GB659604A - Adjutage for the nozzles of radial impulse turbines - Google Patents

Adjutage for the nozzles of radial impulse turbines

Info

Publication number
GB659604A
GB659604A GB2329349A GB2329349A GB659604A GB 659604 A GB659604 A GB 659604A GB 2329349 A GB2329349 A GB 2329349A GB 2329349 A GB2329349 A GB 2329349A GB 659604 A GB659604 A GB 659604A
Authority
GB
United Kingdom
Prior art keywords
adjutage
nozzles
jet
radial impulse
impulse turbines
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
GB2329349A
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
Priority to GB2329349A priority Critical patent/GB659604A/en
Publication of GB659604A publication Critical patent/GB659604A/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
    • F01D17/00—Regulating or controlling by varying flow
    • F01D17/10—Final actuators
    • F01D17/12—Final actuators arranged in stator parts
    • F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/141—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of shiftable members or valves obturating part of the flow path

Landscapes

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

Abstract

659,604. Hydraulic turbines. MICHELL, A. G. M. Sept. 8, 1949, No. 23293. [Class 110(iii)] In an inwardflow hydraulic turbine, the jet issuing from a nozzle 2 is regulated by a block 4 which is carried by a shaft 8 and turned by a lever 13 secured to the shaft. At small openings, a free jet issues as indicated by the dot-and-dash lines. At large openings, the jet is guided by the curved surface 4b of the block. Specification 16137/03, [Class 110], is referred to.
GB2329349A 1949-09-08 1949-09-08 Adjutage for the nozzles of radial impulse turbines Expired GB659604A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2329349A GB659604A (en) 1949-09-08 1949-09-08 Adjutage for the nozzles of radial impulse turbines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2329349A GB659604A (en) 1949-09-08 1949-09-08 Adjutage for the nozzles of radial impulse turbines

Publications (1)

Publication Number Publication Date
GB659604A true GB659604A (en) 1951-10-24

Family

ID=10193289

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2329349A Expired GB659604A (en) 1949-09-08 1949-09-08 Adjutage for the nozzles of radial impulse turbines

Country Status (1)

Country Link
GB (1) GB659604A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0306551A1 (en) * 1987-09-09 1989-03-15 Mitsubishi Jukogyo Kabushiki Kaisha Variable capacity radial flow turbine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0306551A1 (en) * 1987-09-09 1989-03-15 Mitsubishi Jukogyo Kabushiki Kaisha Variable capacity radial flow turbine

Similar Documents

Publication Publication Date Title
GB654344A (en) Method of regulating gas turbine jet-propulsion plants, and means therefor
GB587513A (en) Improvements relating to gas turbine cooling systems
GB659604A (en) Adjutage for the nozzles of radial impulse turbines
GB565952A (en) Improvements in means for generating a mixture of steam and combustion products under pressure
GB847500A (en) Improvements in piping systems or channels for the passage of fluids
GB701320A (en) Improvements in or relating to combustion equipment of gas-turbine engines
GB701561A (en) Improvements relating to gas turbine plant
GB790298A (en) Jet propelled aircraft
GB756319A (en) Improvements in aircraft
GB733727A (en) Improvements in arrangements for deflecting fluid jets
GB910679A (en) Improvements in or relating to propulsion nozzles
GB731418A (en) Improvements in combustion apparatus
GB579140A (en) Improvements in or relating to gas turbines
GB318486A (en) Improvements in and relating to governors for turbines and compressors
GB703701A (en) Fuel supply means for a gas turbine engine
GB584169A (en) Improvements in or relating to power plants for aircraft
GB587612A (en) Improvements in or relating to internal combustion turbine power plants
GB675269A (en) Method and apparatus for producing a fine spray
GB750490A (en) Co-ordinated fuel feed and exhaust jet control for gas turbine engines
GB587126A (en) Improvements in or relating to power-units for aircraft
GB679530A (en) Improvements in gas turbine blades
GB563174A (en) Method of coating surfaces with paints, lacs or other liquids and a spray device for the purpose
GB681474A (en) Improvements in or relating to fuel systems for gas-turbine engines
GB593070A (en) Improvements in or relating to aircraft propulsion
GB723310A (en) Improvements in and relating to jet propulsion units