Integrated connector/airtube for a turbomachine's combustion chamber walls
Number of patents in Portfolio can not be more than 2000
United States of America Patent
Stats
-
Sep 8, 1992
Grant Date -
N/A
app pub date -
Dec 24, 1990
filing date -
Dec 24, 1990
priority date (Note) -
Expired
status (Latency Note)
Importance
Abstract
A structural connector (40) is disclosed for joining together the inner (30) and outer (22) walls of a combustion chamber (20) of a turbomachine (10), such as a gas turbine engine. The structural connector (40) also provides for cooling or combustion airflow between the combustion chamber (20) and a surrounding atmosphere (12). An outer end (42) of the connector (40) is releasably affixed to the outer wall (22) of the combustion chamber (20) while an inner end (48) is allowed limited lateral and axial displacement relative to the inner wall (30) of the combustion chamber (20), thereby accommodating differential expansion and contraction of the walls (30, 22) relative to each other.
First Claim
Family
International Classification(s)
- [Classification Symbol]
- [Patents Count]
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