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THRUST LINK [5 records]

Filter results by subject field Alphabetical list of terms

Filter results by subject field

Alphabetical list of terms

Record 1 2010-04-26

English

Subject field(s)
  • Launchers (Astronautics)
CONT

Swivelling nozzle for a rocket engine. The nozzle comprises a moving diverging portion and a static portion secured to the rear end wall of the combustion chamber of the engine. A cardan mount jointed link device connects the moving diverging portion of the nozzle to the static portion, the moving diverging portion and the static portion being in mutual contact via respective spherical surfaces, and an actuator device acts on the moving diverging portion of the nozzle so as to be able to vary the direction of the thrust vector of the engine by modifying the orientation of the nozzle with sliding of the spherical surfaces one on the other. Resilient return means are interposed between the moving diverging portion of the nozzle and the static portion and act on the moving diverging portion in order to urge it towards the static portion so as to keep the spherical surfaces in mutual contact for any desired orientation of the nozzle.

Key term(s)
  • swiveling nozzle

French

Domaine(s)
  • Lanceurs (Astronautique)
DEF

Tuyère articulée autour d'un ou deux axes et permettant d'orienter l'axe de poussée.

Spanish

Save record 1

Record 2 1992-03-30

English

Subject field(s)
  • Aircraft Propulsion Systems
CONT

The thrust reverser lower track slide link failed due to fatigue cracking.

French

Domaine(s)
  • Propulsion des aéronefs
OBS

sur un aéronef DC 8.

Spanish

Save record 2

Record 3 1987-02-10

English

Subject field(s)
  • Transformation of Momentum (Mechanical Components)
  • Aircraft Systems
CONT

Thrust reverser control cam sector.... Inspect cam sector, cam link, control valve pushrod, bellcrank, bellcrank mounting link & mounting link attach fitting, on aircraft structure, for general condition. Rotate cam sector to disengage cam link roller from cam for inspection.

French

Domaine(s)
  • Transformations de mouvements (Composants mécaniques)
  • Circuits des aéronefs
OBS

secteur-came : terme accepté par le Comité d'étude de la terminologie des cartes de travail du DC-9.

Spanish

Save record 3

Record 4 1981-11-16

English

Subject field(s)
  • Aeroindustry
CONT

The DC-10 pylon is attached to the wing at four points : a) upper and lower monoballs(spherical bearings) in a two-piece front-spar bulkhead the pylon mates with a fitting on the wing's front spar to carry vertical, side and torque loads; b) a two-piece aft pylon bulkhead fitting mates with a clevis fitting attached to the wing box structure to carry side and vertical loads; c) a thrust link joins a fitting at the pylon's upper spar web immediately behind and adjacent to the front-spar bulkhead to two attach angles on the lower surface of the wing box structure to carry engine thrust loads.

French

Domaine(s)
  • Constructions aéronautiques
CONT

Le mât moteur du DC-10 est attaché à l'aile en quatre points distincts : a) les rotules inférieure et supérieure (roulements sphériques) montées sur un cadre-ferme en deux parties du longeron avant du mât s'engagent dans des ferrures fixées sur le longeron frontal de l'aile, pour transmettre les charges verticales, latérales et de torsion; b) une ferrure en deux parties à l'arrière du mât est reliée à une chape fixée à la structure du caisson de voilure pour transmettre les charges verticales et latérales; c) un palier de poussée relie une ferrure fixée sur la nervure du longeron supérieur du mât à deux ferrures de fixation disposées sur la partie inférieure de la structure du caisson de voilure.

Spanish

Save record 4

Record 5 1981-11-16

English

Subject field(s)
  • Aeroindustry
CONT

The DC-10 pylon is attached to the wing at four points : a) upper and lower monoballs(spherical bearings) in a two-piece front-spar bulkhead on the pylon mates with a fitting on the wing's front spar to carry vertical, side and torque loads; b) a two-piece aft pylon bulkhead fitting mates with a clevis fitting attached to the wing box structure to carry side and vertical loads; c) a thrust link joins a fitting at the pylon's upper spar web immediately behind and adjacent to the front-spar bulkhead to two attach angles on the lower surface of the wing box structure to carry engine thrust loads.

French

Domaine(s)
  • Constructions aéronautiques
CONT

Le mât moteur du DC-10 est attaché à l'aile en quatre points distincts : a) les rotules inférieure et supérieure (roulements sphériques) montées sur un cadre-ferme en deux parties du longeron avant du mât s'engagent dans des ferrures fixées sur le longeron frontal de l'aile, pour transmettre les charges verticales, latérales et de torsion; b) une ferrure en deux parties à l'arrière du mât est reliée à une chape fixée à la structure du caisson de voilure pour transmettre les charges verticales et latérales; c) un palier de poussée relie une ferrure fixée sur la nervure du longeron supérieur du mât à deux ferrures de fixation disposées sur la partie inférieure de la structure du caisson de voilure.

Spanish

Save record 5

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