GB368319A - Improvements in or relating to turbines - Google Patents

Improvements in or relating to turbines

Info

Publication number
GB368319A
GB368319A GB3315830A GB3315830A GB368319A GB 368319 A GB368319 A GB 368319A GB 3315830 A GB3315830 A GB 3315830A GB 3315830 A GB3315830 A GB 3315830A GB 368319 A GB368319 A GB 368319A
Authority
GB
United Kingdom
Prior art keywords
pipe
sooting
fuel
turbines
pipes
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
GB3315830A
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
Priority to DE368319X priority Critical
Application filed by MILO AB filed Critical MILO AB
Publication of GB368319A publication Critical patent/GB368319A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/20Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products
    • F02C3/30Adding water, steam or other fluids for influencing combustion, e.g. to obtain cleaner exhaust gases
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C6/00Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas- turbine plants for special use
    • F02C6/003Gas-turbine plants with heaters between turbine stages

Abstract

368,319. Gas turbine plant. AKTIEBOLAGET MILO, 17, Võstra Tradgardsgatan, Stockholm. Nov. 4, 1930, No. 33158. Convention date, March 24. [Class 110 (iii).] In a gas turbine plant the heating of the driving medium is effected by the combustion of fuel in such a manner that the excess of air is less than 25 per cent by weight, and water is injected into the heating apparatus in order to burn up any soot which may be formed. Sooting fuels, or non-sooting fuels such as alcohol, may be used. Fig. 1 shows a plant comprising four turbines 1 .. 4 in series upon a shaft which carries also an air compressor 5 and an electric generator 6. Compressed air is supplied to a combustion chamber 9, and the products pass by a pipe 14 to the turbine 1 and then through the other turbines. A pipe 19 may supply high-pressure gases to the second turbine 2. The working gases are reheated between the turbines by hotgases introduced into the connecting pipes 15, 16, 17 from combustion chambers 23, 27, 30 which are fed with compressed air by a pipe 21 and with fuel by pipes 24, 28, 32. Fig. 2 shows a form of combustion chamber 9 which has a water-jacket 35. A pipe 10, is provided for the admission of sooting fuel and a pipe 11 for non-sooting fuel, both pipes having means to produce whirl. Water from the jacket is introduced into the chamber at the points 38, 39, 40. Specifications 368,318 and 368,702 are referred to.
GB3315830A 1930-03-24 1930-11-04 Improvements in or relating to turbines Expired GB368319A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DE368319X 1930-03-24

Publications (1)

Publication Number Publication Date
GB368319A true GB368319A (en) 1932-03-04

Family

ID=6318065

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3315830A Expired GB368319A (en) 1930-03-24 1930-11-04 Improvements in or relating to turbines

Country Status (1)

Country Link
GB (1) GB368319A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1153570B (en) * 1959-04-17 1963-08-29 Rolls Royce Combustor for gas turbine installations
DE1197280B (en) * 1960-02-25 1965-07-22 Rolls Royce convey smoke precipitation gas turbine engine

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1153570B (en) * 1959-04-17 1963-08-29 Rolls Royce Combustor for gas turbine installations
DE1197280B (en) * 1960-02-25 1965-07-22 Rolls Royce convey smoke precipitation gas turbine engine

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