RU1779232C - Gyroplane - Google Patents
GyroplaneInfo
- Publication number
- RU1779232C RU1779232C SU894613529A SU4613529A RU1779232C RU 1779232 C RU1779232 C RU 1779232C SU 894613529 A SU894613529 A SU 894613529A SU 4613529 A SU4613529 A SU 4613529A RU 1779232 C RU1779232 C RU 1779232C
- Authority
- RU
- Russia
- Prior art keywords
- gyroplane
- plumage
- parts
- rotation
- flight
- Prior art date
Links
Landscapes
- Gyroscopes (AREA)
Abstract
Изобретение относитс к авиационной технике и может быть использовано дл хвостового оперени автожира. Цель изобретени обеспечение безопасного взлета. Цель достигаетс тем, что части 7, 8 и 9 оперени выполнены с возможностью их свободного поворота задней кромкой вниз по отношению к нормальному полету. Оперение выполнено из двух наружных 8 и 9 и внутренней 7 частей. Ось части 8 параллельна плоскости вращени ротора автожира. Автожир снабжен устройствами холостого поворота отклон емых частей оперени и блокировки его в полетном положении. Каждый участок 7, 8 и 9 оперени блокируетс своим возвратом в полетное положение. По крайней мере один из приводов устройства холостого поворота снабжен устройством блокировки своего углового положени . 6 з.п. ф-лы, 8 ил.The invention relates to aeronautical engineering and can be used for the tail assembly of a gyroplane. The purpose of the invention is to ensure safe take-off. The goal is achieved in that the parts 7, 8 and 9 of the feathers are made with the possibility of their free rotation of the trailing edge down with respect to normal flight. The plumage is made of two outer 8 and 9 and the inner 7 parts. The axis of part 8 is parallel to the plane of rotation of the gyroplane rotor. The gyroplane is equipped with devices for idle rotation of deviated parts of the plumage and its blocking in the flight position. Each plumage section 7, 8 and 9 is blocked by its return to the flight position. At least one of the idle drive drives is provided with a lock device for its angular position. 6 c.p. f-ly, 8 ill.
Description
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Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU894613529A RU1779232C (en) | 1989-02-09 | 1989-02-09 | Gyroplane |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU894613529A RU1779232C (en) | 1989-02-09 | 1989-02-09 | Gyroplane |
Publications (1)
Publication Number | Publication Date |
---|---|
RU1779232C true RU1779232C (en) | 1992-11-30 |
Family
ID=21412762
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SU894613529A RU1779232C (en) | 1989-02-09 | 1989-02-09 | Gyroplane |
Country Status (1)
Country | Link |
---|---|
RU (1) | RU1779232C (en) |
-
1989
- 1989-02-09 RU SU894613529A patent/RU1779232C/en active
Non-Patent Citations (1)
Title |
---|
1. Патент US № 2405244, кл. 244-17.21, 1946. 2.Патент US № 2217108, кл. 244-17.21, 1940. 3.Патент US № 2067634, кл.244-83, 1937. * |
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