Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils
Patent
1985-08-09
1987-01-13
Blix, Trygve M.
Aeronautics and astronautics
Aircraft sustentation
Sustaining airfoils
244 324, 244 327, B64C 356
Patent
active
046358811
ABSTRACT:
A foldable wing or airfoil, which is especially but not exclusively adapted for a projectile, and which incorporates interengaging telescopable fin sections. A nose in the foldable wing, which is hingable in the region of one end through a pivot in a longitudinal groove, has a chamber opening facing away from its leading edge and which is located between the wing part surfaces for receiving the interlocking fin sections, which sections are profiled in U-shaped configuration. The chamber also receives a base or root spar which is hinged in the region of its leading end in the chamber, and wherein the front ends of the fin sections straddle the root spar and are each hinged along the root spar offset relative to each other.
REFERENCES:
patent: 2810985 (1957-10-01), Bilder
patent: 4106727 (1978-08-01), Ortell
Brieseck Bernd
Kreuzer Peter
Blix Trygve M.
Diehl GmbH & Co.
Valliere Mark R.
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