FLEXIBLE HINGE ASSEMBLY FOR AIRCRAFT INTERIOR COMPONENTS AND THE LIKE
Number of patents in Portfolio can not be more than 2000
United States of America Patent
Stats
-
N/A
Issued Date -
Oct 4, 2018
app pub date -
Apr 3, 2018
filing date -
Apr 3, 2018
priority date (Note) -
Published
status (Latency Note)
Importance
Abstract
A flexible hinge assembly for aircraft interior components and the like, including: a first structural component, wherein the first structural component includes a core material and one or more skin layers coupled to the core material; a second structural component, wherein the second structural component includes a core material and one or more skin layers coupled to the core material; wherein the one or more skin layers of the first structural component and the one or more skin layers of the second structural component are one or more of coupled together and integrally formed; and a flexure disposed between the first structural component and the second structural component, wherein the flexure is formed by the coupled together and/or integrally formed skin layers.
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