GB1084537A - A compressor or turbine rotor for a gas turbine engine - Google Patents

A compressor or turbine rotor for a gas turbine engine

Info

Publication number
GB1084537A
GB1084537A GB32861/65A GB3286165A GB1084537A GB 1084537 A GB1084537 A GB 1084537A GB 32861/65 A GB32861/65 A GB 32861/65A GB 3286165 A GB3286165 A GB 3286165A GB 1084537 A GB1084537 A GB 1084537A
Authority
GB
United Kingdom
Prior art keywords
blades
clappers
compressor
adjacent
turbine
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
GB32861/65A
Other languages
English (en)
Inventor
Robert Vaughan Blackhurst
William Harrison
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 GB32861/65A priority Critical patent/GB1084537A/en
Priority to US563558A priority patent/US3327995A/en
Priority to DER43722A priority patent/DE1301638B/de
Publication of GB1084537A publication Critical patent/GB1084537A/en
Priority to MY1969151A priority patent/MY6900151A/xx
Expired legal-status Critical Current

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
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
GB32861/65A 1965-07-31 1965-07-31 A compressor or turbine rotor for a gas turbine engine Expired GB1084537A (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
GB32861/65A GB1084537A (en) 1965-07-31 1965-07-31 A compressor or turbine rotor for a gas turbine engine
US563558A US3327995A (en) 1965-07-31 1966-07-07 Bladed rotor
DER43722A DE1301638B (de) 1965-07-31 1966-07-18 Laufschaufelkranz fuer Gasturbinentriebwerke
MY1969151A MY6900151A (en) 1965-07-31 1969-12-31 Contact heat fusing device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB32861/65A GB1084537A (en) 1965-07-31 1965-07-31 A compressor or turbine rotor for a gas turbine engine

Publications (1)

Publication Number Publication Date
GB1084537A true GB1084537A (en) 1967-09-27

Family

ID=10345112

Family Applications (1)

Application Number Title Priority Date Filing Date
GB32861/65A Expired GB1084537A (en) 1965-07-31 1965-07-31 A compressor or turbine rotor for a gas turbine engine

Country Status (4)

Country Link
US (1) US3327995A (de)
DE (1) DE1301638B (de)
GB (1) GB1084537A (de)
MY (1) MY6900151A (de)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1142877A (en) * 1966-06-28 1969-02-12 Rolls Royce Improvements in or relating to bladed rotors, particularly for use in gas turbine engines
US3799701A (en) * 1972-02-28 1974-03-26 United Aircraft Corp Composite fan blade and method of construction
US3796513A (en) * 1972-06-19 1974-03-12 Westinghouse Electric Corp High damping blades
US3936230A (en) * 1974-05-09 1976-02-03 The United States Of America As Represented By The Secretary Of The Air Force Self-supported, self-locating seal for turbine engines
US4257741A (en) * 1978-11-02 1981-03-24 General Electric Company Turbine engine blade with airfoil projection
US4326836A (en) * 1979-12-13 1982-04-27 United Technologies Corporation Shroud for a rotor blade
US5083903A (en) * 1990-07-31 1992-01-28 General Electric Company Shroud insert for turbomachinery blade
US5137426A (en) * 1990-08-06 1992-08-11 General Electric Company Blade shroud deformable protective coating
US5267834A (en) * 1992-12-30 1993-12-07 General Electric Company Bucket for the last stage of a steam turbine
US6039542A (en) * 1997-12-24 2000-03-21 General Electric Company Panel damped hybrid blade
US6282786B1 (en) 1999-08-16 2001-09-04 General Electric Company Method of making injection formed hybrid airfoil
US6099257A (en) * 1999-08-31 2000-08-08 General Electric Company Plastically formed hybrid airfoil
JP2009007981A (ja) * 2007-06-27 2009-01-15 Toshiba Corp 蒸気タービン用長動翼翼列の中間固定支持構造及び蒸気タービン
IN2012DN02173A (de) 2009-09-17 2015-08-21 Bell Helicopter Textron Inc
US8398374B2 (en) * 2010-01-27 2013-03-19 General Electric Company Method and apparatus for a segmented turbine bucket assembly
DE102010041702A1 (de) * 2010-09-30 2012-04-05 Siemens Aktiengesellschaft Koppelbolzen für Turbinenschaufeln

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1618296A (en) * 1925-08-01 1927-02-22 Westinghouse Electric & Mfg Co Turbine-blade lashing
US1749449A (en) * 1928-06-06 1930-03-04 Westinghouse Electric & Mfg Co Turbine blading and lashing therefor
GB358406A (en) * 1930-02-28 1931-10-08 British Thomson Houston Co Ltd Improvements in and relating to elastic fluid turbines
DE819242C (de) * 1949-02-17 1951-10-31 Escher Wyss Ag Beschaufelung an Rotoren von axial durchstroemten Kreiselmaschinen, insbesondere von Dampf-, Gasturbinen und Verdichtern
FR1033197A (fr) * 1951-02-27 1953-07-08 Rateau Soc Amortisseurs de vibrations pour aubages mobiles de turbo-machines
US2771267A (en) * 1952-05-27 1956-11-20 United Aircraft Corp Lacing for compressor blades
FR69842E (fr) * 1956-05-30 1958-12-30 Rateau Soc Amortisseurs de vibrations pour aubages mobiles de turbo-machines
US2912157A (en) * 1957-05-10 1959-11-10 United Aircraft Corp Cambered shroud
US3216699A (en) * 1963-10-24 1965-11-09 Gen Electric Airfoil member assembly

Also Published As

Publication number Publication date
DE1301638B (de) 1969-08-21
US3327995A (en) 1967-06-27
MY6900151A (en) 1969-12-31

Similar Documents

Publication Publication Date Title
GB1084537A (en) A compressor or turbine rotor for a gas turbine engine
GB1270348A (en) Improvements in lightweight turbomachinery blading
GB1268202A (en) Composite blade for an elastic fluid flow machine
GB1271819A (en) Improvements in film cooling of structural members in gas turbine engines
GB1318260A (en) Turbomachinery blades
GB1410014A (en) Gas turbine engine blade
GB1433519A (en) Turbomachine blades made of composite fibres
GB1040825A (en) Improvements in rotor blades and/or stator blades for gas turbine engines
GB1093568A (en) Improvements in or relating to bladed rotors such as compressor rotors
GB1240765A (en) Cooled turbine blades
GB1272200A (en) Axial-flow turbomachine rotors
GB1522594A (en) Supersonic blade cascades
GB1270156A (en) Improvements in transonic blades for axial flow turbines
GB1119258A (en) Improvements in and relating to a composite helicopter blade
GB1158238A (en) Blade Assembly for a Fluid Flow Machine.
GB1217458A (en) Blades for high temperature turbomachines
GB731292A (en) Improvements in processes of making turbine and compressor blades
GB1353114A (en) Turbo-machinery
US2868441A (en) Plastic blades, particularly for a compressor rotor of a gas turbine engine
GB1228996A (de)
GB1302857A (de)
GB1305266A (de)
GB774499A (en) Corrugated-cored elements for use in turbines, compressors and combustion equipment
FR2165264A5 (en) Turbine blades - of synthetic resin incorporate reinforcing plate which is exposed at the leading edge
GB1116580A (en) Stator blade assemblies for axial-flow turbine engines