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GB620983A - Improvements in or relating to motor groups including a high power gas turbine showing a high efficiency for fractionary loads - Google Patents

Improvements in or relating to motor groups including a high power gas turbine showing a high efficiency for fractionary loads

Info

Publication number
GB620983A
GB620983A GB3587/47A GB358747A GB620983A GB 620983 A GB620983 A GB 620983A GB 3587/47 A GB3587/47 A GB 3587/47A GB 358747 A GB358747 A GB 358747A GB 620983 A GB620983 A GB 620983A
Authority
GB
United Kingdom
Prior art keywords
pressure
turbine
gas turbine
fractionary
loads
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
GB3587/47A
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.)
Rateau SA
Original Assignee
Rateau SA
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 Rateau SA filed Critical Rateau SA
Publication of GB620983A publication Critical patent/GB620983A/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
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/003—Gas-turbine plants with heaters between turbine stages
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E20/00—Combustion technologies with mitigation potential
    • Y02E20/14—Combined heat and power generation [CHP]

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)

Abstract

620,983. Gas turbine plant. SOC. RATEAU, and ANXIONNAZ, R. Feb. 6, 1947, No. 3587. Convention date, March 11, 1946. Drawings to Specification. [Class 110(iii)] In a gas turbine plant with three-stage turbines, the high-pressure turbine drives the high-pressure compressor, the low-pressure turbine drives the low-pressure compressor and 'the intermediate pressure turbine provides useful power. Reheating is provided between all the turbine stages and the air is pre-heated by the turbine exhaust. Solid, liquid, or gaseous fuel may be used. Gaseous fuel is compressed in a two-stage compressor and is tapped at points suited to the pressure in the re-heating combustion chambers. The compressed fuel gas is pre-heated by the turbine exhaust. The total compression ratio is not less than eight and at full load the compression ratio of the low-pressure compressor is greater than that of the high-pressure compressor.
GB3587/47A 1946-03-11 1947-02-06 Improvements in or relating to motor groups including a high power gas turbine showing a high efficiency for fractionary loads Expired GB620983A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR620983X 1946-03-11

Publications (1)

Publication Number Publication Date
GB620983A true GB620983A (en) 1949-04-01

Family

ID=8984785

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3587/47A Expired GB620983A (en) 1946-03-11 1947-02-06 Improvements in or relating to motor groups including a high power gas turbine showing a high efficiency for fractionary loads

Country Status (1)

Country Link
GB (1) GB620983A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3166902A (en) * 1962-11-15 1965-01-26 Chandler Evans Corp Fuel control for a regenerative gas turbine engine
US3209536A (en) * 1960-04-04 1965-10-05 Ford Motor Co Re-expansion type gas turbine engine with intercooler fan driven by the low pressure turbine
US3246470A (en) * 1963-03-25 1966-04-19 Holley Carburetor Co Gas turbine fuel control
GB2227796A (en) * 1988-12-06 1990-08-08 Gen Electric Turbine engine

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3209536A (en) * 1960-04-04 1965-10-05 Ford Motor Co Re-expansion type gas turbine engine with intercooler fan driven by the low pressure turbine
US3166902A (en) * 1962-11-15 1965-01-26 Chandler Evans Corp Fuel control for a regenerative gas turbine engine
US3246470A (en) * 1963-03-25 1966-04-19 Holley Carburetor Co Gas turbine fuel control
GB2227796A (en) * 1988-12-06 1990-08-08 Gen Electric Turbine engine
GB2227796B (en) * 1988-12-06 1993-06-09 Gen Electric Turbine engine

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