METHOD OF ASSEMBLING PARTS WITH DIFFERENT COEFFICIENTS OF THERMAL EXPANSION
Number of patents in Portfolio can not be more than 2000
United States of America Patent
Stats
-
N/A
Issued Date -
Mar 27, 2025
app pub date -
Sep 25, 2023
filing date -
Sep 25, 2023
priority date (Note) -
Published
status (Latency Note)
Importance
Abstract
A method of assembling parts of an aircraft engine, the method includes: forming, at a first temperature, a pre-assembly of a first part of the aircraft engine and a second part of the aircraft engine by aligning the first part and the second part such as to be engageable within one another, the second part having a coefficient of thermal expansion that is greater than a coefficient of thermal expansion of the first part; heating the pre-assembly to a second temperature greater than the first temperature to expand the second part relative to the first part; and compressing the pre-assembly until the first part is inserted into the second part to create a contact interface between the first part and the second part.
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