The amphibious STOL aircraft has wings comprising outer and inner segments. The inner segments of the wings are attached to the fuselage of the aircraft while the outer wing segments are detachable and attachable to the inner segments. The outer segments can also be folded relative to the inner segments from an inoperative position adjacent to the side walls of the fuselage to an operative position in which the outer wing segments extend outward from the inner segments and the two segments combine to support the aircraft when airborne.
AMPHIBIOUS STOL AIRCRAFT
AERONEF STOL AMPHIBIE
2018-04-19
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
V/STOL Aircraft for Amphibious Warfare
NTIS | 1964
|The Model K-I6b V/STOL Research Amphibious Aircraft
NTIS | 1967
|NTRS | 1988