Aeronautics and astronautics – Aircraft control – Vertical fins
Patent
1985-09-05
1987-09-15
Barefoot, Galen
Aeronautics and astronautics
Aircraft control
Vertical fins
244 324, 244121, 244124, 244131, 416224, B64C 328, B64C 336
Patent
active
046934359
ABSTRACT:
A high strength, lightweight, heat resistant control surface for a high speed aircraft such as a missile or the like, comprises a heat resistant lightweight composite such as a graphite reinforced polyimide having a leading edge portion comprising a heat resistant metal such as Inconel. The leading edge portion includes a web fixing the leading edge portion to the composite by bonded attachment thereto at a location remote from the leading edge and adjacent surfaces thereby providing delayed exposure of the bond to leading edge heat buildup during flight.
REFERENCES:
patent: 1674674 (1928-06-01), Wooster
patent: 2734586 (1956-02-01), Wright et al.
patent: 3028128 (1962-04-01), Friedrich
patent: 3114319 (1963-12-01), Smith
patent: 3114524 (1963-12-01), Conn, Jr. et al.
patent: 3145000 (1964-08-01), Mackie
patent: 3174711 (1965-03-01), Sullivan
patent: 3430898 (1969-03-01), Parechanian et al.
patent: 3712566 (1973-01-01), Branen et al.
patent: 3808833 (1974-04-01), Allen et al.
patent: 3890749 (1975-06-01), Gunther
patent: 3950115 (1976-04-01), Euler
patent: 4006999 (1977-02-01), Branfley et al.
patent: 4228976 (1980-10-01), Eiselbrecher
Percival William A.
Stoltze Leon
Barefoot Galen
Swiatocha John
United Technologies Corporation
LandOfFree
High speed aircraft control surface does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with High speed aircraft control surface, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and High speed aircraft control surface will most certainly appreciate the feedback.
Profile ID: LFUS-PAI-O-1379774