FIELD: transportation.
SUBSTANCE: proposed set of flaps consists of apparatus for aiding ascentional force in form of leading-edge flaps and/or trailing-edge flaps, movably fitted on the leading edge and/or trailing edge of a wing. The system of flaps has a unit for controlling the flaps so as to regulate change in position of the flaps on the wing, several groups of flaps, each of which has apparatus for aiding ascentional force, and several power-drive stations, each of which is related to one group of flaps. A power-drive station comprises two actuators, linked to the unit of controlling flaps, and two more devices for mechanical linkage of actuators with apparatus for aiding ascentional force. The group of flaps are individually controlled through power-drive stations corresponding to these groups of flaps.
EFFECT: increased functionality of flaps with increase in flexibility of operation of the system of flaps at the same time.
18 cl, 7 dwg
Title | Year | Author | Number |
---|---|---|---|
AIRCRAFT WING | 2014 |
|
RU2557638C1 |
AERODYNAMIC WING OF THE FLYING APPARATUS WITH ADAPTIVE VARIABLE SURFACE | 2016 |
|
RU2660191C2 |
DEVICE TO CONTROL AIRCRAFT WING FLAP SYNCHRONISM | 2008 |
|
RU2475423C2 |
WING PANEL FOR AIRCRAFT | 2018 |
|
RU2727642C2 |
AIRCRAFT WING, AIRCRAFT WINGS CAISSON, CENTER WING, SPAR (VERSIONS) | 2019 |
|
RU2709976C1 |
AIRCRAFT WITH LIFT INCREASING SYSTEM | 2010 |
|
RU2494931C2 |
AIRCRAFT WING LIFT SYSTEM MAIN CONTROL SWITCH (VERSIONS), WING LIFT SYSTEM MAIN CONTROL LEVER, WING LIFT SYSTEM MAIN CONTROL UNIT TRIGGER, WING LIFT SYSTEM MAIN CONTROL UNIT TRIGGER STRUCTURAL CASE | 2012 |
|
RU2506201C2 |
SUBSONIC AIRCRAFT WING | 2004 |
|
RU2264329C1 |
AIRCRAFT WING AND WING STRUCTURE WITH FLOW INFLUENCING MEANS | 2010 |
|
RU2488521C2 |
AIRCRAFT MECHANISED WING | 2012 |
|
RU2502635C1 |
Authors
Dates
2009-02-20—Published
2004-03-26—Filed