FR2443586A1 - STATOREACTOR WITH DRIVE VECTOR CONTROL - Google Patents

STATOREACTOR WITH DRIVE VECTOR CONTROL

Info

Publication number
FR2443586A1
FR2443586A1 FR7929176A FR7929176A FR2443586A1 FR 2443586 A1 FR2443586 A1 FR 2443586A1 FR 7929176 A FR7929176 A FR 7929176A FR 7929176 A FR7929176 A FR 7929176A FR 2443586 A1 FR2443586 A1 FR 2443586A1
Authority
FR
France
Prior art keywords
pressure
statoreactor
hydraulic chamber
vector control
controlling
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.)
Withdrawn
Application number
FR7929176A
Other languages
French (fr)
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.)
Bayern Chemie Gesellschaft fuer Flugchemische Antriebe mbH
Original Assignee
Bayern Chemie Gesellschaft fuer Flugchemische Antriebe mbH
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 Bayern Chemie Gesellschaft fuer Flugchemische Antriebe mbH filed Critical Bayern Chemie Gesellschaft fuer Flugchemische Antriebe mbH
Publication of FR2443586A1 publication Critical patent/FR2443586A1/en
Withdrawn legal-status Critical Current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
    • 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
    • F02K9/84—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using movable nozzles

Abstract

Statoréacteur comportant une partie tuyère de poussée pivotable pour la commande du vecteur de poussée et supportée déplaçable angulairement sur la partie propulseur, côté chambre de combustion, au moyen d'au moins une chambre hydraulique soumise à une pression correspondant à la force de séparation agissant entre les deux dites parties, et un mécanisme d'actionnement pour la commande de la position angulaire de la partie tuyère. Pour la régulation automatique de la pression de la chambre hydraulique 46, il est prévu un amplificateur de pression 52 raccordé, côté sortie, à la chambre hydraulique 46 et actionné en fonction de la pression de la chambre de combustion, côté basse pression.Statoreactor comprising a pivotable thrust nozzle part for controlling the thrust vector and supported angularly displaceable on the thruster part, on the combustion chamber side, by means of at least one hydraulic chamber subjected to a pressure corresponding to the separation force acting between the two said parts, and an actuating mechanism for controlling the angular position of the nozzle part. For the automatic regulation of the pressure of the hydraulic chamber 46, there is provided a pressure amplifier 52 connected, on the output side, to the hydraulic chamber 46 and actuated as a function of the pressure of the combustion chamber, on the low pressure side.

FR7929176A 1978-12-07 1979-11-27 STATOREACTOR WITH DRIVE VECTOR CONTROL Withdrawn FR2443586A1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19782852918 DE2852918A1 (en) 1978-12-07 1978-12-07 JET ENGINE WITH PUSH VECTOR CONTROL

Publications (1)

Publication Number Publication Date
FR2443586A1 true FR2443586A1 (en) 1980-07-04

Family

ID=6056563

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7929176A Withdrawn FR2443586A1 (en) 1978-12-07 1979-11-27 STATOREACTOR WITH DRIVE VECTOR CONTROL

Country Status (4)

Country Link
DE (1) DE2852918A1 (en)
FR (1) FR2443586A1 (en)
GB (1) GB2036669A (en)
IT (1) IT1127663B (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7062651B1 (en) 1999-05-25 2006-06-13 Silverbrook Research Pty Ltd Network printer registration protocol
CN103867341B (en) * 2012-12-14 2016-07-13 上海新力动力设备研究所 A kind of small-scale solid rocket motor ball-and-socket gimbaled nozzle space vector torsion resistant device
CN111322912A (en) * 2020-03-06 2020-06-23 南京理工大学 Thrust vector all-axis swinging spray pipe driven by ball screw in cooperation
CN112431689A (en) * 2020-11-24 2021-03-02 哈尔滨工程大学 Solid rocket engine containing supersonic separation line swinging spray pipe

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1237219A (en) * 1959-06-16 1960-07-29 France Etat Adjustable nozzle
US3298175A (en) * 1963-08-05 1967-01-17 Charles P Morse Method and device for cooling
US3401887A (en) * 1966-05-02 1968-09-17 Thiokol Chemical Corp Controllable rocket nozzle with pressure amplifier for reducing actuating force
FR2068765A1 (en) * 1969-10-23 1971-09-03 Rolls Royce
FR2349739A1 (en) * 1976-04-30 1977-11-25 Sperry Rand Ltd SUSPENSION FOR REACTION PROPULSION TUBE

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1237219A (en) * 1959-06-16 1960-07-29 France Etat Adjustable nozzle
US3298175A (en) * 1963-08-05 1967-01-17 Charles P Morse Method and device for cooling
US3401887A (en) * 1966-05-02 1968-09-17 Thiokol Chemical Corp Controllable rocket nozzle with pressure amplifier for reducing actuating force
FR2068765A1 (en) * 1969-10-23 1971-09-03 Rolls Royce
FR2349739A1 (en) * 1976-04-30 1977-11-25 Sperry Rand Ltd SUSPENSION FOR REACTION PROPULSION TUBE

Also Published As

Publication number Publication date
IT7927681A0 (en) 1979-11-29
DE2852918A1 (en) 1980-06-19
GB2036669A (en) 1980-07-02
IT1127663B (en) 1986-05-21

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Legal Events

Date Code Title Description
ST Notification of lapse