GB366773A - Improvements in or relating to gas turbine aggregates - Google Patents

Improvements in or relating to gas turbine aggregates

Info

Publication number
GB366773A
GB366773A GB8211/31A GB821131A GB366773A GB 366773 A GB366773 A GB 366773A GB 8211/31 A GB8211/31 A GB 8211/31A GB 821131 A GB821131 A GB 821131A GB 366773 A GB366773 A GB 366773A
Authority
GB
United Kingdom
Prior art keywords
accumulator
march
gas turbine
conduit
combustion chamber
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
GB8211/31A
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 GB366773A publication Critical patent/GB366773A/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
    • F02C7/26—Starting; Ignition
    • F02C7/268—Starting drives for the rotor, acting directly on the rotor of the gas turbine to be started
    • F02C7/27—Fluid drives

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)

Abstract

366,773. Motor power plant. AKTIEBOLAGET MILO, 17, Võstra Trõdgardsgatan, Stockholm. March 17, 1931, No. 8211. Convention date, March 31, 1930. [Class 110 (iii).] Starting means for a gas turbine plant include an accumulator 6 which contains compressed air, steam, or other gas. A turbine 1 drives an air compressor 2 which supplies compressed air to a continuous-combustion chamber 11, and conduits 5, 17 lead the heated medium to the turbines 1, 13, which latter drives a power machine 4 such as an electrical generator. Under running conditions a valve 7 is closed. Fuel is supplied to the combustion chamber 11 through a pipe 12. The accumulator may be charged from the compressor 2 through a conduit 18. Several turbines and accumulators mav be used. The quantity of fuel supplied is regulated to prevent undue rise of temperature of the heated medium. The conduit 18 may be dispensed with.
GB8211/31A 1930-03-31 1931-03-17 Improvements in or relating to gas turbine aggregates Expired GB366773A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE366773X 1930-03-31

Publications (1)

Publication Number Publication Date
GB366773A true GB366773A (en) 1932-02-11

Family

ID=6317817

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8211/31A Expired GB366773A (en) 1930-03-31 1931-03-17 Improvements in or relating to gas turbine aggregates

Country Status (1)

Country Link
GB (1) GB366773A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE767491C (en) * 1935-12-09 1952-09-08 Anxionnaz Rene Thermal power plant with gas turbines with constant pressure combustion
US2840987A (en) * 1953-03-23 1958-07-01 Gen Electric Improved method and arrangement for starting reaction type propulsion units using anauxiliary reaction type propulsion unit
US2851113A (en) * 1950-11-08 1958-09-09 Gen Motors Corp Control system for a variable pitch propeller and its driving turbines
US2941790A (en) * 1957-05-01 1960-06-21 Thompson Ramo Wooldridge Inc Gas turbine engine actuated starter and dryer

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE767491C (en) * 1935-12-09 1952-09-08 Anxionnaz Rene Thermal power plant with gas turbines with constant pressure combustion
US2851113A (en) * 1950-11-08 1958-09-09 Gen Motors Corp Control system for a variable pitch propeller and its driving turbines
US2840987A (en) * 1953-03-23 1958-07-01 Gen Electric Improved method and arrangement for starting reaction type propulsion units using anauxiliary reaction type propulsion unit
US2941790A (en) * 1957-05-01 1960-06-21 Thompson Ramo Wooldridge Inc Gas turbine engine actuated starter and dryer

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