COMPOSITE FASTENER
Assignee
Filed
Apr 26, 1989
Granted
May 24, 1994
Location
FAIRFIELD OH US
Abstract
A composite fastener member, in one form, having integral head and shank portions is defined by a plurality of superimposed composite fiber reinforced sheets spirally wound about a longitudinal axis. A plurality of fastener members, oppositely disposed within an opening in an article, define a fastener especially useful in joining lightweight composite structures such as aircraft or aircraft engine components. In another form, the ends of a single spirally wound composite fastener member are splayed to fasten a plurality of sheets.
Source: Google Patents
35 USC §181 Secrecy Order
Imposed
Sep 13, 1988
Rescinded
Nov 9, 1993
Duration
5 years, 1 month
Inventor
- 1GUY C. MURPHY
Record Details
- Patent number
- US 5314282
- Application
- 07342684
- Aerospace match
- Yes
- Dataset source
- 35 USC §181 SO records
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