FR1286886A - Dispositif d'inversion de poussée pour propulseurs comportant un turbo-réacteur àdouble flux - Google Patents

Dispositif d'inversion de poussée pour propulseurs comportant un turbo-réacteur àdouble flux

Info

Publication number
FR1286886A
FR1286886A FR851008A FR851008A FR1286886A FR 1286886 A FR1286886 A FR 1286886A FR 851008 A FR851008 A FR 851008A FR 851008 A FR851008 A FR 851008A FR 1286886 A FR1286886 A FR 1286886A
Authority
FR
France
Prior art keywords
thrusters
reactor
dual
thrust reverser
reverser device
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
FR851008A
Other languages
English (en)
Inventor
Pierre Sandre
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.)
Nord Aviation Societe Nationale de Constructions Aeronautiques
Original Assignee
Nord Aviation Societe Nationale de Constructions Aeronautiques
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
Priority to DEB46090A priority Critical patent/DE1190793B/de
Application filed by Nord Aviation Societe Nationale de Constructions Aeronautiques filed Critical Nord Aviation Societe Nationale de Constructions Aeronautiques
Priority to FR851008A priority patent/FR1286886A/fr
Priority to US168949A priority patent/US3167911A/en
Priority to GB3137/62A priority patent/GB955518A/en
Priority to DEN21125A priority patent/DE1190799B/de
Application granted granted Critical
Publication of FR1286886A publication Critical patent/FR1286886A/fr
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B49/00—Control, e.g. of pump delivery, or pump pressure of, or safety measures for, machines, pumps, or pumping installations, not otherwise provided for, or of interest apart from, groups F04B1/00 - F04B47/00
    • F04B49/22—Control, e.g. of pump delivery, or pump pressure of, or safety measures for, machines, pumps, or pumping installations, not otherwise provided for, or of interest apart from, groups F04B1/00 - F04B47/00 by means of valves
    • F04B49/24—Bypassing
    • 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
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/64—Reversing fan flow
    • F02K1/70—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing
    • 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
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/74—Reversing at least one flow in relation to at least one other flow in a plural- flow engine
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/10—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
    • F02K7/16—Composite ram-jet/turbo-jet engines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B49/00—Control, e.g. of pump delivery, or pump pressure of, or safety measures for, machines, pumps, or pumping installations, not otherwise provided for, or of interest apart from, groups F04B1/00 - F04B47/00
    • F04B49/10—Other safety measures
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B49/00—Control, e.g. of pump delivery, or pump pressure of, or safety measures for, machines, pumps, or pumping installations, not otherwise provided for, or of interest apart from, groups F04B1/00 - F04B47/00
    • F04B49/22—Control, e.g. of pump delivery, or pump pressure of, or safety measures for, machines, pumps, or pumping installations, not otherwise provided for, or of interest apart from, groups F04B1/00 - F04B47/00 by means of valves
    • F04B49/225—Control, e.g. of pump delivery, or pump pressure of, or safety measures for, machines, pumps, or pumping installations, not otherwise provided for, or of interest apart from, groups F04B1/00 - F04B47/00 by means of valves with throttling valves or valves varying the pump inlet opening or the outlet opening

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
FR851008A 1957-09-16 1961-01-27 Dispositif d'inversion de poussée pour propulseurs comportant un turbo-réacteur àdouble flux Expired FR1286886A (fr)

Priority Applications (5)

Application Number Priority Date Filing Date Title
DEB46090A DE1190793B (de) 1957-09-16 1957-09-16 Steuerung fuer durch Drehmotoren angetriebene Schubkolbenpumpen
FR851008A FR1286886A (fr) 1961-01-27 1961-01-27 Dispositif d'inversion de poussée pour propulseurs comportant un turbo-réacteur àdouble flux
US168949A US3167911A (en) 1961-01-27 1962-01-26 Thrust-reversing device for combined turbojet-ramjet units
GB3137/62A GB955518A (en) 1961-01-27 1962-01-26 Thrust-reversal in turbo-jet devices
DEN21125A DE1190799B (de) 1961-01-27 1962-01-27 Einrichtung zur Umkehr der Schubrichtung fuer kombinierte Turbo-Staustrahltriebwerke

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR851008A FR1286886A (fr) 1961-01-27 1961-01-27 Dispositif d'inversion de poussée pour propulseurs comportant un turbo-réacteur àdouble flux

Publications (1)

Publication Number Publication Date
FR1286886A true FR1286886A (fr) 1962-03-09

Family

ID=8747652

Family Applications (1)

Application Number Title Priority Date Filing Date
FR851008A Expired FR1286886A (fr) 1957-09-16 1961-01-27 Dispositif d'inversion de poussée pour propulseurs comportant un turbo-réacteur àdouble flux

Country Status (4)

Country Link
US (1) US3167911A (fr)
DE (1) DE1190799B (fr)
FR (1) FR1286886A (fr)
GB (1) GB955518A (fr)

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1103571A (en) * 1963-10-28 1968-02-14 Bristol Siddeley Engines Ltd Aircraft jet propulsion engines
DE1294823B (de) * 1965-05-12 1969-05-08 Bristol Siddeley Engines Ltd Stroemungskanal, insbesondere mit ringfoermigem Querschnitt, z. B. Mantelstromkanal eines Flugzeugtriebwerkes
US3279182A (en) * 1965-06-07 1966-10-18 Gen Electric Thrust reverser
US3262269A (en) * 1965-06-07 1966-07-26 Gen Electric Thrust reverser
US3280561A (en) * 1965-06-07 1966-10-25 Gen Electric Thrust reverser mechanism
US3262270A (en) * 1965-06-07 1966-07-26 Gen Electric Thrust reverser
US3262268A (en) * 1965-06-07 1966-07-26 Gen Electric Thrust reverser
US3262271A (en) * 1965-07-30 1966-07-26 Gen Electric Thrust reverser
US3386247A (en) * 1966-09-09 1968-06-04 Gen Electric Powerplant with thrust reverser
US3736750A (en) * 1971-03-12 1973-06-05 Rolls Royce Power plant
US3769797A (en) * 1971-10-28 1973-11-06 Us Air Force By-pass engine having a single, thrust diverter valve mechanism for a v/stol aircraft
US4086761A (en) * 1976-04-26 1978-05-02 The Boeing Company Stator bypass system for turbofan engine
US4667900A (en) * 1981-03-05 1987-05-26 Kyusik Kim Ram constriction vane diffuser for jet engine
US5694768A (en) * 1990-02-23 1997-12-09 General Electric Company Variable cycle turbofan-ramjet engine
GB2308866B (en) * 1996-01-04 1999-09-08 Rolls Royce Plc Ducted fan gas turbine engine with secondary duct
US6968701B2 (en) * 2002-01-16 2005-11-29 United Technologies Corporation Engine integrated auxiliary power unit
JP4893110B2 (ja) * 2006-05-31 2012-03-07 株式会社Ｉｈｉ 軸流流体装置
US10451002B2 (en) * 2016-01-22 2019-10-22 Honeywell International Inc. Translating cowl thrust reverser that prevents unintended door rotation
CN110529287B (zh) * 2019-08-13 2022-08-26 中国航发贵阳发动机设计研究所 一种串联式组合冲压发动机用分流机匣
CN113277045B (zh) * 2021-05-20 2022-05-20 南昌航空大学 一种辐流式水下推进器

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH244761A (de) * 1945-08-14 1946-09-30 Escher Wyss Maschf Ag Düsentriebwerk für Flugzeuge.
US2696079A (en) * 1950-04-17 1954-12-07 Peter G Kappus Dual jet aircraft power plant
FR1086315A (fr) * 1953-07-06 1955-02-11 Perfectionnements apportés aux réacteurs combinés
US3036431A (en) * 1959-09-08 1962-05-29 Boeing Co Thrust reverser for jet engines

Also Published As

Publication number Publication date
GB955518A (en) 1964-04-15
DE1190799B (de) 1965-04-08
US3167911A (en) 1965-02-02

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