Connector arrangement for detachable fastening of airplane wings

Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils

Patent

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Details

244120, 244131, A63H 2702, B64C 126

Patent

active

039356647

ABSTRACT:
A connector arrangement for the detachable fastening of airplane wings to the fuselages of model airplanes. The arrangement utilizes generally tongue and groove-like T-shaped connector elements, which are connected to each other within the fuselage, or to a constructional element located therein, by a rubber band under pretensioning. These tongue and groove-like connector elements are adapted to be swivelled or rotated in their extended positions, and may then come into contact with an intermediate member or the outer surface of the fuselage, and are maintained in their rotated positions. In this position, the tongue and groove-like connector element, upon attachment of the airplane wing, may be positioned in a cutout formed in the end surface of the wing.

REFERENCES:
patent: 6451 (1849-05-01), Brooke
patent: 2542042 (1951-02-01), McCoy
patent: 2915762 (1959-12-01), Kivela
patent: 3017137 (1962-01-01), Helmke et al.
patent: 3177612 (1965-04-01), Giossi
patent: 3640491 (1972-02-01), Harrison

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