DE3766264D1 - Schubduese mit regelbarem querschnitt. - Google Patents

Schubduese mit regelbarem querschnitt.

Info

Publication number
DE3766264D1
DE3766264D1 DE8787400118T DE3766264T DE3766264D1 DE 3766264 D1 DE3766264 D1 DE 3766264D1 DE 8787400118 T DE8787400118 T DE 8787400118T DE 3766264 T DE3766264 T DE 3766264T DE 3766264 D1 DE3766264 D1 DE 3766264D1
Authority
DE
Germany
Prior art keywords
section
discharge nozzle
adjustable cross
adjustable
cross
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 - Fee Related
Application number
DE8787400118T
Other languages
English (en)
Inventor
Jean-Louis Joly
Michel Francois Servigne
Manuel Pierre Claramonte
Max Jean-Pierre Calabro
Jean-Pierre Pham
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
Application granted granted Critical
Publication of DE3766264D1 publication Critical patent/DE3766264D1/de
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/80Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • F02K9/86Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using nozzle throats of adjustable cross- section

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Nozzles (AREA)
DE8787400118T 1986-01-20 1987-01-19 Schubduese mit regelbarem querschnitt. Expired - Fee Related DE3766264D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8600693A FR2593236B1 (fr) 1986-01-20 1986-01-20 Ensemble de tuyere perfectionne comportant un col a section de passage reglable

Publications (1)

Publication Number Publication Date
DE3766264D1 true DE3766264D1 (de) 1991-01-03

Family

ID=9331252

Family Applications (1)

Application Number Title Priority Date Filing Date
DE8787400118T Expired - Fee Related DE3766264D1 (de) 1986-01-20 1987-01-19 Schubduese mit regelbarem querschnitt.

Country Status (3)

Country Link
EP (1) EP0233806B1 (de)
DE (1) DE3766264D1 (de)
FR (1) FR2593236B1 (de)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3714425A1 (de) * 1987-04-30 1988-11-17 Messerschmitt Boelkow Blohm Ventileinrichtung fuer partikelbeladene heissgase

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2443186A (en) * 1944-01-03 1948-06-15 Foulks Edwin David Jet propulsion fuel feeding and exhaust control device
US2612747A (en) * 1945-01-25 1952-10-07 Leslie A Skinner Rocket having adjustable discharge passage
US3245620A (en) * 1961-12-13 1966-04-12 Gen Motors Corp Missile steering control
DE2063703A1 (de) * 1970-12-24 1972-07-13 Dynamit Nobel Ag Raketenmotor
US4444006A (en) * 1981-02-04 1984-04-24 Hercules Incorporated Nozzle/valve device for a ducted rocket motor
DE3246540A1 (de) * 1982-12-16 1984-06-20 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Schubduesenanordnung zum verstellen des schubduesenquerschnitts von rueckstosstriebwerken fuer flugkoerper
DE8532148U1 (de) * 1985-11-14 1986-04-17 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Ventileinrichtung zum Steuern strömender Medien mit hoher Temperatur und hohem Druck

Also Published As

Publication number Publication date
FR2593236B1 (fr) 1989-09-29
FR2593236A1 (fr) 1987-07-24
EP0233806A1 (de) 1987-08-26
EP0233806B1 (de) 1990-11-22

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee