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GB568661A - Improvements in or relating to internal combustion turbine plant - Google Patents

Improvements in or relating to internal combustion turbine plant

Info

Publication number
GB568661A
GB568661A GB493742A GB493742A GB568661A GB 568661 A GB568661 A GB 568661A GB 493742 A GB493742 A GB 493742A GB 493742 A GB493742 A GB 493742A GB 568661 A GB568661 A GB 568661A
Authority
GB
United Kingdom
Prior art keywords
rotors
turbine plant
shaft
relating
internal combustion
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
GB493742A
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 GB493742A priority Critical patent/GB568661A/en
Publication of GB568661A publication Critical patent/GB568661A/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
    • F02C3/14—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant
    • F02C3/16—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant the combustion chambers being formed at least partly in the turbine rotor or in an other rotating part of the plant
    • 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
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/08—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising at least one radial stage
    • F02C3/085—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising at least one radial stage the turbine being of the radial-flow type (radial-radial)

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)

Abstract

568,661. Shaft couplings. UMPLEBY, F. April 15, 1942, Nos. 4937 and 11863. [Class 80 (ii)] [Also in Groups XXVI and XXXIII] In a gas turbine plant which may be used for the jet propulsion of aircraft, the rotors 23 are splined to the shaft 19 and the radial flow stage rotor 21 is free on the shaft, but secured to the rotors 23 by rubber discs 22 vulcanized to the rotors 21, 23. The rotors are held against axial displacement by a split ring 24 and this ring is prevented from opening at high speeds by a bush 25 which is slipped over it.
GB493742A 1942-04-15 1942-04-15 Improvements in or relating to internal combustion turbine plant Expired GB568661A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB493742A GB568661A (en) 1942-04-15 1942-04-15 Improvements in or relating to internal combustion turbine plant

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB493742A GB568661A (en) 1942-04-15 1942-04-15 Improvements in or relating to internal combustion turbine plant

Publications (1)

Publication Number Publication Date
GB568661A true GB568661A (en) 1945-04-16

Family

ID=9786651

Family Applications (1)

Application Number Title Priority Date Filing Date
GB493742A Expired GB568661A (en) 1942-04-15 1942-04-15 Improvements in or relating to internal combustion turbine plant

Country Status (1)

Country Link
GB (1) GB568661A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2365668A1 (en) * 2008-11-20 2011-10-10 Antonia Sempere Navarro Improvements introduced in the application of spanish patent n. 200802995 for "magnetic turbine". (Machine-translation by Google Translate, not legally binding)
US10808614B2 (en) * 2016-06-09 2020-10-20 Hieta Technologies Limited Radial flow turbine heat engine

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2365668A1 (en) * 2008-11-20 2011-10-10 Antonia Sempere Navarro Improvements introduced in the application of spanish patent n. 200802995 for "magnetic turbine". (Machine-translation by Google Translate, not legally binding)
US10808614B2 (en) * 2016-06-09 2020-10-20 Hieta Technologies Limited Radial flow turbine heat engine

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