GB609771A - Improvements relating to the manufacture of bladed turbine discs, compressor rotors or the like - Google Patents

Improvements relating to the manufacture of bladed turbine discs, compressor rotors or the like

Info

Publication number
GB609771A
GB609771A GB881846A GB881846A GB609771A GB 609771 A GB609771 A GB 609771A GB 881846 A GB881846 A GB 881846A GB 881846 A GB881846 A GB 881846A GB 609771 A GB609771 A GB 609771A
Authority
GB
United Kingdom
Prior art keywords
per cent
sieve
refractory material
mould
silicate
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
GB881846A
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.)
Power Jets Research and Development Ltd
Original Assignee
Power Jets Research and Development Ltd
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 Power Jets Research and Development Ltd filed Critical Power Jets Research and Development Ltd
Priority to GB881846A priority Critical patent/GB609771A/en
Publication of GB609771A publication Critical patent/GB609771A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22CFOUNDRY MOULDING
    • B22C9/00Moulds or cores; Moulding processes
    • B22C9/02Sand moulds or like moulds for shaped castings
    • B22C9/04Use of lost patterns

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Mold Materials And Core Materials (AREA)

Abstract

In a method of casting rotary bladed bodies such as turbine discs, (see Group XXII), a wax model is coated with a suspension of silica or other refractory oxide or silicate in a solution containing sodium silicate or ethyl silicate as a binder. The mould is formed by pouring around the coated wax model, finely ground refractory material in suspension, a preferred composition consisting of 10 lbs. of solid refractory material comprising 60 per cent calcined fireclay "grog" and 40 per cent of silica flour, and 1 litre of a liquid consisting of 25 per cent tetra ethyl silicate, 50 per cent alcohol or methylated spirit, and 25 per cent of a solution of 15 per cent concentrated hydrochloric acid in 80 per cent aqueous alcohol. The refractory material has a grading as follows:- Silica Flour-All through 200 B.S.S. sieve. Grog-2 per cent on 10 B.S.S. sieve. 20 per cent through 10 or 30 B.S.S. sieve. 18 per cent through 30 or 60 B.S.S. sieve. 17 per cent through 60 or 100 B.S.S. sieve. 20 per cent through 100 or 170 B.S.S. sieve. Remainder through 170 B.S.S. sieve. The setting of the mould may be accelerated by the addition to the mould material of a refractory material and alkali such as magnesium oxide or other basic compound.
GB881846A 1946-03-21 1946-03-21 Improvements relating to the manufacture of bladed turbine discs, compressor rotors or the like Expired GB609771A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB881846A GB609771A (en) 1946-03-21 1946-03-21 Improvements relating to the manufacture of bladed turbine discs, compressor rotors or the like

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB881846A GB609771A (en) 1946-03-21 1946-03-21 Improvements relating to the manufacture of bladed turbine discs, compressor rotors or the like

Publications (1)

Publication Number Publication Date
GB609771A true GB609771A (en) 1948-10-06

Family

ID=9859810

Family Applications (1)

Application Number Title Priority Date Filing Date
GB881846A Expired GB609771A (en) 1946-03-21 1946-03-21 Improvements relating to the manufacture of bladed turbine discs, compressor rotors or the like

Country Status (1)

Country Link
GB (1) GB609771A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1363028A1 (en) * 2001-06-06 2003-11-19 BorgWarner Inc. Cast titanium compressor wheel

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1363028A1 (en) * 2001-06-06 2003-11-19 BorgWarner Inc. Cast titanium compressor wheel
US6904949B2 (en) 2001-06-06 2005-06-14 Borgwarner, Inc. Method of making turbocharger including cast titanium compressor wheel
US8702394B2 (en) 2001-06-06 2014-04-22 Borgwarner, Inc. Turbocharger including cast titanium compressor wheel

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