FR1057271A - Improvements to the control of one flow of fluid by another flow and applications of these improvements - Google Patents

Improvements to the control of one flow of fluid by another flow and applications of these improvements

Info

Publication number
FR1057271A
FR1057271A FR1057271DA FR1057271A FR 1057271 A FR1057271 A FR 1057271A FR 1057271D A FR1057271D A FR 1057271DA FR 1057271 A FR1057271 A FR 1057271A
Authority
FR
France
Prior art keywords
flow
fluid
applications
control
another
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
Other languages
French (fr)
Inventor
Jean-Henri Bertin
Marcel Kadosch
Francois-Marie-Louis Maunoury
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.)
Safran Aircraft Engines SAS
Original Assignee
Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
SNECMA SAS
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 Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA, SNECMA SAS filed Critical Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
Application granted granted Critical
Publication of FR1057271A publication Critical patent/FR1057271A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/28Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto using fluid jets to influence the jet flow
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K3/00Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/08Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
    • F02K3/105Heating the by-pass flow
    • F02K3/11Heating the by-pass flow by means of burners or combustion chambers

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR1057271D 1952-05-21 1952-05-21 Improvements to the control of one flow of fluid by another flow and applications of these improvements Expired FR1057271A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1057271T 1952-05-21

Publications (1)

Publication Number Publication Date
FR1057271A true FR1057271A (en) 1954-03-08

Family

ID=9597856

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1057271D Expired FR1057271A (en) 1952-05-21 1952-05-21 Improvements to the control of one flow of fluid by another flow and applications of these improvements

Country Status (2)

Country Link
FR (1) FR1057271A (en)
NL (1) NL178522C (en)

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2865170A (en) * 1955-08-12 1958-12-23 Snecma Method of jet deflection and apparatus therefor
US2885856A (en) * 1956-03-23 1959-05-12 Curtiss Wright Corp Apparatus for increasing compressor pressure ratios in a gas turbine engine
US2916873A (en) * 1958-10-22 1959-12-15 Advanced Res Associates Inc Jet deflecting apparatus
DE1073242B (en) * 1960-01-14 Power Jets (Research &. Develop ment) Limited London Jet propulsion nozzle
US2952123A (en) * 1956-05-25 1960-09-13 Lockheed Aircraft Corp Directional controls for propulsive jets
US2990905A (en) * 1957-05-13 1961-07-04 Lilley Geoffrey Michael Jet noise suppression means
US3010280A (en) * 1958-03-25 1961-11-28 United Aircraft Corp Variable-expansion nozzle
US3020714A (en) * 1956-07-03 1962-02-13 Snecma Device for controlling the jet of a reaction propulsion motor
US3066485A (en) * 1957-12-11 1962-12-04 Bertin & Cie Steering device for rocket-propelled vehicles
US3101591A (en) * 1961-03-28 1963-08-27 Thompson Ramo Wooldridge Inc Vapor-gas injection thrust vector control system
US3132478A (en) * 1961-07-13 1964-05-12 Thompson Ramo Wooldridge Inc Solid propellant gas rotary valve
US3137126A (en) * 1961-01-11 1964-06-16 North American Aviation Inc Method and means for forming a gaseous passage
US3147590A (en) * 1961-03-16 1964-09-08 Thompson Ramo Wooldridge Inc Reaction motor with nozzle vector control having ablative port means and cooled valve means
EP1698774A3 (en) * 2005-03-02 2012-11-21 Rolls-Royce Plc A turbine engine and a method of operating a turbine engine

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1073242B (en) * 1960-01-14 Power Jets (Research &. Develop ment) Limited London Jet propulsion nozzle
US2865170A (en) * 1955-08-12 1958-12-23 Snecma Method of jet deflection and apparatus therefor
US2885856A (en) * 1956-03-23 1959-05-12 Curtiss Wright Corp Apparatus for increasing compressor pressure ratios in a gas turbine engine
US2952123A (en) * 1956-05-25 1960-09-13 Lockheed Aircraft Corp Directional controls for propulsive jets
US3020714A (en) * 1956-07-03 1962-02-13 Snecma Device for controlling the jet of a reaction propulsion motor
US2990905A (en) * 1957-05-13 1961-07-04 Lilley Geoffrey Michael Jet noise suppression means
US3066485A (en) * 1957-12-11 1962-12-04 Bertin & Cie Steering device for rocket-propelled vehicles
US3010280A (en) * 1958-03-25 1961-11-28 United Aircraft Corp Variable-expansion nozzle
US2916873A (en) * 1958-10-22 1959-12-15 Advanced Res Associates Inc Jet deflecting apparatus
US3137126A (en) * 1961-01-11 1964-06-16 North American Aviation Inc Method and means for forming a gaseous passage
US3147590A (en) * 1961-03-16 1964-09-08 Thompson Ramo Wooldridge Inc Reaction motor with nozzle vector control having ablative port means and cooled valve means
US3101591A (en) * 1961-03-28 1963-08-27 Thompson Ramo Wooldridge Inc Vapor-gas injection thrust vector control system
US3132478A (en) * 1961-07-13 1964-05-12 Thompson Ramo Wooldridge Inc Solid propellant gas rotary valve
EP1698774A3 (en) * 2005-03-02 2012-11-21 Rolls-Royce Plc A turbine engine and a method of operating a turbine engine

Also Published As

Publication number Publication date
NL178522C (en)

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