FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to helicopter swash plates. Helicopter swash plate consists of two parallel lift guides 1 arranged in one plane and rigidly secured to helicopter frame 2, stationary ring 3, and rotary ring 6. Eccentrics 17 connected by bars 18 with slides 5 are arranged at lower part of said lift guides. Stationary ring 3 is coupled by axles 4 with runners 5 arranged inside lift guide 1. Rotary ring 6 with plate 9 is arranged inside stationary ring 3. Rods 10 are secured to said plate to vary angle of attack of propellers. Levers 15, 15 for transverse and lengthwise control are interconnected by drawbars and walking beams with control stick in helicopter cabin wile pitch-rev-up handle is engaged with eccentrics 17.
EFFECT: increased travel of angle of attack of propellers.
3 dwg
Title | Year | Author | Number |
---|---|---|---|
SUMMING MECHANISM FOR CONTROL SYSTEMS OF COMMON AND CYCLIC PITCH OF HELICOPTERS OF THREE-POINT CONTROL SYSTEM WITH INCLINED ARRANGEMENT OF HYDRAULIC ACTUATORS | 2014 |
|
RU2578706C1 |
COAXIAL CARRIER SYSTEM | 2016 |
|
RU2641552C1 |
AIRCRAFT TWO COAXIAL ROTORS SYSTEM | 2017 |
|
RU2662621C1 |
METHOD TO CONTROL ROTOR OF ROTARY WING FLYING VEHICLE AND DEVICE TO THIS END | 2005 |
|
RU2371351C2 |
SYSTEM OF TWO COAXIAL ROTORS OF AIRCRAFT | 2019 |
|
RU2709081C1 |
COAXIAL LOAD-BEARING SYSTEM | 2020 |
|
RU2751168C1 |
METHOD OF CONTROL OF MAIN ROTOR OF FLYING VEHICLE AND DEVICE FOR REALIZATION OF THIS METHOD | 2000 |
|
RU2203835C2 |
MAIN ROTOR | 2005 |
|
RU2281885C1 |
COAXIAL MAIN ROTOR OF ROTORCRAFT | 2021 |
|
RU2756861C1 |
HELICOPTER | 2004 |
|
RU2263607C1 |
Authors
Dates
2013-06-20—Published
2011-08-24—Filed