GB372377A - Improvements in or relating to turbines - Google Patents

Improvements in or relating to turbines

Info

Publication number
GB372377A
GB372377A GB33156/30A GB3315630A GB372377A GB 372377 A GB372377 A GB 372377A GB 33156/30 A GB33156/30 A GB 33156/30A GB 3315630 A GB3315630 A GB 3315630A GB 372377 A GB372377 A GB 372377A
Authority
GB
United Kingdom
Prior art keywords
gas turbine
multistage
turbine plant
turbines
relating
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
GB33156/30A
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.)
Milo AB
Original Assignee
Milo AB
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 Milo AB filed Critical Milo AB
Publication of GB372377A publication Critical patent/GB372377A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/36—Open cycles

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Other Liquid Machine Or Engine Such As Wave Power Use (AREA)

Abstract

372,377. Gas turbine plant. AKTIEBOLAGET MILO, 17, Vastra Tradgardsgatan, Stockholm. Nov. 4, 1930, No. 33156. Convention date, March 24. Drawings to Specification. [Class 110 (iii).] A gas turbine plant comprises a multistage air-compression system, means for heating the compressed air at constant pressure to a temperature not less than 800‹ C., and a multistage radial flow reaction turbine system. The turbine system may include one or more machines of the oppositely-running rotor type. Specifications 368,317, 368,318, and 368,702 are referred to.
GB33156/30A 1930-03-24 1930-11-04 Improvements in or relating to turbines Expired GB372377A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE372377X 1930-03-24

Publications (1)

Publication Number Publication Date
GB372377A true GB372377A (en) 1932-05-04

Family

ID=6331838

Family Applications (1)

Application Number Title Priority Date Filing Date
GB33156/30A Expired GB372377A (en) 1930-03-24 1930-11-04 Improvements in or relating to turbines

Country Status (1)

Country Link
GB (1) GB372377A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2526409A (en) * 1945-01-09 1950-10-17 Lockheed Aircraft Corp Turbo-propeller type power plant having radial flow exhaust turbine means
DE767173C (en) * 1939-07-12 1951-12-06 Sulzer Ag Gas heater
US2686631A (en) * 1948-05-08 1954-08-17 United Aircraft Corp Coolant injection system for gas turbines

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE767173C (en) * 1939-07-12 1951-12-06 Sulzer Ag Gas heater
US2526409A (en) * 1945-01-09 1950-10-17 Lockheed Aircraft Corp Turbo-propeller type power plant having radial flow exhaust turbine means
US2686631A (en) * 1948-05-08 1954-08-17 United Aircraft Corp Coolant injection system for gas turbines

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