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 use

Info

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
Application number
GB4097464A
Inventor
Frederick William Walto Morley
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to GB4097464A priority Critical patent/GB1061217A/en
Publication of GB1061217A publication Critical patent/GB1061217A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/16Form or construction for counteracting blade vibration
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P15/00Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
    • B23P15/04Making 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.
GB4097464A 1964-10-07 1964-10-07 An arrangement for damping vibrations in members which are subject to undesired vibration in use Expired GB1061217A (en)

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)

* Cited by examiner, † Cited by third party
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

Cited By (3)

* Cited by examiner, † Cited by third party
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

Similar Documents

Publication Publication Date Title
GB1008487A (en) Method for fastening blades into the rotors of turbine or like machines
GB910046A (en) Bearing cap
GB1203083A (en) A method for producing bearings
GB1061217A (en) An arrangement for damping vibrations in members which are subject to undesired vibration in use
ES478827A1 (en) Automatic chilled water setpoint temperature control
GB1390936A (en) Fat
GB893787A (en) Improvements relating to damped bodies and methods of manufacturing them
GB712692A (en) Improvements in or relating to bearing arrangements
JPS5331208A (en) Lubricator for closed compressor and the like
GB1409628A (en) Nickel base alloy containing hafnium
SU148303A1 (en) Gas Lubricated Bearing
FR1226775A (en) Synthetic lubricant, especially for aircraft gas turbines
GB1352853A (en) Method of forming ceramic articles and articles formed by such a method
GB1198793A (en) Improvements in or relating to Circular Saw Blades
GB887130A (en) Improvements in or relating to a method of making a bezel ring with lugs
Minin Motion of the Envelope of a Variable Mass
CA663382A (en) Aviation gas turbine lubricants
FR1104891A (en) Improvements made to the start-up of turbine engines, especially those intended for rocket thrusters
ZEIDLER et al. Optimization of a combined Ruzicka and Snowdon vibration isolation system(Performance characteristics of combined Ruzicka and Snowdon vibration isolation system)
Stafford Recent Technological Trends in Relation to Man
FR896388A (en) Cooling circuit of combustion engines, in particular of aircraft engines
AU3847358A (en) Vibration damping shroud for gas turbine engines
Dent Webster's Sources
GB464167A (en) Improvements in or relating to slicing machines
CA608827A (en) Transpiration cooled turbine blade and method of making the same