GB355028A - Rotor blade for explosion turbines - Google Patents

Rotor blade for explosion turbines

Info

Publication number
GB355028A
GB355028A GB24607/30A GB2460730A GB355028A GB 355028 A GB355028 A GB 355028A GB 24607/30 A GB24607/30 A GB 24607/30A GB 2460730 A GB2460730 A GB 2460730A GB 355028 A GB355028 A GB 355028A
Authority
GB
United Kingdom
Prior art keywords
rotor blade
parts
explosion turbines
turbines
explosion
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
GB24607/30A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Publication of GB355028A publication Critical patent/GB355028A/en
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
    • F01D5/14—Form or construction
    • F01D5/141—Shape, i.e. outer, aerodynamic form

Abstract

A blade for a combustion turbine is formed of an alloy containing 10 parts iron, 65 parts nickel, 15 parts chromium, and 7 parts molybdenum.
GB24607/30A 1929-08-22 1930-08-16 Rotor blade for explosion turbines Expired GB355028A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE355028X 1929-08-22

Publications (1)

Publication Number Publication Date
GB355028A true GB355028A (en) 1931-08-20

Family

ID=6289852

Family Applications (1)

Application Number Title Priority Date Filing Date
GB24607/30A Expired GB355028A (en) 1929-08-22 1930-08-16 Rotor blade for explosion turbines

Country Status (4)

Country Link
US (1) US1800730A (en)
BE (1) BE372479A (en)
FR (1) FR699920A (en)
GB (1) GB355028A (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2447896A (en) * 1946-02-01 1948-08-24 Armco Steel Corp High-temperature turbine
US2686654A (en) * 1948-10-19 1954-08-17 Thompson Prod Inc Coated member and method of making the same
US3041040A (en) * 1955-12-23 1962-06-26 Gen Electric Metal clad blade
US20090324419A1 (en) * 2006-07-25 2009-12-31 Luciano Cozza Highly corrosion-resistant movable blade assembly for a steam turbine, in particular a geothermal impulse turbine

Also Published As

Publication number Publication date
BE372479A (en) 1930-08-05
US1800730A (en) 1931-04-14
FR699920A (en) 1931-02-21

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