GB728710A - Improvements in and relating to axial-flow turbines and the like - Google Patents

Improvements in and relating to axial-flow turbines and the like

Info

Publication number
GB728710A
GB728710A GB2462/53A GB246253A GB728710A GB 728710 A GB728710 A GB 728710A GB 2462/53 A GB2462/53 A GB 2462/53A GB 246253 A GB246253 A GB 246253A GB 728710 A GB728710 A GB 728710A
Authority
GB
United Kingdom
Prior art keywords
blade
root
blades
pieces
piece
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
GB2462/53A
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.)
Sulzer Escher Wyss AG
Original Assignee
Escher Wyss AG
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 Escher Wyss AG filed Critical Escher Wyss AG
Publication of GB728710A publication Critical patent/GB728710A/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
    • F01D5/30Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/3053Fixing blades to rotors; Blade roots ; Blade spacers by means of pins

Abstract

728,710. Turbines and compressors. ESCHER WYSS AKT.-GES. Jan. 28, 1953 [Feb. 13, 1952], No. 2462/53. Class 110 (3). In an axial-flow turbine or compressor, blades are mounted in slots in a blade carrier, the slots extending substantially parallel to the chords of the blades and having parallel lateral faces. The blades have a constant cross-sectional profile throughout their length and one or more root pieces are fitted to each blade where the blades are mounted in the blade carrier so as to form a prismatic-shaped root having parallel lateral faces which lie against the faces of the associated slot. The blades and root pieces are secured by pins, at least one for each blade, which extend through the blade carrier, blade and root piece. The root piece may be welded to the blade. In Fig. 2, the blade 3 is mounted in a slot 2 in the rotor disc 1 and the root portion is formed by two root pieces 4, 5 at either side of the root end of the blade, the blade being secured in position by two pins 6. In a second embodiment in which one face of the blade is plane, only one root piece is provided. In an embodiment in which the blade is hollow and is formed of sheet metal, two root pieces are used and they bear against each other beyond the leading and trailing edges of the blade. Alternatively, an additional piece 17, Fig. 5, may be inserted into the hollow blade in the region of the root pieces.
GB2462/53A 1952-02-13 1953-01-28 Improvements in and relating to axial-flow turbines and the like Expired GB728710A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH728710X 1952-02-13

Publications (1)

Publication Number Publication Date
GB728710A true GB728710A (en) 1955-04-27

Family

ID=4532169

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2462/53A Expired GB728710A (en) 1952-02-13 1953-01-28 Improvements in and relating to axial-flow turbines and the like

Country Status (6)

Country Link
BE (1) BE517285A (en)
CH (1) CH298592A (en)
DE (1) DE942236C (en)
FR (1) FR1070291A (en)
GB (1) GB728710A (en)
NL (1) NL81262C (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4767275A (en) * 1986-07-11 1988-08-30 Westinghouse Electric Corp. Locking pin system for turbine curved root side entry closing blades

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3073568A (en) * 1958-06-27 1963-01-15 Edward A Stalker Composite blades for turbines, compressors and the like
US4605355A (en) * 1983-03-31 1986-08-12 Competition Aircraft, Inc. Propeller
DE3710321C1 (en) * 1987-03-28 1988-06-01 Mtu Muenchen Gmbh Fan blade, especially for prop fan engines
FR2990462B1 (en) 2012-05-14 2014-05-30 Snecma DEVICE FOR ATTACHING AUBES TO A TURBOMACHINE ROTOR DISC

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE391880C (en) * 1921-05-14 1924-07-29 Christian Lorenzen Blade attachment for gas turbines with combustion air passed through the turbine blades
US2402418A (en) * 1943-01-20 1946-06-18 Westinghouse Electric Corp Turbine apparatus
DE829685C (en) * 1945-03-17 1952-01-28 Bayerische Motoren Werke Ag Attachment of the blades in the wheel disc, especially of exhaust gas turbines
FR955013A (en) * 1946-11-20 1950-01-07
FR970578A (en) * 1948-08-19 1951-01-05 Bohler & Cie Ag Geb Hollow blades for turbines, in particular for gas turbines, and method for their manufacture
FR981133A (en) * 1949-02-21 1951-05-22 Parsons C A & Co Ltd Process for the manufacture of hollow blades for internal combustion turbines
FR989043A (en) * 1949-04-19 1951-09-04 Rateau Soc Blades for turbine engine wheels and in particular gas blades
BE498667A (en) * 1949-08-27

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4767275A (en) * 1986-07-11 1988-08-30 Westinghouse Electric Corp. Locking pin system for turbine curved root side entry closing blades

Also Published As

Publication number Publication date
CH298592A (en) 1954-05-15
NL81262C (en)
DE942236C (en) 1956-04-26
BE517285A (en)
FR1070291A (en) 1954-07-21

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