GB279770A - Improvements in multistage gas turbines - Google Patents

Improvements in multistage gas turbines

Info

Publication number
GB279770A
GB279770A GB27110/27A GB2711027A GB279770A GB 279770 A GB279770 A GB 279770A GB 27110/27 A GB27110/27 A GB 27110/27A GB 2711027 A GB2711027 A GB 2711027A GB 279770 A GB279770 A GB 279770A
Authority
GB
United Kingdom
Prior art keywords
chambers
combustion
devices
fuel
turbine
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
GB27110/27A
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
Publication of GB279770A publication Critical patent/GB279770A/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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Feeding And Controlling Fuel (AREA)

Abstract

279,770. Kohler, C. Nov. 10, 1926, [Convention date]. Working-fluid supply.-In a multistage turbine in which the driving medium contains excess of air and is re-heated between the successive units by internal combustion of coal gas and liquid fuel, the combustion chambers preceding the earlier turbine units are provided not only with devices for the combustion of coal dust, but also with devices for burning liquid fuel more readily combustible than coal dust. The chambers preceding the last turbine unit may be furnished only with devices for burning liquid fuel. In the form shown, three turbine units A, B, C are preceded by combustion chambers 3 into which open coal-dust feed pipes 6 and liquid-fuel feed pipes 5. An excess of air is admitted through the pipes 4 into the chambers 3 preceding the first unit A. Air inlet pipes may be provided in the other chambers 3. The supply of fuel to the chambers 3 can be controlled by common valves 7, 8, or by valves peculiar to each chamber.
GB27110/27A 1926-11-10 1927-10-12 Improvements in multistage gas turbines Expired GB279770A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH279770X 1926-11-10

Publications (1)

Publication Number Publication Date
GB279770A true GB279770A (en) 1927-11-03

Family

ID=4482360

Family Applications (1)

Application Number Title Priority Date Filing Date
GB27110/27A Expired GB279770A (en) 1926-11-10 1927-10-12 Improvements in multistage gas turbines

Country Status (1)

Country Link
GB (1) GB279770A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2500334A (en) * 1944-06-19 1950-03-14 Aerojet Engineering Corp Jet motor operable by monopropellant and method of operating it
US2621476A (en) * 1942-03-16 1952-12-16 Rateau La Courneuve Soc Gas turbine installation operating on gaseous fuels
US2658340A (en) * 1945-02-01 1953-11-10 Power Jets Res & Dev Ltd Apparatus for igniting fuel in fast-moving hot gas streams
US4338782A (en) * 1979-11-23 1982-07-13 Marchand William C Gas turbine combustion system utilizing renewable and non-critical solid fuels with residue remover to minimize environmental pollution
US4550563A (en) * 1979-11-23 1985-11-05 Marchand William C Gas turbine combustion system utilizing renewable and non-critical solid fuels with residue remover to minimize environmental pollution
GB2289721A (en) * 1994-05-26 1995-11-29 Abb Management Ag Gas turbine engine fuel control
EP1995433A1 (en) * 2007-05-24 2008-11-26 Siemens Aktiengesellschaft Gas turbo group and method for controlling a gas turbo group

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2621476A (en) * 1942-03-16 1952-12-16 Rateau La Courneuve Soc Gas turbine installation operating on gaseous fuels
US2500334A (en) * 1944-06-19 1950-03-14 Aerojet Engineering Corp Jet motor operable by monopropellant and method of operating it
US2658340A (en) * 1945-02-01 1953-11-10 Power Jets Res & Dev Ltd Apparatus for igniting fuel in fast-moving hot gas streams
US4338782A (en) * 1979-11-23 1982-07-13 Marchand William C Gas turbine combustion system utilizing renewable and non-critical solid fuels with residue remover to minimize environmental pollution
US4550563A (en) * 1979-11-23 1985-11-05 Marchand William C Gas turbine combustion system utilizing renewable and non-critical solid fuels with residue remover to minimize environmental pollution
GB2289721A (en) * 1994-05-26 1995-11-29 Abb Management Ag Gas turbine engine fuel control
GB2289721B (en) * 1994-05-26 1998-03-18 Abb Management Ag Method of controlling a gas-turbine group
EP1995433A1 (en) * 2007-05-24 2008-11-26 Siemens Aktiengesellschaft Gas turbo group and method for controlling a gas turbo group
WO2008142020A1 (en) * 2007-05-24 2008-11-27 Siemens Aktiengesellschaft Gas turbo set and method for controlling a gas turbo set
US8689560B2 (en) 2007-05-24 2014-04-08 Siemens Aktiengesellschaft Gas turbo set and method for controlling a gas turbo set

Similar Documents

Publication Publication Date Title
GB412970A (en) Improvements in and relating to gas turbine cycles with interstage reheating
GB497188A (en) An internal combustion engine for use at high altitudes charged by turbo-blowers
GB279770A (en) Improvements in multistage gas turbines
GB544719A (en) Improvements in plants for producing a mixture of hot air and combustion products under pressure
GB671702A (en) Thermal power plant
GB604028A (en) Improvements in or relating to thermal power plants
GB492831A (en) Improvements in gas turbine plants of the continuous combustion type
GB469311A (en) Improvements in and relating to gas turbine plant
GB328263A (en) Improvements in and relating to internal combustion engine plants
GB621954A (en) Improvements in or relating to thermal power plant
GB294978A (en) Method of working explosion turbines with coal dust
GB191318049A (en) Improvements in Hot Air Turbines.
GB268861A (en) Improvements in systems of gas turbine aggregates
GB278790A (en) An internal combustion turbine
GB186083A (en) Improved method of and apparatus for the economic transformation of the energy of steam by turbines
GB492081A (en) Improvements in gas turbine power plants of the continuous combustion type
GB568087A (en) A process for the generation of power using turbines
GB368319A (en) Improvements in or relating to turbines
GB267233A (en) Improvements in and relating to explosion turbines
GB239434A (en) Improvements in combustion-product engines
SU101704A1 (en) Gas turbine electric station with gas generator
GB407151A (en) Improvements in and relating to steam generating plants
GB597475A (en) Power plant
GB722230A (en) Improvements in gas turbine plant
GB450626A (en) Improvements in mechanically fired locomotives