Thrust reverser cascade element of an aircraft gas turbine

Publikation: Geistiges Eigentum › Patentanmeldung/Patent

Beitragende

Abstract

The present invention relates to a thrust reverser cascade element of an aircraft gas turbine with a rigid frame and with several thrust reverser profiles mounted in the frame, wherein the thrust reverser cascade element is made of fiber-plastic composite.

Details

The present invention relates to a thrust reverser cascade element of an aircraft gas turbine with a rigid frame and with several thrust reverser profiles mounted in the frame, wherein the thrust reverser cascade element is made of fiber-plastic composite.
OriginalspracheEnglisch
IPC (Internationale Patentklassifikation)F02K 1/54
VeröffentlichungsnummerUS 10,113,507
Anmeldedatum21 Mai 2015
Land/GebietUSA/Vereinigte Staaten
Prioritätsdatum26 Mai 2014
PrioritätsnummerDE102014210025
PublikationsstatusVeröffentlicht - 30 Okt. 2018
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