DE412623C - Turbinengehaeuse - Google Patents

Turbinengehaeuse

Info

Publication number
DE412623C
DE412623C DEE30760D DEE0030760D DE412623C DE 412623 C DE412623 C DE 412623C DE E30760 D DEE30760 D DE E30760D DE E0030760 D DEE0030760 D DE E0030760D DE 412623 C DE412623 C DE 412623C
Authority
DE
Germany
Prior art keywords
turbinengehaeuse
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
DEE30760D
Other languages
English (en)
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.)
ERSTE BRUENNER MASCHINEN FAB
Original Assignee
ERSTE BRUENNER MASCHINEN FAB
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
Priority to AT412623X priority Critical
Application filed by ERSTE BRUENNER MASCHINEN FAB filed Critical ERSTE BRUENNER MASCHINEN FAB
Application granted granted Critical
Publication of DE412623C publication Critical patent/DE412623C/de
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
    • F01D9/00Stators
    • F01D9/02Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/047Nozzle boxes
    • 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
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/26Double casings; Measures against temperature strain in casings
    • F01D25/265Vertically split casings; Clamping arrangements therefor
DEE30760D 1924-05-06 1924-05-13 Turbinengehaeuse Expired DE412623C (de)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AT412623X 1924-05-06

Publications (1)

Publication Number Publication Date
DE412623C true DE412623C (de) 1925-04-24

Family

ID=3673789

Family Applications (1)

Application Number Title Priority Date Filing Date
DEE30760D Expired DE412623C (de) 1924-05-06 1924-05-13 Turbinengehaeuse

Country Status (1)

Country Link
DE (1) DE412623C (de)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1009638B (de) * 1955-12-07 1957-06-06 Bbc Brown Boveri & Cie Dampfdichte Ringflanschverbindung zweier Gehaeuseteile einer Dampfturbine
DE1095293B (de) * 1955-07-19 1960-12-22 Siemens Ag Connection of two built-in parts of a turbine
DE1108237B (de) * 1954-09-25 1961-06-08 Siemens Ag Steam or gas turbine with a housing that is not divided in the axial plane
US4431373A (en) * 1980-05-16 1984-02-14 United Technologies Corporation Flow directing assembly for a gas turbine engine

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1108237B (de) * 1954-09-25 1961-06-08 Siemens Ag Steam or gas turbine with a housing that is not divided in the axial plane
DE1095293B (de) * 1955-07-19 1960-12-22 Siemens Ag Connection of two built-in parts of a turbine
DE1009638B (de) * 1955-12-07 1957-06-06 Bbc Brown Boveri & Cie Dampfdichte Ringflanschverbindung zweier Gehaeuseteile einer Dampfturbine
US4431373A (en) * 1980-05-16 1984-02-14 United Technologies Corporation Flow directing assembly for a gas turbine engine

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