To provide a wing for a flying body with high and various flexibility in a wing longitudinal direction while keeping high wing shape holding performance in a wing width direction and high different-flexibility in the wing longitudinal direction.
On each inner surface of an upper flexible wing 10U and a lower flexible wing 10L composed of a CFRP rod 1 molded to have anisotropy in an axial direction, and an elastic member 2 filled in a clearance of the CFPR rod 1, a plurality of pressure tubes 20U, 20L are scattered in the wing longitudinal direction. The pressure tubes 20U, 20L are decompressed in an initial state. The pressure tubes 20L are compressed when the wing is deformed upward, and the pressure tubes 20U is compressed when the wing is deformed downward. The upper flexible wing 10U and the lower flexible wing 10L are oriented so as to make the axial direction of the CFRP rod 1 match the wing width direction.
ISHIKAWA TAKASHI
OGASAWARA TOSHIO
TAKEDA SHINICHI
JPH11512998A | 1999-11-09 | |||
JPH11512998A | 1999-11-09 |
US6145791A | 2000-11-14 | |||
US6082667A | 2000-07-04 | |||
US6015115A | 2000-01-18 | |||
US4725021A | 1988-02-16 | |||
US4261534A | 1981-04-14 | |||
US3957232A | 1976-05-18 | |||
US6145791A | 2000-11-14 | |||
US6082667A | 2000-07-04 | |||
US6015115A | 2000-01-18 | |||
US4725021A | 1988-02-16 | |||
US4261534A | 1981-04-14 | |||
US3957232A | 1976-05-18 |
Masuo Yamada
Fumio Sato
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