Thrust reverser cascade element of an aircraft gas turbine
Research output: Intellectual property › Patent application/Patent
Contributors
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.
| Original language | English |
|---|---|
| IPC (International Patent Classification) | F02K 1/54 |
| Patent number | US 10,113,507 |
| Filing date | 21 May 2015 |
| Country/Territory | United States of America |
| Priority date | 26 May 2014 |
| Priority number | DE102014210025 |
| Publication status | Published - 30 Oct 2018 |
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