FR2629871B1 - Commande par vecteur de poussee, ameliorant la manoeuvrabilite d'aeronefs propulses par reaction et methode d'utilisation de cette commande - Google Patents

Commande par vecteur de poussee, ameliorant la manoeuvrabilite d'aeronefs propulses par reaction et methode d'utilisation de cette commande

Info

Publication number
FR2629871B1
FR2629871B1 FR898903619A FR8903619A FR2629871B1 FR 2629871 B1 FR2629871 B1 FR 2629871B1 FR 898903619 A FR898903619 A FR 898903619A FR 8903619 A FR8903619 A FR 8903619A FR 2629871 B1 FR2629871 B1 FR 2629871B1
Authority
FR
France
Prior art keywords
control
maneuverability
jet
improving
thrust vector
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 - Lifetime
Application number
FR898903619A
Other languages
English (en)
French (fr)
Other versions
FR2629871A1 (fr
Inventor
Felix Aulehla
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.)
Airbus Defence and Space GmbH
Original Assignee
Messerschmitt Bolkow Blohm AG
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 Messerschmitt Bolkow Blohm AG filed Critical Messerschmitt Bolkow Blohm AG
Publication of FR2629871A1 publication Critical patent/FR2629871A1/fr
Application granted granted Critical
Publication of FR2629871B1 publication Critical patent/FR2629871B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • F02K1/12—Varying effective area of jet pipe or nozzle by means of pivoted flaps
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C15/00—Attitude, flight direction, or altitude control by jet reaction
    • B64C15/02—Attitude, flight direction, or altitude control by jet reaction the jets being propulsion jets
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • F02K9/90—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using deflectors
    • 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
    • F05D2250/00—Geometry
    • F05D2250/70—Shape
    • F05D2250/71—Shape curved
    • F05D2250/711—Shape curved convex
    • 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
    • F05D2250/00—Geometry
    • F05D2250/70—Shape
    • F05D2250/71—Shape curved
    • F05D2250/712—Shape curved concave

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Measuring Volume Flow (AREA)
  • Control Of Turbines (AREA)
  • Exhaust Silencers (AREA)
FR898903619A 1988-04-07 1989-03-20 Commande par vecteur de poussee, ameliorant la manoeuvrabilite d'aeronefs propulses par reaction et methode d'utilisation de cette commande Expired - Lifetime FR2629871B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE3811616A DE3811616C1 (enExample) 1988-04-07 1988-04-07

Publications (2)

Publication Number Publication Date
FR2629871A1 FR2629871A1 (fr) 1989-10-13
FR2629871B1 true FR2629871B1 (fr) 1992-05-07

Family

ID=6351528

Family Applications (1)

Application Number Title Priority Date Filing Date
FR898903619A Expired - Lifetime FR2629871B1 (fr) 1988-04-07 1989-03-20 Commande par vecteur de poussee, ameliorant la manoeuvrabilite d'aeronefs propulses par reaction et methode d'utilisation de cette commande

Country Status (3)

Country Link
US (1) US4957249A (enExample)
DE (1) DE3811616C1 (enExample)
FR (1) FR2629871B1 (enExample)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3909347A1 (de) * 1989-03-22 1990-09-27 Mtu Muenchen Gmbh Schubduese zur schubvektorsteuerung fuer mit strahltriebwerken ausgeruestete fluggeraete
US5031836A (en) * 1990-07-10 1991-07-16 United Technologies Corporation Flexible fairing for airframe/nozzle interface
DE4207103C1 (enExample) * 1992-03-06 1993-09-16 Deutsche Aerospace Airbus Gmbh, 21129 Hamburg, De
US6260794B1 (en) * 1999-05-05 2001-07-17 General Electric Company Dolphin cascade vane
US10472072B2 (en) * 2015-11-25 2019-11-12 Hamilton Sundstrand Corporation Supply tube for sensor
RU2657400C1 (ru) * 2017-07-10 2018-06-13 Акционерное общество "Конструкторское бюро химавтоматики" Жидкостный ракетный двигатель с насадком из углерод-углеродного композиционного материала (уукм)
CN109356749B (zh) * 2018-11-20 2020-08-25 西安航天动力技术研究所 一种固体火箭发动机变推力信号反馈系统

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB759268A (en) * 1953-07-14 1956-10-17 Power Jets Res & Dev Ltd Method of mounting instruments in turbines and compressors
FR1211773A (fr) * 1958-10-08 1960-03-18 Snecma Dispositif d'adaptation d'une tuyère convergente-divergente à des régimes variables
US3045947A (en) * 1959-04-24 1962-07-24 Bertin & Cie Ejectors, particularly for producing lift in aircraft
US3414195A (en) * 1966-06-17 1968-12-03 Saunders Walter Selden Sweeping jet wing aircraft with actuator strip flap and emergency vtol capability
US4074878A (en) * 1975-06-23 1978-02-21 Sherman Irving R Programmed flap system for an aircraft having wings
US4052007A (en) * 1975-11-25 1977-10-04 United Technologies Corporation Flap-type two-dimensional nozzle
US4182501A (en) * 1977-03-04 1980-01-08 Astech Thrust reverser for jet engine forming active extension of jet tube
FI782193A7 (fi) * 1977-07-16 1979-01-17 Jastram Werke Foerfarande foer aostadkommande av skjutkraft vid styrdrivanordningar foer fartyg och en haerfoer avsedd styrdrivanordning
US4519746A (en) * 1981-07-24 1985-05-28 United Technologies Corporation Airfoil blade
GB2125352B (en) * 1982-08-18 1986-02-19 Walker Wingsail Syst Pressure sensing on rigid sails
US4654140A (en) * 1985-11-18 1987-03-31 Chen Yen Ming Pressure indicating device for indicating clogging condition of a filter

Also Published As

Publication number Publication date
DE3811616C1 (enExample) 1989-07-27
US4957249A (en) 1990-09-18
FR2629871A1 (fr) 1989-10-13

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Legal Events

Date Code Title Description
ST Notification of lapse