GB704669A - Improvements in jet propulsion engines - Google Patents

Improvements in jet propulsion engines

Info

Publication number
GB704669A
GB704669A GB16686/50A GB1668650A GB704669A GB 704669 A GB704669 A GB 704669A GB 16686/50 A GB16686/50 A GB 16686/50A GB 1668650 A GB1668650 A GB 1668650A GB 704669 A GB704669 A GB 704669A
Authority
GB
United Kingdom
Prior art keywords
turbines
jet propulsion
compressor
compressors
disposed
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
GB16686/50A
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 GB704669A publication Critical patent/GB704669A/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
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/15—Control or regulation
    • F02K1/16—Control or regulation conjointly with another control

Abstract

704,669. Jet propulsion plant; gas turbine plant. SOC. RATEAU, and ANXIONNAZ, R. July 4, 1950 [July 22, 1949], No. 16686/50. Class 110 (3) Relates to a jet turbine engine having a low pressure axial-flow compressor feeding outer and inner ducts terminating in separate or combined jet propulsion nozzles and having a high-pressure, axial-flow compressor together with one or more combustion chambers and one or more turbines for driving said compressors disposed in said inner duct. Such an engine comprises a boosting system having means for injecting water with or without a liquid fuel such as methanol into the combustion chambers k of the engine, combustion heating means 2 in the outer duct or in the combined jet propulsion nozzle and means such as a member 3 controlling outlet ports 3a for adjusting the cross-sectional area of the outer or combined jet propulsion nozzle. The jet turbine engine comprises compressors g, which are driven by turbines h, I respectively. In a modification, the compressors are mechanically coupled together through suitable gearing and are jointly driven by the said turbines. The jet turbine engine may also include water injection nozzles 4 disposed as shown, a burner 5 and water or water/methanol injection nozzles 6 arranged between the turbines together with burners 7 and a bullet 8 arranged in the inner nozzle n. At least one of the stator blades of the low-pressure compressor is adjustably mounted. Moreover a throttle 10 is disposed in the outer flow i, a valve 11 is positioned downstream of the low-pressure compressor to connect the compressor j with the atmosphere and a bleed line 12 is arranged beween the turbines. The said adjustable members are mechanically, hydraulically or electrically controlled directly by the pilot or through an adjusting system. Specifications 650,661 and 650,710 are referred to.
GB16686/50A 1949-07-22 1950-07-04 Improvements in jet propulsion engines Expired GB704669A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR704669X 1949-07-22

Publications (1)

Publication Number Publication Date
GB704669A true GB704669A (en) 1954-02-24

Family

ID=9066367

Family Applications (1)

Application Number Title Priority Date Filing Date
GB16686/50A Expired GB704669A (en) 1949-07-22 1950-07-04 Improvements in jet propulsion engines

Country Status (1)

Country Link
GB (1) GB704669A (en)

Cited By (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2934889A (en) * 1956-02-14 1960-05-03 United Aircraft Corp Noise abatement means
DE1084981B (en) * 1957-01-25 1960-07-07 Konink Luchtvaart Mij N V Aircraft engine
US2986002A (en) * 1957-06-05 1961-05-30 Curtiss Wright Corp Leaky-type exhaust nozzle for jet propulsion devices
DE1115527B (en) * 1957-05-21 1961-10-19 English Electric Co Ltd Thrust nozzle for jet engines
US3016698A (en) * 1959-07-02 1962-01-16 Gen Motors Corp Bypass engine
DE1131467B (en) * 1959-04-30 1962-06-14 Daimler Benz Ag Compound engine for propulsion of aircraft
US3060680A (en) * 1957-12-30 1962-10-30 Rolls Royce By-pass gas-turbine engine and control therefor
US3088280A (en) * 1959-04-17 1963-05-07 Rolls Royce Reducing smoke in gas turbine engine exhaust
US3108767A (en) * 1960-03-14 1963-10-29 Rolls Royce By-pass gas turbine engine with air bleed means
US3111005A (en) * 1963-11-19 Jet propulsion plant
US3149461A (en) * 1960-11-18 1964-09-22 Snecma Composite reaction engine for aircraft with wide ranges of speed
US3238716A (en) * 1962-03-15 1966-03-08 Nord Aviation Combined turbojet-ramjet units
US3285567A (en) * 1963-11-29 1966-11-15 Bristol Siddeley Engines Ltd Axial flow turbines and compressors
US3316717A (en) * 1965-09-15 1967-05-02 Gen Motors Corp Dual fan engine
US3369361A (en) * 1966-03-07 1968-02-20 Gale M. Craig Gas turbine power plant with sub-atmospheric spray-cooled turbine discharge into exhaust compressor
DE1268438B (en) * 1960-05-06 1968-05-16 Rolls Royce Bypass gas turbine jet engine
US3472487A (en) * 1967-10-06 1969-10-14 Avco Corp Wide speed range gas power converter
US3476486A (en) * 1966-04-12 1969-11-04 Dowty Rotol Ltd Gas turbine engines
US3514952A (en) * 1964-07-01 1970-06-02 Us Air Force Variable bypass turbofan engine
US3635029A (en) * 1968-09-06 1972-01-18 Snecma Composite gas turbine ramjet engine
GB2139705A (en) * 1983-05-14 1984-11-14 Satoru Suzuki Boosting apparatus for a turbo-jet engine
EP2426342A3 (en) * 2006-10-12 2012-05-09 United Technologies Corporation Turbofan engine with variable bypass nozzle exit area and method of operation

Cited By (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3111005A (en) * 1963-11-19 Jet propulsion plant
US2934889A (en) * 1956-02-14 1960-05-03 United Aircraft Corp Noise abatement means
DE1084981B (en) * 1957-01-25 1960-07-07 Konink Luchtvaart Mij N V Aircraft engine
DE1115527B (en) * 1957-05-21 1961-10-19 English Electric Co Ltd Thrust nozzle for jet engines
US2986002A (en) * 1957-06-05 1961-05-30 Curtiss Wright Corp Leaky-type exhaust nozzle for jet propulsion devices
US3060680A (en) * 1957-12-30 1962-10-30 Rolls Royce By-pass gas-turbine engine and control therefor
US3088280A (en) * 1959-04-17 1963-05-07 Rolls Royce Reducing smoke in gas turbine engine exhaust
DE1131467B (en) * 1959-04-30 1962-06-14 Daimler Benz Ag Compound engine for propulsion of aircraft
US3016698A (en) * 1959-07-02 1962-01-16 Gen Motors Corp Bypass engine
US3108767A (en) * 1960-03-14 1963-10-29 Rolls Royce By-pass gas turbine engine with air bleed means
DE1268438B (en) * 1960-05-06 1968-05-16 Rolls Royce Bypass gas turbine jet engine
US3149461A (en) * 1960-11-18 1964-09-22 Snecma Composite reaction engine for aircraft with wide ranges of speed
US3238716A (en) * 1962-03-15 1966-03-08 Nord Aviation Combined turbojet-ramjet units
US3285567A (en) * 1963-11-29 1966-11-15 Bristol Siddeley Engines Ltd Axial flow turbines and compressors
US3514952A (en) * 1964-07-01 1970-06-02 Us Air Force Variable bypass turbofan engine
US3316717A (en) * 1965-09-15 1967-05-02 Gen Motors Corp Dual fan engine
US3369361A (en) * 1966-03-07 1968-02-20 Gale M. Craig Gas turbine power plant with sub-atmospheric spray-cooled turbine discharge into exhaust compressor
US3476486A (en) * 1966-04-12 1969-11-04 Dowty Rotol Ltd Gas turbine engines
US3472487A (en) * 1967-10-06 1969-10-14 Avco Corp Wide speed range gas power converter
US3635029A (en) * 1968-09-06 1972-01-18 Snecma Composite gas turbine ramjet engine
GB2139705A (en) * 1983-05-14 1984-11-14 Satoru Suzuki Boosting apparatus for a turbo-jet engine
EP2426342A3 (en) * 2006-10-12 2012-05-09 United Technologies Corporation Turbofan engine with variable bypass nozzle exit area and method of operation
US8480350B2 (en) 2006-10-12 2013-07-09 United Technologies Corporation Turbofan engine with variable bypass nozzle exit area and method of operation

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