TERMIUM Plus^®

Record 1,  Textual support,  English

Record number: 1, Textual support number: 1 CONT

The reverse thrust system provides means of decelerating aircraft during the landing roll, thus reducing landing roll length. The thrust reverser units are attached at the turbine outlet case of each engine.... The reversers are controlled by reverse thrust levers and operated by 13th stage engine bleed air. When not in use, the reversers are held in the locked position by 13th stage air and a mechanical lock. Each engine throttle has an additional handle which is used to actuate the thrust reversers. The reverse thrust lever pivots about a point near to the top of the throttle. If reverse trust is required, the throttle must be retarded to closed and then the reverse thrust lever must be pulled up. Further aft movement of the lever will increase reverse thrust.  3, record 1, English, - reverse%20thrust%20lever

Record 1,  Textual support,  French

Record number: 1, Textual support number: 1 CONT

Après le toucher, [le pilote] tira précautionneusement la manette d'inversion de poussée du n° 2 jusqu'à l'inversion maximale.  2, record 1, French, - manette%20d%27inversion%20de%20pouss%C3%A9e

Record number: 1, Textual support number: 1 OBS

Dans le domaine aéronautique, [...] l'inversion de poussée est un dispositif permettant d'orienter vers l'avant la poussée exercée par un moteur à hélice ou à réaction dans le but de ralentir l'avion et de reduire les distances lors de l'atterrissage. L'inversion de poussée est surtout utilisée sur les avions civils, ou sur les avions militaires qui en sont dérivés (avions de transport, ravitailleurs, etc...), mais elle équipe également quelques avions de combat comme le Tornado ou le SAAB 37 Viggen.  3, record 1, French, - manette%20d%27inversion%20de%20pouss%C3%A9e

Record number: 1, Textual support number: 2 OBS

manette : Clef, levier, poignée commandant un mécanisme et que l'on manœuvre à la main.  4, record 1, French, - manette%20d%27inversion%20de%20pouss%C3%A9e

Record number: 1, Textual support number: 3 OBS

manette d'inversion de poussée : terme uniformisé par les Comités d'uniformisation de la terminologie aéronautique (CUTA) - Maintenance et Opérations aériennes.  5, record 1, French, - manette%20d%27inversion%20de%20pouss%C3%A9e

Record 1,  Textual support,  Spanish

Record 2,  Textual support,  English

Record number: 2, Textual support number: 1 OBS

The distance from the start of the take-off roll to the point at which the aeroplane reaches 35 feet above the runway elevation, where failure of the critical engine is recognized at V1 [decision speed].  1, record 2, English, - one%2Dengine%2Dinoperative%20take%2Doff%20distance

Record 2,  Textual support,  French

Record number: 2, Textual support number: 1 OBS

Distance depuis le début du roulement au décollage jusqu'au point où l'avion atteint 35 pieds au-dessus de l'altitude de la piste, lorsqu'une panne du moteur le plus défavorable est détectée à la V1 [vitesse de décision].  1, record 2, French, - distance%20de%20d%C3%A9collage%20avec%20un%20moteur%20inop%C3%A9rant

Record 2,  Textual support,  Spanish

Record 3,  Textual support,  English

Record number: 3, Textual support number: 1 DEF

The distance from the start of the take-off roll to the point at which the aeroplane reaches 35 feet or, in the case of a small aeroplane, 50 feet, above the runway elevation.  1, record 3, English, - all%2Dengines%2Doperating%20take%2Doff%20distance

Record 3,  Textual support,  French

Record number: 3, Textual support number: 1 DEF

Distance depuis le début du roulement au décollage jusqu'au point où l'avion atteint 35 pieds ou, dans le cas d'un petit avion, 50 pieds, au-dessus de l'altitude de la piste.  1, record 3, French, - distance%20de%20d%C3%A9collage%20avec%20tous%20les%20moteurs%20op%C3%A9rants

Record 3,  Textual support,  Spanish

Record 4,  Textual support,  English

Record number: 4, Textual support number: 1 CONT

These conditions resulted in a tendency to roll erratically, and in conjunction with the extreme turbulence, caused loss of control and subsequent overloading of the wing to the point of failure.  1, record 4, English, - overloading%20of%20the%20wing

Record 4,  Textual support,  French

Record number: 4, Textual support number: 1 CONT

L'examen des débris a révélé que toutes les fractures sont attribuables à des surcharges instantanées ou à des déchirements.  1, record 4, French, - surcharge%20sur%20l%27aile

Record 4,  Textual support,  Spanish

Record 5,  Textual support,  English

Record number: 5, Textual support number: 1 CONT

When the accident aircraft reached the approximate point in space where the lead pair of aircraft had rejoined, it began a very fast negative G "barrel" roll to the right, completing a full roll in about 3. 5 seconds. Although the aircraft roll rate slowed at wings level, the negative G continued and shortly thereafter the roll to the right commenced again.  2, record 5, English, - negative%20g

Record number: 5, Textual support number: 1 OBS

A negative g force is a downward acceleration.  3, record 5, English, - negative%20g

Record number: 5, Textual support number: 2 OBS

Subject to acceleration in the vertical plane in the opposite-to-normal sense, e.g. aircraft in sustained inverted flight or in pushover from steep climb to steep dive; wings are bent "downwards" (relative to aircraft attitude) and pilot can experience "red-out." This condition is intermittently inevitable in severe turbulence but is normally prohibited for non-aerobatic aircraft.  4, record 5, English, - negative%20g

Record number: 5, Textual support number: 3 OBS

negative g: term officially approved by the Aeronautical Terminology Standardization Committee (ATSC) - Helicopters.  5, record 5, English, - negative%20g

Record 5,  Textual support,  French

Record number: 5, Textual support number: 1 CONT

Lorsque ce dernier a atteint le point dans l'espace où les deux avions de tête s'étaient rejoints, il a amorcé un tonneau barriqué très rapide à G négatif vers la droite, réalisant un tonneau complet en 3,5 secondes environ. La vitesse de roulis de l'avion a diminué lorsque les ailes sont revenues en palier, mais l'accélération négative a persisté et, peu après, l'avion s'est de nouveau engagé dans un roulis à droite.  2, record 5, French, - g%20n%C3%A9gatif

Record number: 5, Textual support number: 1 OBS

g négatif : terme uniformisé par les Comités d'uniformisation de la terminologie aéronautique (CUTA) - Hélicoptères et Maintenance.  3, record 5, French, - g%20n%C3%A9gatif

Record 5,  Textual support,  Spanish

Record 6,  Textual support,  English

Record number: 6, Textual support number: 1 CONT

The turn and slip indicator is a combination of two instruments; the turn needle and the ball. The needle is gyro operated to show rate of turn. The ball reacts to centrifugal force to indicate the quality of a turn.  3, record 6, English, - needle

Record number: 6, Textual support number: 2 CONT

The turn and slip indicator consists of two instruments combined. The turn indicator, above, consists of an electrically driven gyroscope connected to a pointer. It indicates rate, by magnitude of deflection, and direction, by direction of deflection of the pointer, of the turn. The slip indicator consists of a small ball in a curved tube. If the glider is not correctly aligned in the turn then the ball will roll out from the center point.  4, record 6, English, - needle

Record number: 6, Textual support number: 1 OBS

pointer: not to be confused with the "airplane pointer" on the heading indicator.  5, record 6, English, - needle

Record 6,  Textual support,  French

Record number: 6, Textual support number: 1 CONT

La bille et l'indicateur de virage. Ces deux instruments sont souvent réunis sur un même cadran. L'indicateur de virage prend souvent la forme d'une aiguille. D'où l'appellation globale que l'on utilise parfois «la bille-aiguille». La bille : Elle renseigne le pilote sur la symétrie du vol. Son principe est basé sur les forces d'inertie que subit l'avion en virage. L'aiguille : Elle indique le sens et le taux du virage. Elle est associée à un gyroscope dont la référence est la verticale. [...] Lorsque l'aiguille s'incline à droite, l'avion est en virage à droite (idem à gauche) [...] l'aiguille indique un taux de virage en degré par seconde [...] un virage de 360° s'effectuera en deux minutes.  2, record 6, French, - aiguille

Record number: 6, Textual support number: 1 OBS

aiguille : terme uniformisé par les Comités d'uniformisation de la terminologie aéronautique (CUTA) - Opérations aériennes et Maintenance.  3, record 6, French, - aiguille

Record 6,  Textual support,  Spanish

Record 7,  Textual support,  English

Record number: 7, Textual support number: 1 DEF

A boundary between grains in polycrystalline material [under the shape of] a discontinuity of the material structure having an effect on its fundamental properties.  2, record 7, English, - grain%20boundary

Record number: 7, Textual support number: 1 CONT

Pattern observed in convection at large aspect ratios; thick lines mark the place of sinking fluid; the texture is made of large grain with a slowly varying roll orientation bounded by smaller grains and lateral wall; notice the presence of line and point defects called grain boundaries and dislocations(after Pocheau and Croquette, 1984).  3, record 7, English, - grain%20boundary

Record 7,  Textual support,  French

Record number: 7, Textual support number: 1 DEF

Zone limitrophe entre les grains d'un matériau polycristallin se présentant sous la forme d'une discontinuité de la structure du matériau ayant un rôle à jouer dans l'établissement de ses propriétés de base.  2, record 7, French, - joint%20de%20grains

Record number: 7, Textual support number: 1 CONT

Texture observée en convection à grand facteur de forme et composée d'un large grain où l'orientation des rouleaux varie lentement, bordé de grains plus petits près des parois latérales; on note la présence de défauts linéaires et ponctuels respectivement appelés joints de grains et dislocations; les lignes épaisses marquent l'emplacement des courants descendants (d'après Pocheau et Croquette, 1984).  3, record 7, French, - joint%20de%20grains

Record 7,  Textual support,  Spanish

Record 8,  Textual support,  English

Record number: 8, Textual support number: 1 CONT

The local orbital reference system is defined at each point of the orbit by three unit vectors. These vectors are derived from the satellite position and velocity vectors : Vector L is colinear with position vector P(on the axis between the Earth's centre and the satellite). It defines the yaw axis. Vector T is perpendicular to the orbital plane(vector L, vector V). It defines the pitch axis. Vector R completes the set of orthogonal axes. It lies in the plane defined by Vectors L and V and defines the roll axis. It does not coincide exactly with the velocity vector due to the eccentricity of the orbit.  3, record 8, English, - roll%20axis

Record number: 8, Textual support number: 2 CONT

Spacecraft axes. The three orthogonal axes of rotation :roll, pitch and yaw. If the spacecraft has a recognisable longitudinal axis or a specified forward direction of flight, the axes are analogous to those of an aircraft, where the roll axis is the longitudinal axis; the pitch axis is in the plane of the wings; and the yaw axis is the "vertical" axis, orthogonal to both the roll and pitch axes. The axes are mutually perpendicular, with an "origin" at the vehicle's centre of mass. For a winged spacecraft such as a Space Shuttle, the similarity with an aircraft is obvious. For expendable launch vehicles the roll axis is the axis which is vertical at launch and the other axes are more-or-less arbitrarily assigned since the vehicle rotates about the roll axis in flight.... The axes of a cylindrical spacecraft(e. g. Apollo, Suyuz, etc.) are similar to those of an ELV [Expendable Launch Vehicle] at launch, but one orbit assume the axis-definition of an aircraft(i. e. defined relative to the pilot's seat). The axes of a satellite mirror those of an aircraft "flying along the orbital arc" : the roll axis is aligned with the direction of travel; the yaw axis passes through the sub-satellite point; and the pitch axis is orthogonal to the other two. For a satellite in an equatorial orbit, the pitch axis is aligned approximately with the Earth's spin axis. The pitch axis is also the spin axis for the spin-stabilised satellite.  4, record 8, English, - roll%20axis

Record number: 8, Textual support number: 1 OBS

In the compilation of engineering drawings the three orthogonal axes are often labelled in Cartesian fashion : x=roll, y=pitch, z=yaw. For the three-axis stabilised spacecraft, the x-axis and y-axis are otherwise known as the east-west and north-south axes, respectively; the z-axis passes through the sub-satellite point. This leads to the definition of the box-shaped satellite's faces as follows : the "plus-x face" faces east; the "minus-x face" faces west; +y faces south;-y faces north; +z is the Earth-pointing face; and-z is the "anti-Earth face. "  4, record 8, English, - roll%20axis

Record number: 8, Textual support number: 2 OBS

roll axis; axis of roll: terms officially approved by the International Space Station official approval Group (ISSOAG) and by the RADARSAT-2 Terminology Approval Group (RTAG).  5, record 8, English, - roll%20axis

Record 8,  Textual support,  French

Record number: 8, Textual support number: 1 CONT

Le repère orbital local est défini en chaque point de l'orbite par les trois vecteurs unitaires. Ces vecteurs sont construits à partir du vecteur position et du vecteur vitesse du satellite : le vecteur L est colinéaire au vecteur position P (sur l'axe centre Terre, satellite). Il définit l'axe de lacet. Le vecteur T est perpendiculaire au plan de l'orbite (vecteur L, vecteur V). Il définit l'axe de tangage. Le vecteur R complète le trièdre. Il appartient au plan (vecteur L, vecteur V) et définit l'axe de roulis. Il ne coïncide pas exactement avec le vecteur vitesse à cause de l'excentricité de l'orbite.  1, record 8, French, - axe%20de%20roulis

Record number: 8, Textual support number: 1 OBS

axe de roulis : terme uniformisé par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI) et par le Groupe de travail de la terminologie de RADARSAT-2 (GTTR).  2, record 8, French, - axe%20de%20roulis

Record 8,  Textual support,  Spanish

Record 9,  Textual support,  English

Record number: 9, Textual support number: 1 CONT

The local orbital reference system is defined at each point of the orbit by three unit vectors. These vectors are derived from the satellite position and velocity vectors : Vector L is colinear with position vector P(on the axis between the Earth's centre and the satellite). It defines the yaw axis. Vector T is perpendicular to the orbital plane(vector L, vector V). It defines the pitch axis. Vector R completes the set of orthogonal axes. It lies in the plane defined by Vectors L and V and defines the roll axis. It does not coincide exactly with the velocity vector due to the eccentricity of the orbit.  2, record 9, English, - pitch%20axis

Record number: 9, Textual support number: 2 CONT

Spacecraft axes. The three orthogonal axes of rotation :roll, pitch and yaw. If the spacecraft has a recognisable longitudinal axis or a specified forward direction of flight, the axes are analogous to those of an aircraft, where the roll axis is the longitudinal axis; the pitch axis is in the plane of the wings; and the yaw axis is the "vertical" axis, orthogonal to both the roll and pitch axes. The axes are mutually perpendicular, with an "origin" at the vehicle's centre of mass. For a winged spacecraft such as a Space Shuttle, the similarity with an aircraft is obvious. For expendable launch vehicles the roll axis is the axis which is vertical at launch and the other axes are more-or-less arbitrarily assigned since the vehicle rotates about the roll axis in flight.... The axes of a cylindrical spacecraft(e. g. Apollo, Suyuz, etc.) are similar to those of an ELV [Expendable Launch Vehicle] at launch, but one orbit assume the axis-definition of an aircraft(i. e. defined relative to the pilot's seat). The axes of a satellite mirror those of an aircraft "flying along the orbital arc" : the roll axis is aligned with the direction of travel; the yaw axis passes through the sub-satellite point; and the pitch axis is orthogonal to the other two. For a satellite in an equatorial orbit, the pitch axis is aligned approximately with the Earth's spin axis. The pitch axis is also the spin axis for the spin-stabilised satellite.  3, record 9, English, - pitch%20axis

Record number: 9, Textual support number: 1 OBS

In the compilation of engineering drawings the three orthogonal axes are often labelled in Cartesian fashion : x=roll, y=pitch, z=yaw. For the three-axis stabilised spacecraft, the x-axis and y-axis are otherwise known as the east-west and north-south axes, respectively; the z-axis passes through the sub-satellite point. This leads to the definition of the box-shaped satellite's faces as follows : the "plus-x face" faces east; the "minus-x face" faces west; +y faces south;-y faces north; +z is the Earth-pointing face; and-z is the "anti-Earth face. "  3, record 9, English, - pitch%20axis

Record number: 9, Textual support number: 2 OBS

pitch axis: term officially approved by the International Space Station official approval Group (ISSOAG) and by the RADARSAT-2 Terminology Approval Group (RTAG).  4, record 9, English, - pitch%20axis

Record 9,  Textual support,  French

Record number: 9, Textual support number: 1 CONT

Le repère orbital local est défini en chaque point de l'orbite par les trois vecteurs unitaires. Ces vecteurs sont construits à partir du vecteur position et du vecteur vitesse du satellite : Le vecteur L est colinéaire au vecteur position P (sur l'axe centre Terre, satellite). Il définit l'axe de lacet. Le vecteur T est perpendiculaire au plan de l'orbite (vecteur L, vecteur V). Il définit l'axe de tangage. Le vecteur R complète le trièdre. Il appartient au plan (vecteur L, vecteur V) et définit l'axe de roulis. Il ne coïncide pas exactement avec le vecteur vitesse à cause de l'excentricité de l'orbite.  2, record 9, French, - axe%20de%20tangage

Record number: 9, Textual support number: 1 OBS

axe de tangage : terme uniformisé par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI) et par le Groupe de travail de la terminologie de RADARSAT-2.  3, record 9, French, - axe%20de%20tangage

Record 9,  Textual support,  Spanish

Record 10,  Textual support,  English

Record number: 10, Textual support number: 1 DEF

The rotation of a vehicle about its vertical (Z) axis, i.e. movement in azimuth.  2, record 10, English, - yaw

Record number: 10, Textual support number: 1 CONT

The local orbital reference system is defined at each point of the orbit by three unit vectors. These vectors are derived from the satellite position and velocity vectors : vector L is colinear with position vector P(on the axis between the Earth's centre and the satellite). It defines the yaw axis. Vector T is perpendicular to the orbital plane(vector L, vector V). It defines the pitch axis. Vector R completes the set of orthogonal axes. It lies in the plane defined by vectors L and V and defines the roll axis. It does not coincide exactly with the velocity vector due to the eccentricity of the orbit.  3, record 10, English, - yaw

Record number: 10, Textual support number: 1 OBS

yaw: term officially approved by the International Space Station Official Approval Group (ISSOAG) and by the RADARSAT-2 Terminology Approval Group (RTAG).  4, record 10, English, - yaw

Record 10,  Textual support,  French

Record number: 10, Textual support number: 1 DEF

Mouvement d'un corps autour d'un axe perpendiculaire aux axes de roulis et de tangage.  2, record 10, French, - lacet

Record number: 10, Textual support number: 1 CONT

Le repère orbital local est défini en chaque point de l'orbite par les trois vecteurs unitaires. Ces vecteurs sont construits à partir du vecteur position et du vecteur vitesse du satellite : Le vecteur L est colinéaire au vecteur position P (sur l'axe centre Terre, satellite). Il définit l'axe de lacet. Le vecteur T est perpendiculaire au plan de l'orbite (vecteur L, vecteur V). Il définit l'axe de tangage. Le vecteur R complète le trièdre. Il appartient au plan (vecteur L, vecteur V) et définit l'axe de roulis. Il ne coïncide pas exactement avec le vecteur vitesse à cause de l'excentricité de l'orbite.  3, record 10, French, - lacet

Record number: 10, Textual support number: 1 OBS

lacet : terme uniformisé par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI) et par le Groupe de travail de la terminologie de RADARSAT-2 (GTTR).  4, record 10, French, - lacet

Record 10,  Textual support,  Spanish

Record 11,  Textual support,  English

Record number: 11, Textual support number: 1 CONT

The ISS attitude will vary between +15 degrees and-15 degrees for each roll and yaw axis of LVLH [Local Vertical/Local Horizontal] and between +15 degrees to-20 degrees for the pitch axis... At any point on the ISS non-articulated portion, which means the portion excluding rotating elements such as photovoltaic arrays and Thermal Control System(TCS) radiators, the ISS will provide estimates of the ISS LVLH attitude to an accuracy of 3 degrees per axis(3 sigma) and inertial rates to an accuracy of 0. 01 degrees per second per axis(3 sigma). When controlling to the TEA [Torque Equilibrium Attitude] with non-propulsive effectors, the ISS will maintain attitude stability to 3. 5 degrees per axis per orbit.  2, record 11, English, - ISS%20attitude

Record number: 11, Textual support number: 1 OBS

ISS attitude: term officially approved by the International Space Station official approval Group (ISSOAG).  3, record 11, English, - ISS%20attitude

Record 11,  Textual support,  French

Record number: 11, Textual support number: 1 OBS

attitude de la Station spatiale : terme uniformisé par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI).  2, record 11, French, - attitude%20de%20la%20Station%20spatiale

Record 11,  Textual support,  Spanish

Record 12,  Textual support,  English

Record number: 12, Textual support number: 1 CONT

In the last lesson we learned to turn using the ailerons to roll the aeroplane into a banked attitude, and the elevator to raise the nose slightly to maintain the required lift by increasing the wings’ angle of attack. But the rudder plays an important part here as well. As we roll into the turn adverse yaw will try to point the nose in the wrong direction and so we will need to apply rudder in the direction of the turn as we roll. Once we are established in the turn the design of modern ailerons is such that adverse yaw is greatly reduced and we may not need to continue to apply rudder to keep the ball in the middle.  1, record 12, English, - apply%20rudder

Record number: 12, Textual support number: 1 PHR

Apply right, left rudder.  2, record 12, English, - apply%20rudder

Record 12,  Textual support,  French

Record number: 12, Textual support number: 1 PHR

Donner du pied à gauche, à droite.  1, record 12, French, - donner%20du%20pied

Record 12,  Textual support,  Spanish

Record 13,  Textual support,  English

Record number: 13, Textual support number: 1 CONT

Internet Explorer, a web browser that allows users to access the Internet, allows developers to construct high-quality content and allows administrators to roll out multiple access point with minimal administration.  3, record 13, English, - multiple%20access%20point

Record 13,  Textual support,  French

Record number: 13, Textual support number: 1 CONT

Des points d'accès multiples peuvent également être utilisés pour équilibrer la charge. En utilisant plusieurs points d'accès, vous pouvez fractionner le trafic réseau sur deux cellules ou plus, plutôt que d'avoir une seule cellule congestionnée par l'intégralité du trafic.  1, record 13, French, - point%20d%27acc%C3%A8s%20multiple

Record 13,  Textual support,  Spanish

Record 14,  Textual support,  English

Record number: 14, Textual support number: 1 OBS

The distance from the start of the take-off roll to the point midway between the lift-off point and the point at which the aeroplane reaches 35 feet above the runway elevation, where failure of the critical engine is recognized at V1.  1, record 14, English, - one%2Dengine%2Dinoperative%20take%2Doff%20run

Record 14,  Textual support,  French

Record number: 14, Textual support number: 1 OBS

Roulement au décollage avec un moteur inopérant ou 115 pour cent du roulement au décollage avec tous les moteurs opérants, selon la plus élevée de ces deux valeurs.  1, record 14, French, - roulement%20au%20d%C3%A9collage%20avec%20un%20moteur%20inop%C3%A9rant

Record number: 14, Textual support number: 2 OBS

Source : Règlement de l'aviation, Partie 1.  1, record 14, French, - roulement%20au%20d%C3%A9collage%20avec%20un%20moteur%20inop%C3%A9rant

Record 14,  Textual support,  Spanish

Record 15,  Textual support,  English

Record number: 15, Textual support number: 1 DEF

Distance from the start of the take-off roll to the point midway between the lift-off point and the point at which the aeroplane reaches 35 feet or, in the case of a small aircraft that is an aeroplane, 50 feet above the runway elevation.  1, record 15, English, - all%2Dengines%2Doperating%20take%2Doff%20run

Record 15,  Textual support,  French

Record number: 15, Textual support number: 1 DEF

Distance depuis le début du roulement au décollage jusqu'au point situé à mi-chemin entre le point de décollage et le point où l'avion atteint 35 pieds ou, dans le cas d'un petit aéronef qui est un avion, 50 pieds, au-dessus de l'altitude de la piste.  1, record 15, French, - roulement%20au%20d%C3%A9collage%20avec%20tous%20les%20moteurs%20op%C3%A9rants

Record number: 15, Textual support number: 1 OBS

Source(s) : Règlement de l'aviation canadien - Partie I.  1, record 15, French, - roulement%20au%20d%C3%A9collage%20avec%20tous%20les%20moteurs%20op%C3%A9rants

Record 15,  Textual support,  Spanish

Record 16,  Textual support,  English

Record number: 16, Textual support number: 1 CONT

The unique results achieved with supercalendering are due to the intermediate fibrous rolls(sometimes referred to as bowls or filled rolls) which possess elastic or plastic properties. With the application of load on the nips, the metal rolls cause a depression or deformation on the fibrous rolls at the point of contact, and the deformation spreads out on either side of the nip(Figure 18-28). When rotated, this spread area will creep because of the constant effort of the material to return to its normal shape. This flow causes a relative motion of the filled roll surface against the metal roll surface, thus producing rolling friction, which helps to give the polishing and smoothing effects. The intensity of action is governed by the amount of plastic flow and by the nip contact pressure.  2, record 16, English, - filled%20roll

Record 16,  Textual support,  French

Record number: 16, Textual support number: 1 CONT

Satinage. La calandre à satiner, ou supercalandre (gloss calender, supercalender), et la calandre à friction (friction calender, friction glazing calender) sont des dispositifs hors machine (off-machine) qui donnent au papier un aspect satiné ou surglacé par polissage énergique entre des rouleaux de métal et des rouleaux de fibres comprimées (filled roll, compressed fibre roll, paper roll), de coton ou de papier, et rectifiés au tour.  1, record 16, French, - rouleau%20de%20fibres%20comprim%C3%A9es

Record 16,  Textual support,  Spanish

Record 17,  Textual support,  English

Record number: 17, Textual support number: 1 CONT

Pattern observed in convection at large aspect ratios; thick lines mark the place of sinking fluid; the texture is made of large grain with a slowly varying roll orientation bounded by smaller grains and lateral wall; notice the presence of line and point defects called grain boundaries and dislocations(after Pocheau and Croquette, 1984).  1, record 17, English, - dislocation

Record 17,  Textual support,  French

Record number: 17, Textual support number: 1 CONT

Texture observée en convection à grand facteur de forme et composée d'un large grain où l'orientation des rouleaux varie lentement, bordé de grains plus petits près des parois latérales; on note la présence de défauts linéaires et ponctuels respectivement appelés joints de grains et dislocations; les lignes épaisses marquent l'emplacement des courants descendants (d'après Pocheau et Croquette, 1984).  1, record 17, French, - dislocation

Record 17,  Textual support,  Spanish

Record 18,  Textual support,  French

Record 18,  Textual support,  Spanish

Record 19,  Textual support,  English

Record number: 19, Textual support number: 1 DEF

A process for compacting the paper web in the plane of the paper and imparting a high degree of stretchability by passing the web between a roll and, for example, an endless rubber blanket. The blanket is extended immediately before the point of contact with the web and allowed to return to its normal state during the passage of the web through the space between the roll and the rubber blanket.  1, record 19, English, - micro%2Dcreping

Record number: 19, Textual support number: 1 OBS

This should not be confused with creping.  1, record 19, English, - micro%2Dcreping

Record number: 19, Textual support number: 2 OBS

This term has been standardized by ISO.  2, record 19, English, - micro%2Dcreping

Record 19,  Textual support,  French

Record number: 19, Textual support number: 1 DEF

Opération consistant à rétrécir la bande de papier dans le plan du papier et à lui donner une extensibilité élevée en la faisant passer entre un rouleau et, par exemple, un feutre caoutchouté sans fin. Celui-ci est étiré immédiatement avant son point de contact avec la bande et on le laisse revenir à son état normal pendant le passage de la bande entre le rouleau et le feutre caoutchouté.  2, record 19, French, - microcr%C3%AApage

Record number: 19, Textual support number: 1 OBS

A ne pas confondre avec le crêpage.  2, record 19, French, - microcr%C3%AApage

Record number: 19, Textual support number: 2 OBS

Terme normalisé par l'ISO et l'AFNOR.  3, record 19, French, - microcr%C3%AApage

Record 19,  Textual support,  Spanish

Record 20,  Textual support,  English

Record number: 20, Textual support number: 1 CONT

Flyover Noise Reference Point : the point on the extended centre line of the runway 1500 m(5000 ft) from the start of the take-off roll(...)  1, record 20, English, - flyover%20noise%20reference%20point

Record 20,  Textual support,  French

Record number: 20, Textual support number: 1 CONT

Point de référence du bruit de survol au décollage: point situé sur le prolongement de l'axe de piste à 1500 m (5000 pieds) du début du roulement au décollage (...)  1, record 20, French, - point%20de%20r%C3%A9f%C3%A9rence%20du%20bruit%20de%20survol%20au%20d%C3%A9collage

Record 20,  Textual support,  Spanish

Record 21,  Textual support,  French

Record 21,  Textual support,  Spanish

Record 22,  Textual support,  English

Record number: 22, Textual support number: 1 OBS

This point in "false breathing" should be emphasized : the head should never be thrown from side to side but moves gradually in time with the natural roll of the body.  1, record 22, English, - false%20breathing

Record 22,  Textual support,  French

Record number: 22, Textual support number: 1 OBS

Un point à souligner dans la "fausse respiration": la tête ne doit jamais être secouée d'un côté à l'autre, elle doit plutôt se mouvoir graduellement d'après le roulement naturel du corps.  1, record 22, French, - fausse%20respiration

Record 22,  Textual support,  Spanish