Ejection cone having a flexible aerodynamic attachment
Number of patents in Portfolio can not be more than 2000
United States of America Patent
Stats
-
Nov 21, 2023
Grant Date -
Oct 27, 2022
app pub date -
Sep 2, 2020
filing date -
Sep 5, 2019
priority date (Note) -
In Force
status (Latency Note)
Importance
Abstract
The invention relates to an assembly for an aircraft turbomachine, comprising a central element (1) for the ejection of gas, and a connecting flange (9) interposed between, upstream, a gas outlet (22a) made of metal for a turbomachine, and, at the downstream end, the central element (1). The connecting flange comprises an annular portion (9a) and flexible tabs (11) having axially:
- a first end (111a) where the tab is connected to the said annular portion, anda second free end (111b), projecting radially inwardly with respect to the first end and to which said tab is attached with the central element (1).
First Claim
Family
International Classification(s)
Cited Art Landscape
Patent Citation Ranking
Recipient Email Address
Recipient Email Address
Comment
Recipient Email Address
Add to Portfolio(s)
To add this patent to one, or more, of your portfolios, simply click the add button.
This Patent is in these Portfolios:
Add to additional portfolios:
Last Refreshed On:
Changes done successfully