CH228273A - Turbo engine. - Google Patents

Turbo engine.

Info

Publication number
CH228273A
CH228273A CH228273DA CH228273A CH 228273 A CH228273 A CH 228273A CH 228273D A CH228273D A CH 228273DA CH 228273 A CH228273 A CH 228273A
Authority
CH
Switzerland
Prior art keywords
turbo engine
turbo
engine
Prior art date
Application number
Other languages
German (de)
Inventor
Aktiengesellschaft Gebr Sulzer
Original Assignee
Sulzer 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 Sulzer Ag filed Critical Sulzer Ag
Publication of CH228273A publication Critical patent/CH228273A/en

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
CH228273D 1942-04-24 1942-04-24 Turbo engine. CH228273A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH228273T 1942-04-24

Publications (1)

Publication Number Publication Date
CH228273A true CH228273A (en) 1943-08-15

Family

ID=4455483

Family Applications (1)

Application Number Title Priority Date Filing Date
CH228273D CH228273A (en) 1942-04-24 1942-04-24 Turbo engine.

Country Status (1)

Country Link
CH (1) CH228273A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1152122A2 (en) * 2000-05-01 2001-11-07 United Technologies Corporation Turbomachinery blade
US20110206527A1 (en) * 2010-02-24 2011-08-25 Rolls-Royce Plc Compressor aerofoil

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1152122A2 (en) * 2000-05-01 2001-11-07 United Technologies Corporation Turbomachinery blade
EP1152122A3 (en) * 2000-05-01 2003-09-17 United Technologies Corporation Turbomachinery blade
US20110206527A1 (en) * 2010-02-24 2011-08-25 Rolls-Royce Plc Compressor aerofoil
EP2360377A3 (en) * 2010-02-24 2014-11-12 Rolls-Royce plc A compressor aerofoil
US9046111B2 (en) 2010-02-24 2015-06-02 Rolls-Royce Plc Compressor aerofoil

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