MECHANICAL SYSTEM OF AEROPLANE CONTROL

MECHANICAL SYSTEM OF AEROPLANE CONTROL

The present invention comprises a control stick (1) connected by means of a wire (2) to a control organ (3) in the pitch channel and connected by means of a wire (4) to the ailerons (5) in the roll channel. The control stick (1) is also connected to the ailerons (5) in the roll channel by means of a...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: ZHUKOV EVGENIJ M, TETERIN VLADIMIR D, SEROV SERGEJ N, GUDKOV VALERIJ V, LEVITIN IGOR M
Format: Patent
Sprache:eng
Schlagworte:
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Beschreibung
Zusammenfassung:The present invention comprises a control stick (1) connected by means of a wire (2) to a control organ (3) in the pitch channel and connected by means of a wire (4) to the ailerons (5) in the roll channel. The control stick (1) is also connected to the ailerons (5) in the roll channel by means of a wire (2), the first crank (6), a non-linear mechanism (8), a parallelogram mechanism consisting of the second crank (9), the third L-shaped crank (11), the fourth T-shaped crank (12) and an additional wire (13), as well as a wire (14). The first crank (6) is hingedly secured by one of its ends on the first hinged support (7) and is connected through its rocker with the input of the non-linear mechanism (8) whose output is movably connected to one of the ends of the second crank (9) the rocker of which is secured on the second hinged support (10).