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GB189124A - Improvements in the diaphragms of internal combustion turbines - Google Patents

Improvements in the diaphragms of internal combustion turbines

Info

Publication number
GB189124A
GB189124A GB31060/22A GB3106022A GB189124A GB 189124 A GB189124 A GB 189124A GB 31060/22 A GB31060/22 A GB 31060/22A GB 3106022 A GB3106022 A GB 3106022A GB 189124 A GB189124 A GB 189124A
Authority
GB
United Kingdom
Prior art keywords
diaphragm
diaphragms
internal combustion
way
water
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
GB31060/22A
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.)
SOC IT ERNESTO BREDA
Original Assignee
SOC IT ERNESTO BREDA
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 SOC IT ERNESTO BREDA filed Critical SOC IT ERNESTO BREDA
Publication of GB189124A publication Critical patent/GB189124A/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
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Supercharger (AREA)

Abstract

189,124. Soc. Italiana E. Breda. Nov. 14, 1921, [Convention date]. Cooling parts; blades; casings.-In internalcombustion turbines, water is circulated through the hollow two-part diaphragm X and through the hollow guide blades b, which are formed of bent sheet metal welded at the contacting edges anJ fixed at each end in the metal of the diaphragm. The water from the turbine jacket circulates in the case of the lower half diaphragm by way of an inlet port c and outlet ports d, e, and in the case of the upper half by way of inlet ports f, h and an outlet port g.
GB31060/22A 1921-11-14 1922-11-14 Improvements in the diaphragms of internal combustion turbines Expired GB189124A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IT189124X 1921-11-14

Publications (1)

Publication Number Publication Date
GB189124A true GB189124A (en) 1923-08-23

Family

ID=11153640

Family Applications (1)

Application Number Title Priority Date Filing Date
GB31060/22A Expired GB189124A (en) 1921-11-14 1922-11-14 Improvements in the diaphragms of internal combustion turbines

Country Status (1)

Country Link
GB (1) GB189124A (en)

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