RU1779232C - Gyroplane - Google Patents

Gyroplane

Info

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
Application number
SU894613529A
Other languages
Russian (ru)
Inventor
Рабуйт Дени
Original Assignee
Дени Рабуйт (FR)
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Дени Рабуйт (FR) filed Critical Дени Рабуйт (FR)
Priority to SU894613529A priority Critical patent/RU1779232C/en
Application granted granted Critical
Publication of RU1779232C publication Critical patent/RU1779232C/en

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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SU894613529A 1989-02-09 1989-02-09 Gyroplane RU1779232C (en)

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)

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
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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