GB588097A - Improvements in or relating to internal combustion turbine power plants - Google Patents

Improvements in or relating to internal combustion turbine power plants

Info

Publication number
GB588097A
GB588097A GB7526/44A GB752644A GB588097A GB 588097 A GB588097 A GB 588097A GB 7526/44 A GB7526/44 A GB 7526/44A GB 752644 A GB752644 A GB 752644A GB 588097 A GB588097 A GB 588097A
Authority
GB
United Kingdom
Prior art keywords
duct
turbines
jet
air
relating
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
GB7526/44A
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.)
Power Jets Research and Development Ltd
Original Assignee
Power Jets Research and Development Ltd
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 Power Jets Research and Development Ltd filed Critical Power Jets Research and Development Ltd
Publication of GB588097A publication Critical patent/GB588097A/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
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/08—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
    • F02K3/105—Heating the by-pass flow
    • F02K3/115—Heating the by-pass flow by means of indirect heat exchange
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/08—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
    • F02K3/105—Heating the by-pass flow
    • F02K3/11—Heating the by-pass flow by means of burners or combustion chambers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/20—Heat transfer, e.g. cooling
    • F05D2260/211—Heat transfer, e.g. cooling by intercooling, e.g. during a compression cycle
    • 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
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Pre-Mixing And Non-Premixing Gas Burner (AREA)

Abstract

588,097. Gas turbine plant. POWER JETS (RESEARCH & DEVELOPMENT), Ltd., and CONSTANT, H. April 22, 1944, No. 7526. [Class 110 (iii)] A gas turbine plant for the jet-propulsion of aircraft comprises H.P. and L.P. turbines 31, 19 respectively, driving H.P. and L.P. compressors 32, 20, the turbines being arranged next to one another and between the air compressors. A reheating combustion chamber 45 is placed between the turbines. The L.P. turbine also drives, through a reduction gear 56, a ducted fan 53 which delivers part of its air to the L.P. compressor and part to a duct 15 leading to an augment or jet. An intercooler 60 is placed in the duct 15 and the turbine exhaust duct 47 leads to a separate propulsion jet. In a modification, there is no intercooler, the turbines discharge into the single duct 15 and the air in the duct is heated by an oil burner.
GB7526/44A 1944-04-22 1944-04-22 Improvements in or relating to internal combustion turbine power plants Expired GB588097A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB263834X 1944-04-22

Publications (1)

Publication Number Publication Date
GB588097A true GB588097A (en) 1947-05-14

Family

ID=10242782

Family Applications (1)

Application Number Title Priority Date Filing Date
GB7526/44A Expired GB588097A (en) 1944-04-22 1944-04-22 Improvements in or relating to internal combustion turbine power plants

Country Status (2)

Country Link
CH (1) CH263834A (en)
GB (1) GB588097A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2398891A1 (en) * 1977-07-25 1979-02-23 Gen Electric TURBOMACHINE WITH REGULATED OPERATING CYCLE
WO2010009708A1 (en) * 2008-07-19 2010-01-28 Mtu Aero Engines Gmbh Engine comprising a core engine and thruster connected downstream
RU2770077C1 (en) * 2020-11-11 2022-04-14 Владимир Константинович Литвинов Method for operation of a double-circuit gas turbine engine and double-circuit gas turbine engine

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2398891A1 (en) * 1977-07-25 1979-02-23 Gen Electric TURBOMACHINE WITH REGULATED OPERATING CYCLE
WO2010009708A1 (en) * 2008-07-19 2010-01-28 Mtu Aero Engines Gmbh Engine comprising a core engine and thruster connected downstream
RU2770077C1 (en) * 2020-11-11 2022-04-14 Владимир Константинович Литвинов Method for operation of a double-circuit gas turbine engine and double-circuit gas turbine engine

Also Published As

Publication number Publication date
CH263834A (en) 1949-09-15

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