FIELD: aviation.
SUBSTANCE: group of inventions relates to a method and a device for controlling aerodynamic loads on folding tips of wings of aircraft. To control aerodynamic loads determining position of movable control surface on aircraft wing, as well as change in its position between extended and folded when it is not in flight. Device comprises a processor configured to generate instructions for executing steps of the method, two controllers for communication with wing aircraft tips.
EFFECT: enabling control of wing aircraft tips.
14 cl, 9 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| DEVICE AND METHOD FOR VERIFYING THE RELIABILITY OF A COMMAND OF A PROCESS CONTROL SYSTEM OF AN AIRCRAFT | 2017 |
|
RU2756740C2 |
| METHODS AND DEVICES TO CONTROL AND MONITOR FOLDING WINGTIP DRIVE SYSTEM AND MATERIAL COMPUTER-READABLE STORAGE MEDIUM | 2017 |
|
RU2747392C2 |
| FRAMEWORK | 2016 |
|
RU2645522C1 |
| ACTIVE SYSTEM OF EARLY BREAKING TRAILING VORTICES | 1998 |
|
RU2223892C2 |
| WING WITH AERODYNAMIC CURTAIN | 2016 |
|
RU2646686C2 |
| FLYING VEHICLE WING | 2004 |
|
RU2264327C2 |
| DECREASING VELOCITY IN STREAM FIELD AT ENGINE INLET | 2012 |
|
RU2570186C2 |
| AIRCRAFT CONFIGURATION HAVING SPIN RESISTANCE | 2013 |
|
RU2640669C2 |
| WING TIP (OPTIONS) | 2017 |
|
RU2655571C1 |
| METHOD AND SYSTEM FOR INDICATION OF AIRCRAFT BALANCING ON TAKEOFF | 2018 |
|
RU2773992C2 |
