Aircraft radome and integral attaching structure

Details Aircraft radome and integral attaching structure Aircraft radome and integral attaching structure

1995-09-26

1998-10-13

Barefoot, Galen L.

Aeronautics and astronautics

Aircraft structure

Fuselage and body construction

244121, 244131, B64C 136

Patent

active

058200770

ABSTRACT:
A radome structure having an integrally attached attaching structure for attachment to an aircraft is disclosed, the attaching structure being affixed to a rearward portion of the radome. The attaching structure preferably comprises, at least in part, a core material which is capable of strengthening the attaching structure, thereby making it stronger than the material from which the radome shell is fabricated.

REFERENCES:
patent: 3545146 (1970-12-01), Kerr
patent: 3616140 (1971-10-01), Copeland et al.
patent: 3757698 (1973-09-01), Jacobson
patent: 3978256 (1976-08-01), James
patent: 4011819 (1977-03-01), Kessler
patent: 4086378 (1978-04-01), Kan et al.
patent: 4344995 (1982-08-01), Hammer
patent: 4520364 (1985-05-01), Perry
patent: 4581615 (1986-04-01), Levy
patent: 5103239 (1992-04-01), Verzemnieks et al.
patent: 5129990 (1992-07-01), Binnie, Jr. et al.
patent: 5223067 (1993-06-01), Hamamolo
patent: 5460673 (1995-10-01), Cahuzac

Affiliated with

Also associated with

Rating

Aircraft radome and integral attaching structure does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Aircraft radome and integral attaching structure, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Aircraft radome and integral attaching structure will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-305584