NACELLE WITH THRUST REVERSER
A nacelle for an aircraft having a thrust reverser including a translating cowl and a blocking panel. The blocking panel is connected by a pivot connection and is connected to the translating cowl by a sliding connection including an engagement member slidingly engaged in a track, the track having a...
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Format | Patent |
Language | English French |
Published |
31.01.2019
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Subjects | |
Online Access | Get full text |
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Abstract | A nacelle for an aircraft having a thrust reverser including a translating cowl and a blocking panel. The blocking panel is connected by a pivot connection and is connected to the translating cowl by a sliding connection including an engagement member slidingly engaged in a track, the track having a first portion parallel to the longitudinal axis of the outer casing and a second portion non-parallel to the longitudinal axis. Motion of the translating cowl along the longitudinal axis slides the engagement member within the track, and is performed without moving the blocking panel when the engagement member is within the first portion of the track. The motion of the translating cowl causes the blocking panel to pivot about the pivot connection when the engagement member is within the second portion of the track.
La présente invention concerne une nacelle pour aéronef comprenant un inverseur de poussée comprenant un capot de translation et un panneau de blocage. Le panneau de blocage est raccordé par un raccordement pivot et est raccordé au capot de translation par un raccordement coulissant comprenant un élément de mise en prise mis en prise de manière coulissante dans une piste, la piste ayant une première partie parallèle à l'axe longitudinal du boîtier externe et une seconde partie non parallèle à l'axe longitudinal. Le mouvement du capot de translation le long de l'axe longitudinal fait coulisser l'élément de mise en prise à l'intérieur de la piste, et est réalisé sans déplacer le panneau de blocage lorsque l'élément de mise en prise se trouve à l'intérieur de la première partie de la piste. Le mouvement du capot de translation amène le panneau de blocage à pivoter autour du raccordement pivot lorsque l'élément de mise en prise se trouve à l'intérieur de la seconde partie de la piste. |
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AbstractList | A nacelle for an aircraft having a thrust reverser including a translating cowl and a blocking panel. The blocking panel is connected by a pivot connection and is connected to the translating cowl by a sliding connection including an engagement member slidingly engaged in a track, the track having a first portion parallel to the longitudinal axis of the outer casing and a second portion non-parallel to the longitudinal axis. Motion of the translating cowl along the longitudinal axis slides the engagement member within the track, and is performed without moving the blocking panel when the engagement member is within the first portion of the track. The motion of the translating cowl causes the blocking panel to pivot about the pivot connection when the engagement member is within the second portion of the track.
La présente invention concerne une nacelle pour aéronef comprenant un inverseur de poussée comprenant un capot de translation et un panneau de blocage. Le panneau de blocage est raccordé par un raccordement pivot et est raccordé au capot de translation par un raccordement coulissant comprenant un élément de mise en prise mis en prise de manière coulissante dans une piste, la piste ayant une première partie parallèle à l'axe longitudinal du boîtier externe et une seconde partie non parallèle à l'axe longitudinal. Le mouvement du capot de translation le long de l'axe longitudinal fait coulisser l'élément de mise en prise à l'intérieur de la piste, et est réalisé sans déplacer le panneau de blocage lorsque l'élément de mise en prise se trouve à l'intérieur de la première partie de la piste. Le mouvement du capot de translation amène le panneau de blocage à pivoter autour du raccordement pivot lorsque l'élément de mise en prise se trouve à l'intérieur de la seconde partie de la piste. |
Author | TWEEDIE, Alan |
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DocumentTitleAlternate | NACELLE COMPRENANT UN INVERSEUR DE POUSSÉE |
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Notes | Application Number: WO2018GB52089 |
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PublicationYear | 2019 |
RelatedCompanies | SHORT BROTHERS PLC |
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Snippet | A nacelle for an aircraft having a thrust reverser including a translating cowl and a blocking panel. The blocking panel is connected by a pivot connection and... |
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SubjectTerms | BLASTING COMBUSTION ENGINES HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS |
Title | NACELLE WITH THRUST REVERSER |
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