The present invention relates to an aircraft gas turbine thrust-reversing device with an engine having an engine cowling whose rear area can be moved in the axial direction of the engine from a closed forward-thrust position into a rearward moved thrust-reversing position in which a free, substantially annular space to a front and fixed area of the engine cowling is present, where on the engine cowling guide rails are arranged, inside which mounting elements can be moved by means of rolling or sliding elements, with which mounting elements the rear area of the engine cowling is mounted, characterized in that the guide rails have an oval and C-shaped cross-section, provided on a longitudinal side with a slot-like opening, and are mounted using mounting projections arranged centrally and opposite to one another and designed in one piece with the C-shaped cross-section.
FLUGGASTURBINENSCHUBUMKEHRVORRICHTUNG MIT FÜHRUNGSSCHIENE
AVIATION GAS TURBINE THRUST REVERSING DEVICE WITH GUIDE RAIL
DISPOSITIF D'INVERSION DE POUSSEE DE TURBINE A GAZ VOLATILE EQUIPE D'UN RAIL DE GUIDAGE
2018-05-09
Patent
Electronic Resource
German
Verfahren zur Herstellung einer Führungsschiene sowie Führungsschiene
European Patent Office | 2021
|VERFAHREN ZUR HERSTELLUNG EINER FÜHRUNGSSCHIENE SOWIE FÜHRUNGSSCHIENE
European Patent Office | 2021
|