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.
| Originalsprache | Englisch |
|---|---|
| IPC (Internationale Patentklassifikation) | F02K 1/54 |
| Veröffentlichungsnummer | US 10,113,507 |
| Anmeldedatum | 21 Mai 2015 |
| Land/Gebiet | USA/Vereinigte Staaten |
| Prioritätsdatum | 26 Mai 2014 |
| Prioritätsnummer | DE102014210025 |
| Publikationsstatus | Veröffentlicht - 30 Okt. 2018 |
No renderer: customAssociatesEventsRenderPortal,dk.atira.pure.api.shared.model.researchoutput.Patent