FR2408037A1 - Tuyere chaude - Google Patents

Tuyere chaude

Info

Publication number
FR2408037A1
FR2408037A1 FR7733442A FR7733442A FR2408037A1 FR 2408037 A1 FR2408037 A1 FR 2408037A1 FR 7733442 A FR7733442 A FR 7733442A FR 7733442 A FR7733442 A FR 7733442A FR 2408037 A1 FR2408037 A1 FR 2408037A1
Authority
FR
France
Prior art keywords
hot tip
hot
rings6
monobloc2
propergols
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.)
Granted
Application number
FR7733442A
Other languages
English (en)
Other versions
FR2408037B1 (fr
Inventor
Max Calabro
Herve Girard
Alain Le Corre
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 Group SAS
Original Assignee
Airbus Group 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 Airbus Group SAS filed Critical Airbus Group SAS
Priority to FR7733442A priority Critical patent/FR2408037A1/fr
Priority to IT29247/78A priority patent/IT1099864B/it
Priority to GB7842942A priority patent/GB2007773B/en
Priority to DE2848114A priority patent/DE2848114C3/de
Publication of FR2408037A1 publication Critical patent/FR2408037A1/fr
Application granted granted Critical
Publication of FR2408037B1 publication Critical patent/FR2408037B1/fr
Granted 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

L'INVENTION CONCERNE LES TUYERES POUR PROPULSEURS. ELLE A POUR OBJET UNE TUYERE CHAUDE ORIENTABLE, CONSTITUEE PAR UNE UNIQUE PIECE MONOBLOC2 REALISEE PAR TISSAGE TRIDIMENTIONNEL D'UN SUBSTRAT EN CARBONE. CETTE PIECE EST CEINTUREE DE DEUX ANNEAUX6, 7 D'ISOLATION THERMIQUE, PAR L'INTERMEDIAIRE DESQUELS S'EFFECTUENT LA SUSPENSION ET LA COMMANDE D'ORIENTATION DE LA TUYERE. APPLICATION AUX TUYERES POUR PROPULSEURS A PROPERGOLS SOLIDES.
FR7733442A 1977-11-07 1977-11-07 Tuyere chaude Granted FR2408037A1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR7733442A FR2408037A1 (fr) 1977-11-07 1977-11-07 Tuyere chaude
IT29247/78A IT1099864B (it) 1977-11-07 1978-10-30 Ugello caldo
GB7842942A GB2007773B (en) 1977-11-07 1978-11-02 Nozzle for propulsion units
DE2848114A DE2848114C3 (de) 1977-11-07 1978-11-06 Heißdüse für Raketentriebwerke

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7733442A FR2408037A1 (fr) 1977-11-07 1977-11-07 Tuyere chaude

Publications (2)

Publication Number Publication Date
FR2408037A1 true FR2408037A1 (fr) 1979-06-01
FR2408037B1 FR2408037B1 (fr) 1981-11-27

Family

ID=9197340

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7733442A Granted FR2408037A1 (fr) 1977-11-07 1977-11-07 Tuyere chaude

Country Status (4)

Country Link
DE (1) DE2848114C3 (fr)
FR (1) FR2408037A1 (fr)
GB (1) GB2007773B (fr)
IT (1) IT1099864B (fr)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0015216A1 (fr) * 1979-02-27 1980-09-03 AEROSPATIALE Société Nationale Industrielle Agencement de pilotage d'un propulseur d'engin à propergol solide
FR2470253A1 (fr) * 1979-11-23 1981-05-29 Snecma Tuyere orientable pour propulseur a reaction
US4452038A (en) * 1981-11-19 1984-06-05 S.N.E.C.M.A. System for attaching two rotating parts made of materials having different expansion coefficients

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4967599A (en) * 1980-05-19 1990-11-06 Societe Europeenne De Propulsion Mechanical and insulating connection between a nozzle and the filament-wound casing of the combustion chamber of a solid propellant rocket motor
RU2529749C1 (ru) * 2013-07-17 2014-09-27 Открытое акционерное общество Научно-производственное объединение "Искра" Установка для определения окислительной стойкости углерод-углеродного композиционного материала
RU2632393C1 (ru) * 2016-07-04 2017-10-04 Акционерное общество Центральный научно-исследовательский институт специального машиностроения Подвесной шарнир поворотного сопла из композиционных материалов и способ его изготовления

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3140584A (en) * 1959-05-07 1964-07-14 Thiokol Chemical Corp Steering device for rocket-powered vehicles
FR1554059A (fr) * 1968-01-17 1969-01-17
FR2122567A1 (fr) * 1971-01-21 1972-09-01 Imp Metal Ind Kynoch Ltd
DE2350103A1 (de) * 1973-10-05 1975-04-10 Bayern Chemie Gmbh Flugchemie Schwenkduese an einem gasleitrohr eines raketentriebwerks

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1203646B (de) * 1962-12-21 1965-10-21 Studebaker Corp Geschichtete, faserverstaerkte Kunststoffwandung fuer Flugkoerper, Raketenantriebe u. dgl.
US3826708A (en) * 1970-05-18 1974-07-30 Mc Donnell Douglas Corp Rocket nozzle liner construction

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3140584A (en) * 1959-05-07 1964-07-14 Thiokol Chemical Corp Steering device for rocket-powered vehicles
FR1554059A (fr) * 1968-01-17 1969-01-17
FR2122567A1 (fr) * 1971-01-21 1972-09-01 Imp Metal Ind Kynoch Ltd
DE2350103A1 (de) * 1973-10-05 1975-04-10 Bayern Chemie Gmbh Flugchemie Schwenkduese an einem gasleitrohr eines raketentriebwerks

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0015216A1 (fr) * 1979-02-27 1980-09-03 AEROSPATIALE Société Nationale Industrielle Agencement de pilotage d'un propulseur d'engin à propergol solide
FR2470253A1 (fr) * 1979-11-23 1981-05-29 Snecma Tuyere orientable pour propulseur a reaction
EP0029773A1 (fr) * 1979-11-23 1981-06-03 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Tuyère orientable pour propulseur à réaction
US4363445A (en) * 1979-11-23 1982-12-14 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Thrust-vectoring nozzle for jet propulsion system
US4452038A (en) * 1981-11-19 1984-06-05 S.N.E.C.M.A. System for attaching two rotating parts made of materials having different expansion coefficients

Also Published As

Publication number Publication date
GB2007773A (en) 1979-05-23
DE2848114B2 (de) 1980-10-16
FR2408037B1 (fr) 1981-11-27
IT1099864B (it) 1985-09-28
DE2848114A1 (de) 1979-05-17
IT7829247A0 (it) 1978-10-30
DE2848114C3 (de) 1981-07-09
GB2007773B (en) 1982-04-21

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Legal Events

Date Code Title Description
ST Notification of lapse