GB710938A - Improvements in or relating to rotor blades for axial-flow fluid machines - Google Patents

Improvements in or relating to rotor blades for axial-flow fluid machines

Info

Publication number
GB710938A
GB710938A GB124251A GB124251A GB710938A GB 710938 A GB710938 A GB 710938A GB 124251 A GB124251 A GB 124251A GB 124251 A GB124251 A GB 124251A GB 710938 A GB710938 A GB 710938A
Authority
GB
United Kingdom
Prior art keywords
blade
stiffener
axial
edge
tip
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
GB124251A
Inventor
Norman Battle
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 GB124251A priority Critical patent/GB710938A/en
Publication of GB710938A publication Critical patent/GB710938A/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
    • F01D5/20Specially-shaped blade tips to seal space between tips and stator
    • 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
    • F01D5/147Construction, i.e. structural features, e.g. of weight-saving hollow blades

Abstract

710,938. Turbine and compressor blades. ROLLS-ROYCE, Ltd. April 7, 1952 [Jan. 16, 1951], No. 1242/51. Class 110(3) [Also in Group XXII] A rotor blade for an axial-flow turbine or compressor of a gas-turbine engine has a stiffener piece 15 formed as a plate separate from the blade and secured at the tip of the blade as by welding, one edge 15a of the stiffener being curved to the shape of the concave surface of the blade, and the other edge 15b being parallel to the line joining the leading and trailing edges of the blade at the blade tip. A step or groove 12, 13 is formed at the blade tip by an edge milling operation, and the stiffener piece has the shape of a segment of the milling cutter 14. The axis 14a of the milling cutter is inclined to the spanwise axis 11a of the blade. The stiffener piece may be formed of greater length than required, the excess metal 15c being removed after securing in position. The stiffener piece lies at an angle to the tangent to the surface of the surrounding shroud ring.
GB124251A 1951-01-16 1951-01-16 Improvements in or relating to rotor blades for axial-flow fluid machines Expired GB710938A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB124251A GB710938A (en) 1951-01-16 1951-01-16 Improvements in or relating to rotor blades for axial-flow fluid machines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB124251A GB710938A (en) 1951-01-16 1951-01-16 Improvements in or relating to rotor blades for axial-flow fluid machines

Publications (1)

Publication Number Publication Date
GB710938A true GB710938A (en) 1954-06-23

Family

ID=9718584

Family Applications (1)

Application Number Title Priority Date Filing Date
GB124251A Expired GB710938A (en) 1951-01-16 1951-01-16 Improvements in or relating to rotor blades for axial-flow fluid machines

Country Status (1)

Country Link
GB (1) GB710938A (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5282721A (en) * 1991-09-30 1994-02-01 United Technologies Corporation Passive clearance system for turbine blades
US5688107A (en) * 1992-12-28 1997-11-18 United Technologies Corp. Turbine blade passive clearance control
US6347301B1 (en) * 1999-02-02 2002-02-12 Bearden, Iii Fred E. Conference communication facilitator and method of use
EP1953344A1 (en) 2007-02-05 2008-08-06 Siemens Aktiengesellschaft Turbine blade
EP2336492A1 (en) 2009-12-16 2011-06-22 Siemens Aktiengesellschaft Guide vane with a winglet for an energy converting machine and machine for converting energy comprising the guide vane
EP1693552A3 (en) * 2005-02-16 2011-09-14 Rolls-Royce Plc A turbine blade
US20140010643A1 (en) * 2011-03-11 2014-01-09 Alstom Technology Ltd. Method of fabricating a steam turbine deflector
US8840361B2 (en) 2010-09-09 2014-09-23 Rolls-Royce Plc Fan blade with winglet

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5282721A (en) * 1991-09-30 1994-02-01 United Technologies Corporation Passive clearance system for turbine blades
US5688107A (en) * 1992-12-28 1997-11-18 United Technologies Corp. Turbine blade passive clearance control
US6347301B1 (en) * 1999-02-02 2002-02-12 Bearden, Iii Fred E. Conference communication facilitator and method of use
EP1693552A3 (en) * 2005-02-16 2011-09-14 Rolls-Royce Plc A turbine blade
EP1953344A1 (en) 2007-02-05 2008-08-06 Siemens Aktiengesellschaft Turbine blade
EP2336492A1 (en) 2009-12-16 2011-06-22 Siemens Aktiengesellschaft Guide vane with a winglet for an energy converting machine and machine for converting energy comprising the guide vane
WO2011072892A1 (en) 2009-12-16 2011-06-23 Siemens Aktiengesellschaft Guide vane with a winglet for an energy converting machine and machine for converting energy comprising the guide vane
US9175574B2 (en) 2009-12-16 2015-11-03 Siemens Aktiengesellschaft Guide vane with a winglet for an energy converting machine and machine for converting energy comprising the guide vane
US8840361B2 (en) 2010-09-09 2014-09-23 Rolls-Royce Plc Fan blade with winglet
US20140010643A1 (en) * 2011-03-11 2014-01-09 Alstom Technology Ltd. Method of fabricating a steam turbine deflector
US9604323B2 (en) * 2011-03-11 2017-03-28 General Electric Technology Gmbh Method of fabricating a steam turbine deflector

Similar Documents

Publication Publication Date Title
GB1284538A (en) Blade for a fluid flow machine
GB1130285A (en) Method of making an aerofoil shaped blade for a fluid flow machine
GB1366924A (en) Compressor blades
GB1270156A (en) Improvements in transonic blades for axial flow turbines
GB1491556A (en) Rotor blades for turbomachines
GB1500858A (en) Blade for thermal axial-flow turbo machines
GB1408491A (en) Composite turbomachinery blade root configuration
GB710938A (en) Improvements in or relating to rotor blades for axial-flow fluid machines
GB1432994A (en) Compressor for gas turbine engines
GB1419381A (en) Fan for gas turbine engines
GB1513338A (en) Rotor blade for a gas turbine engine
GB1151937A (en) Bladed Rotors for Fluid Flow Machines
GB1033759A (en) Aerofoil-shaped blade
GB712523A (en) Improvements in or relating to guide vane assemblies in annular fluid ducts
GB1107024A (en) Improvements in and relating to blades for turbo-machines
GB1231424A (en)
GB609322A (en) Improvements relating to axial-flow compressors and like machines, and blading thereof
GB1406098A (en) Fluid flow machines
GB846583A (en) Improvements in or relating to rotor blading of fluid machines, for example, of compressors and turbines of gas turbine engines
GB1158813A (en) Stator vane for a gas turbine engine
GB731456A (en) Improvements in or relating to bladed rotors of axial-flow machines and blade elements therefor
GB622767A (en) Improvements in or relating to the blades of axial flow compressors and turbines andthe means for fixing them
GB1294593A (en) Improvements in radial flow turbines
GB751127A (en) Improvements in turbine or compressor blades
JPS5566602A (en) Impeller of turbo machine