FIELD: aircraft engineering.
SUBSTANCE: invention relates to aircraft engineering, particularly to mechanical systems of control surface cable run uncoupling. Proposed device comprises control stick, rods, braces, grips and uncoupling mechanism. Section with rigid cable run is introduced into cable run channel between control stick and cable run sector. Aforesaid uncoupling mechanism represents two coaxial bell cranks with horn-like grips revolving on one axle with bell cranks. Grips and braces make a pivoted parallelogram which, in extreme position, makes a kinematic lock.
EFFECT: reduced weight and uncoupling mechanism dimensions, higher reliability.
3 dwg
Title | Year | Author | Number |
---|---|---|---|
CONTROL SYSTEM OF AIRCRAFT CONTROL SURFACES | 2000 |
|
RU2178372C2 |
SYSTEM FOR CONTROL OVER AIRCRAFT AIRFOIL VITALS | 2014 |
|
RU2572011C1 |
ULTRA LOW MASS AIRPLANE | 2005 |
|
RU2336200C2 |
DEVICE FOR CHANGING GEAR RATION IN AIRCRAFT CONTROL SYSTEM | 1977 |
|
SU668197A1 |
HELICOPTER CONTROL SYSTEM | 2023 |
|
RU2819837C1 |
AIRCRAFT LANDING GEAR WELL FRONT FLAP DRIVE | 2010 |
|
RU2427502C1 |
AIRCRAFT LANDING GEAR FRONT LEG CONTROL DEVICE | 2009 |
|
RU2395428C1 |
DEVICE FOR OPENING HATCH COVER | 1995 |
|
RU2104217C1 |
DEVICE FOR DAMPING OF LONGITUDINAL VIBRATIONS OF EKRANOPLAN ON TANGAGE ANGLE | 2015 |
|
RU2634660C2 |
Authors
Dates
2009-11-27—Published
2008-01-31—Filed