRATION DAMPING DEVICE FOR MOBILE BLADES OF A GAS TURBINE ENGINE |
GB2142387A (en) * | 1983-07-02 | 1985-01-16 | Rolls Royce | An aerofoil for a gas turbine engine |
US7794210B2 (en) | 2006-07-29 | 2010-09-14 | Rolls-Royce Plc | Turbomachine blade |
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