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FR-3163407-B1 - Thrust reverser comprising multiple deployable deflection membranes featuring an assembly providing improved performance

FR3163407B1FR 3163407 B1FR3163407 B1FR 3163407B1FR-3163407-B1

Abstract

The invention relates to a thrust reverser for an aircraft propulsion system, comprising a first and a second deployable deflection diaphragm (32), and a diaphragm support frame (66) comprising a first upstream end (66a) and a second downstream end (66b), each of the first and second deployable deflection diaphragms (32) defining an air inlet opening (110) in the diaphragm, delimited by an opening contour (112) comprising a first and a second lateral portion of the opening contour (112a, 112a'), the first lateral portion of the opening contour (112a) of the first diaphragm and the second lateral portion of the opening contour (112a') of the second diaphragm being engaged on the frame (66) by means of rails (114a, 114a'). Figure for the abstract: Fig. 6

Inventors

  • LE BOULICAUT LOÏC HERVÉ ANDRÉ
  • JOURDAN FABIEN
  • VALLEROY LAURENT GEORGES
  • CONTE FRANÇOIS
  • STADLER DIDIER

Assignees

  • SAFRAN NACELLES

Dates

Publication Date
20260501
Application Date
20240613
Priority Date
20240613