GB390448A - Improvements in or relating to gas turbine plants particularly for propulsion of ships - Google Patents

Improvements in or relating to gas turbine plants particularly for propulsion of ships

Info

Publication number
GB390448A
GB390448A GB29698/32A GB2969832A GB390448A GB 390448 A GB390448 A GB 390448A GB 29698/32 A GB29698/32 A GB 29698/32A GB 2969832 A GB2969832 A GB 2969832A GB 390448 A GB390448 A GB 390448A
Authority
GB
United Kingdom
Prior art keywords
turbine
gas turbine
compressor
propulsion
ships
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
GB29698/32A
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 GB390448A publication Critical patent/GB390448A/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
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/36—Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user

Abstract

390,448. Gas turbine plant. AKTIEBOLAGET MILO, 32, Kungsgatan, Stockholm. Oct. 24, 1932, No. 29698. Convention date, Oct. 24, 1931. [Class 110 (iii).] In a gas turbine plant, particularly for ship propulsion, extra power is obtained by clutching-in an additional compressor. The Figure shows two double-rotation turbines 1, 2 working in series. The turbine 1 drives compressors 3, 4, and the turbine 2 drives generators 5, 6, and a compressor 8. An additional compressor 7 may be clutched to the shaft of the generator 5, in which case the normal air inlet is closed by a valve 20. The air passes in series through the compressor 7 (when in use), compressors 8, 3, 4, air preheater 14, combustion chamber 16, turbine 1, combustion chamber 18, and turbine 2. A modification is described in which a single-rotation axial-flow turbine is used.
GB29698/32A 1931-10-24 1932-10-24 Improvements in or relating to gas turbine plants particularly for propulsion of ships Expired GB390448A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE390448X 1931-10-24

Publications (1)

Publication Number Publication Date
GB390448A true GB390448A (en) 1933-04-06

Family

ID=6374097

Family Applications (1)

Application Number Title Priority Date Filing Date
GB29698/32A Expired GB390448A (en) 1931-10-24 1932-10-24 Improvements in or relating to gas turbine plants particularly for propulsion of ships

Country Status (1)

Country Link
GB (1) GB390448A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1097211B (en) * 1958-05-27 1961-01-12 Bbc Brown Boveri & Cie Gas turbine power plant
US8935912B2 (en) 2011-12-09 2015-01-20 United Technologies Corporation Gas turbine engine with variable overall pressure ratio

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1097211B (en) * 1958-05-27 1961-01-12 Bbc Brown Boveri & Cie Gas turbine power plant
US8935912B2 (en) 2011-12-09 2015-01-20 United Technologies Corporation Gas turbine engine with variable overall pressure ratio

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