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GB600608A - 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
GB600608A
GB600608A GB719644A GB719644A GB600608A GB 600608 A GB600608 A GB 600608A GB 719644 A GB719644 A GB 719644A GB 719644 A GB719644 A GB 719644A GB 600608 A GB600608 A GB 600608A
Authority
GB
United Kingdom
Prior art keywords
jet
relating
propulsion
internal combustion
power plants
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
GB719644A
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
Filing date
Publication date
Application filed by Power Jets Research and Development Ltd filed Critical Power Jets Research and Development Ltd
Priority to CH263472D priority Critical patent/CH263472A/en
Publication of GB600608A publication Critical patent/GB600608A/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
    • F02K3/11—Heating the by-pass flow by means of burners or combustion chambers
    • 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
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/06—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with front fan

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fluidized-Bed Combustion And Resonant Combustion (AREA)

Abstract

600,608. Jet propulsion plant. POWER JETS (RESEARCH & DEVELOPMENT), Ltd., CONSTANT, H., and HAWTHORNE, W. R. April 18, 1944. No. 7196. [Class 110 (iii)] In a gas turbine plant for jet-propulsion of aircraft, the H.P. and L.P. turbines 24, 16 drive the H.P. and L.P. compressors 23, 14 respectively. The L.P. turbine also drives, through a speed-reduction gear 45 a ducted fan rotor 40 from which a part of the delivery is led to the L.P. compressor and the remainder passes through duct 10 to the propulsion jet. Reheating between the turbines may be provided by a second set of combustion chambers 61 and fuel may also be burned, as at 60, 63, in the turbine exhaust and the jet-augmentor duct 10.
GB719644A 1944-04-18 1944-04-18 Improvements in or relating to internal combustion turbine power plants Expired GB600608A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CH263472D CH263472A (en) 1944-04-18 1945-12-28 Combustion turbine jet propulsion on aircraft.

Publications (1)

Publication Number Publication Date
GB600608A true GB600608A (en) 1948-04-14

Family

ID=1628896

Family Applications (1)

Application Number Title Priority Date Filing Date
GB719644A Expired GB600608A (en) 1944-04-18 1944-04-18 Improvements in or relating to internal combustion turbine power plants

Country Status (1)

Country Link
GB (1) GB600608A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2645412A (en) * 1949-09-28 1953-07-14 United Aircraft Corp Locking device for split-compressor type turbopower plants
EP2930330A1 (en) * 2014-04-09 2015-10-14 Rolls-Royce plc Gas turbine engine
US20160363047A1 (en) * 2013-08-20 2016-12-15 United Technologies Corporation High thrust geared gas turbine engine

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2645412A (en) * 1949-09-28 1953-07-14 United Aircraft Corp Locking device for split-compressor type turbopower plants
US20160363047A1 (en) * 2013-08-20 2016-12-15 United Technologies Corporation High thrust geared gas turbine engine
EP2930330A1 (en) * 2014-04-09 2015-10-14 Rolls-Royce plc Gas turbine engine
US10072572B2 (en) 2014-04-09 2018-09-11 Rolls-Royce Plc Gas turbine engine

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