GB113273A - Improvements in Guide Channels for Multistage Axial Flow Steam or Gas Turbines. - Google Patents

Improvements in Guide Channels for Multistage Axial Flow Steam or Gas Turbines.

Info

Publication number
GB113273A
GB113273A GB181?/18A GB18118A GB113273A GB 113273 A GB113273 A GB 113273A GB 18118 A GB18118 A GB 18118A GB 113273 A GB113273 A GB 113273A
Authority
GB
United Kingdom
Prior art keywords
channel
axial flow
gas turbines
guide channels
flow steam
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
GB181?/18A
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.)
Societe Anonyme des Ateliers de Constructions Mecaniques Escher Wyss et Cie SA
Original Assignee
Societe Anonyme des Ateliers de Constructions Mecaniques Escher Wyss et Cie SA
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 Societe Anonyme des Ateliers de Constructions Mecaniques Escher Wyss et Cie SA filed Critical Societe Anonyme des Ateliers de Constructions Mecaniques Escher Wyss et Cie SA
Publication of GB113273A publication Critical patent/GB113273A/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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Control Of Turbines (AREA)

Abstract

113,273. Soc. Anon. des Ateliers de Constructions MÚcaniques Escher, Wyss, et Cie. Feb. 6, 1917, [Convention date]. Axial-flow type; blades, &c.-In a multi-stage turbine having a guide-channel 7 of S-shaped median section between the stages 1, 2, 3 and the stages 4, 5, 6 so as to direct the working fluid from one wheel to another of considerably different diameter, eddies in the channel 7 are reduced by subdividing it by one or more guidewalls 8. In Fig. 2 the channel 12 is shown rubdivided by walls 13, 14 extending along only part of its length.
GB181?/18A 1917-02-06 1918-01-31 Improvements in Guide Channels for Multistage Axial Flow Steam or Gas Turbines. Expired GB113273A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH113273X 1917-02-06

Publications (1)

Publication Number Publication Date
GB113273A true GB113273A (en) 1919-01-02

Family

ID=32477118

Family Applications (1)

Application Number Title Priority Date Filing Date
GB181?/18A Expired GB113273A (en) 1917-02-06 1918-01-31 Improvements in Guide Channels for Multistage Axial Flow Steam or Gas Turbines.

Country Status (1)

Country Link
GB (1) GB113273A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20190136702A1 (en) * 2017-11-09 2019-05-09 Honeywell International Inc. Inter-turbine ducts with flow control mechanisms

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20190136702A1 (en) * 2017-11-09 2019-05-09 Honeywell International Inc. Inter-turbine ducts with flow control mechanisms
US10502076B2 (en) * 2017-11-09 2019-12-10 Honeywell International Inc. Inter-turbine ducts with flow control mechanisms
US11131205B2 (en) 2017-11-09 2021-09-28 Honeywell International Inc. Inter-turbine ducts with flow control mechanisms

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